RBAC 60 — Qualification and Use of Flight Simulation Training Devices

REGULAMENTO BRASILEIRO

DA AVIAÇÃO CIVIL

RBAC nº 60

EMENDA nº 0 0

Título:

REQUISITOS PARA QUALIFICAÇÃO E USO DE

DISPOSITIVOS DE TREINAMENTO PARA SIMULAÇÃO

DE VOO

REQUIREMENTS FOR QUALIFICATION AND USE OF

FLIGHT SIMULATION TRAINING DEVICE

Aprovação: Resolução nº 545 , de 1 8 .03.2020 . [ Emenda nº 00] Origem: SPO PREAMBLE PRE Â MBUL O This regulation is published in Portuguese and Este regulamento é publicado em língua in English, formatted in two columns , on the portuguesa e em língua inglesa , formatado em right is the Portuguese text and on the left is the duas colunas, a da direita em português e a da English version. The Portuguese text is the esquerda em inglês, sendo o texto em official. português o texto oficial.

SECTION CONTENTS SUMÁRIO 60.1 Applicability 60.1 Aplicabilidade 60.3 Definitions 60.3 Definições 60.4 Qualification p erformance s tandards (QPS) 60.4 Requisitos de desempenho para qualificação (QPS) 60.5 Quality management system (QMS) 60.5 Sistema de gerenciamento d a qualidade (QMS) 60.7 Sponsor requirements 60.7 Requisitos para o operador de FSTD 60.9 Additional responsibilities of the sponsor 60.9 Responsabilidades adicionais do operador 60.11 FSTD use 60.11 Uso do FSTD 60.13 FSTD objective data requirements 60.13 Requisitos de dados objetivos do FSTD 60.14 Special equipment and personnel requirements 60.14 Requisitos de equipamentos e speciais e de for qualification of the FSTD pessoal para qualificação de FSTD 60.15 Initial qualification requirements 60.15 Requisitos para qualificação inicial 60.16 Additional qualifications for a currently 60.16 Qualificaçõe s adicionais para um FSTD qualified FSTD atualmente qualificado 60.17 Previously qualified FSTDs 60.17 FSTD s qualificados previamente 60.19 Inspection, continuing qualification 60.19 Requisitos de inspeção, avaliação para evaluation, and maintenance requirements qualificação recorrente e manutenção 60.20 Logging FSTD discrepancies 60.20 Registro de discrep â ncias do FSTD 60.21 Interim qualification of FSTDs for new aircraft 60.21 Qualificação provisória de FSTD s de novos types or models tipos ou modelos de aero naves 60.23 Modifications to FSTDs 60.23 Modificações a FSTDs 60.25 Operation with missing, malfunctioning, or 60.25 Operação do FSTD com component es inoperative (MMI) components faltantes, com mau funcionamento ou inoperante s Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 60.27 Automatic suspension of qualification and 60.27 Suspensão autom á tic a da qualificação e procedures for restoration of qualification procedimentos para restauração da qualificação 60.29 Suspension and revocation of qualification by 60.29 Suspensão e revogação da qualificação pela ANAC ANAC 60.31 Recordkeeping and reporting 60.31 Registro s e documentação 60.33 [ Reserved ] 60.33 [ Reservado ] 60.35 [ Reserved ] 60.35 [ Reservado ] 60.37 FSTD qualification based on the evaluation 60.37 Qualificação de FSTD baseada em conducted by an ICAO contracting State avaliação realizada por um país signatário da ICAO Appendix A – Qualification Performance Standards for Apêndice A – Requisitos de Desempenho para Airplane Full Flight Simulator s Qualificação de S imulador de Voo (FFS) de avião Appendix B – Qualification Performance Standards for Apêndice B – Requisitos de Desempenho para Airplane Flight Training Devices Qualificação de Dispositivo de Treinamento de Voo (FTD) de avião Appendix C – Qualification Performance Standards for Apêndice C – Requisitos de Desempenho para Helicopter Full Flight Simulators Qualificação de Simulador de Voo (FFS) de helicótero Appendix D – Qualification Performance Standards for Apêndice D – Requis itos de Desempenho para Helicopter Flight Training Devices Qualificação de Dispositivo de Treinamento de Voo (FTD) de helicóptero Appendix E – Qualification Performance Standards for Apêndice E – Requisitos para o Sistema de Quality Management Systems for Flight Simulation Training Gerenciamento da Qualidade (QMS) para FSTD Devices Origem: S P O 2 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 60.1 Applicability 60.1 Aplicabilidade (a) This regulation prescribes the rules (a) Este regulamento estabelec e as regras governing the initial and continuing de qualificação inicial e recorrente e d o uso qualification and use of all aircraft f light de d ispositivos de t reinamento para s imulation t raining d evices (FSTD) used for s i mulação de v oo ( FSTD ) utilizados para meeting training, evaluation, or flight cumprir os requisitos de treinamento, exames experience requirements of any RBAC. de profic iência ou experiência de voo estabelecidos em um RBAC .

(b) This reg ulation is applied to each person (b) Este regulamento se aplica a pessoas ou or organization using or applying to use a organizações que utilize m ou que solicitem FSTD to meet any requirement e stablished in a utilizar um FSTD para cumprir qualquer RBAC. requisito estabelecido em um RBAC .

(c) This regulation does not apply to those (c) Este regulamento não se aplica aos FSTD classified as aviation training device FSTD classificados como treinador de voo (ATD) , as defined in paragraph ( c ) ( 16 ) of por instrumentos (ATD) , conforme definido section 60.3 of this regulation . n o parágrafo ( c ) ( 16 ) da seção 60.3 deste Regulamento .

60.3 Definitions 60.3 Defi ni ções (a) In the scope of this regulation are valid (a) No escopo deste regulamento são all definitions contained in RBAC 01 and válidas todas as definições contidas no RBAC RBHA 91 , or RBAC that could be substitute it . nº 01 e no RBHA 91 , ou RBAC que venha a substituí - lo .

(b) This regulation uses terms and (b) Este RBAC utiliza termos e definições definitions in the English language na língua inglesa por entender que estes já são understanding that they are widely used by the amplamente utilizados pe la ind ú stria e industry and sponsor s. operadores.

(c) For purposes of this regulation, the (c) Para os propósitos deste regulamento, following definitions and expressions are used: são válidas as seguintes definições e expressões: ( 1 ) Special e valuation . A FSTD ( 1 ) Avaliação e special . U ma avaliação evaluation for purposes other than initial, de FSTD para propósitos outros do que upgrade or continuing qualification. inicial, eleva ção de nível ou recorrente.

( 2 ) Predicted d ata . E stimations or ( 2 ) Dados e stimados . E stimativas ou extrapolations of existing flight test data or extrapolações de dados de ensaio em voo, ou data from other simulation models using dados de outros modelos de simulação engineering analyses, engineering simulations, utilizando análise s e simulações de design data, or wind tunnel data. engenharia, dados de projeto ou de túnel de vento.

(3) Statement of Compliance (SOC). A (3) Declaração de conformidade declaration that a specif ic requirement has (SOC) . Uma declaração atestando que um been met and explaining how the requirement requisito específico é cumprido e como ele é was met. cumprido.

( 4 ) Flight s imulation t raining d evice ( 4 ) Dispositivo de t reinamento para ( FSTD ) . A full flight simulator (FFS), a flight s imulação de v oo (FSTD). U m simulador de Origem: S P O 3 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 training device (FTD) or an aviation training voo (FFS), um dispositivo de treinamento de device (ATD) . voo (FTD) ou um treinador de voo por instrumentos (ATD).

( 5 ) Flight t raining d evice (FTD) . A ( 5 ) Dispositivo de t reinamento de voo replica of aircraft instruments, equipment, (FTD) . Consiste em uma réplica dos panels, and contr ols in an open flight deck area instrumentos, equipamentos, painéis e or an enclosed aircraft flight deck replica. It controles de uma aeronave em uma área includes the equipment and computer confinada ou não da cabine de pilotagem .

programs necessary to represent aircraft (or set Inc lui os equipamentos e programas of aircraft) operations in ground and flight necessários para representar a operação da conditions having the full range of capabiliti es aeronave em solo e em voo, tendo toda a of the systems installed in the device as capacida de dos sistemas instalados no described in this RBAC and the qualification dispositivo conforme descrito n este RBAC e performance standard (QPS) for a specific n os requisitos de desempenho para FTD qualification level. qualificação (QPS) para um nível específico de qualificação de FTD .

( 6 ) Qualification Test Guide (QTG) . T he ( 6 ) Guia de Tes tes de Qualificação primary reference document used for (QTG) . D ocumento primário de referência eval uating an aircraft FSTD. It contains test utilizado para avaliar um FSTD de um a results, statements of compliance and aeronave. Contém os resultados de testes, capability, the configuration of the aircraft declarações de conformidade e capacidade, a simulated and other information for the configuração da aeonave simulada e outras evaluator to assess the FSTD against the informações para o avaliador julgar o FSTD applicable regulatory criteria. de acordo com os critérios regulatórios aplicáveis.

( 7 ) Master Qualification Test G uide ( 7 ) Guia Mestre de Testes de (MQTG) . T he ANAC - approved Qualification Qualificação (MQTG) . O Guia de Testes de Test Guide with the addition of the ANAC - Qualificação , aprovado pela ANAC , witnessed test results, applicable to each adicionado dos resultados dos testes individual FSTD. presenciados pela ANAC, aplicá vel a cada FSTD individual.

( 8 ) Sponsor . A certificate holder who ( 8 ) Operador de FSTD. Um detentor de seeks or maintains FSTD qualification and is certif ic ado que solicita ou possui um FSTD responsible for the prescribed actions as qualificado, responsável pelas at ribuições prescribed in this regulation . impostas por este regulamento.

( 9 ) Approved t raining p rogram. An ( 9 ) Programa de t reinamento ANAC - approved training program or course a provado . Programa de treinamento ou curso for an aircraft of a certificate holder or a public de uma aeronave , aprovado pela ANAC , para body. um detentor de certificado ou órgão público .

( 1 0 ) Management r epresentative . A ( 1 0 ) Representante do o perador .

person designated by the sponsor to serves as Pessoa designada pelo operador para ser o the primary contact point for all matters contato primário para todos os assuntos entre between the sponsor and the ANAC. o operador e a ANAC.

( 11 ) Qualification Performance ( 11 ) Requisitos de Desempenho para Standard (QPS) . Th e collection of procedures Qualificação (QPS) . C onjunto de and criteria used when conducting objectiv e proced imentos e critérios utilizados n a Origem: S P O 4 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 and subjective tests, to establish FSTD condução de testes objetivos e subjetivos, qualification levels. para estabelecer ní veis de qualificação d e FSTD.

( 12 ) Full f light s imulator (FFS) . A ( 12 ) Simulador de v oo (FFS) . Consiste replica of a specific type, make, model, or em uma réplica dos instrumentos, series aircraft. It includes the equipment and equipamentos, painéis e controles do tipo software necessary to represent aircraft específico ou do modelo e série de uma operations in ground and flight conditions, and aeronave. Inclui os equipamentos e has the full range of capabilities of the systems programas necessários para representar a installed in the device as described in this operação da aeronave em solo e em voo, RBAC and the QPS for a specific FFS tendo toda a capacidade dos sistemas qualification level. instalados no dispositivo conforme descrito neste regulamento e n o QPS para um nível específico de qualificação de F FS .

( 13 ) Quality m anagement s ystem (QMS) . ( 13 ) Sistema de g erenciamento da A flight simulation quality - systems that can be q ualidade (QMS). U m sistema de qualidade used for external quality - assurance purposes. It que pode ser utilizado para propósitos de is designed to identify the processes needed ; garantia da qualidade em auditorias externas.

determine the sequence and interaction of the É concebido para identificar a necessidade de processes ; determine criteria and methods processos específicos; determinar a sequência required to ensure the eff ective operation and e interação entre os processos ; determinar os control of the processes ; ensure the availability critéri os e métodos para garantir a efetiva of information necessary to support the operação e controle dos processos ; garantir a operation and monitoring of the processes ; disponibilidade da informação para suportar a measure, monitor and analyze the processes ; operação e monitorar os processos ; mensurar, and implement the actions necessary to achieve monitorar e analisar os processos ; e planned res ults. implementar as ações necessárias para alcança r os resultados planejados.

( 14 ) Objective t est . A quantitative ( 14 ) Testes o bjetivos . Consiste em uma measurement and evaluation of FSTD medida e avaliação quantitativa do performance. desempenho de um FSTD.

( 15 ) Subjective t est . A qualitative ( 15 ) Testes s ubjetivos . Consiste em um a assessment of the performance and operation análise qualitativa do desempenho e operação of the FSTD. de um FSTD .

( 16 ) Aviation t raining d evice (ATD). A ( 16 ) Treinador de v oo por i nstrumento device designed to simulate an instrument (ATD). D ispositivo com o qual é possível flight in a class aircraft. simular a operação de uma aeronave classe em um voo por instrumentos .

( 17 ) FSTD use means use, permit the use ( 17 ) Utilizar um FSTD . U tilizar, or offer the use of a FSTD in order to fulfill permitir o uso ou oferecer o uso de um FSTD requirements of flight training, proficiency com o fim de cumpri r requisitos de exam or obtaining flight experience to comply treinamento de voo, exame de proficiência ou with any RBAC requirements . para obtenção de experiência de voo de tripulantes , para cumprir qualquer requisito estabelecido em um RBAC .

Origem: S P O 5 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 60.4 Qualifi cation p erformance s tandards 60.4 Requisitos de desempenho para ( QPS ) qualificação ( QPS ) (a) The Qualification Performance (a) Os requisitos de desempenho para Standards are published in appendices to this qualificação são publicados em apêndices RBAC as follows: deste regulamento : ( 1 ) Appendix A contains the QPS for ( 1 ) O Apêndice A contém o QPS para Airplane Flight Simulators. Simulador de Voo de Avião.

( 2 ) Appendix B contains the QPS for ( 2 ) O Apêndice B contém o QPS para Airplane Flight Training Devices. Dispositivo de Treinamento de Voo de Avião.

( 3 ) Appendix C contains the QPS for ( 3 ) O Apêndice C contém o QPS para Helicopter Flight Simulators. Simulador de Vo o de Helicóptero ( 4 ) Appendix D contains the QPS for ( 4 ) O Apêndice D contém o QPS para Helicopter Flight Training Devices. Dispositivo de Treinamento de Voo de Helicóptero 60.5 Quality management system ( QMS ) 60.5 Sistema de g erenciamento d a q ualidade ( QMS ) (a) A sponsor may use a FSTD only if the (a) U m operador somente poderá utilizar sponsor has established and follows a QMS, um FSTD se este operador t iver estabelecido currently approved by the ANAC , for the e s eguir um QMS, aprovado pela ANAC, para continuing surveillance and analysis of the monitorar e analisar continuamente a sponsor's performance and effectiveness in capacidade do operador em disponibilizar um providing a satisfactory FSTD for use on a FSTD satisfatório para uso frequente. O QMS regular basis . The QMS must comply with the deve cumprir o determinado no Apêndice E determination of Appendix E of this RBAC. deste RBAC (b) The QMS program must provide , (b) O QMS deve prover , além de um besides a p rocess for identifying deficiencies in processo de identificação de deficiências do the system, a process for documenting how the sistema, um processo para documentar com o QMS will be changed to address these o QMS será modificado para sanar estas deficiencies. deficiências.

(c) Whenever the ANAC finds that the (c) Sempre que a ANAC julgar que o QMS QMS program does not adequately address the não garant e procedimentos adequados para o procedures necessary to meet the requirements cumprimento dos requisitos deste of this RBAC , the sponsor must, after regulamento, o operador deverá, após ser notification by the ANAC , change th e program notificado pela ANAC, alterar o QMS para in order to the procedures meet the que ele atenda os requisitos deste requirements of this RBAC . Each such change regulamento. Cada alteração deve ser must be approved by the ANAC prior to aprovada pela ANAC antes de ser adota da.

implementation.

60.7 Sponsor requirements 60.7 Requisitos para o operador de FSTD (a) An organization is eligible to apply to be (a) Uma organização é elegível a ser um a sponsor if the following conditions are met: operador de FSTD se as seguintes condições forem cumpridas: Origem: S P O 6 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 (1) t he organization holds, or is an (1) a organização possui r , ou for um applicant for, a certificate under RBAC 119, requerente para possuir, um certificado 141, or 142 ; and conforme o RBAC nº 119, 141 ou 142; e (2) t he FSTD will be used in the (2) o FSTD for utilizado no programa sponsor´s ANAC - approved training program de treinamento aprovado pela ANAC do for the aircraft being simulated. operador , para a aeronave simulada .

(b) A n organization is a sponsor if the (b) Uma organização é um operador de following conditions are met: FSTD se as seguintes condições forem cumpridas: (1) t he organization is a certificate holder (1) a organização for detentora de um under RBAC 119, 141, or 142 ; certificado conforme o RBAC nº 119, 141 ou 142; (2) t he organization has an ANAC - (2) a organização possui r um programa approved training program for an aircraft or set de treinamento aprovado pela ANAC para of aircraft and at least one FSTD, sponsored by uma aeronave ou conjunto de aeronave s e , the organization, is used with in this training pel o menos um FSTD, operado pela program , at least once every 12 months ; organização, for utilizado neste programa de treinamento , pelo menos uma vez a cada 12 meses ; ( 3 ) t he organization has a QMS curr ently ( 3 ) a organização possui r um QMS approved by the ANAC in accordance with aprovado pela ANAC de acordo com a seção section 60.5 of this regulation; and 60.5 deste regulamento; e ( 4 ) ANAC has accepted the organization ( 4 ) a ANAC aceitou a organização as the sponsor of the FSTD and that acceptance como operador do FSTD e esta aceitação não has not been revoked by the ANAC . foi revogada pela ANAC.

(c) In addition to the FSTD described in (c) Adicionalmente ao FSTD descrito no paragraph (b) (2) of this section, a sponsor may parágrafo (b)(2) desta seção, um operador de sponsor any number of other FSTDs regardless FSTD pode operar quaisquer outros FSTDs , of specific aircraft or set of aircraft provided independentemente da aeronave simulada, either: desde que : (1) a ll of the other FSTDs are used within (1) t odos os outros FSTDs sejam the sponsor´s or another certificate ho lder´s utilizados dentro do programa de treinamento ANAC - approved training program for the aprovado pela ANAC, do operador do FSTD aircraft, at least once every 12 months; or ou de outro detentor de certificado, para a aero nave simulada , pelo menos uma vez a cada 12 meses ; ou (2) t he sponsor obtains a written (2) o operador obtenha uma declaração statement at least annually from a qualified escrita a cada 12 meses , de um piloto pilot who has flown the aircraft or set of qualificado que tenha voado a aeronave ou aircraft (as appropriate) during the preceding conjunto de aeronaves (como apropriado) nos 12 - month period stating that the subject 12 meses precedentes, atestando que o FSTD's performance and handling qualities, desempenho e a qualidade de voo do FSTD within the normal operating envelope, representam a aeronav e ou conjunto de represent the simulated aircraft or set of aeronaves simulada s . O operador deve manter aircraft. The sponsor must retain the two most Origem: S P O 7 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 current written statements for review by the as duas últimas declarações escritas para ANAC . consulta da ANAC.

( d ) A public administration body is el i gible ( d ) Um órgão da administração pública é to be a sponsor and will be considered a s elegível a ser um operador de FSTD e será sponsor if the following conditions are met: considerado um operador de FSTD se as seguintes condições forem cumpridas: (1) t he public body has an ANAC - (1) o órgão público possui r um approved training program for an aircraft or set programa de treinamento aprovado pela of aircraft and at least one FSTD, sponsored by ANAC para uma aeronave ou conjunto de the body , is used within this training program , aeronaves e , pelo menos um FSTD, operado at least once every 12 months ; and pel o órgão , for utilizado neste programa de treinamento, pelo menos uma vez a cada 12 meses ; e (2) t he public body has a QMS currently (2) o órgão público possuir um QMS, approved by the ANAC in accordance with aprovado pela ANAC de acordo com a seção section 60.5 of this regulation . 60.5 deste regulamento .

60.9 Additional responsibilities of the 60. 9 Responsabilidades adicionais do sponsor operador (a) The sponsor must allow ANAC upon (a) O operador, quando solicitado, deve request to inspect the FSTD as soon as permitir à ANAC realizar inspeções no FSTD practicable. This inspection may include all tão logo quanto praticável. Esta inspeção records and documents relating to the FSTD, to pode inclui r todos os registros e documentos determine its compliance with the regula t ions. relacionados ao FSTD, para verifica ção dos requisitos vigentes.

(b) The sponsor must do the following for (b) Para cada FSTD, o operador deve: each FSTD: (1) e stablish a mechanism to receive (1) e stabelecer um mecanismo para written reports regarding the FSTD and its receber re latos escritos sobre o FSTD e sua operation in accordance with the approved operação, de acordo com o QMS aprovado ; e sponsor´s Q M S ; and (2) p ost in or adjacent to the FSTD the (2) f ixar no FSTD ou em local Statement of Qualification issued by the adjacente, o Certificado de Qualificação ANAC . An electronic copy of the Statement of emitido pela ANAC. Uma cópia eletrônica do Qualification that may be accessed by an Certificado de Qualificação que possa ser appropriate terminal or display in or adjacent acessada no FSTD ou em local adjacente é to the FSTD is satisfactory. aceitável .

(c) Each sponsor must identify to the ANAC (c) Cada operador de FSTD deve indicar à a person to be the management representative. ANAC uma pessoa que será o representante do operador.

(1) One person may serve as a (1) Uma pessoa pode ser o m anagement r epresentative for more than one representante do operador de mais de um FSTD, but one FSTD must not have more than FSTD, mas um FSTD não pode ter mais de one person serving in this function . uma pessoa atuando nesta função.

Origem: S P O 8 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 (2) The m anagement r epresentative must (2) O representante do operador deve be a person related to the sponsor and must ser uma pessoa vinculada à organização e have the responsibility and authority to: deve possuir a responsabilidade e autoridade para: (i) m onitor the on - going qualification (i) m onitorar a qualificação em of assigned FSTDs to ensure that all matters andamento do FSTD a ele designado para regarding FSTD qualification are being carried garantir que todos os as pectos referentes à out as provided for in this RBAC ; qualificação do FSTD estão sendo conduzidos de acordo com as disposições deste regulamento; (ii) e nsure that the QMS is properly (ii) g arantir que o QMS seja established, implemented and maintained; and propriamente estabelecido, exec utado e mantido ; e (iii) r egularly brief the sponsor 's (iii) r egularmente informar à management on the status of the on - going gerência do operador sobre a situação da FSTD qualification program and the qualificaçã o vigente do(s) FSTD(s) e da effectiveness and efficiency of the QMS. efetividade do QMS.

(3) The m anagement r epresentative (3) O representante do operador é o serves as the primary contact point for all contato primário para todos os assuntos entre matters between the sponsor and the ANAC o operador e a A NAC que dizem respeito à regarding the qualification of that FSTD as qualificação daquele FSTD conforme provided for in this RBAC . disposto neste regulamento.

(4) The m anagement r epresentative may (4) O representante do operador poderá delegate the duties described in paragraph delegar a terceiros as atribuições descritas nos (c)(2) and (c)(3) of this section to an individual parágrafos (c)(2) e (c)(3) desta seção em cada at each of the sponsor's locations. uma das localidades em que opera.

60.11 FSTD use 60.11 Uso do FSTD (a) A person may use a FSTD only if the (a) U ma pessoa somente pode utilizar um FSTD: : FSTD se este: : ( 1 ) h as a single sponsor who is qualified ( 1 ) tiver um único op erador que seja under section 60.7 of this regulation . The qualificado conforme a seção 60.7 deste sponsor may arrange with another person for r egulamento . O operador pode utilizar services of document preparation and serviços de terceiro s para preparação e presentation, as well as FSTD inspection, apresentação de documentação, bem como maintenance, repair or servicing; however, the para inspecionar, realizar manutenção, reparo sponsor remains responsible for ensuring that ou auxílio técnico ao FSTD ; entretanto, o these functions are conducted in a manner and operador permanece responsável por garantir with a result of continually meeting the que estas atribuições sejam conduzidas de requirements of this regulation ; forma a manter o cumprimento dos requisitos deste regulamento ; ( 2 ) i s qualified as described in the ( 2 ) e st iver qualificado conforme Statement of Qualification ; descrito no seu Certificado de Qualificação ; Origem: S P O 9 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 ( 3 ) r emains qualified, through ( 3 ) p ermane cer qualificado, por meio satisfactory inspection, continuing de inspeções satisfatórias, avaliações qualification evaluations, appropriate recorrentes, manutenção apropriada e for maintenance, and is available for use in dis ponibilizado para uso conforme os accordance with the requirements of this requisitos deste regulamento ; regulation; ( 4 ) u se the software and hardware that ( 4 ) u tiliz ar o software e o hardware que w ere evaluated as satisfactory by the ANAC foram avaliados como satisfatório s pela and, if modified, modified only in accordance ANAC e, se modificado, modificado somente with the provisions of this regulation . conforme as disposições deste regulamento.

However, this section does not apply to routine Entretanto, este item não se aplica para software or hardware changes that do not fall mudanças rotineiras de software ou hardware under the requirements of s ection 60.23 of this que não se enquadrem nos requisitos da seção regulation ; and 60.23 deste regulamento ; e ( 5 ) i s operated in accordance with the (5 ) for operado de acordo com as provisions and limitations of section 60.25 of provisões e limitações d a seção 60.25 deste this regulation . regulamento .

60.13 FSTD objective data requirements 60.1 3 Requisitos de dados objetivos do FSTD (a) Except as provided in paragraph (b) and (a) Exceto como previsto nos parágrafos (c) of this section, for the purposes of (b) e (c) desta seção, a fim de validar o validating FSTD performance and handling desempenho e as características do FSTD qualities during evaluation for qualification, durante a avaliação de qualificação, os dados the data made available to the ANAC (the da aeronave disponibilizados para a ANAC validation data package) must include the (pacote de dados de validação) devem incluir aircraft manufacturer's flight test data and all os dados de ensaio em voo do fabricante da relevant data developed after the type aeronave e todos os dados relevantes certificate was issued ( for example , data desenvolvidos após a emissão do certificado developed in response to an airworthiness de tipo da aeronave ( por exemplo , dados directive) if such data results affect the desenvolvidos em r esposta a uma diretriz de performance, handling qualities, function s, or aeronavegabilidade) se estes dados afet ar em other characteristics of the aircraft . o desempenho , a qualidade de voo, as funcionalidades ou outras características da aeronave .

(b) The validation data package may (b) O pacote de dados de validação par a contain flight test data from a source in basear uma qualificação de FSTD pode conter addition to or independent of the aircraft dados de ensaio em voo de uma fonte manufacturer's data in support of a FSTD adicional ou independente dos dados do qualification, but only if this data is gathered fabricante da aeronave, mas apenas se estes and developed by that source in accordance dados for e m obtidos e desenvolvidos por esta with flight test methods, including a flight test fonte de acordo com os métodos de ensaio em plan . voo, incluindo um plano de en saio em voo.

(c) The validation data package may also ( c) O pacote de dados de validação contain predicted data, engineering simulation também pode conter dados estima dos , dados data, data from pilot owner or pilot operating de simulação de engenharia, dados dos Origem: S P O 10 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 manuals, or data from public domain sources, manuais do proprietário ou de operação da provided this data is acceptable to the ANAC . aeronave, ou dados de outras fontes públicas, If found acceptable the data may then be used desde que estes dados sejam aceit áveis pela in particular applications for FSTD ANAC. Se considerados aceitáveis , os dados qualification. poderão ser utilizados em casos específicos para a qualificação do FSTD.

(d) Data or other material or elements must (d) Os dados de validação ou qualquer be submitted in a form and manner acceptable outro material devem ser submetidos em um to ANAC . formato aceitável pela ANAC .

(e) ANAC may require additional objective (e) A ANAC poderá exigir dados de data, which may include , if necessary, flight validação adicionais, que podem incluir , se testing, if the validation data package does not necessário, ensaio em voo , caso o pacote de support FSTD qualification require ments as dados de validação apresentado não atenda os described in this regulation for the intended requisitos de qualificação do FSTD , qualification level . conforme requerido por este regulamento para o nível de qualificação pretendido.

(f) When a FSTD sponsor learns, or is (f) Quando o operador de um FSTD advised by an aircraft manufacturer or other souber, ou for avisado pelo fabricante da data provider, that an addition to, an aeronave , ou por outro provedor de dados , amendment to, o r a revision of data that may que exi s te uma adição, emenda, ou uma relate to FSTD performance or handling revisão dos dados de validação , que possam characteristics is available, ANAC must be impact ar as características de desempenho ou notified by the sponsor . qualidade de voo do FSTD , o operador deverá notificar a ANAC .

60.14 Special equipment and personnel 60.1 4 Requisitos de equipamentos requirements for qualification of the FSTD especiais e de pessoal para qualificação de FSTD (a) When notified by the ANAC , the (a) Quando solicitado pela ANAC, o sponsor must make available all special operador deve disponibilizar todos os equipment and qualified pers onnel needed to equipamentos especiais e pessoal qualificado accomplish or assist in the accomplishment of necessários para realizar ou auxiliar na tests during initial qualification, continuing realização dos testes durante a qualificação qualification, or special evaluations. inicial, qualificação recorrente ou avaliações especiais do FSTD.

60.15 Initial qualification requirements 60.15 Requisitos para qualificação inicial (a) For each FSTD, the sponsor must (a) Para cada FSTD, o operador deve submit, with 90 days in advance, a request to enviar à ANAC uma solicitação de avaliação ANAC to evaluate the FSTD for initial do FSTD para qualificação inicial em um qualification at a specific level , which must be nível específico com antecedência mínima de confirmed by ANAC . The request must be 90 dias à data de a valiação pretendida, cuja submitted in the form and manner determined confirmação dar - se - á de acordo com a by ANAC . disponibilidade da ANAC . A solicitação deve Origem: S P O 11 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 ser feita no formato e na maneira determinada pela ANAC .

(b) The management representative , (b) O representante do operador, descrito described in the paragraph 60.9(c) of this n o parágrafo 60. 9 (c) deste regulamento, deve regulation, must sign a statement stating the providenciar declaração assinada afirmando following: que: (1) t he performance and handling (1) o desempenho e a qualidade de voo qualities of the FST D represent those of the do FSTD representam aqueles da aeronave ou aircraft or set of aircraft within the normal conjunto de aeronaves sendo simulada dentro operating envelope. This statement must be do seu envelope normal de operação. Esta made by a qualified pilot in the aircraft or set declaração deve ser feita por um piloto of aircraft being simulated after having flown qualificado na aeronave ou conjunto de all of the Operations Tasks listed in the QPS aeronaves sendo simulada ap ós ter realizado relevant to the qualification level of the FSTD ; todas as tarefas operacionais listadas no QPS relevante ao nível de qualificação pretendido do FSTD ; (2) t he FSTD systems and sub - systems (2) o s sistemas e subsistemas do FSTD (including the simulated aircraft systems) (incluindo os sistemas simulados da functionally represent those in the aircraft or aeronave) representam o funcionamento set of aircraft. This statement must be made by daqueles da aeronave ou conjunto de a qualified pilot in the aircraft or set of aircraft aeronaves. Esta declaração deve ser feita por being simulated or by a person t rained on um piloto qualificado na aeronave ou simulator systems/sub - systems and trained on conjunto de aeronaves sendo simulada, ou por the operation of the simulated aircraft systems ; uma pessoa treinada em sistemas e and subsistemas de FSTDs e treinada na operação dos sistemas da aeronave simulada ; e (3) t he coc kpit represents the (3) a cabine de comando representa a configuration of the specific type; or aircraft configuração do tipo específico ou do modelo make, model and series aircraft being e série da aeronave sendo simulada, como simulated, as appropriate. This statement must apropriado. Esta declaração deve ser feita por be made by a qualified pilot in the aircraft or um piloto qualificado na aeronave ou set of aircraft being simulated, or by a person conjunto de aeronaves sendo simulada , ou por trained on the configuration and operation of uma pessoa treinada em configuração e the aircraft simulated . operação da aeronave simulada .

( c) E ach FSTD evaluated for initial (c) C ada FSTD avaliado para qualificação qualification must meet the qualification inicial deve cumprir os requisitos de perfor mance standard s, as defined in section desempenho para qualificação, definidos na 60.4 of this regulation , that are in effect at the seção 60.4 deste regulamento , que estiverem time of the evaluation . The exceptions are: em vigor na época da avaliação . As exceções são: (1) i f the ANAC publishes a change to (1) c aso a ANAC publique uma revisão the existing standard or publishes a new a o requisito existente ou publique um novo standard for the evaluation for initial requisito para qualificação inicial , um qu alification , a sponsor may request that the operador que já ti ver encomendado um FSTD ANAC apply the standard that was in effect poderá solicitar que a ANAC utilize o when a FSTD was ordered for delivery . In this requisito que estava em vigor à época da Origem: S P O 12 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 case, t he evaluation must be conducted withi n encomenda. Neste caso, a avaliação deverá 24 months following the publication of the ocorrer em até 24 meses contados a partir da change to the existing standard or publication publicação da revisão d o requisito , ou da of the new standard ; and publicação do novo requi sito ; e (2) an FSTD manufactured before the (2) um FSTD fabricado anteriormente à publication of this regulation and which is data de publicação deste regulamento e que qualified by the aviation authority of a esteja qualificado por autoridade aeronáutica contracting State to the Convention on de um país signatário da Convenção de International Civil Aviation may be evaluated Aviação Civil Internacional poderá ser for initial qualification in accordance to its avaliado para qualificação inicial, de acordo original qualification basis, provided it is com os requisitos estabelecidos na sua base authorized by ANAC. de qualificação original, desde que autorizado pela ANAC.

( d ) The standards used for the evaluation for ( d ) Os requisitos utilizados na avaliação initial qualification will be used for all para qualificação inicial serão utilizados para subsequent evaluations of the FSTD. todas as avaliações subsequentes do FSTD.

(e) The subjective tests that form the basis ( e ) Os testes subjetivos que compõem a for the statements described in paragraph (b) of declaração descrita no parágrafo (b) desta this section and the objective tests referenced seção e os testes objetivos realizados para in paragraph (f) of this section must be atender aos requisitos do parágrafo (f) desta accomplished at the sponsor's training facility . seção devem ser realizados na localidade permanente onde o FSTD será operado.

(f) The organization seeking to qualify the ( f ) A organização que pretende ter o FSTD FSTD must provide the A NAC access to the qualificado deve prover à ANAC acesso ao FSTD for the length of time necessary for the FSTD pelo tempo necessário para completar ANAC to complete the required evaluation of a avaliação do FSTD para qualificação the FSTD for initial qualification, which inicial , o que inclui a realização d e testes includes the conduct and evaluation of objetivos, subjetivos e funcionais, bem como objective and subjective tests, including a verificação de requisitos gerais de FSTD, general FSTD requirements , as described in conforme descrito no QPS, para determinar the QPS, to determine that the FSTD meets the que o FSTD cumpre todos os requisitos standards for the qualification level sought . aplicáveis a o nível de q ualificação pretendido .

(g) When the FSTD an evaluation for initial ( g ) Quando uma avaliação de qualificação qualification is succeeded , the ANAC issues a inicial de FSTD é concluída com sucesso, a Statement of Qualification that includes all of ANAC emite um Certificado de Qualificação the following: que inclui o seguinte: (1) the i dentification of the sponsor ; (1) a i dentificação do operador ; (2) the i dentification of the make, model, (2) a i dentificação do fabricante, and series of the aircraft or set of aircraft being modelo e série da aeronave ou conjunto de simulated ; aeronaves sendo simuladas ; (3) the i dentification of the configuration (3) a i dentificação da configuração da of the aircraft or set of aircraft being simulated aeronave ou conjunto de aeronaves sendo ( e.g. , engine model or models, flight simuladas (ex: modelo ou modelos do motor, instruments, or navigation or other systems) ; instrumentos de voo, sistemas de navegação) ; Origem: S P O 13 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 (4) a statement that the FSTD is qualified (4) u m certificado de que o FSTD está as either a FTD or a FFS; qualificado como FTD ou FFS ; (5) the i dentification of the qualification (5) a i dentificação do nível de level of the FSTD ; qualificação do FSTD ; (6) a statement that the qualification of (6) u ma declaração de que a the FSTD includes the tasks set out in the QPS qualificação do FSTD inclui todas as tarefas relevant to the qualification level of the FSTD operacionais definidas no QPS relevante ao with the exception of those tasks not evaluated nível de qualificação pretendido, com or considered unsatisfactory by ANAC ; and exceção daquelas tarefas não avaliadas ou consideradas insatisfatórias pela ANAC ; e (7) a statement referencing any (7) u ma declaração referenciando deviations th at have been granted and included quaisquer desvios que tenham sido in the permanent qualification basis of the concedidos e incluídos na base de FSTD. qualificação permanente do FSTD.

(h) After ANAC completes the evaluation ( h ) Após a ANAC concluir a avaliação for initial qualification, the sponsor must para qualificação inicial, o operador deve update the Qualification Test Guide (QTG), atualizar o QTG contendo os resultados dos with the results of the ANAC - witnessed. testes executados na presença da ANAC.

(i) Upon issuance of the Statement of ( i ) Com a emissão do Certificado de Qualification the updated QTG becomes the Qualificação, o QTG atualizado torna - se o Master Qualification Test Guide (MQTG). The MQTG. O MQTG deve ser disponibilizado à MQTG must be made available to ANAC upon ANAC quando solicitado.

request.

60.16 Additional qualifications for a 60.16 Qualificações adicionais para um currently qualified FSTD FSTD atualmente qualificado (a) A currently qualified FSTD is required (a) Um FSTD atualmente qualificado deve to undergo an additional qualification process passar por um processo de qualificação if a user intends to use the FSTD beyond the adicional caso pretenda utilizar o FSTD além qual ification issued for that FSTD. This da sua qualificação original . Este processo process consists of the following: consiste no seguinte: (1) t he sponsor must : (1) o operador deve: (i) s u bmit to ANAC all modifications (i) s ubmeter à ANAC to das as to the MQTG that are required to support the modificações ao MQTG requeridas para additional qualification ; basear a qualificação adicional; (ii) d escribe to ANAC all (ii) d escrever à ANAC todas as modifications to the FSTD that are required to modificações ao FSTD que são requeridas support the additional qualification ; and para basear a qualificação adicional; e (iii) s ubmit to ANAC a statement , as (iii) s ubmeter à ANAC uma described in paragraph 60.15(b) of this declaraç ão, como descrita n o parágrafo regulation, that a rated and qualified pilot in the 60.15(b) deste regulamento , que um piloto aircraft or set of aircraft being simulated has habilitado e qualificado na aeronave ou subjectively evaluated the FSTD in those areas conjunto de aeronaves sendo simulada not previously evaluated ; and Origem: S P O 14 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 avaliou subjetivamente o FSTD naquelas áreas não avaliadas anteriormente ; e (2) t he FSTD must successfull y pass a n (2) o FSTD deve ser aprovado em uma evaluation as determined by ANAC. avaliação como determinado pela ANAC.

(b) In determin ing the criteria of the (b) Ao determina r o s critérios para a evaluation mentioned in paragraph (a)(2) of avaliação menciona da n o parágrafo (a)(2) this section, ANAC considers factors such as desta seção, a ANAC considera fatores tais the existing qualification of the FSTD, any como a qualificação atual do FSTD, as modifications to the FSTD hardware or modificações de hardware e software software that are involved, and any additions envolvidas, os acréscimos ou modificações ao or modifications to the MQTG , among others . MQTG , dentre outros .

(c) The FSTD is qualified for the additional (c) O FSTD estará qualificado para os usos uses when ANAC issues an amended adicionais quando a ANAC emitir uma Statement of Qualification in accordance with revisão do Ce rtificado de Qualificação de paragraph 60.15( i ) of this regulation . acordo com o parágrafo 60. 15( i ) deste regulamento .

(d) The sponsor may only modify the FSTD (d) O operador só pode modificar o FSTD as described in section 60.23 of this regulation . como descrito na seção 60.23 deste regulamento .

60.17 Previously qualified FSTDs 60. 17 FSTDs qualificados previamente (a) Unless otherwise specified by an FS T D (a) Exceto para os casos especificados em directive , or as specified in paragraph ( d ) of uma diretriz de FSTD , ou como especificado this section, a n FSTD qualified by ANAC no parágrafo ( d ) desta seção, um FSTD before the issue of this regulation will retain its qualificado pela ANAC anteriormente à data qualification basis as long as it continues to de publicação deste regulamento poderá meet the standards, including the objective test manter a mesma base de qualificação results recorded in the MQTG and subjective utilizada à época da qualificação inicial deste tests, under which it was originally evaluated, FSTD, desde que os requisitos daquela b ase regardless of sponsor. However, t he sponsor of continuem sendo cumpridos, incluindo os such a n FSTD must comply with the other testes objetivos do seu MQTG e os testes applicable provisions of this regulation . subjetivos, independentemente do operador.

Entretanto, o operador de tal FSTD deverá adequar - se a todos os outros requisitos aplicáveis dispostos neste regulamento.

( b ) I f the FSTD qualification is suspended ( b ) Se a qualificação do FSTD for under section 60.27 of this regulation and : suspensa conforme seção 60.27 deste regulamento e: (i) r estored under section 60.27 of this ( i ) f or restaurada conforme seção regulation in less than 24 months , then the 60.27 deste regulamento em menos de 24 qu alification basis (in terms of objective tests meses, a base de qualificação (incluindo os and subjective tests) for the re - qualification testes objetivos e subjetivos ) para as futuras will be those of which the FSTD was originally qualificações recorrentes será a mesma evaluated and qualified ; or utilizada à época da qualificação inicial deste FSTD ; ou Origem: S P O 15 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 (ii) n ot restored under section 60.27 of (ii) n ão for restaurada conforme this regulation for 24 months or mor e, then the seção 60. 27 deste regulamento em 24 meses FSTD will be evaluated for initial qualification ou mais, então o FSTD deverá ser avaliado in accordance with the section 60.15 of this para qualificação inicial conforme a seção regulation , at the time of re - qualification 60.15 deste regulamento , quando a application. requalificação for solicitada .

( c ) Except as provided in paragraph ( d ) of ( c ) Exceto como previsto no parágrafo ( d ) this section, any change in FSTD qualification desta seção, qualquer mudança no nível de level requires an evaluation for initial qualificação do FST D requer uma avaliação qualification in accordance with 60.15 of this para qualificação inicial conforme seção regulation . 60.15 deste regulamento .

( d ) A sponsor may request that a n FSTD be ( d ) Um operador pode solicitar que um permanently downgraded. In such a case, FSTD tenha o seu nível de qualificação ANAC may downgrade a qualified FSTD permanentemente degradado. Neste caso, a without requiring and without conducting an ANAC degradará o nível de qualificação do initial evaluation for the new qualification FSTD sem a necessidade de conduzir uma level. Subsequent continuing qualification avaliação para qualificação inicial. As evaluations will use the existing MQTG, avalia ções futuras para qualificação modified as necessary to reflect the new recorrente utilizarão o MQTG existente, qualificati on level. modificado como necessário para refletir o novo nível de qualificação.

( e ) When the sponsor has appropriate ( e ) Um operador que possua dados de validation data available and receives approval validação da aeronave adequados disponíveis from ANAC , the sponsor may a dopt tests and e que receba aprovação da ANAC, poderá associated tolerances described in the current adotar os testes e as tolerâncias estabelecidas qualification standards as the tests and na base de qualificação atual como os testes e tolerances applicable for the continuing tolerâncias aplicáveis para as futuras qualification of a previously qualified FSTD. qualificações recorrentes de um FSTD The updated test(s) and tolerance(s) must be previamente qualificado. As atualizações de made a permanent part of the MQTG. teste(s) e tolerância(s) deverão tornar - se parte permanente do MQTG.

60.19 Inspection, continuing qualification 60.19 Requisitos de inspeção, avaliação evaluation, and maintenance requirements para qualificação recorrente e manutenção (a) Inspection. A sponsor may only use a n (a) Inspeção. U m operador somente FSTD if the sponsor does: poderá utilizar um FSTD se : (1) a ccomplish all appropriate objective (1) realizar todos os testes objetivos tests each year as specified in the QPS , or in apropriados, progressivamente durante cada the original qualification basis of the FSTD, or ano, confor me especificado no QPS , ou na as may be amended by a n FSTD d irective ; and base de qualificação original do FSTD , ou como requerido por uma diretriz de FSTD ; e (2) c omplete a functional preflight check (2) realizar uma inspeção pré voo within the preceding 24 hours. funcional nas 24 horas precedent es.

(b) Continuing qualification evaluation. (b) Avaliação para qualificação recorrente.

Origem: S P O 16 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 (1) This evaluation consists of objective (1) Esta avaliação consiste de testes tests, and subjective tests, as described in the objetivos e subjetivos, como descrito pelo QPS , or in the original qualification basis of QPS , ou pela base de qualificação original do the FSTD , or as may be amended by a n FSTD FSTD , ou como requerido por uma diretriz de d irective . FSTD .

(2) The sponsor must contact ANAC to ( 2 ) O operador deve entrar em contato schedule the FSTD for continuing qualification com a ANAC para agendar a avaliação para evaluations not later than 60 days before the qualificação recorrente do FSTD com pel o evaluation is due , which must be confirmed by menos 60 dias de antecedência ao dia da ANAC . avaliação pretendida, cuja confirmação dar - se - á de acordo com a disponibilidade da ANAC .

(3) The sponsor must provide the ANAC (3) O operador deve fornecer a ANAC access to the objective test results in the acesso aos resultados dos testes objetivos do MQTG and access to the FSTD for the length MQTG e acesso ao FSTD o tempo necessário of time necessary to complete the required para completar a avaliação para quali ficação continuing qualification evaluations . recorrente.

(4) The frequency of ANAC - conducted ( 4 ) A frequência das avaliações para continuing qualification evaluations for each qualificação recorrente conduzidas pela FSTD will be established by the ANAC and ANAC para cada FSTD será estabelecida pela specified in the Statement of Qualification . ANAC e especificada no seu C ertificado de Q ualificação.

( 5 ) Continuing qualification evaluation ( 5 ) A avaliação para qualificação may occur at any time in the three months recorrente pode ocorrer a qualquer momento p receding the expiration date of the Statement nos três meses que antecedem o vencimento of Qualification . do Certificado de Qualificação vigente.

(6) No sponsor may use a n FSTD unless (6) Nenhum operador pode utiliz a r um the FSTD has passed an ANAC - conducted FSTD a menos que o FSTD tenha passado por continuing evaluation within the period uma avaliação para qualificaç ão recorrente , specified in the Statement of Qualification . conduzida pela ANAC, dentro do período especificado no seu Certificado de Qualificação.

(c) Maintenance. The sponsor is responsible (c) Manutenção. O operador é responsável for continuing corrective and preventive pela manutenção corretiva e preventiva do maintenance on the FSTD to ensure that it FSTD a fim de garantir o cumprimento dos continues to meet the actual requirements. The requisitos vigentes. O operador é responsável sponsor is responsible for: por: (1) m aintains a discrepancy log ; and (1) manter o registro das discrepâncias; e (2) e nsures that, when a discrepancy is (2) garantir que, quando encontrada found , the following requirements are met: uma discrepância, as seguintes providências sejam tomadas: (i) the description of each discrepancy (i) seja incluída no registro a is included in the discrepancy log and it descrição da discrepância e esta permane ça remains in the log until the discrepancy is no registro até que seja corrigida conforme Origem: S P O 17 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 corrected as specified in paragraph 60.25(b) of especificado no parágrafo 60.25(b) deste this regulation; regulamento; (ii) the description of the corrective (ii) seja incluída no registro a ação action taken , the identity of the individual who corretiva adotada, a identificação do autor da made the correction and the date that the correção e a data em que ela ocorreu; e corrective action was ta ken is included in the discrepancy log ; and (iii) t he discrepancy log is kept in a (iii) que o registro de discrepâncias form and manner acceptable by ANAC , within seja mantido em uma forma aceitável pela the FSTD or in an adjacent location . An ANAC, dentro do FSTD ou em local electronic re gister that can be accessed by a adjacente. Um registro eletrônico que possa computer or display located in the FSTD or in ser acessado por um terminal ou monitor an adjacent location is acceptable. localizado no FSTD ou em local adjacente é aceitável.

60.20 Logging FSTD discrepancies 60.20 Registro de discrepâncias do FSTD (a) Each instructor, check airman, or (a) Cada instrutor, examinador representative of the ANAC conducting credenciado ou servidor da ANAC training, evaluation, or flight experience, and conduzindo ou acompanhando treinamento, each person conducting the preflight avaliação ou experiência de voo, e cada inspection who finds out a discrepancy, any pessoa conduzindo a inspeção pré voo que missing, malfunctioning, or inoperative verifique uma discrepância, qualquer components in the FSTD, must include or componente faltante, com mau cause to be included a description of that funcionamento ou inoperante no FSTD, discrepancy into the discrepancy log . deverá incluir ou fazer com que seja incluída a descrição desta discrepância no registro de discrepâncias.

60.21 Interim qualification of FSTDs for 60. 2 1 Qualificação provisória de FSTDs de new aircraft types or models novos tipos ou modelos de aeronaves (a) A sponsor may apply for and ANAC (a) Um operador pode solicitar e a ANAC may issue an interim qualification level for a n pode emitir uma qualificação provis ó ria para FSTD for a new type or model of aircraft, even um FSTD que simule um novo tipo ou though the aircraft manufacturer's aircraft data modelo de aeronave, mesmo que o pacote de package is preliminary, if the sponsor provides dados do fabricante da aeronave seja the following to the satisfaction of ANAC: preliminar, mediante a aceitação dos seguintes documentos : (1) t he aircraft manufacturer's data, (1) o s dados do fabricante da aeronave, which consists of at least predicted data, que podem ser estimados, validados por um validated by a limited set of flight test data; pacote limitado de dados de ensaio em voo ; (2) t he aircraft manufacturer's (2) a descrição do fabricante da description of the prediction methodology used aeronave da metodologia de predição to develop the predicted data; and utilizada para desenvolver os dados; e (3) t he QTG test results. (3 ) o s resultados do QTG .

Origem: S P O 18 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 (b) A n FSTD that has been issued interim (b) Uma qualificação interina de FTSD é qualification is deemed to have been issued considerada uma qualificação inicial, a menos initial qualification , unless the ANAC rescinds que a ANAC revogue a qualificação. A the qualification. Interim qualification expire s qualificação provisó ria de um FSTD termina two years after the issuance of Statement of dois anos após a emissão do Certificado de Qualification of this FSTD , unless the ANAC Qualificação deste FSTD, a menos que a determines that specific conditions warrant ANAC determine que condições otherwise. excepcionais devam ser aplicadas.

(c) Within 12 months of the release of the (c) Dentro de 12 meses após a final aircraft data package by the aircraft disponibilização pelo fabricante do pacote manufacturer, but no later than two years after final de dados da aeronave, mas não após 2 the issuance of the interim Statement of anos da emissão do C ertificado de Qualification , the sponsor must apply for Q ual ificação interina, o requerente deverá initial qualification in accordance with section solicitar uma avaliação para qualificação 60.15 of this regulation, based on the final inicial de acordo com a seção 60.15 deste aircraft data package approved by the aircraft regulamento, baseada no pacote final de manufacturer, unless the ANAC determines dados da aeronave, aprovado pelo fabricante that specific conditions warrant otherwise. da aeronave, a menos que a ANAC determine que condições excepcionais devam ser aplicadas.

(d) A n FSTD with interim qualification may (d) Um FSTD com uma qualificação be modified only in accordance with section provisória só pode ser modificado conforme a 60.23 of this regulation . seção 60.2 3 deste regulamento .

60.23 Modifications to FSTDs 60.2 3 Modificações a FSTDs (a) . For the purposes of this regulation, a n (a) Para os propósitos deste regulamento, FSTD is said to have been modified when: um FSTD é considerado como tendo sido modificado quando: (1) e quipment or devices intended to (1) f orem adicionados ou removidos simulate aircraft appliances are added to or equipamentos ou dispositivos que simulem as removed from FSTD, which change the características da aeronave, resultando em Statement of Qualification or the MQTG; or uma alter ação no Certificado de Qualificação ou no MQTG; ou (2) c hanges are made to either software (2) forem realizadas alterações no or hardware that are intended to impact flight hardware ou software do FSTD, com a or ground dynamics; changes are made that intenção de impactar a simulação da dinâmica impact performance or handling characteristics de solo ou de voo; forem realizadas alterações of the FSTD (including motio n, visual, control com a int enção de impactar o desempenho e a loading, or sound systems for those FSTD qualidade de voo do FSTD (incluindo o levels requiring sound tests and control loading e os sistemas de movimento, measurements); or changes are made to the visual ou som); ou forem realizadas MQTG. Changes to the MQTG which do not alterações no MQTG. Alterações no MQTG affect required objective testing results or que não afetarem os resultados dos testes validation data approved during the i nitial objetivos requeridos o u os dados de validação evaluation of the FSTD are not considered aprovados na avaliação para qualificação modifications under this section.

Origem: S P O 19 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 inicial do FSTD não são consideradas modificações para os propósitos dessa seção.

(b) FSTD d irective. When the ANAC (b) Diretriz de FSTD. Quando a ANAC , determines that FSTD modification is por meio de uma diretriz, determinar a necessary for safety of flight reason s, the necessidade de uma modificação no FSTD, sponsor of each affected FSTD must ensure para assegurar a segurança das operações, o that the FSTD is modified according to the operador de cada FSTD afetado deve garantir FSTD d irective. o comprimento d esta .

(c) Using the modified FSTD . The sponsor (c) Utilização de um FSTD m odificado. O may only use a n FSTD with the proposed operador só pode utilizar um FSTD com a modification if : modificação proposta se : (1) t he sponsor has notified ANAC of ( 1 ) o operador t iver notifica do à ANAC their intent to incorporate the proposed a intenção de incorporar a modificação modification, and one of the following has proposta , e pelo menos um dos seguintes occurred; eventos tenha ocorrido: (i) the ANAC r esponded the (i ) a ANAC respondeu que a modification was approved; or modificação foi aprovada; ou (ii) t he sponsor has successfully (ii) o operador realizou com sucesso completed any evaluation the ANAC qualquer avaliação que a ANAC determinou designated as necessary before the modified ser necessária, antes que ele seja recolocado FSTD is implemented ; and em operação com a modificação proposta ; e (2) t he notification is submitted with the (2) a notificação for submetida à ANAC content as and in a form and a manner as com seu conteúdo e forma conforme specified in the applicable QMS . especificado no QMS aplicável .

(d) When a modification is made to a n (d) Quando uma modificação for realizada FSTD that affects the Statement of em um FSTD e esta afeta r o Certificado de Qualification, as described in 60.23(a), the Qualificação, conforme a parágrafo 60. 2 3 (a) sponsor must add an addendum to the deste regulamento, o operador deve anexar o Statement of Qualification until a n updated adendo ao Certificado até que seja emitido S tatement is issued . um Certificado de Qualificação atualizado.

(e) MQTG update . E ach time a n FSTD is (e) Atualização do MQTG. C ada vez que modified and an objective test or other MQTG um FSTD for modificado e esta modificação section is affected by the modification , t he afet ar um teste objetivo ou outra seção do MQTG must be updated with current objective MQTG , o MQTG deve ser atualizado d e test results in accordance with the paragraphs acordo com os resultados dos testes objetivos 60.15(h) and (i) of this regulation , and with descritos n os parágrafos 60.15(h) e (i) deste appropriate objective data in accordance with regulamento , fundamentados em dados the section 60.13 of this regulation . If a n FSTD objetivos conforme a seção 60.13 deste d irective is the cause of this update, th is regulmento . Se uma diretriz da ANAC for a directi ve to make the modification and the causa da atualização, est a diretriz para record of the modification completion must be real izar a modificação e os registros da kept in the MQTG. conclusão da modificação devem ser arquivados no MQTG.

Origem: S P O 20 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 60.25 Operation with missing, 60.25 Operação do FSTD com malfunctioning, or inoperative components componentes faltantes, com mau funcionamento ou inoperante s (a) No person may knowingly use a n FSTD (a) Nenhuma pessoa pode , for any maneuver, procedure, or task that is to intencionalmente , utilizar um FSTD para be accomplished when there is a missing, executar qualquer manobra, procedimento ou malfunctioning, or inoperative (MMI) tarefa quando houver componente f altante, component that i s required to be present and com mau func ionamento ou inope rante correctly operate for the satisfactory ( missing, malfunctioning, or inoperative - completion of that task. MMI) , caso este componente seja requerido para executar s a tisfatoriamente aquela manobra, procedimento ou tarefa .

(b) Each MMI component , as described in ( b) Todo componente MMI , conforme paragraph (a) of this section, or any MMI descrito no parágrafo (a) desta seção, component installed and required to operate requerido para atender ao funcionamento correctly to meet the current Statement of correto do FSTD, conforme o Certificado de Qualification, must be repaired or replaced Qualificação em vigor , deve ser reparado ou within 30 calendar days, unless otherwise substituído dentro de 30 dias, exceto quando authorized by ANAC. autorizado de maneira diferente pela ANAC.

(c) A list of the current MMI components (c) Uma lista dos componentes MMI deve must be readily available in or adjacent to the estar disponível no FSTD ou em local FSTD for review by users of the device. adjacente para ser consultada pelos usuários .

Electronic access to this list via an appropriate Acesso eletrônico para esta lista por meio de terminal or display in or adjacent to the FSTD um terminal ou monitor localizado no FSTD is satisfactory. The discrepan cy log may be ou em local adjacente é aceitável . O registro used to satisfy this requirement provided each de discrepâncias pode ser utilizado para currently MMI component is listed in the cumprir este requisito, desde que cada discrepancy log. componente MMI no momento esteja listado no registro de discrepâncias .

60.27 Automatic suspension of qualification 60. 27 Suspensão automática d a and procedures for restoration of qualificação e procedimentos para qualification restauração da qualificação (a) A n FSTD qualification is automat ically (a) A qualificação de um FSTD é suspended when any of the following occurs: automaticamente suspensa quando qualquer uma das situações a seguir ocorrer: (1) t he FSTD is not used in any ANAC - (1) o FSTD não for utilizado , nos approved flight training program within the últimos 12 meses, em um programa de last 12 months in accordance with the treinamento aprovado pela ANAC de acordo paragraphs 60.7(b)( 2 ) or ( c )( 1 ) of this com os parágrafos 60.7 (b)( 2 ) ou (c)(1) deste regulation and the sponsor does not obtain and regulamento e o operador não obt iver n e m maintain a written statement as described in the mant iv e r uma declaração escrita em paragraph 60.7( c) (2) of this regulation; conformidade com o parágrafo 60.7(c)(2) d este regulamento; Origem: S P O 21 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 (2) t he FSTD is not inspected in (2) o FSTD não for inspecionado, accordance with the section 60.19 of this avaliado e mantido conforme a seção 60. 19 regulation; deste regulamento; (3) t he FSTD is physically moved from (3) o FSTD for fisicamente movido de one location and installed in a different uma localização e instalado em uma location, regardless of distance ; localização diferente , independentemente da distância ; (4) t he MQTG is missing or otherwise (4) o MQTG est iver por qualquer not available and a replacement is not made motivo indisponível e um sobressalente não within 30 days ; or for confeccionado em 30 dias ; or (5) if the F S TD were out of service for a (5) o FSTD for inativado por período prolonged period . The ANAC will the prolongado . A ANAC determinará o critério evaluation criteria for an F STD that has been de retorno a serviço do FSTD baseada no removed from active status based on the número de avaliações contínuas de number of continuing qualification evaluations qualificação e inspeções progressivas de an d inspections established in paragraph acordo com o parágrafo 60.19(a) deste 60.19(a) missed during the period of inactivity . regulamento perdidas dur ante o período de inatividade.

(b) If the FSTD qualification is suspended (b) Em caso de suspensão d a qualificação under paragraph (a) of this section, suspension do FSTD conforme o parágrafo ( a) desta may be re voked if either of the following seção, a suspensão poderá ser re vogada desde provisions is met: que uma das seguintes condições seja atendida: (1) t he FSTD must successfully pass an (1) o FSTD deve ser aprovado em uma avaliação como determinad o pela ANAC; ou evaluation as determined by ANAC; o r (2) t he ANAC advises the sponsor that an (2) a ANAC comunica r ao operador que evaluation is not necessary. uma avaliação não é necessária.

(c) In determin ing the criteria for the (c) Ao determina r os critérios para a evaluation mentioned in paragraph (b) (1) of avaliação mencionada no parágrafo ( b ) (1) this section, the ANAC considers factors such desta seção, a ANAC considera fatores tais as the number of continuing qualification como a quantidade de avaliaç ões recorrentes evaluations missed, the number of sponsor - perdidas, a quantidade de inspeções não conducted quarterly inspections missed, the conduzidas pelo operador , o cuidado tomado care that had been taken of the device since the com o FSTD desde a sua última avaliação , last evaluation , among others . dentre outros .

60. 29 Suspension and revocation of 60.29 Suspensão e revogação da qualification by ANAC qualificação pela ANAC (a) The ANAC may suspend . partially or (a) A ANAC pode suspender parcialmente totally, an operator or a FSTD qualification ou totalmente a qualificação de um FSTD when it is found that: quando for constatado que: (1) the FSTD’s qualification standards (1) o FSTD deixou de atender aos are no longer met ; padrões de qualificação; Origem: S P O 22 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 (2) the operator simulated the (2) o operador simulou o cumprimento compliance of any of the requirements and de qualquer dos requisitos e padrões mínimos minimum qualification standards or provided de qualificação ou forneceu informações incomplete, inaccurate or false information incompletas, inexatas ou falsas com a with the purpose of obtaining a FSTD finalidade de obter um Certificado de Stat ement of Qualification; or Qualificação de FSTD; ou (3) the operator i s not able to (3) o operador não consegue demonstrate that the QMS is implemented and demonstrar que o QMS esteja implantado e operating, or being implemented, in operando, ou em proce sso de implantação de accordance with the section 60. 5 of this acordo com a seção 60.5 deste regulamento.

regulation .

(b) The ANAC may revoke a FSTD’s or an (b) A ANAC pode revogar um Certificado operator’s Statement of Qualification when the de Qualificação de FSTD quando o operador operator or the FSTD is suspended and it is ou o FSTD tiver sido suspenso e for found that the operator does not have interest constatado que o operador não tem interesse or capacity t o regularize the situation. ou capacidade para regularizar a situação.

(c ) If the qualification of a FSTD is (c) Se a qualificação de um FSTD for suspended in accordance with paragraph ( a ) of suspensa conforme o parágrafo (a) desta this section, the suspension may be re voked in seção, a suspensão poderá ser revogada de accordance to the criteria described in acordo com os critérios expostos no parágrafo paragraph 60.27(b) of this regulation . 60.27(b) deste regulamento.

(d ) In determin ing the criteria for the (d) Ao determinar os critérios para a evaluation referred to in paragraph 60.27(b)(1) avaliação mencionada no parágrafo of this regulation for the re vocation of the 60.27(b)(1) deste regulamento para a suspension , ANAC considers factors such as revogação da suspensão, a ANAC considera the reason to suspend the qualification, any fatores tais como o motivo da suspensão da repairs or replacements that may have been qualificação, os reparos que possam ter sido completed , the number of continuing necessários, a quantidade de avaliações qualification evaluations missed, the number recorrentes perdidas, a quantidade de of sponsor - conducted quarterly inspections inspeções não conduzidas pelo operador e o missed, and the care that had been taken of the cuidado tomado com o FSTD desde a device since the loss of qualification , among suspensão da qualificação, dentre outros.

others .

60.31 Record keeping and reporting 60. 31 Registros e documentação (a) The FSTD sponso r must maintain the (a) O operador de FSTD deve manter os following records for each FSTD operate d : s eguintes registros para cada FSTD que opere: (1) t he MQTG and each amendment (1) o MQTG com todas as suas revisões thereto ; e emendas ; (2) a record of all FSTD modifications (2) u m registro de todas as affected by the section 60.23 of this regulation modificações de FSTD afetadas p ela seção since the issuance of the original Statement of 60.2 3 deste regulamento desde a emissão do Qualification ; primeiro Certificado de Qualificação ; Origem: S P O 23 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 (3) a copy of all of the following: (3) u ma cópia de cada um dos seguintes registros: (i) r esults of the qualification (i) r esultados das avaliações de evaluations (initial and each upgrade) since the qualificação (inici al e cada elevação de nível) issuance of the original Statement of desde a emissão do primeiro Certificado de Qualification ; Qualificação ; (ii) r esults of the objective tests (ii) r esultados dos testes objetivos conducted in accordance with the section conduzidos de acordo com o parágrafo 60.19(a) of this regulation for a period of 2 60.19 (a) deste regulamento po r um período years ; de 2 anos ; (iii) r esults of the previous three (iii) r esultados das três últimas continuing qualification evaluations, or the avaliações de qualificação recorrente, ou das continuing qualification evaluations from the avalições recorrentes que ocorreram nos 2 previous 2 years, whichever covers a longer últimos anos, a qual cobrir um período de period ; and tempo maior ; e (iv) reports obtain ed in accordance (iv) relatos obtidos de acordo com o with the paragraph 60.9(b) of this regulation parágrafo 60. 9 (b) deste regulamento por um for a period of at least 90 days ; and período de pelo menos 90 dias ; e (4) a record of all discrepancies entere d (4) u m registro de todas as in the discrepancy log over the previous 2 discrepâncias inseridas no registro de years, including the following: discrepâncias nos 2 últimos anos, incluindo: (i) a list of the components or (i) u ma lista dos componentes ou equipment that were or are MMI; equipamentos que estiveram ou estão MMI; (ii) t he action taken to correct the (ii) a ação corretiva tomada para discrepancy ; sanar a discrepância ; (iii) t he dat e that the corrective action (iii) a data na qual a ação corretiva was taken ; and foi tomada ; e (iv) t he identity of the person that (iv) a identificação da pessoa que determin ed that the discrepancy has been determinou que a discrepância foi sanada.

corrected.

(b) The records specified in this section (b) Os registros especificados nest a seção must be maintained in plain language form or devem ser mantidos escritos em língua in coded form if the coded form is able to portuguesa ou inglesa, ou de forma preserv e and retriev e the information in a codificada, se a forma de codificação for manner acce ptable to the ANAC . capaz de preserva r e recupe ra r a informação de forma aceitável pela ANAC.

60.3 3 [Reserved] 60.33 [Reservado] 60.3 5 [ Reserved] 60.35 [Reservado] Origem: S P O 24 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 60.37 FSTD qualification based on the 60.37 Qualificação de FSTD baseada em evaluation conducted by an ICAO avaliação realizada por um país signatário contracting State da ICAO (a) Validation. T he evaluation and (a) Validação. A avaliação e qualificação qualification of a n FSTD by a contracting State de um FSTD realizada por um país signatário to the Convention on International Civil da Convenção de Aviação Civil Internacional Aviation may be used as the basis for issuing a poderá ser utilizada como base para a emissão Brazilian S tatement of Q ualification by the de um Certificado de Qualificação brasileiro ANAC to the sponsor of that FSTD , provided pela ANAC, para o operador daquele FSTD, the FSTD qualification performance standards se os padrões de desempenho para and surveil lance of that State are consistent qualificação e vigilância de FSTD daquele with this regulation , in accordance with criteria país forem consistentes com os deste RBAC defined in Suplementary Instr u ctions. conforme critérios a serem estabelecidos em Instrução Suplementar .

(b) An FSTD sponsored by a foreign civil (b) Um FSTD operado por Centro de aviation training center certified by a Treinamento da Aviação Civil (CTAC) contracting State to the Convention o n certificado por um país signatário da International Civil Aviation will be recognized Convenção de Aviação Ci vil Internacional as validated by ANAC if: será considerado validado pela ANAC se: (1) the FSTD qualification is valid with (1) A qualificação do FSTD estiver the foreign civil aviation authority; válida junto à Autoridade de Aviação Civil estrangeira; (2) the foreign civil aviation training center certificate is validated by ANAC in (2) O certificado do CTAC estrangeiro accordance with RBA C 142; estiver validado pela ANAC em conformidade com RBAC nº 142; e (3) the FSTD qualification performance standards and surveillance of that State are (3) Os padrões de desempenho para consistent with this regulation. qualificação e vigilância de FSTD daquele país forem consistentes com os deste RBAC.

( c ) The ANAC may evaluate and establish ( c ) A ANAC poderá avaliar e estabelecer restrictions t o a n FSTD qualified by an ICAO restrições a um FSTD qualificado por um país contracting State. signatário da ICAO.

Origem: S P O 25 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 APÊNDICE A ( APPENDIX A ) QUALIFICATION PERFORMANCE REQUISITOS DE DESEMPENHO PARA STANDARDS FOR AIRPLANE FULL QUALIFICAÇÃO DE SIMULADOR DE FLIGHT SIMULATORS VOO (FFS) DE AVIÃO ( a ) In order to be qualified at a particular ( a ) Para ser qualificado a um determinado qual ification level, the FFS must meet the nível, o FFS deve cumprir os requisitos standards listed in tables A1, A2 , A3 and A 4 of listados nas tabelas A1, A2 , A3 e A 4 deste this appendix , avaiable only in english . apêndice , disponíveis apenas em língua inglesa.

( b ) Each FFS must have a QTG, acceptable ( b ) Cada FFS deve possuir um QTG, aceito to the ANAC, that includes: pela ANAC, contendo: ( 1) Objective data obtained from ( 1 ) Dados objetivos obtidos de ensaio em traditional aircraft testing or another approved voo da aeronave ou outra fonte de dados source ; aprovada; (2) The results of FFS objective tests ; (2) Os resultados dos testes obj etivos do FFS; (3) The result s of FFS subjective tests ; (3) Os resultados dos testes subjetivos do and F F S; e (4) A description of the equipment (4) Uma descrição do equipamento necessary to perform the evaluation for initial necessário para executar a s avaliaç ões para qualification and the continuing qualification qualificação inicial e para qualificação evaluations. recorrente.

Origem: S P O 26 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Table A1 - General technical requirements for level A, B, C and D full - flight simulators - Airplane Qualification General technical requirements Level The lowest level of FFS technical complexity.

An enclosed full - scale replica of the airplane cockpit/flight deck including simulation of all systems, instruments, navigational equipment, communications, and caution and warning systems.

An instructor’s station with seat should be provided. Seats for t he flight crew members and two seats for inspectors/observers should also be provided.

Control forces and displacement characteristics should correspond to those of the replicated airplane and they should respond in the same manner as the airplane under t he same flight conditions.

A The use of class - specific data tailored to the specific airplane type with fidelity sufficient to meet the objective tests, functions and subjective tests is allowed.

Generic ground effect and ground handling models are permitt ed.

Motion, visual and sound systems sufficient to support the training, testing and checking credits sought are required.

The visual system should provide at least 45 degrees horizontal and 30 degrees vertical field of view per pilot.

The response to co ntrol inputs should not be greater than 300 ms more than that experienced on the airplane.

See table A2 for more simulator requirements.

As for level A, plus: Validation flight test data should be used as the basis for flight and performance and systems’ characteristics.

B Additionally, ground handling and aerodynamics programming to include ground effect reaction and handling characteristics should be derived fr om validation flight test data.

See table A2 for more simulator requirements.

The second highest level of FFS fidelity.

As for level B, plus: A daylight/twilight/night visual system is required with a continuous, cross - cockpit, minimum collimated visual field of view providing each pilot with 176 degrees horizontal and 36 degrees vertical field of view.

A six - degrees - of - freedom motion system sh ould be provided.

The sound simulation should include the sounds of precipitation and other significant airplane noises perceptible to the pilot and should be able to reproduce the sounds of a C crash landing.

The response to control inputs ( motion and inst rument cues) should not be greater than 100 ms more than that experienced on the airplane. For a visual system cues should not be greater than 120 ms more than that experienced on the airplane.

Wind shear simulation should be provided.

An upset prevention and recovery training (UPRT) instructor operating station (IOS) feedback mechanism should be available.

See table A2 for more simulator requirements.

The highest level of FFS fidelity.

As for level C, plus: D Extended set of sound and motion buffet tests.

Improved aerodynamic modeling.

See table A2 for more simulator requirements.

Origem: S P O 27 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Table A 2 - General Simulator Requirements Entry Simulator Number General Simulator Requirements Levels Notes/Information 1. General Flight Deck Configuration. See below NA The simulator must have a flight deck that is a replica of the airplane simulated with For simulator purposes, the flight 1.a. A,B,C,D controls, equipment, observable flight deck indicators, circuit breakers, and deck consists of all that space bulkheads properly located, functionally accurate and replicating the airplane. The forward of a cross section of the direction of movement of controls and switches must be identical to the airplane. flight deck at the most extreme aft Pilot seats must allow the occupant to achieve the design “eye position” established sett ing of the pilots' seats, for t he airplane being simulated. Equipment for the operation of the flight deck including additional required windows must be included, but the actual windows need not be operable. Additional crewmember duty stations and equipment such as fire axes, extinguishers, and spare light bulbs must be available in those required bulkheads aft of the the FFS but may be relocated to a suitable location as near as practical to the original pilot seats. For clarification, position. Fire axes, landing gear pins, and any similar purpose instruments need only bulkheads containing only items be represented in silhouette . such as landing gear pin storage compartments, fire axes and The use of electronically displayed images with physical overl ay or masking for extinguish ers, spare light bulbs, simulator instruments and/or instrument panels is acceptable provided: and aircraft document pouches are (1) All instruments and instrument panel layouts are dimensionally correct with not considered essential and may differences, if any, being imperceptible to the pilot; be omitted.

(2) Instruments replicate those of the airplane including full instrument functionality and embedded logic; (3) Instruments displayed are free of quantization (stepping); (4) Instrument display characteristics replicate those of the airplane including: resolution, colors, luminance, brig htness, fonts, fill patterns, line styles and symbology; (5) Overlay or masking, including bezels and bugs, as applicable, replicates the airplane panel(s); (6) Instrument controls and switches replicate and operate with the same technique, effort, travel and in the same direction as those in the airplane; Origem: S P O 28 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information (7) Instrument lighting replicates that of the airplane and is operated from the FSTD control for that lighting and, if applicable, is at a level commensurate with other lighting operated by that same control; and (8) As applicable, instruments must have faceplates that replicate those in the airplane; and (1) The display image of any three dimensional instrument, such as an electro - NA 1.a. C,D mechanical instrument, should appear to have the same three dimension al depth as the replicated instrument. The appearance of the simulated instrument, when viewed from the principle operator’s angle, should replicate that of the actual airplane instrument. Any instrument reading inaccuracy due to viewing angle and parallax present in the actual airplane instrument should be duplicated in the simulated instrument display image.

Viewing angle error and parallax must be minimized on shared instruments such and engine displays and standby indicators.

1.b. Those circuit breakers that affect procedures or result in observable flight deck A,B,C,D NA indications must be properly located and functionally accurate.

2. Programming. See below NA 2.a. A flight dynamics model that accounts for various combinations of drag and thrust A,B,C,D The SOC should include a range of normally encountered in flight must correspond to actual flight conditions, including tabulated target values to enable a the effect of change in airplane attitude, thrust, drag, altitude, temperature, gross demonstration of the mass weight, moments of inertia, center of gravity locati on, and configuration. properties model to be conducted from the instructor's station. The An SOC is required.

data at a minimum should contain 3 weight conditions including zero fuel weight and maximum taxi weight with a least 2 different combinations of zero fuel weight, fuel weight and payload for each Origem: S P O 29 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information condition.

2.a. For Level C and Level D simulators, the effects of pitch attitude and of fuel slosh on NA C,D the aircraft center of gravity must be simulated.

2.b. The simulator must have the computer capacity, accuracy, resolution, and NA A,B,C,D dynamic response needed to meet the qualification level sought.

An SOC is required.

2.c. Surface operations must be represented to the extent that allows turns within the A NA confines of the runway and adequate controls on the landing and roll - out from a crosswind approach to a landing.

2.d. Ground handling and aerodynamic programming must i nclude the following: NA See below 2.d.1. Ground effect. Ground effect includes B,C,D modeling that accounts for roundout, flare, touchdown, lift, drag, pitching moment, trim, and power while in ground effect.

2.d.2. Ground reaction. B,C,D Ground reaction includes modeling that accounts for strut deflections, Ground reaction modeling must produce the appropriate effects during bounced or tire friction, and side forces. This is skipped landings, including the effects and indications of ground contact due to the reaction of the airplane landing in an abnormal aircraft attitude (e.g. tailstrike or nosewheel contact). An uponcontact with the runway SOC is requ ired.

during landing, and may differ with changes in factors such as gross weight, airspeed, or rate of descent on touchdown.

Ground handling characteristics, including aerodynamic and ground reaction In developing gust models for use 2.d.3. B,C,D modeling including steering inputs, operations with crosswind, braking, thrust in training, the FSTD sponsor Origem: S P O 30 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information reversing, deceleration, and turning radius. should coordinate with the data provider to ensure that the gust An SOC is required describing source data used to constru ct gusting models do not exceed the crosswind profiles.

capabilities of the aerodynamic and ground models.

Aerodynamic and ground reaction modeling to support training in crosswinds and In developing gust models for use 2.d.3. C,D gusting crosswinds up to the aircraft’s maximum demonstrated crosswind in training, th e FSTD sponsor component. Realistic gusting crosswind profiles must be available to the instructors should coordinate with the data that have been tuned in intensity and variation to require pilot intervention to avoid provider to ensure that the gust runway departure during takeoff or landing roll. models do not exceed the capabilities of the aerodynamic and An SOC is required describing source data used to construct gusting ground models.

crosswind profiles.

If the aircraft being simulated is one of the aircraft listed in section 121.35 8 of If desired, Level A and B 2.e. C,D RBAC 121 , Low - altitude windshear system equipment requirements, the simulator simulators may qualify for must employ windshear models that provide training for recognition of windshear windshear training by meeting phenomena and the execution of recovery procedures. Models must be available to these standards.

the instructor/evaluator for the following critical phases of flight: Windshear models may consist of (1) Prior to takeoff rotation; independent variable winds in multiple simultaneous components.

(2) At liftoff; The simulator should employ a (3) During initial climb; and method to ensure the required (4) On final approach, below 500 ft AGL. survivable and non - survivable windshear scenarios are repeatable Only those simulators meeting these requirements may be used to satisfy the in the training environment.

training requirements of RBAC 121 pertaining to a certificate holder’s approved low - altitude windshear flight training program.

The addition of realistic levels of turbulence associated with each required windshear profile must be available and selectable to the instructor.

In addition to the four basic windshear models required for qualification, at least Origem: S P O 31 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information two additional “complex” windshear models must be available to the instr uctor which represent the complexity of actual windshear encounters. These models must be available in the takeoff and landing configurations and must consist of independent variable winds in multiple simultaneous components.

2.f. The sim ulator must provide for manual and automatic testing of simulator hardware C,D Automatic “flagging” of out - of - and software programming to determine compliance with simulator objective tests. tolerance situations is encouraged.

An SOC is required.

Relative responses of the motion system, visual system, and flight deck instruments, The intent is to verify t hat the 2.g. See below measured by latency tests or transport delay tests. Motion onset should occur before simulator provides instrument, the start of the visual scene change (the start of the scan of the f irst video field motion, and visual cues that are, containing different information) but must occur before the end of the scan of that within the stated time delays, like video field. Instrument response may not occur prior to motion onset. Test results the airplane responses. For must be within the following limits: airplane response, acceleration in the appropriate, corresponding rotational axis is preferred.

2.g.1. 300 milliseconds of the airplane response. A,B NA 2.g.2. 100 milliseconds of the airplane response (motion and instrument cues) C,D NA 120 milliseconds of the airplane response (visual system cues) 2.h. The simulator must accurately reproduce the following runway conditions: C,D NA (1) Dry; (2) Wet; (3) Icy;.

(4) Patchy Wet; (5) Patchy Icy; and Origem: S P O 32 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information (6) Wet on Rubber Residue in Touchdown Zone; An SOC is required.

2.i. The simulator must simulate: C,D Simulator pitch, side loading, and directional control characteristics (1) brake and tire failure dynamics, including antiskid failure; and should be representative of the (2) decreased brake efficiency due to high brake temperatures, if airplane.

applicable.

An SOC is required Engine and Airframe Icing SOC should be provided describing 2.j. C,D the effects which provide training Modeling that includes the effects of icing, where appropriate, on the airframe, in the specific skills required for aerodynamics, and the engine(s). Icing models must simulate the aerodynamic recognition of icing phenomena degradation effects of ice accretion on the airplane lifting surfaces including loss of and execution of recovery. The lift, decrease in stall angle of attack, change in pitching moment, decrease in control SOC should describe the source effectiveness, and changes in control forces in addition to any overall increase in data and any analytical methods drag. Aircraft systems (such as the stall protection system and autoflight syste m) used to develop ice accretion must respond properly to ice accretion consistent with the simulated aircraft.

models including verification that Aircraft OEM data or other acceptable analytical methods must be utilized to these effect s have been tested.

develop ice accretion models. Acceptable analytical methods may include wind Icing effects simulation models are tunnel analysis and/ or engineering analysis of the aerodynamic effects of icing on only required for those airplanes the lifting surfaces coupled with tuning and supplemental subjective assessment by a authorized for operations in icing subject matter expert pilot.

conditions.

SOC and tests required.

2.k. The aerodynamic modeling in the simulator must include: D (1) Low - altitude level - flight ground effect; (2) Mach effect at high altitude; (3) Normal and reverse dynamic thrust effect on control surfaces; Origem: S P O 33 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information (4) Aeroelastic representations; and (5) Nonlinearities due to sideslip.

An SOC is required and must include references to computations of aeroelastic representation s and of nonlinearities due to sideslip.

The simulator must have aerodynamic and ground reaction modeling for the effects 2.l. B,C,D NA of reverse thrust on directional control, if applicable.

An SOC is required.

High Angle of Attack Modeling The requirements in this section 2.m. C,D only apply to those FSTDs that are Aerodynamic stall modeling that includes degradation in static/dynamic lateral - qualified for full stall training tasks.

directional stability, degradation in control response (pitch, roll, and yaw), uncommanded roll response or roll - off requiring significant control deflection to Sponsors may elect to not qualify counter , apparent randomness or non - repeatability, changes in pitch stability, Mach an FSTD for full stall training effects, and stall buffet, as appropriate to the aircraft type. tasks; however, t he FSTD’s qualification will be restricted to The aerodynamic model must incorporate an angle of attack and sideslip range to approach to stall training tasks that support the training tasks. At a mi nimum, the model must support an angle of attack terminate at the activation of the range to ten degrees beyond the stall identification angle of attack. The stall stall warning system.

identification angle of attack is defined as the point where the behavior of the airplane gives the pilot a clear and distinct ive indication through the inherent flight characteristics or the characteristics resulting from the operation of a stall Specific guidance should be identification device (e.g., a stick pusher) that the airplane has stalled.

available to the instructor which The model must be capable of capturing the variations seen in the stall clearly communicates the flight characteristics of the airplane (e.g., the presence or absence of a pitch break, configurations and s tall maneuvers deterrent buffet, or other indications of a stall where present on the aircraft). The that have been evaluated in the aerodynamic modeling must support stall training maneuvers in the following flight FSTD for use in training.

conditions: (1) Stall entry at wings level (1g); Origem: S P O 34 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information (2) Stall entry in turning flight of at least 25° bank angle (accelerated stall); (3) Stall entry in a power - on condition (required only for propeller driven aircraft); and (4) Aircraft configurations of second segment climb, high altitude cruise (near performance limited condition), and approach or landing.

A Statement of Compliance (SOC) is required which describes the aerodynamic modeling methods, validation, and checkout of the stall characteristics of the FSTD.

The SOC must also include verification that the FSTD has been evaluated by a subject matter expert pilot acceptable to the ANAC.

Where known limitations exist in the aerodynamic model for particular stall maneuvers (such as air craft configurations and stall entry methods), these limitations must be declared in the required SOC.

FSTDs qualified for full stall training tasks must also meet the instructor operating station (IOS) requirements for upset prevention and recovery traini ng (UPRT) tasks as described in section 2.n. of this table.

This section generally applies to 2.n. Upset Prevention and Recovery Training (UPRT). C,D the qualification of airplane upset Aerodynamics Evaluation: The simulator must be evaluated for specific upset recovery training maneuvers or recovery maneuvers for the purpose of determining that the combination of angle of unusual attitude attack and sideslip does not exceed the range of flight test validated training maneuvers that exceed one data or wind tunnel/analytical data while performing the recovery maneuver. The or more of the following following minimum set of required upset recovery maneuvers m ust be evaluated in conditions: this manner and made available to the instructor/evaluator. Other upset recovery scenarios as developed by the FSTD sponsor must be evaluated in the same manner: Pitch attitude greater than 25 degrees, nose up (1) A nose - high, wings level aircraft upset; Pitch attitude greater than 10 (2) A nose - low aircraft upset ; and degrees, nose down (3) A high bank angle aircraft upset.

Origem: S P O 35 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information Upset Scenarios: IOS selectable dynamic airplane upsets must provide guidance to Bank angle greater than 45 degrees the instructor concerning the method used to drive the FSTD into an upset condition, Flight at airspeeds inappropriate for including any malfunction or degradation in th e FSTD’s functionality required to conditions.

initiate the upset. The unrealistic degradation of simulator functionality (such as FSTDs used to conduct upset degrading flight control effectiveness) to drive an airplane upset is generally not acceptable unless used purely as a tool for repositio ning the FSTD with the pilot out recovery maneuvers at angles of attack above the stall warning of the loop.

system activation must meet the Instructor Operating System (IOS): The simulator must have a feedback mechanism requirements for high angle of in place to notify the instructor/evaluator when the simulator’s validated attack modeling as described in aerodynamic envelope and aircraft operating limits have been exceeded during an section 2.m.

upset recovery training task. This feedback mechanism must include: Special consideration should be (1) FSTD validation envelope. This must be in the form of an alpha/beta given to the motion syste m envelope (or equivalent method) depicting the “confidence level” of the response during upset prevention aerodynamic model d epending on the degree of flight validation or source of and recovery maneuvers.

predictive methods The envelopes must provide the instructor real - time Notwithstanding the limitations of feedback on the simulation during a maneuver. There must be a minimum of a simulator motion, specific (2) flaps up and flaps down envelope available; emphasis should be placed on tuning out motion system (3) F light control inputs. This must enable the instructor to assess the pilot’s responses.

flight control displacements and forces (including fly - by - wire as appropriate); and Consideration should be taken with flight envelope protected airplanes (4) Airplane operational limits. This must display the aircraft operating limits as artificially positioning the during the man euver as applicable for the configuration of the airplane.

airplane to a specified attitude may Statement of Compliance (SOC): An SOC is required that defines the source data incorrectly initialize flight control used to construct the FSTD validation envelope. The SOC must also verify that each laws.

upset prevention and recovery featu re programmed at the instructor station and the associated training maneuver has been evaluated by a suitably qualified pilot using methods described in this section. The statement must confirm that the recovery maneuver can be performed such that the FSTD does not exceed the FSTD validation envelope, or when exceeded, that it is within the realm of confidence in Origem: S P O 36 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information the simulation accuracy.

3. Equipment Operation. See below NA 3.a. All relevant instrument indications involved in the simulation of the airplane must A,B,C,D NA automatically respond to control movement or external disturbances to the simulated airplane; e.g., turbulence or windshear. Numerical values must be presented in the appropriate units.

For Level C and Level D simulators, instrument indications must also respond to effe cts resulting from icing.

Communications, navigation, caution, and warning equipment must be installed and 3.b. A,B,C,D operate within the tolerances applicable for the airplane.

Instructor control of internal and external navigational aids. Navigation aids must be usable within range or line - of - sight without restriction, as applicable to the geographic area.

Complete navigation database for at least 3 airports with corresponding precision 3.b.1. C,D NA and non - precision approach procedures, including navigational database updates.

Complete navigation database for at least 1 airport with corresponding precision and 3.b.2. A,B NA non - precision approach procedures, including navigational database updates.

Simulated airplane systems must operate as the airplane systems operate under Airplane system operation should 3.c. A,B,C,D normal, abnormal, and emergency operating conditions on the ground and in flight. be predicated on, and traceable to, the system data supplied by the Once activated, proper systems operation must result from system management by airplane manufacturer, original the crew member a nd not require any further input from the instructor's controls.

equipment manufacturer or alternative approved data for the airplane system or component.

At a minimum, alternate approved data should validate the operation of all normal, abnormal, and Origem: S P O 37 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information emergency operating procedures and training tasks the FSTD is qualified to conduct.

3.d. The simulator mus t provide pilot controls with control forces and control travel that A,B,C,D NA correspond to the simulated airplane. The simulator must also react in the same manner as in the airplane under the same flight conditions.

Control systems must replicate airplane operat ion for the normal and any non - normal modes including back - up systems and should reflect failures of associated systems.

Appropriate cockpit indications and messages must be replicated.

3.e. Simulator control feel dynamics must replicate the airplane. This must be determined C,D NA by comparing a recording of the control feel dynamics of the simulator to airplane measurements. For initial and upgrade qualification evaluations, the control dynamic characteristics must be measured and rec orded directly from the flight deck controls, and must be accomplished in takeoff, cruise, and landing flight conditions and configurations.

For aircraft equipped with a stick pusher system, control forces, displacement, and 3.f. C,D The requirements in this section surface position must correspond to that of the airplane being simulated.

only apply to those FSTDs that A Statement of Compliance (SOC) is required verifying that the stick pusher system are qualified for full stall has been modeled, programmed, and validated using the aircraft manufacturer’s training tasks.

design data or other acceptab le data source. The SOC must address, at a minimum, stick pusher activation and cancellation logic as well as system dynamics, control displacement and forces as a result of the stick pusher activation.

Tests required.

4. Instructor or Evaluator Facilities. See below NA Origem: S P O 38 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information In addition to the flight crewmember stations, the simulator must have at least two The ANAC will consider 4.a. A,B,C,D suitable seats for the instructor/check airman and ANAC inspector. These seats must alternatives to this standard for provide adequate vision to the pilot's panel and forward windows. All seats other additional seats based on un ique than f light crew seats need not represent those found in the airplane, but must be flight deck configurations.

adequately secured to the floor and equipped with similar positive restraint devices.

The simulator must have controls that enable the instructor/evaluator to control all 4.b. A,B,C,D NA required system variables and insert all abnormal or emergency conditions into the simulated airplane systems as described in the sponsor’s ANAC - approved training program; or as described in the relevant operating manual as appropriate.

4.c. The simulator must have instructor controls for all environmental effects expected to A,B,C,D NA be available at the IOS; e.g., clouds, visibility, icing, precipitation, temperature, storm cells and microbursts, turbulence, and intermediate and high altitude wind speed and direction.

4.d. The simulator must provide the instructor or evaluator the ability to present ground C,D For example, another airplane and a ir hazards. crossing the active runway or converging airborne traffic.

5. Motion System. See below NA The simulator must have motion (force) cues perceptible to the pilot that are For example, touchdown cues 5.a. A,B,C,D representative of the motion in an airplane. should be a function of the rate of descent (RoD) of the simulated airplane.

5.b. The simulator must have a motion (force cueing) system with a minimum of three A,B NA degrees of freedom (at least pitch, roll, and heave).

An SOC is required.

The simulator must have a motion (force cueing) system that produces cues at least 5.c. C,D NA equivalent to those of a six - degrees - of - freedom, synergistic platform motion system Origem: S P O 39 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information (i.e., pitch, roll, yaw, heave, sway, and surge).

An SOC is required.

The simulator must provide for the recording of the motion system response time.

5.d. A,B,C,D NA An SOC is required.

5.e. The simulator must provide motion effects programming to include: See below NA (1) Thrust effect with brakes set; If there are known flight 5.e.1. B,C,D conditions where buffet is the first (2) Runway rumble, oleo deflections, effects of ground speed, uneven runway, indication of the stall, or where no centerline lights, and taxiway characteristics; stall bu ffet occurs, this (3) Buffets on the ground due to spoiler/speedbrake extension and thrust characteristic should be included reversal; in the model.

(4) Bumps associated with the landing gear; (5) Buffet during extension and retraction of landing gear; (6) Buffet in the air due to flap and spoiler/speedbrake extension; (7) Approach - to - stall buffet and stall buffet (where applicable); (8) Representative touchdown cues for main and nose gear; (9) Nose wheel scuffing, if applicable; (10) Mach and maneuver buffet; (11) Engine failures, malfunctions, and engine damage (12) Tail and pod strike; (13) Taxiing effects such as lateral and directional cues resulting from steering NA 5.e.2. C,D and braking inputs; (14) Buffet due to atmospheric disturbances (e.g. buffets due to turbulence, Origem: S P O 40 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information gusting winds, storm cells, windshear, etc.) in three linear axes (isotropic); (15) Tire failure dynamics; and (16) Other significant vibrations, buffets and bumps that are not mention ed above (e.g. RAT), or checklist items such as motion effects due to pre - flight flight control inputs.

5.f. The simulator must provide characteristic motion vibrations that result from D The simulator should be operation of the airplane if the vibration marks an event or airplane state that can be programmed and instrumented in sensed in the flight deck. such a manner that the characteristic buffet modes can be measured and compared to airplane data.

6. Visual System. See below NA 6.a. The simulator must have a visual system providing an out - of - the - flight deck view. A,B,C,D NA The simulator must provide a continuous collimated field - of - view of at least 45 º Additional field - of - view capability 6.b. A,B horizontally and 30 º vertically per pilot seat or the number of degrees necessar y to may be added at the sponsor’s meet the visual ground segment requirement, whichever is greater. Both pilot seat discretion provided the minimum visual systems must be operable simultaneously. The minimum horizontal field - of - fields of view are retained.

view coverage must be plus and minus one - half (½) of the minimum continuous field - of - view requirement, centered on the zero degree azimuth line relative to the aircraft fuselage.

An SOC is required and must explain the system geometry measurements including system linearity and field - of - view.

6.c. (Reserved) NA NA The simulator must provide a continuous collimated visual field - of - view of at least The horizontal field - of - view is 6.d. C,D 176° horizontally and 36° vertically or the number of degrees necessary to meet the tradition ally described as a 180º visual ground segment requirement, whichever is greater. The minimum horizontal field - of - view. However, the field - field - of - view coverage must be plus and minus one - half (½) of the minimum of - view is technically no less than Origem: S P O 41 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information continuous field - o f - view requirement, centered on the zero degree azimuth line 176º. Additional field - of - view relative to the aircraft fuselage. capability may be added at the sponsor’s discretion provided the An SOC is required and must explain the system geometry measurements including minimum fields of view are system linearity and field - of - view.

retained.

The visual system must be free from optical discontinuities and artifacts that create Non - realistic cues might include 6.e. A,B,C,D non - realistic cues. image “swimming” and image “roll - off,” that may lead a pilot to make incorrect assessments of speed, acceleration, or situational a wareness.

The simulator must have operational landing lights for night scenes. Wher e used, 6.f. A,B,C,D NA dusk (or twilight) scenes require operational landing lights.

6.g. The simulator must have instructor controls for the following: A,B,C,D NA (1) Visibility in statute miles (km) and runway visual range (RVR) in ft.(m); (2) Airport selection; and (3) Airport lighting.

The simulator must provide visual system compatibility with dynamic response 6.h. A,B,C,D NA programming.

The simulator must show that the segment of the ground visible from the simulator This will show the modeling 6.i. A,B,C,D flight deck is the same as from the airplane flight deck (within established accuracy of RVR, glideslope, and tolerances) when at the correct airspeed, in the landing configuration, at the localizer for a given weight, appropriate height abo ve the touchdown zone, and with appropriate visibility. configuration, and speed within the airplane's operational envelope for a normal approach and landing .

The simulator must provide visual cues necessary to assess sink rates (provide depth NA 6.j. B,C,D Origem: S P O 42 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information perception) during takeoffs and landings, to include: (1) Surface on runways, taxiways, and ramps; and (2) Terrain features.

6.k. The simulator must provide for accurate portrayal of the visual environment relating A,B,C,D Visual attitude vs. simulator to the simulator attitude. attitude is a comparison of pitch and roll of the horizon as displayed in the visual scene compared to the display on the att itude indicator.

The simulator must provide for quick confirmation of visual system color, RVR, 6.l. C,D NA focus, and intensity.

An SOC is required.

6.m. The simulator must be capable of producing at least 10 levels of occulting. C,D NA Night Visual Scenes. When used in training, testing, or checking activities, the 6.n. A,B,C,D NA simulator must provide night visual scenes with sufficient scene content to recognize the airport, the terrain, and major landmarks around the airport.

The scene content must allow a pilot to successfully accomplish a visual landing.

Scenes must include a definable horizon and typical terrain characteristics such as fields, roads and bodies of water and surfaces illuminated by airplane landing lights.

6 .o. Dusk (or Twilight) Visual Scenes. When used in training, testing, or checking C,D NA activities, the simulator must provide dusk (or twilight) visual scenes with sufficient scene content to recognize the airport, the terrain, and major landmarks around the airpo rt. The scene content must allow a pilot to successfully accomplish a visual landing. Dusk (or twilight) scenes, as a minimum, must provide full color presentations of reduced ambient intensity, sufficient surfaces with appropriate textural cues that inclu de self - illuminated objects such as road networks, ramp lighting and airport signage, to conduct a visual approach, landing and airport movement (taxi). Scenes must include a definable horizon and typical terrain Origem: S P O 43 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information characteristics such as fields, roads and b odies of water and surfaces illuminated by airplane landing lights. If provided, directional horizon lighting must have correct orientation and be consistent with surface shading effects. Total night or dusk (twilight) scene content must be comparable in d etail to that produced by 10,000 visible textured surfaces and 15,000 visible lights with sufficient system capacity to display 16 simultaneously moving objects.

An SOC is required.

Daylight Visual Scenes. The simulator must provide daylight visual scenes with 6.p. C,D NA sufficient scene content to recognize the airport, the terrain, and major landmarks around the airport. The scene content must allow a pilot to successfully accomplish a visual landing. Any ambient lighting must not “washout” the displayed visual scene.

Total daylight scene content must be comparable in detail to that produced by 10,000 visible textured surfaces and 6,000 visible lights with sufficient system capacity to display 16 simultaneously moving objects. The visual display must be free of apparent and distracting quantization and other distracting visual effects while the simulator is in motion.

An SOC is required.

The simulator must provide operational visual scenes that portray physical For example: short runways, 6.q. C,D relationships known to cause landing illusions to pilots. landing approaches over water, uphill or downhill runways, rising terrain on the approach path, unique topographic fea tures.

The simulator must provide special weather representations of light, medium, and 6.r. C,D NA heavy precipitation near a thunderstorm on takeoff and during approach and landing.

Representations need only be presented at and below an altitude of 2,000 ft. (610 m) above the airport surface and within 10 miles (16 km) of the airport.

The simulator must present visual scenes of wet and snow - covered runways, 6.s. C,D NA including runway lighting reflections for wet conditions, partially obscured lights for Origem: S P O 44 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information snow conditions, or suitable alternative effects.

The simulator must present realistic color and directionality of all airport lighting.

6.t. C,D NA The following weather effects as observed on the visual system must be Scud effects are low, detached, and 6.u. C,D simulated and respective instructor controls provided. irregular clouds below a defined cloud layer.

(1) Multiple cloud layers with adjustable bases, tops, sky coverage and scud effect; Atmospheric model should support representative effects of (2) Storm cells activation and/or deactivation; wake turbulence and mountain (3) Visibility and runway visual range (RVR), including fog and patchy fog waves as needed to enhance effect; UPRT training.

(4) Effects on ownship external lighting; The mountain wave model should support the atmospheric climb, (5) Effects on airport lighting (including variable intensity and fog effects); descent, and roll rates which can be (6) Surface contaminants (including wind blowing effect); encountered in mountain wave and (7) Variable precipitation effects (rain, hail, snow); rotor conditions.

(8 ) In - cloud airspeed effect; and (9) Gradual visibility changes entering and breaking out of cloud.

6.v. The simulator must provide visual effects for: C,D Visual effects for light poles and raised edge lights are for the (1) Light poles; purpose of pro viding additional depth perception during takeoff, (2) Raised edge lights as appropriate; and landing, and taxi training tasks.

(3) Glow associated with approach lights in low visibility before physical lights Three dimensional modeling of the are seen, actual poles and stanchions is not required.

A minimum of one (1) representative airport model required for simulator The model identifications must be 6.w A,B qualification . The fidelity of the airport model must be sufficient for the aircrew to acceptable to the ANAC, selectable Origem: S P O 45 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information visually identify the airport; determine the position of the simulated airplane within from the IOS, and listed on the a night v isual scene; successfully accomplish take - offs, approaches, and landings; SOQ.

and maneuver around the airport on the ground as necessary.

6.x A minim um of three (3) real - world airport models required for simulator C,D The model identifications must be qualification. Must be consistent with published data used for airplane operations. acceptable to the ANAC, selectable Each model should be in a different visual scene to permit assessment of FSTD from the IOS, and listed on the automatic visual scene change s. SOQ.

7. Sound System. See below NA The simulator must provide flight deck sounds that result from pilot actions that 7.a. A,B,C,D NA correspond to those that occur in the airplane.

The volume control must have an indication of sound level setting which meets all For Level D simulators, this 7.b. A,B,C,D indication should be readily qualification requirements.

available to the instructor on or about the IOS and is the sound level setting required to meet the objective testing requirements.

For all other simulator levels, this indication is the sound level setting as evaluated during the simulator’s initial evaluation.

The simulator must accurately simulate the sound of precipitation, windshield For simulators qualified for full 7.c. C,D wipers, and other significant airplane noises perceptible to the pilot during normal stall training tasks, sounds and abnormal operations, and include the sound of a crash (when the simulator is associated with stall buffet should landed in an unu sual attitude or in excess of the structural gear limitations); normal be replicated if significant in the engine and thrust reversal sounds; and the sounds of flap, gear, and spoiler extension airplane.

and retraction.

Sounds must be directionally representative.

Origem: S P O 46 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Number General Simulator Requirements Levels Notes/Information A SOC is required.

The simulator must provide realistic amplitude and frequency of flight deck noises NA 7.d. D and sounds. Simulator perf ormance must be recorded, compared to amplitude and frequency of the same sounds recorded in the airplane, and be made a part of the QTG .

Origem: S P O 47 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Table A 3 - Table of Tasks vs. Simulator Level – Subjective Requirements In order to be qualified at the simulator qualification level indicated, the simulator must be able to perform at least the tasks associated with that level of qualification.

Entry Simulator Number Subjective Requirements Levels Notes/Information 1. Preflight Procedures. See below 1.a. Preflight Inspection (flight deck only) A,B,C,D 1.b. Engine Start A,B,C,D 1.c. Taxiing B(R),C,D 1.d. Pre - takeoff Checks A,B,C,D 2. Takeoff and Departure Phase. See below 2.a. Normal and Crosswind Takeoff B(R),C,D 2.b. Instrument Takeoff A,B,C,D 2.c. Engine Failure During Takeoff A(a),B,C,D 2.d. Rejected Takeoff A,B,C,D 2.e. Departure Procedure A,B,C,D 3. Inflight Maneuvers. See below 3.a. Steep Turns A,B,C,D 3.b. High Angle of Attack Maneuvers See below 3.b.1 Approaches to Stall A,B,C,D Stall maneuvers at angles of attack 3.b.2 Full Stall C,D above the activation of the stall warning system.

Origem: S P O 48 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Subjective Requirements Number Levels Notes/Information Required only for FSTDs qualified to conduct full stall training tasks as indicated on the Statement of Qualification.

3.c. Engine Failure — Multiengine Airplane A,B,C,D 3.d. Engine Failure — Single - Engine Airplane A,B,C,D 3.e. Specific Flight Characteristics incorporated into the user’s ANAC A(a),B(a),C(a),D(a) approved flight training program.

Recovery From Unusual Attitudes Within the normal flight 3.f. A,B,C,D envelope supported by applicable simulation validation data.

Upset recovery or unusual attitude 3.g. Upset Prevention and Recovery Training (UPRT) C,D training maneuvers within the FSTD’s validation envelope that are intended to exceed pitch attitudes greater than 25 degrees nose up; pitch attitudes greater than 10 degrees nose down, and bank angles greater than 45 degrees.

4. Instrument Procedures. See below 4.a. Standard Terminal Arrival / Flight Management System Arrivals A,B,C,D Procedures Origem: S P O 49 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Subjective Requirements Number Levels Notes/Information 4.b. Holding A,B,C,D 4.c. Precision Instrument See below e.g., Autopilot, Manual (Flt. Dir.

4.c.1. All engines operating. A,B,C,D Assisted), Manual (Raw Data) 4.c.2. One engine inoperative. A,B,C,D e.g., Manual (Flt. Dir. Assisted), Manual (Raw Data) 4.d. Non - precision Instrument Approach A,B,C,D e.g., NDB, VOR, VOR/DME, VOR/TAC, RNAV, LOC, LOC/BC, ADF, and SDF.

4.e. Circling Approach A,B,C,D Specific authorization required.

4.f. Missed Approach See below 4.f.1. Normal. A,B,C,D 4.f.2. One engine Inoperative. A,B,C,D 5. Landings and Approaches to Landings. See below 5.a. Normal and Crosswind Approaches and Landings B(R),C,D 5.b. Landing From a Precision / Non - Precision Approach B(R),C,D Approach and Landing with (Simulated) Engine Failure – 5.c. B(R),C,D Multiengine Airplane 5.d. Landing From Circling Approach B(R),C,D 5.e. Rejected Landing A,B,C,D Origem: S P O 50 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Subjective Requirements Number Levels Notes/Information Landing From a No Flap or a Nonstandard Flap Configuration 5.f. B(R),C,D Approach 6. Normal and Abnormal Procedures. See below 6.a. Engine (including shutdown and restart) A,B,C,D 6.b. Fuel System A,B,C,D 6.c. Electrical System A,B,C,D 6.d. Hydraulic System A,B,C,D 6.e. Environmental and Pressurization Systems A,B,C,D 6.f. Fire Detection and Extinguisher Systems A,B,C,D 6.g. Navigation and Avionics Systems A,B,C,D 6.h. Automatic Flight Control System, Electronic Flight Instrument A,B,C,D System, and Related Subsystems 6.i. Flight Control Systems A,B,C,D 6.j. Anti - ice and Deice Systems A,B,C,D 6.k. Aircraft and Personal Emergency Equipment A,B,C,D 7. Emergency Procedures. See below 7.a. Emergency Descent (Max. Rate) A,B,C,D 7.b. Inflight Fire and Smoke Removal A,B,C,D 7.c. Rapid Decompression A,B,C,D 7.d. Emergency Evacuation A,B,C,D Origem: S P O 51 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry Simulator Subjective Requirements Number Levels Notes/Information 8. Postflight Procedures. See below 8.a. After - Landing Procedures A,B,C,D 8.b. Parking and Securing A,B,C,D ‘‘(a)’’ — indicates that the system, task, or procedure may be examined if the appropriate aircraft system or control is simulated in t he FSTD and is working properly.

‘‘(R)’’ — indicates that the simulator may be qualified for t his task for continuing qualification training. ‘‘A,B,C,D’’ — indicates that the simulator must be able to perform this task for this level of qualification Origem: S P O 52 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Table A 4 - Table of Simulator System Tasks – Subjective Requirements In order to be qualified at the simulator qualification level indicated, the simulator must be able to perform at least the t asks associated with that level of qualification.

Entry Simulator Number Levels Notes/Information Subjective Requirements 1. Instructor Operating Station (IOS), as appropriate. See below NA 1.a. Power switch(es). A,B,C,D NA Airplane conditions. e.g., GW, CG, Fuel loading and 1.b. A,B,C,D Systems.

1.c. Airports / Runways. A,B,C,D e.g., Selection, Surface, Presets, Lighting controls.

e.g., Clouds, Visibility, RVR, Temp, 1.d. Environmental controls. A,B,C,D Wind, Ice, Snow, Rain, and Windshear.

1.e. Airplane system malfunctions (Insertion / deletion) A,B,C,D NA 1.f. Locks, Freezes, and Repositioning. A,B,C,D NA 2. Sound Controls. See below NA 2.a. On / off / adjustment A,B,C,D NA 3. Motion / Control Loading System. See below NA 3.a. On / off / emergency stop. A,B,C,D NA 4. Observer Seats / Stations. See below NA 4.a. Position / Adjustment / Positive restraint system. A,B,C,D NA Origem: S P O 53 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 APÊNDICE B ( APPENDIX B) QUALIFICATION PERFORMANCE REQUISITOS DE DESEMPENHO STANDARDS FOR AIRPLANE FLIGHT PARA QUALIFICAÇÃO DISPOSITIVO TRAINING DEVICES DE TREINAMENTO DE VOO (FTD) DE AVIÃO (a) In order to be qualified at a particular ( a ) Para ser qualificado a um determinado qual ification level, the FTD must meet the nível, o FTD deve cumprir os requisitos standards listed in tables B1, B2 , B3 and B 4 of listados nas tabelas B1, B2 , B3 e B 4 deste this appendix , avaiable only in english. . apêndice , disponíveis apenas em língua inglesa.

(b) Except for level 4 FTD , e ach FTD must (b) Exceto para FTD nível 4, c ada F TD have a QTG, acceptable to the ANAC, that deve possuir um QTG, aceito pela ANAC, includes: contendo: (1) Objective data obtained from (1) Dados objetivos obtidos de ensaio traditional aircraft testing or another approved em voo da aeronave ou outra fonte de dados source; aprovada; (2) The results of F T D objective tests; (2) Os resultados dos testes objetivos do F TD ; (3) The results of F TD subjective tests ; (3) Os resultados dos testes subjetivos and do F TD ; e (4) A description of the equipment (4) Uma descrição do equipamento necessary to perform the evaluation for initial necessário para executar as avaliações para qualifi cation and the continuing qualification qualificação inicial e para qualificação evaluations. recorrente.

Origem: S P O 54 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Table B1 – General technical r equirements for FTD levels - Airplane FTD Level General technical requirements A device that may have an open airplane - specific flight deck area, or an enclosed airplane - specific flight deck and at least one operating system.

Air/ground logic is required (no aerodynamic programming required). All displays may be flat/LCD panel repre sentations or actual representations of displays in the 4 aircraft.

All controls, switches, and knobs may be touch sensitive activation (not capable of manual manipulation of the flight controls) or may physically replicate the aircraft in control operation .

See table B2 for more FTD requirements.

A device that may have an open airplane - specific flight deck area, or an enclosed airplane - specific flight deck; generic aerodynamic programming; at least one operating system; and control loading that is representative of the simulated airplane only at an approach speed and configuration.

All displays may be flat/LCD panel representations or actual representations of 5 displays in the aircraft.

Primary and secondary flight controls (e.g., rudder, aileron, elevator, flaps, spoilers/speed brakes, engine cont rols, landing gear, nosewheel steering, trim, brakes) must be physical controls.

All other controls, switches, and knobs may be touch sensitive activation.

See table B2 for more FTD requirements.

A device that has an enclosed airplane - specific flight deck; airplane - specific aerodynamic programming; all applicable airplane systems operating; control loading that is representative of the simulated airplane throughout its ground and flight envelope; a nd significant sound representation.

All displays may be flat/LCD panel representations or actual representations of displays in the aircraft, but all controls, switches, and knobs must physically replicate the aircraft in control operation.

See table B2 for more FTD requirements.

A Level 7 device is one that has an enclosed airplane - specific flight deck and aerodynamic program with all applicable airplane systems operating and control loading that is representative of the simulated airplane throughout its ground and flight envelope and significant sound representation.

All displays may be flat/LCD panel representations or actual representations of 7 displays in the aircraft, but all controls, switches, and knobs must physically replicate the aircraft in control operation.

It also ha s a visual system that provides an out - of - the - flight deck view, providing cross - flight deck viewing (for both pilots simultaneously) of a field - of - view of at least 180° horizontally and 40° vertically.

See table B2 for more FTD requirements.

Origem: S P O 55 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Table B 2 – General FTD Requirements Entry General FTD Requirements FTD Level Notes/Information Number 1. General Flight deck Configuration. See next NA The FTD must have a flight deck that is a replica of the airplane simulated with For FTD purposes, the flight deck 1.a. 6,7 controls, equipment, observable flight deck indicators, circuit breakers, and bulkheads consists of all that space forward of properly located, functionally accurate and replicating the airplane. The direction of a cross section of the fuselage at the movement of controls and switches must be identical to that in the airplane. Pilot most extreme aft setting of the seat(s) must afford the capability for the occupant to be able to achieve the design “eye pilots' seats including additional, position.” Equipment for the operation of the flight deck windows must be included, required flight crewmember duty but the actual windows need not be operable. Fire axes, extinguishers, and spare light stations and those required bulbs must be available in the flight FTD, but may be relocated to a suitable location bulkheads aft of the pilot seats. For as near as practical to the original position. Fire axes, landing gear pins, and any clarification, bulkheads containing similar purpose instruments need only be represented in silhouette. only items such as landing gear pin storage compartments, fire axes and The use of electronically displayed images with physical overlay or masking for FTD extinguishers, spare light bulbs, instruments and/or instrument panels is acceptable provided: aircraft documents pouches are not (1) All instruments and instrument panel la youts are dimensionally correct with considered essential and may be differences, if any, being imperceptible to the pilot; omitted.

(2) Instruments replicate those of the airplane including full instrument functionality and embedded logic; For Level 6 FTDs, flight deck window panes may be omitted (3) Instruments displayed are free of quantization (stepping); where non - distracting and (4) Instrument display characteristics replicate those of the airplane including: subjectively acceptable to conduct resolution, colors, luminance, brightness, fonts, fill patterns, line styles and qualified training tasks.

symbology; (5) Overlay or masking, including bezels and bugs, as applicable, replicates the airplane panel(s); (6) Instrument controls and switches replicate and operate with the same technique, effort, travel and in the same direction as those in the Origem: S P O 56 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number airplane; (7) Instrument lighting replicates that of the airplane and is operated from t he FSTD control for that lighting and, if applicable, is at a level commensurate with other lighting operated by that same control; and (8) As applicable, instruments must have faceplates that replicate those in the airplane; and Level 7 FTD only; The display image of any three dimensional instrument, such as an electro - mechanical instrument, should appear to have the same three dimensional depth as the replicated instrument. The appearance of the simulated instrument, when viewed from the principle operator’s angle, should replicate that of the actual airplane instrument. Any instrument reading inaccuracy due to viewing angle and parallax present in the actual airplane instrument should be duplicated in the simulated instrument display image.

Viewing angle err or and parallax must be minimized on shared instruments such and engine displays and standby indicators.

The FTD must have equipment (e.g., instruments, panels, systems, circuit breakers, 1.b. 4,5 None and controls) simulated sufficiently for the authorized training/checking events to be accomplished. The installed equipment must be located in a spatially correct location and may be in a flight deck or an open flight deck area. Additional equipment required for the authorized training/checking events must be available in the FTD, but may be located in a suitable location as near as practical to the spatially correct position.

Actua tion of equipment must replicate the appropriate function in the airplane. Fire axes, landing gear pins, and any similar purpose instruments need only be represented in silhouette.

1.c. Those circuit breakers that affect procedures or result in observable flight deck 7 None indications must be properly located and functionally accurate.

2. Programming. See next None Origem: S P O 57 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number The FTD must provide the proper effect of aerodynamic changes for the combinations 2.a.1 5,6 None of drag and thrust normally encountered in flight. This must include the effect of change in airplane attitude, thrust, drag, altitude, temperature, and configuration.

Level 6 additionally requires the effects of changes in gross weight and center of gravity.

Level 5 requires only generic aerodynamic programming. An S OC is required.

A flight dynamics model that accounts for various combinations of drag and thrust None 2.a.2 7 normally encountered in flight must correspond to actual flight conditions, including the effect of change in airplane attitude, thrust, drag, altitude, temperature, gross weight, moments of inertia, center of gravity location, and configuration.

The effects of pitch attitude and of fuel slosh on the aircraft center of gravity mus t be simulated.

An SOC is required.

The FTD must have the computer capacity, accuracy, resolution, and dynamic None 2.b. 4,5,6,7 response needed to meet the qualification level sought.

An SOC is required.

Relative responses of the flight deck instruments must be measured by latency tests, or The intent is to verify that the FTD 2.c.1 5,6 transport delay tests, and may not exceed 300 milliseconds. The instruments must provides instrument cues that are, respond to abrupt input at the pilot's position within the allotted time, but not before within the stated time delays, like the time when the airpla ne responds under the same conditions. the airplane responses. For airplane response, acceleration in (1) Latency: The FTD instrument and, if applicable, the motion system and the the appropriate, corresponding visual system response must not be prior to that time when the airplane rotational axis is preferred.

responds and may respond up to 300 milliseconds after that time under t he same conditions.

(2) T ransport Delay: As an alternative to the Latency requirement, a transport delay objective test may be used to demonstrate that the FTD system does not Origem: S P O 58 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number exceed the specified limit. The sponsor must measure all the delay encountered by a step signal migrating from the pilot’s control through all the simulation software modules in the correct order, using a handshaking protocol, finally through the normal output interfaces to the instrument display and, if applicable, the motion system, and the visual system.

Relative respon ses of the motion system, visual system, and flight deck instruments, The intent is to verify that the FTD 2.c.2. 7 measured by latency tests or transport delay tests. Motion onset should occur before provides instrument, motion, and the start of the visual scene change (the start of the scan of the first video field visual cues that are, within the containing diffe rent information) but must occur before the end of the scan of that stated time delays, like the airplane video field. Instrument response may not occur prior to motion onset. Test results must responses. For airplane response, acceleration in the appropriate, be within the following limits: corresponding rotat ional axis is 100 ms for the motion (if installed) and instrument systems; and 120 ms for the visual preferred.

system.

2.d. Ground handling and aerodynamic programming must include the following: See next None Ground effect includes modeling 2.d.1. Ground effect. 7 that accounts for roundout, flare, touchdown, lift, drag, pitching moment, trim, and power while in ground effect.

2.d.2. Ground reaction. 7 Ground reaction includes modeling that accounts for strut deflections, tire friction, and side forces. This is the reaction of the airplane upon contact with the runway during landing, and may differ with changes in factors such as gross weight, airspeed, or rate of descent on touchdown.

Origem: S P O 59 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number 2.d.3. Ground handling characteristics, including aerodynamic and ground reaction modeling 7 None including steering inputs, operations with crosswind, gusting crosswind, braking, thrust reversing, deceleration, and turning radius.

If the aircraft being simulated is one of the aircraft listed in section 121.358 of RBAC Windshear models may consist of 2.e. 7 121 , Low - altitude windshear system equipment requirements, the FTD must employ independent variable winds in windshear models that provide training for recognition of windshear phenomena and multiple simultaneous components.

the execution of recovery procedures. Models must be available to the The FTD should employ a method instructor/evaluator for the following critical phas es of flight: to ensure the required survivable (1) Prior to takeoff rotation; and non - survivable windshear scenarios are repeatable in the (2) At liftoff; training environment.

(3) During initial climb; and For Level 7 FTDs, windshear (4) On final approach, below 500 ft AGL.

training tasks may only be qualified for aircraft equipped with a The addition of realistic levels of turbulence associated with each required windshear synthetic stall warning syst em. The profile must be available and selectable to the instructor.

qualified windshear profile(s) are In addition to the four basic windshear models required for qualification, at least two evaluated to ensure the synthetic additional “complex” windshear models must be available to the instructor which stall warning (and not the stall represent the complexity of actual windshear encounters. These models must be buffet) is first indication of the stall.

available in the takeoff and landing configurations and must consist of independent variable winds in multiple simultan eous components. The Windshear Training Aid provides two such example “complex” windshear models that may be used to satisfy this requirement.

The FTD must provide for manual and automatic testing of FTD hardware and Automatic “flagging” of out - of - 2.f. 7 software programming to determine compliance with FTD objective tests. tolerance situations is encouraged.

An SOC is required.

The FTD must accurately reproduce the following runway conditions: None 2.g. 7 Origem: S P O 60 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number (1) Dry; (2) Wet; (3) Icy; (4) Patchy Wet; (5) Patchy Icy; and (6) Wet on Rubber Residue in Touchdown Zone.

An SOC is required.

FTD pitch, side loading, and 2.h. The FTD must simulate: 7 directional control characteristics (1) brake and tire failure dynamics, including antiskid failure; and should be representative of the (2) decreased brake efficiency due to high brake temperatures, if applicable. airplane.

An SOC is required SOC should be provided describing 2.i. Engine and Airframe Icing 7 the effects which provide training in Modeling that includes the effects of icing, where appropriate, on the airframe, the specific skills required for aerodynamics, and the engine(s). Icing models must simulate the aerodynamic recognition of icing phenomena and degradation effects of ice accretion on the airplane lifting surfaces including loss of execution of recovery. The SOC lift, decre ase in stall angle of attack, change in pitching moment, decrease in control should describe the source data and effectiveness, and changes in control forces in addition to any overall increase in drag.

any analytic al methods used to Aircraft systems (such as the stall protection system and autoflight system) must develop ice accretion models respond properly to ice accretion consistent with the simulated aircraft.

including verification that these Aircraft OEM data or other acceptable analytical methods must be utilized to develop effects have been tested.

ice accretion models that are representative of the simulated aircraft’s performance Icing effects simulation models are degradation in a ty pical in - flight icing encounter. Acceptable analytical methods may only required for those airplanes include wind tunnel analysis and/or engineering analysis of the aerodynamic effects of authorized for operations in icing icing on the lifting surfaces coupled with tuning and supplemental subjective conditions. Icing simulation models Origem: S P O 61 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number assessment by a subject matter expert pilot. should be developed to provide training in the specific skills SOC required.

required for recognition of ice accumulation and execution of the required response.

NA 2.j. The aerodynamic modeling in the FTD must include: 7 (1) Low - altitude level - flight ground effect; (2) Mach effect at high altitude; (3) Normal and reverse dynamic thrust effect on control surfaces; (4) Aeroelastic representations; and (5) Nonlinearities due to sideslip.

An SOC is required and must include references to computations of aeroelastic representation s and of nonlinearities due to sideslip.

2.k. The FTD must have aerodynamic and ground reaction modeling for the effects of 7 None reverse thrust on directional control, if applicable.

An SOC is required.

3. Equipment Operation. See next None All relevant instrument indications involved in the simulation of the airplane must 3.a. 5,6,7 None automatically respond to control movement or external disturbances to the simulated airplane; e.g., turbulence or windshear. Numerical values must be presented in the appropriate units.

For Level 7 FTDs, instrument indications must also respond to effects resulting from icing.

Navigation equipment must be installed and operate within the tolerances applicable 3.b.1. 5,6 None Origem: S P O 62 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number for the airplane.

Levels 6 must also include communication equipment (inter - phone and air/ground) like that in the airplane and, if appropriate to the operation being condu cted, an oxygen mask microphone system.

Level 5 need have only that navigation equipment necessary to fly an instrument approach.

3.b.2. Communications, navigation, caution, and warning equipment must be installed and 7 NA operate within the tolerances applicable for the airplane.

Instructor control of internal and external navigational aids. Navigation aids must be usable within range or line - of - sight without restriction, as applicable to the geographic area.

Complete navigation database for at least 3 airports with corresponding precision and 3.b.3. 7 None non - precision approach procedures, including navigational database updates.

Installed systems must simulate the applicable airplane system operation, both on the 3.c.1. 4,5,6 None gr ound and in flight. Installed systems must be operative to the extent that applicable normal, abnormal, and emergency operating procedures included in the sponsor’s training programs can be accomplished.

Level 6 must simulate all applicable airplane flight , navigation, and systems operation.

Level 5 must have at least functional flight and navigational controls, displays, and instrumentation.

Level 4 must have at least one airplane system installed and functional.

Simulated airplane systems must operate as the airplane systems operate under normal, Airplane system operation should 3.c.2. 7 abnormal, and emergency operating conditions on the ground and in flight. be predicated on, and traceable to, the system data supplied by the Once activated, proper systems operation must result from system management by the airplane manufacturer, original crew member and not req uire any further input from the instructor's controls.

equipment manufacturer or Origem: S P O 63 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number alternative approved data for the airplane system or component.

At a minimum, alternate approved data should validate the operation of all normal, abnormal, and emergency operating procedures and training tasks the FSTD is qualified to conduct.

The lighting environment for panels and instruments must be sufficient for the Back - lighted panels and instruments 3.d. 4,5,6,7 operation being conduct ed. may be installed but are not required.

The FTD must provide control forces and control travel that corresponds to the 3.e. 6,7 None airplane being simulated. Control forces must react in the same manner as in the airplane under the same flight conditions.

For Level 7 FTDs, control systems must replicate airplane operation for the normal and any non - normal modes including back - up systems and should reflect failures of associated systems. Appropriate cockpit indicati ons and messages must be replicated.

The FTD must provide control forces and control travel of sufficient precision to None 3.f. 5 manually fly an instrument approach.

3.e. FTD control feel dynamics must replicate the airplane. This must be determined by 7 None comparing a recording of the control feel dynamics of the FTD to airplane measurements. For initial and upgrade qualification evaluations, the control dynamic characteristics must be measured and recorded directly from the flight deck control s, and must be accomplished in takeoff, cruise, and landing flight conditions and configurations.

4. Instructor or Evaluator Facilities. See next None Origem: S P O 64 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number In addition to the flight crewmember stations, suitable seating arrangements for an These seats need not be a replica of 4.a.1. 4,5,6 instructor/check airman and ANAC Inspector must be available. These seats must an aircraft seat and may be as provide adequate view of crewmember's panel(s). simple as an office chair placed in an appropriate posi tion.

In addition to the flight crewmember stations, the FTD must have at least two suitable The ANAC will consider 4.a.2. 7 seats for the instructor/check airman and ANAC inspector. These seats must provide alternatives to this standard for adequate vision to the pilot's panel and forward windows. All seats other than flight additional seats based on unique crew seats need not represent those found in the airplane, but must be adequately flight deck configurations.

secured to the floor and equipped with similar positive restraint devices.

The FTD must have instructor controls that permit activation of normal, abnormal, and 4.b.1. 4,5,6 None emergency conditions as appropriate. Once activated, proper system operation must result from system management by the crew and not require input from the instructor controls.

The FTD must have controls that enable the instructor/evaluator to control all required 4.b.2. 7 None system variables and insert all abnormal or emergency conditions into the simulated airplane systems as d escribed in the sponsor’s ANAC - approved training program; or as described in the relevant operating manual as appropriate.

The FTD must have instructor controls for all environmental effects expected to be 4.c. 7 None available at the IOS; e.g., clouds, visibility, icing, precipitation, temperature, storm cells and microbursts, turbulence, and intermediate and high altitude wind speed and direction.

The FTD must provide the instructor or evaluator the ability to present ground and air For example, another airplane 4.d. 7 hazards. crossing the active runway or converging airborne traffic.

5. Motion System. See next Origem: S P O 65 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number The FTD may have a motion system, if desired, although it is not required. If a motion The motion system standards set out 5.a. 5,6,7 system is installed and additional training, testing, or checking credits are being sought in RBAC 60, Appendix A for at on the basis of having a motion system, the motion system least Level A simulators is acceptable.

operation may not be distracting and must be coupled closely to provide integrated sensory cues. The motion system must also respond to abrupt input at the pilot's position within the allotted time, but not before the time when the airplane responds under the same conditions.

If a motion system is installed, it must be measured by latency tests or transport delay The motion system standards set out 5.b. 6,7 tests and may not exceed 300 milliseconds. Instr ument response may not occur prior to in RBAC 60, Appendix A for at motion onset. least Level A simulators is acceptable.

6. Visual System. See next None 6.a. The FTD may have a visual system, if desired, although it is not required. If a visual 4,5,6 None system is installed, it must meet the following criteria: 6.a.1. The visual system must respond to abrupt input at the pilot's position. 5,6 None An SOC is required.

6.a.2. 4,5,6 The visual system must be at least a single channel, non - collimated display. None An SOC is required.

6.a.3. The visual system must provide at least a field - of - view of 18° vertical / 24° horizontal 4,5,6 None for the pilot flying.

An SOC is required.

6.a.4. The visual system must provide for a maximum parallax of 10° per pilot. 4,5,6 None An SOC is required.

6.a.5. 4,5,6 The visual scene content may not be distracting. None Origem: S P O 66 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number An SOC is required.

6.a.6. The minimum distance from the pilot’s eye position to the surface of a direct view None display may not be less than the distance to any front panel instrument.

An SOC is required.

6.a.7. The visual system must provide for a minimum resolution of 5 arc - minutes for both 4,5,6 None computed and displayed pixel size.

An SOC is required.

6.b. If a visual system is installed and additional training, testing, or checking credits are 6 Directly projected, non - collimated being sought on the basis of having a visual system, a visual system meeting the visual displays may prove to be standards set out for at least a Level A FFS (see Appendix A of this RBAC ) will be unacceptable for dual pilot re quired. A “direct - view,” non - collimated visual system (with the other requirements applications.

for a Level A visual system met) may be considered satisfactory for those installations where the visual system design “eye point” is appropriately adjusted for each pilot’s position such that the parallax error is at or less than 10º simultaneously for each pilot.

An SOC is required.

6.c. The FTD must have a visual system providing an out - of - the - flight deck view. 7 None The FTD must provide a continuous visual field - of - view of at least176° horizontally The horizontal field - of - view is 6.d. 7 and 36° vertically or the number of degrees necessary to meet the visual ground traditionally descr ibed as a 180º segment requirement, whichever is greater. The minimum horizontal field - of - view field - of - view. However, the field - coverage mus t be plus and minus one - half (½) of the minimum continuous field - of - of - view is technically no less than view requirement, centered on the zero degree azimuth line relative to the aircraft 176º. Additional field - of - view fuselage. capability may be added at the sponsor’s discretion provided the An SOC is required and must explain the system geometry measurements including minimum fields of view are system linearit y and field - of - view.

retained.

Collimation is not required but parallax effects must be minimized (not greater than 10° for each pilot when aligned for the point midway between the left and right seat Origem: S P O 67 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number eyepoints).

The visual system must be free from optical discontinuities and artifacts that create Non - realistic cues might include 6.e. 7 non - realistic cues. image “swimming” and image “roll - off,” that may lead a pilot to make incorrect assessments of speed, acceleration, or situational awareness.

The FTD must have operational landing lights for night scenes. Where used, dusk (or 6.f. 7 None twilight) scenes require operational landing lights.

The FTD must have instructor controls for the following: None 6.g. 7 (1) Visibility in statute miles (km) and runway visual range (RVR) in ft.(m); (2) Airport selection; and (3) Airport lighting.

6.h. The FTD must provide visual system compatibility with dynamic response 7 None programming.

The FTD must show that the segment of the ground visible from the FTD flight deck is This will show the modeling 6.i. 7 the same as from the airplane flight deck (within established tolerances) when at the accuracy of RVR, glideslope, and correct airspeed, in the landing configuration, at the appropriate height above the localizer for a given weight, configuration, and speed within the touchdown zone, and with appropriate visibility.

airplane's operational envelope for a normal approach and landing.

The FTD must provide visual cues necessary to assess si nk rates (provide depth None 6.j. 7 perception) during takeoffs and landings, to include: (1) Surface on runways, taxiways, and ramps; and (2) Terrain features.

Origem: S P O 68 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number The FTD must provide for accurate portrayal of the visual environment relating to the Visual attitude vs. FTD attitude is a 6.k. 7 FTD attitude. comparison of pitch and roll of the horizon as displayed in the visual scene compared to the display on the attitude indicator.

The FTD must provide for quick confirmation of visual system color, RVR, focus, and 6.l. 7 None intensity.

An SOC is required.

6.m. The FTD must be capable of producing at least 10 levels of occulting. 7 None Night Visual Scenes. When used in training, testing, or checking activities, the FTD 6.n. 7 None must provide night visual scenes with sufficient scene content to recognize the airport, the terrain, and major landmarks around the airport. The scene content must allow a pilot to successfully accomplish a visual landing. Scenes must include a definable horizon and typical terrain characteristics such as fields, roads and bodies of water and surfaces illuminated by airplane landing lights.

Dusk (or Twilight) Visual Scenes. When used in training, testing, or checking 6.o. 7 None activities, the FTD must provide dusk (or twilight) visual scenes with sufficient scene content to recognize the airport, the terrain, and major landmarks around the airport.

The scene content must allow a pilot to successfully accomplish a visual landing. Dusk (or twilight) scenes, as a minimum, must provide full color presentations of reduced ambient intensity, sufficient surfaces with appropriate textural cues that include self - illuminated object s such as road networks, ramp lighting and airport signage, to conduct a visual approach, landing and airport movement (taxi). Scenes must include a definable horizon and typical terrain characteristics such as fields, roads and bodies of water and surface s illuminated by airplane landing lights. If provided, directional horizon lighting must have correct orientation and be consistent with surface shading effects. Total night or dusk (twilight) scene content must be comparable in detail to Origem: S P O 69 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number that produced by 10,000 visible textured surfaces and 15,000 visible lights with sufficient system capacity to display 16 simultaneously moving objects.

An SOC is required.

Daylight Visual Scenes. The FTD must provide daylight visual scenes with sufficient None 6.p. 7 scene content to recognize the airport, the terrain, and major landmarks around the airport. The scene content must allow a pilot to successfully accomplish a visual landing. Any ambient lighting must not “washout” the displayed visual scene. Total daylight scene content must be comparable in detail to that produced by 10,000 visible textured surfaces and 6,000 visible lights with sufficient system capacity to display 16 simultaneously moving objects. The visual display must be free of a pparent and distracting quantization and other distracting visual effects while the FTD is in motion.

An SOC is required.

The FTD must provide operational visual scenes that portray physical relationships For example: short runways, 6.q. 7 known to cause landing illusions to pilots. landing approaches over water, uphill or downhill runways, rising terrain on the approach path, unique topographic features.

The FTD must provide special weather representations of light, medium, and heavy 6.r. 7 None precipitation near a thunderstorm on takeoff and during approach and landing.

Representations need only be presented at and below an altitude of 2,000 ft. (610 m) above the airport surface and within 10 miles (16 km) of the airport.

The FTD mu st present visual scenes of wet and snow - covered runways, including 6.s. 7 None runway lighting reflections for wet conditions, partially obscured lights for snow conditions, or suitable alternative effects.

6.t. The FTD must present realistic color and directionality of all airport lighting. 7 None Origem: S P O 70 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number The following weather effects as observed on the visual system must be Scud effects are low, detached, and 6.u. 7 simulated and respective instructor controls provided. irregular clouds below a defined cloud layer.

(1) Multiple cloud layers with adjustable bases, tops, sky coverage and scud effect; (2) Storm cells activation and/or deactivation; (3) Visibility and runway visual range (RVR), including fog and patchy fog effect; (4) Effects on ownship external lighting; (5) Effects on airport lighting (including variable intensity and fog effects); (6) Surface contaminants (including wind blowing effect); (7) Variable precipitation effects (rain, hail, snow); (8) In - cloud airspeed effect; and (9) Gradual visibility changes entering and breaking out of cloud.

6.v. The simulator must provide visual effects for: 7 Visual effects for light poles and raised edge lights are for the (1) Light poles; purpose of providing additional (2) Raised edge lights as appropriate; and depth perception during takeoff, landing, and taxi training tasks.

(3) Glow associated with approach lights in low visibility before physical lights Three dimensional modeling of the are seen .

actual poles and stanchions is not req uired.

The model identifications must be 6.w A minimum of three (3) real - world airport models required for simulator qualification. 7 acceptable to the sponsor’s TPAA, Must be consistent with published data used for airplane operations. Each model selectable from the IOS, and listed should be in a different visual scene to permit assessment of FSTD automatic visual on the SOQ.

scene changes.

7. Sound System. See next None Origem: S P O 71 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry General FTD Requirements FTD Level Notes/Information Number 7.a. The FTD must provide flight deck sounds that result from pilot actions that correspond 6,7 None to those that occur in the airplane.

7.b. The volume control must have an indication of sound level setting which meets all 7 This indication is of the sound qualification requirements. level setting as evaluated during the FTD’s initial evaluation.

The FTD must accurately simulate the sound of precipitation, windshield wipers, 7.c. 7 None and other significant airplane noises perceptible to the pilot during normal and abnormal operations, and include the sound of a crash (when the FTD is landed in an unusual attitude or in excess of the structural gear limitations); normal engine and thrust reversal sounds; and the sounds of flap, gear, and spoiler extension and retraction.

Sounds must be directionally representative . An SOC is required.

7.d. The FTD must provide realistic amplitude and frequency of flight deck noises and 7 None sounds. FTD performance must be recorded, subjectively assessed for the initial evaluation, and be made a part of the QTG.

Origem: S P O 72 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Table B 3 - Table of Tasks vs. FTD Level – Subjective Requirements In order to be qualified at the FTD qualification level indicated, the FTD must be able to perform at least the tasks associa ted with that level of qualification. See Notes 1, 2 and 3 at the end of the Table.

Entry Subjective Requirements FTD Level Notes/Information Number 1. Preflight Procedures. See next None 1.a. Preflight Inspection (flight deck only) 4(a),5(a),6,7 None 1.b. Engine Start 4(a),5(a),6,7 None 1.c. Taxiing 7(t) None 1.d. Pre - takeoff Checks 4(a),5(a),6,7 None 2. Takeoff and Departure Phase. See next None 2.a. Normal and Crosswind Takeoff 7(t) None 2.b. Instrument Takeoff 7(t) None 2.c. Engine Failure During Takeoff 7(t) None 2.d. Rejected Takeoff (requires visual system) 6(a),7 None 2.e. Departure Procedure 5,6,7 None 3. Inflight Maneuvers. See next None 3.a. Steep Turns 5,6,7 None Approaches to Stalls 3.b 5(a),6,7 Approach to stall maneuvers qualified only where the aircraft does not exhibit stall buffet as the first indication of the stall.

3.c. Engine Failure — Multiengine Airplane 5(a),6,7 None 3.d. Engine Failure — Single - Engine Airplane 5(a),6,7 None Origem: S P O 73 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Subjective Requirements FTD Level Notes/Information Number 3.e. 4(a),5(a),6(a),7(a) Specific Flight Characteristics incorporated into the user’s ANAC Level 4 FTDs have no minimum approved flight training program. requirement for aerodynamic programming and are generally not qualified to conduct in - flight maneuvers.

3.f. Windshear Recovery 7(t) For Level 7 FTD, windshear recovery may be qualified at the Sponsor’s option. See Table B 2 for specific requirements and limitations.

4. Instrument Procedures. See next None 4.a. Standard Terminal Arrival / Flight Management System Arrivals 5(a),6,7 None Procedures 4.b. Holding 5(a),6,7 None 4.c. Precision Instrument None 4.c.1. All engines operating. 5(a),6,7 e.g., Autopilot, Manual (Flt. Dir.

Assisted), Manual (Raw Data) One engine inoperative. e.g., Manual (Flt. Dir. Assisted), 4.c.2. 7(t) Manual (Raw Data) 4.d. Non - precision Instrument Approach 5(a),6,7 e.g., NDB, VOR, VOR/DME, VOR/TAC, RNAV, LOC, LOC/BC, ADF, and SDF.

4.e. Circling Approach (requires visual system) 6(a),7 Specific authorization required.

4.f. Missed Approach None 4.f.1. Normal. 5(a),6,7 None 4.f.2. One engine Inoperative. 7(t) None 5. Landings and Approaches to Landings. See next None Origem: S P O 74 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Subjective Requirements FTD Level Notes/Information Number 5.a. Normal and Crosswind Approaches and Landings 7(t) None 5.b. Landing From a Precision / Non - Precision Approach 7(t) None 5.c. Approach and Landing with (Simulated) Engine Failure – Multiengine 7(t) None Airplane 5.d. Landing From Circling Approach 7(t) None 5.e. Rejected Landing 7(t) None 5.f. Landing From a No Flap or a Nonstandard Flap Configuration Approach 7(t) None 6. Normal and Abnormal Procedures. See next None 6.a. Engine (including shutdown and restart) 4(a),5(a),6,7 None 6.b. Fuel System 4(a),5(a),6,7 None 6.c. Electrical System 4(a),5(a),6,7 None 6.d. Hydraulic System 4(a),5(a),6,7 None 6.e. Environmental and Pressurization Systems 4(a),5(a),6,7 None 6.f. Fire Detection and Extinguisher Systems 4(a),5(a),6,7 None 6.g. Navigation and Avionics Systems 4(a),5(a),6,7 None 6.h. Automatic Flight Control System, Electronic Flight Instrument System, 4(a),5(a),6,7 None and Related Subsystems 6.i. Flight Control Systems 4(a),5(a),6,7 None 6.j. Anti - ice and Deice Systems 4(a),5(a),6,7 None 6.k. Aircraft and Personal Emergency Equipment 4(a),5(a),6,7 None 7. Emergency Procedures. See next None 7.a. Emergency Descent (Max. Rate) 5(a),6,7 None 7.b. Inflight Fire and Smoke Removal 5(a),6,7 None 7.c. Rapid Decompression 5(a),6,7 None Origem: S P O 75 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Subjective Requirements FTD Level Notes/Information Number 7.d. Emergency Evacuation 4(a),5(a),6,7 None 8. Postflight Procedures. See next None 8.a. After - Landing Procedures 4(a),5(a),6,7 None 8.b. Parking and Securing 4(a),5(a),6,7 None Note 1: An “(a)” in the table indicates that the system, task, or procedure, although not required to be present, may be examined if the appropriate airplane system is simulated in the FTD and is working properly.

Note 2: Items not installed or not functional on the FTD and not appearing on the SOQ Configuration List, ar e not required to be listed as exceptions on the SOQ.

Note 3: A “(t)” in the table indicates that the task may only be qualified for introductory initial or recurrent qualificatio n training. These tasks may not be qualified for proficiency testing or check ing credits in an ANAC approved flight training program .

Origem: S P O 76 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Table B 4 - Table of FTD System Tasks – Subjective Requirements In order to be qualified at the FTD qualification level indicated, the FTD must be able to perform at least the tasks associa ted with that level of qualification .

Entry Subjective Requirements FTD Level Notes/Information Number 1. Instructor Operating Station (IOS). See next NA 1.a. Power switch(es). 4,5,6 NA Airplane conditions.

1.b. e.g., GW, CG, Fuel loading, 4(a),5,6 Systems, Ground. Crew 1.c. Airports / Runways. e.g., Selection and Presets; Surface and Lighting controls if equipped 4,5,6 with a visual system.

Environmental controls.

1.d. 4,5,6 e.g., Temp, Wind.

1.e. Airplane system malfunctions (Insertion / deletion) 4(a),5,6 NA 1.f. Locks, Freezes, and Repositioning. 4,5,6 NA 1.g. Sound Controls. (On / off / adjustment) 4,5,6 NA Motion / Control Loading System, as appropriate. On / off / emergency stop 1.h. 4(a),5(a),6(a) NA 2. Observer Seats / Stations. See next NA 2.a. Position / Adjustment / Positive restraint system. 4,5,6 NA Note 1: An “(a)” in the table indicates that the system, task, or procedure, although not required to be present, may be exam ined if the appropriate system is in the FTD and is working properly.

Origem: S P O 77 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 APÊNDICE C (APPENDIX C) QUALIFICATION PERFORMANCE REQUISITOS DE DESEMPENHO PARA STANDARDS FOR HELICOPTER FULL QUALIFICAÇÃO DE SIMULADOR DE FLIGHT SIMULATORS VOO (FFS) DE HELICÓTERO (a) In order to be qualified at a particular ( a ) Para ser qualificado a um determinado qual ification level, the FFS must meet the nível, o FFS deve cumprir os requisitos standards listed in tables C1, C2 , C3 and C 4 of listados nas tabelas C1, C2 , C3 e C 4 deste this appendix , avaia ble only in english. . apêndice , disponíveis apenas em língua inglesa.

(b) Each FFS must have a QTG, acceptable (b) Cada FFS deve possuir um QTG, aceito to the ANAC, that includes: pela ANAC, contendo: (1) Objective data obtained from (1) Dados objetivos obtidos de ensaio traditional aircraft testing or another approved em voo da aeronave ou outra fonte de dados source; aprovada; (2) The results of FFS objective tests; (2) Os resultados dos testes objetivos do FFS; (3) The results of FFS subjective tests ; (3) Os resultados dos testes subjetivos and do FFS; e (4) A description of the equipment (4) Uma descrição do equipamento necessary to perform the evaluation for initial necessário para executar as avaliaç ões para qualification and the continuing qualification qualificação inicial e para qualificação evaluations. recorrente.

Origem: S P O 78 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Table C1 - General technical requirements for level B, C and D full - flight simulators - Helicopter General technical requirements Qualification Level The lowest level of FFS technical complexity for a helicopter.

An enclosed full - scale replica of the helicopter cockpit with representative pilots’ seats, including simulation of all systems, instruments, navigational equipment, communications and caution and warning systems.

An instructor’s station with seat should be provided and at least one additional seat for inspectors/observers.

Static control forces and displacement characteristics should correspond to that of the replicated helicopter and they s hould reflect the helicopter under the same static flight conditions.

Motion, visual and sound systems sufficient to support the training, testing and checking credits sought are required.

B The response to control inputs should not be greater than 150 ms more than that experienced on the helicopter.

Validation flight test data should be used as the basis for flight and performance and systems characteristics.

Additionally ground handling and aerodynamics programming to include ground effect reaction and handling characteristics should be derived from validation flight test data.

A motion system having a minimum of three degrees of freedom (pitch, roll, and heave) to accomp lish the required training tasks should be provided. A reduced six - axis motion performance envelope is acceptable.

See table C2 for more s imulator r equirements .

The second highest level of simulator performance. As for level B plus: A daylight/dusk/nigh t visual system is required with a continuous field of view per pilot of not less than 146 ° horizontal and 36 º vertical.

The sound simulation should include the sounds of precipitation and significant helicopter noises perceptible to the pilot and should be able to reproduce the sounds C of a crash landing.

The response to control inputs should not be greater than 100 ms more than that experienced on the helicopter.

Turbulence and other atmospheric models should be provided to support the training, testing and checking credit sought.

See table C2 for more s imulator r equirements .

The highest level of simulator performance.

As for level C plus: A full daylight/dusk/night visual system is required with a continuous field of view D per pilot of not less than 176 ° horizontal and 56 ° vertical and an extended set of sound and motion buffet tests.

See table C2 for more s imulator r equirements .

Origem: S P O 79 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Table C 2 - General Simulator Requirements Entry Simulator General Simulator Requirements Notes/Information Number Levels 1. General Flight Deck Configuration. See next None 1.a. The simulator must have a flight deck that is a replica of the helicopter being simulated. B,C,D For simulator purposes, the The simulator must have controls, equipment, observable flight deck indicators, circuit flight deck consists of all that breakers, and bulkheads properly located, functionally accurate and repl icating the space forward of a cross section helicopter. The direction of movement of controls and switches must be identical to that of t he fuselage at the most in the helicopter. Pilot seats must afford the capability for the occupant to be able to extreme aft setting of the pilots' achieve the design “eye position” established for the helicopter b eing simulated. seats including additional, required flight crewmember duty Equipment for the operation of the flight deck windows must be included, but the actual stations and those required windows need not be operable. Fire axes, extinguishers, and spare light bulbs must be bulkheads aft of the pilot seats.

available in the FFS but may be relocated to a suitable location a s near as practical to the For clarification, bulkheads original position. Fire axes, landing gear pins, and any similar purpose instruments need containing only items such as only be represented in silhouette.

landing gear pin storage compartments, fire axes and extinguishers, spare light bulbs, and aircraft documents pouches are not considered essential and may be omitted.

1.b. Those circuit breakers that affect procedures or result in observable flight deck indications B,C,D None must be properly located and functionally accurate.

2. Programming. See next None 2.a. A flight dynamics model that accounts for various combinations of air speed and power B,C,D None normally encountered in flight must correspond to actual flight conditions, including the effect of change in helicopter attitude, aerodynamic and propulsive forces and moments, altitude, temperature, mass, center of gravity location, and configuration.

An SOC is required.

Origem: S P O 80 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Simulator General Simulator Requirements Notes/Information Number Levels 2.b. B,C,D None The simulator must have the c omputer capacity, accuracy, resolution, and dynamic response needed to meet the qualification level sought.

An SOC is required.

2.c. Ground handling (where appropriate) and aerodynamic programming must include the See next None following: 2.c.1. Ground effect. B,C,D Applicable areas include flare and touch down from a running Level B does not require hover programming. An SOC is required.

landing as well as for in - ground - effect (IGE) hover. A reasonable simulation of ground effect includes modeling of lift, drag, pitching moment, trim, and power while in ground effect.

2.c.2. B,C,D Ground reaction. Reaction of the helicopter upon contact with the landing surface Level B does not require hover programming. An SOC is required.

during landing (e.g., strut deflection, tire or skid friction, side forces) may differ with changes in gross weight, airspeed, rate of descent on touchdown, and slide slip.

2.d. The simulator must provide for manual and automatic testing of simulator hardware an d C,D This may include an automated software programming to determine compliance with simulator objective tests. system, which could be used for conducting at least a portion of An SOC is required.

the QTG tests. Automatic “flagging” of out - of - tolerance situations is encouraged.

2.e. See next The relative responses of the motion system, visual system, and flight deck instruments The intent is to verify that the Origem: S P O 81 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Simulator General Simulator Requirements Notes/Information Number Levels must be measured by latency tests or transport delay tests. Motion onset must occur simulator provides instrument, before the end of the scan of that video field. Instrument response may not occur prior to motion, and visual cues that are motion onset. Test results must be within the following limits: like the helicopter responses within the stated time delays. It is preferable motion onset occur before the start of the visual scene change (the start of the scan of the first video field containing different information). For helicopter response, acceleration in the appropriate corre sponding rotational axis is preferred.

2.e.1. B Response must be within 150 milliseconds of the helicopter response. None 2.e.2. C,D Response must be within 100 milliseconds of the helicopter response. None 2.f. The simulator must simulate brake and tire failure dynamics (including antiskid failure, if C,D The simulator should represent appropriate). the motion (in the appropriate axes) and the directional control An SOC is required.

characteristics of the helicopter when experiencing simulated brake or tire failures.

2.g. The aerodynamic modeling in the simulator must include: C,D NA (1) Ground effect, (2) Effects of airframe and rotor icing (if applicable), (3) Aerodynamic interference effects between the rotor wake and fuselage, (4) Influence of the rotor on control and stabilization systems, (5) Representations of settling with power, and Origem: S P O 82 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Simulator General Simulator Requirements Notes/Information Number Levels (6) Retreating blade stall. An SOC is required.

None 2.h. The simulator must provide for realistic mass properties, including gross weight, center of B,C,D gravity, and moments of inertia as a function of payload and fuel loading An SOC is required.

3. Equipment Operation. See next None 3.a. All relevant instrument indications involved in the simulation of the helicopter must B,C,D None automatically respond to control movement or external disturbances to the simulated helicopter; e.g., turbulence or windshear. Numerical values must be presented in the a ppropriate units.

3.b. Communications, navigation, caution, and warning equipment must be installed and B,C,D NA operate within the tolerances applicable for the helicopter being simulated.

3.c. Simulated helicopter systems must operate as the helicopter systems operate under B,C,D None normal, abnormal, and emergency operating conditions on the ground and in flight.

3.d. The simulator must provide pilot controls with control forces and control travel that B,C,D None correspond to the simulated helicopter. The simulator must also react in the same manner as the helicopter under the same flight conditions.

None 3.e. Simulator control feel dynamics must replicate the helicopter simulated. This must be C,D determined by comparing a reco rding of the control feel dynamics of the simulator to helicopter measurements. For initial and upgrade evaluations, the control dynamic characteristics must be measured and recorded directly from the flight deck controls, and must be accomplished in takeo ff, cruise, and landing conditions and configurations.

4. Instructor / Evaluator Facilities. See next None 4.a. B,C,D In addition to the flight crewmember stations, the simulator must have at least two The ANAC will consider suitable seats for the instructor/check airman and ANAC inspector. These seats must alternatives to this standard for provide adequate vision to the pilot's panel and forward windows. All seats other than additional seats based on uni que f light crew seats need not represent those found in the helicopter but must be adequately flight deck configurations Origem: S P O 83 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Simulator General Simulator Requirements Notes/Information Number Levels secured to the floor and equipped with similar positive restraint devices.

None 4.b. The simulator must have controls that enable the instructor/evaluator to control all B,C,D required system variables and insert all abnormal or emergency conditions into the simulated helicopter systems as described in the sponsor’s ANAC - approved training progra m, or as described in the relevant operating manual as appropriate.

4.c. The simulator must have instructor controls for all environmental effects expected to be B,C,D None available at the IOS; e.g., clouds, visibility, icing, precipitation, temperature, storm cells, and wind speed and direction.

4.d. The simulator must provide the instructor or evaluator the ability to present ground and air C,D For example, another aircraft crossing the active runway and hazards.

converging airborne traffic.

4.e. The simulator must provide the instructor or evaluator the ability to present the effect of C,D This is a selectable con dition re - circulating dust, water vapor, or snow conditions that develop as a result of rotor that is not required for all downwash. operations on or near the surface.

5. Motion System. See next 5.a. The simulator must have motion (force) cues perceptible to the pilot that are B,C,D For example, touchdown cues representative of the motion in a helicopter. should be a function of the rate of descent (RoD) of the simulated helicopter.

5.b. The simulator must have a motion (force cueing) system with a minimum of three degrees B None of freedom (at least pitch, roll, and heave).

An SOC is required.

5.c. The simulator must have a motion (force cueing) system that produces cues at least C,D None equivalent to those of a six - degrees - of - freedom, synergistic platform motion system (i.e., pitch, roll, yaw, heave, sway, and surge).

Origem: S P O 84 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Simulator General Simulator Requirements Notes/Information Number Levels An SOC is required.

5.d. The simulator must provide for the recording of the motion system response time. B,C,D None An SOC is required.

5.e. The simulator must provide motion effects programming to include the following: See next None 5.e. (1) Runway rumble, oleo deflections, effects of ground speed, uneven runway, B,C,D None characteristics.

(2) Buffets due to transverse flow effects.

(3) Buffet during extension and retraction of landing gear.

(4) Buffet due to retreating blade stall.

(5) Buffet due to vortex ring (settling with power).

(6) Representative cues resulting from touchdown.

(7) High speed rotor vibrations.

(8) Tire failure dynamics. C,D None (9) Engine malfunction and engine damage.

(10) Airframe ground strike.

5.e. (11) Motion vibrations that result from atmospheric disturbances. D For air turbulence, general purpose disturbance models are acceptable if, when used, they produce test results that approximate demonstrable flight test data.

5.f. The simulator must provide characteristic motion vibrations that result from operation of D The simulator should be the helicopter (for example, retreating blade stall, extended landing gear, settling with programmed and instrumented power) in so far as vibration marks an event or helicopter state, which can be sensed in the in such a manner that the Origem: S P O 85 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Simulator General Simulator Requirements Notes/Information Number Levels flight deck. characteristic buffet modes can be measured and compared to helicopter data.

6. Visual System. See next Additional horizontal field - of - view capability may be added at the sponsor’s discretion provided the minimum field - of - view is retained.

6.a. B,C,D The simulator must have a visual system providing an out - of - the - flight deck view. None 6.b. The simulator must provide a continuous field - of - view of at least 75 º horizontally and 30 º B None vertically per pilot seat. Both pilot seat visual systems must be operable simultaneously.

The minimum horizontal field - of - view coverage must be plus and minus one - half (½) of the minimum continuous field - of - view requirement, centered on the zero degree azimuth line relative to the aircraft fuselage. An SOC must explain the geometry of the installation.

An SOC is required.

6.c. The simulator must provide a continuous visual field - of - view of at least 146° horizontally C Optimization of the vertical and 36° vertically per pilot seat. Both pilot seat visual systems must be operable field - of - view may be considered simultaneously. Horizontal field - of - view is centered on the zero degree azimuth line with respect to the specific relative to the aircraft fuselage. The minimum horizontal field - of - vi ew coverage must be helicopter flight deck cut - off plus and minus one - half (½) of the minimum continuous field - of - view requirement, angle.

centered on the zero degree azimuth line relative to the aircraft fuselage. An SOC must The sponsor may request the explain the geometry of the installation. Capability for a field - of - view in excess of the ANAC to evaluate the FFS for minimum is not required for qualification at Level C. However, where specific tasks specific authorization(s) for the require extended fields of view beyond the 146º by 36º (e.g., to accommodate the use of following: “chin windows” where the accommodation is either integral wit h or separate from the primary visual system display), then the extended fields of view must be provided. When Specific areas within the database needing higher considering the installation and use of augmented fields of view, the sponsor must meet resolution to support landings, with the ANAC to determine the training, testing, checkin g, and experience tasks for Origem: S P O 86 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Simulator General Simulator Requirements Notes/Information Number Levels which the augmented field - of - view capability may be required. take - offs and ground cushion exercises and training away An SOC is required.

from a heliport , including elevated heliport, helidecks and confined areas.

For cross - country flights, sufficient scene details to allow for ground to map navigation over a sector length equal to 30 minutes at an average cruise speed.

For offshore airborne radar approach es (ARA), harmonized visual/radar representations of installations.

6.d. The simulator must provide a continuous visual field - of - view of at least 176° horizontally D Optimization of the vertical and 56° vertically per pilot seat. Both pilot seat visual systems must be operable field - of - view may be considered simultaneously. Horizontal field - of - view is centered on the zero degree azimuth li ne with respect to the specific relative to the aircraft fuselage. The minimum horizontal field - of - view coverage must be helicopter flight deck cut - off plus and minus one - half (½) of the minimum continuous field - of - view requirement, angle.

centered on the zero degree azimuth line relative to the aircraft fuselage. An SOC must The sponsor may request the explain the geometry of the installation. Capability for a field - of - view in excess of the ANAC to evaluate the FFS for minimum is not required for qualification at Level D. However, where specific tasks specific authorization(s) for the require extended fields of view beyond the 176º by 56º (e.g., to accommodate the use of following: “chin windows” where the accommodation is either integral with or separate from the primary visual system display), then the extended fields of view must be provided. When Specific areas within the database needing higher considering the installation and use of augmented fields of view, the spo nsor must meet resolution to support landings, with the ANAC to determine the training, testing, checking, and experience tasks for which the augmented field - of - view capability may be required. take - offs and ground cushion exercises and training away Origem: S P O 87 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Simulator General Simulator Requirements Notes/Information Number Levels An SOC is required. from a heliport, including elevated heliport, helidecks and confined areas.

For cross - country flights, sufficient scene details to allow for ground to map navigation over a sector length equal to 30 minutes at an average cruise speed.

For offshore airborne radar approaches (ARA), harmonized visual/radar representations of installations.

6.e. B,C,D The visual system must be free from optical discontinuities and artifacts that create non - Non - realistic cues might include realistic cues. image “swimming” and image “roll - off,” that may lead a pilot to make incorrect assessments of speed, acceleration and/or situational awareness.

6.f. The simulator must have operational landing lights for night scenes. B,C,D None Wher e used, dusk (or twilight) scenes require operational landing lights.

6.g. The simulator must have instructor controls for the following: B,C,D None (1) Visibility in statute miles (kilometers) and runway visual range (RVR) in ft.

(meters).

(2) Airport or landing area selection.

(3) Airport or landing area lighting.

Origem: S P O 88 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Simulator General Simulator Requirements Notes/Information Number Levels Each airport scene displayed must include the following: 6.h. B,C,D None (1) Airport runways and taxiways.

(2) Runway definition: (a) Runway surface and markings.

(b) Lighting for the runway in use, including runway threshold, edge, centerline, touchdown zone, VASI (or PAPI), and approach lighting of appropriate colors, as appropriate.

(c) Taxiway lights.

6.i. The simulator must provide visual system compatibility with dynamic response B,C,D None programming.

6.j. The simulator must show that the segment of the ground visible from the simulator flight B,C,D This will show the modeling deck is the same as from the helicopter flight deck (within established tolerances) when at accuracy of the scene with the corre ct airspeed and altitude above the touchdown zone. respect to a pre - determined position from the end of the runway “in use.” 6.k. The simulator must provide visual cues necessary to assess rate of change of height, None B height AGL, and translational displacement and rates during takeoffs and landings.

6.l. C,D The simulator must provide visual cues necessary to assess rate of change of height, None height AGL, as well as translational displacement and rates during takeoff, low altitude/low airspeed maneuvering, hover, and landing.

6.m. The simulator must provide for accurate portrayal of the visual environment relating to B,C,D Visual attitude vs. simulator the simulator attitude. attitude is a comparison of pitch and roll of the horizon as displayed in the visual scene compared to the display on the attitude indicator Origem: S P O 89 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Simulator General Simulator Requirements Notes/Information Number Levels 6.n C,D The simulator must provide for quick confirmation of visual system color, RVR, focus, None and intensity.

An SOC is required.

6.o. C,D The simulator must be capable of producing at least 10 levels of occulting. None 6.p. Night Visual Scenes. The simulator must provide night visual scenes with sufficient B,C,D None scene content to recognize the airport, the terrain, and major landmarks around the airport.

The scene content must allow a pilot to successfully accomplish a visual landi ng. Night scenes, as a minimum, must provide presentations of sufficient surfaces with appropriate textural cues that include self - illuminated objects such as road networks, ramp lighting, and airport signage, to conduct a visual approach, a landing, and a irport movement (taxi).

Scenes must include a definable horizon and typical terrain characteristics such as fields, roads and bodies of water and surfaces illuminated by helicopter landing lights.

6.q. Dusk (Twilight) Visual Scenes. The simulator must provide dusk (or twilight) visual C,D None scenes with sufficient scene content to recognize the airport, the terrain, and major landmarks around the airport. The scene content must allow a pilot to successfully acc omplish a visual landing. Dusk (or twilight) scenes, as a minimum, must provide full color presentations of reduced ambient intensity, sufficient surfaces with appropriate textural cues that include self - illuminated objects such as road networks, ramp ligh ting and airport signage, to conduct a visual approach, landing and airport movement (taxi).

Scenes must include a definable horizon and typical terrain characteristics such as fields, roads and bodies of water and surfaces illuminated by representative a ircraft lighting (e.g., landing lights). If provided, directional horizon lighting must have correct orientation and be consistent with surface shading effects . Total scene content must be comparable in detail to that produced by 10,000 visible textured su rfaces and 15,000 visible lights with sufficient system capacity to display 16 simultaneously moving objects.

An SOC is required.

6.r. Daylight Visual Scenes. The simulator must have daylight visual scenes with sufficient C,D None scene content to recognize the airport, the terrain, and major landmarks around the airport.

Origem: S P O 90 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Simulator General Simulator Requirements Notes/Information Number Levels The scene content must allow a pilot to successfully accomplish a visual lan ding. No ambient lighting may “washout” the displayed visual scene. Total scene content must be comparable in detail to that produced by 10,000 visible textured surfaces and 6,000 visible lights with sufficient system capacity to display 16 simultaneously moving objects.

The visual display must be free of apparent and distracting quantization and other distracting visual effects while the simulator is in motion.

An SOC is required.

6.s The simulator must provide operational visual scenes that port ray physical relationships C,D For example: short runways, known to cause landing illusions to pilots. landing approaches over water, uphill or downhill runways, rising terrain on the approach path, unique topographic features.

6.t. The simulator must provide special weather representations of light, medium, and heavy C,D None precipitation near a thunderstorm on takeoff and during approach and landing.

Representations need only be presented at and below an altitude of 2,000 ft. (610 m) above the airport surface and within 10 miles (16 km) of the airport.

6.u. The simulator must present visual scenes of wet and snow - covered runways, including C,D The ANAC will consider runway lighting reflections for wet conditions, and partially obscured lights for snow suitable alternative effects.

conditions.

6.v. C,D The simulator must present realistic color and directionality of all airport lighting. None 6.w. B A minimum of one (1) representative airport and one (1) representative helicopter landing The model identifications must area model. The airport and the helicopter landing area may be contained within the same be acceptable to the ANAC, model. If this option is selected, the approach path to the airport runway(s) and the selectable from the IOS, and approach path to the helicopter landing area must be different. The model(s) used to meet listed on the SOQ.

the following requirements may be demonstrated at either a fictional or a real - world airport or helicopter landing area .

Origem: S P O 91 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Simulator General Simulator Requirements Notes/Information Number Levels 6.x. C,D There must be at least the following airport/helicopter landing areas : The model identifications must be acceptable to the ANAC, (1) At least one (1) representative airport.

selectable from the IOS, and (2) At least three representative non - airport landing areas, as follows: listed on the SOQ.

(a) At least one (1) representative helicopter landing area situated on a substantially elevated surface with respect to the surrounding structures or terrain (e.g., building top, offshore oil rig).

(b) At least one (1) helicopter landing area that meets the definition of a “confined landing area.” (c) At least one (1) helicopter landing area on a sloped surface where the slope is at least 2½°.

7. Sound System. See next None 7.a. The simulator must provide flight deck sounds that result from pilot actions that B,C,D None correspond to those that occur in the helicopter.

7.b. B,C,D Volume control, if installed, must have an indication of the sound level setting. None 7.c. The simulator must accurately simulate the sound of precipitation, windshield wipers, and C,D None other significant helicopter noises perceptible to the pilot during normal and abnormal operations, and include the sound of a crash (when the simulator is landed in an unusual attitude or in excess of the structural gear limitations); normal engine sounds; and the sounds of gear extension and retraction.

An SOC is require d.

7.d. The simulator must provide realistic amplitude and frequency of flight deck noises and D None sounds. Simulator performance must be recorded, compared to amplitude and frequency of the same sounds recorded in the helicopter, and made a part of the QTG.

Origem: S P O 92 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Table C 3 – Table of Tasks vs. Simulator Level – Subjective Requirements The simulator must be able to perform the tasks associated with that level of qualification.

Entry Simulator Number Subjective Requirements Levels Notes/Information 1. Preflight Procedures. See next None 1.a. Preflight Inspection (Flight deck Only) switches, indicators, systems, and equipment. B,C,D None 1.b. APU/Engine start and run - up. See next None 1.b.1. Normal start procedures. B,C,D None 1.b.2. Alternate start procedures. B,C,D None 1.b.3. Abnormal starts and shutdowns (hot start, hung start). B,C,D None 1.c. Taxiing – Ground. B,C,D None 1.d. Taxiing – Hover. B,C,D None 1.e. Pre - takeoff Checks. B,C,D None 2. Takeoff and Departure Phase. See next None 2.a. Normal takeoff. See next None 2.a.1. From ground. B,C,D None 2.a.2. From hover. C,D None 2.a.3 Running. B,C,D None 2.b. Instrument. B,C,D None 2.c. Powerplant Failure During Takeoff. B,C,D None 2.d. Rejected Takeoff. B,C,D None 2.e. Instrument Departure. B,C,D None 3. Climb. See next None Origem: S P O 93 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Simulator Notes/Information Number Subjective Requirements Levels 3.a. Normal. B,C,D None 3.b. Obstacle clearance. B,C,D None 3.c. Vertical. B,C,D None 3.d. One engine inoperative. B,C,D None 4. In - flight Maneuvers. See next None 4.a. Turns (timed, normal, steep). B,C,D None 4.b. Powerplant Failure – Multiengine Helicopters. B,C,D None 4.c. Powerplant Failure – Single - Engine Helicopters. B,C,D None 4.d. Recovery From Unusual Attitudes. B,C,D None 4.e. Settling with Power. B,C,D None None 4.f. Specific Flight Characteristics incorporated into the user’s ANAC approved flight B(a),C(a),D(a) training program.

5. Instrument Procedures. See next None 5.a. Instrument Arrival. B,C,D None 5.b. Holding. B,C,D None 5.c. Precision Instrument Approach. See next None 5.c.1. Normal – All engines operating. B,C,D None 5.c.2. Manually controlled – One or more engines inoperative. B,C,D None 5.d. Non - precision Instrument Approach. B,C,D None 5.e. Missed Approach. See next None 5.e.1. All engines operating. B,C,D None Origem: S P O 94 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Simulator Notes/Information Number Subjective Requirements Levels 5.e.2. One or more engines inoperative. B,C,D None 5.e.3. Stability augmentation system failure. B,C,D None 6. Landings and Approaches to Landings. See next None 6.a. Visual Approaches (normal, steep, shallow). B,C,D None 6.b. Landings. See next None 6.b.1. Normal/crosswind. See next None 6.b.1.a. Running. B,C,D None 6.b.1.b. From Hover. C,D None 6.b.2. One or more engines inoperative. B,C,D None 6.b.3. Rejected Landing. B,C,D None 7. Normal and Abnormal Procedures. See next None 7.a. Powerplant. B,C,D None 7.b. Fuel System. B,C,D None 7.c. Electrical System. B,C,D None 7.d. Hydraulic System. B,C,D None 7.e. Environmental System(s). B,C,D None 7.f. Fire Detection and Extinguisher Systems. B,C,D None 7.g. Navigation and Aviation Systems. B,C,D None 7.h. Automatic Flight Control System, Electronic Flight Instrument System, B,C,D None and Related Subsystems.

7.i. Flight Control Systems. B,C,D None Origem: S P O 95 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Entry Simulator Notes/Information Number Subjective Requirements Levels 7.j. Anti - ice and Deice Systems. B,C,D None 7.k. Aircraft and Personal Emergency Equipment. B,C,D None 7.l. Special Missions tasks (e.g., Night Vision goggles, Forward Looking Infrared System, B(a),C(a),D None External Loads and as listed on the SOQ.)

8. Emergency procedures (as applicable). See next None 8.a. Emergency Descent. B,C,D None 8.b. Inflight Fire and Smoke Removal. B,C,D None 8.c. Emergency Evacuation. B,C,D None 8.d. Ditching. B,C,D None 8.e. Autorotative Landing. B,C,D None 8.f. Retreating blade stall recovery. B,C,D None 8.g. Mast bumping. B,C,D None 8.h. Loss of tail rotor effectiveness. B,C,D None 8.i. Vortex recovery B,C,D None 9. Postflight Procedures. See next None 9.a After - Landing Procedures. B,C,D None 9.b. Parking and Securing. See next None 9.b.1. Rotor brake operation. B,C,D None 9.b.2. Abnormal/emergency procedures. B,C,D None Note: An “(a)” in the table indicates that the system, task, or procedure may be examined if the appropriate aircraft system or control is simulated in t he FFS and is working properly.

Origem: S P O 96 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1ºde abril de 2020. Emenda n º 00 Table C 4 – Table of Tasks vs. Simulator Level – Subjective Requirements The simulator must be able to perform the tasks associated with that level of qualification.

Entry Simulator Notes/Information Number Levels Subjective Requirements 1. Instructor Operating Station (IOS), as appropriate. See next None 1.a. Power switch(es). None B,C,D 1.b. Helicopter conditions. B,C,D e.g., GW, CG, Fuel loading, Systems, Ground. Crew 1.c. Airports / Heliports / Helicopter Landing Areas B,C,D e.g., Selection, Surface, Presets, Lighting controls.

Environmental controls. e.g., Clouds, Visibility, RVR, 1.d. B,C,D Temp, Wind, Ice, Snow, Rain, and Windshear.

1.e. Helicopter system malfunctions (Insertion / deletion) B,C,D None 1.f. Locks, Freezes, and Repositioning. B,C,D None 2. Sound Controls. See next None 2.a. On / off / adjustment B,C,D None 3. Motion / Control Loading System. See next None 3.a. On / off / emergency stop B,C,D None 4. Observer Seats / Stations. See next None 4.a. Position / Adjustment / Positive restraint system. B,C,D None Origem: S P O 97 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 APÊNDICE D (APPENDIX D ) QUALIFICATION PERFORMANCE REQUISITOS DE DESEMPENHO PARA STANDARDS FOR HELICOPTER QUALIFICAÇÃO DE DISPOSITIVO DE FLIGHT TRAINING DEVICES TREINAMENTO DE VOO (FTD) DE HELICÓPTERO (a) In order to be qualified at a particular ( a ) Para ser qualificado a um determinado qual ification level, the FTD must meet the nível, o FTD deve cumprir os requisitos standards listed in tables D1, D2 , D3 and D 4 of listados nas tabelas D1, D2 , D3 e D 4 deste this appendix , avaiable only in english. . apêndice , disponíveis apenas em língua inglesa.

(b) Except for level 4 FTD, each FTD must (b) Exceto para FTD nível 4, cada FTD have a QTG, acceptable to the ANAC, that deve possuir um QTG, aceito pela ANAC, includes: contendo: (1) Objective data obtained from (1) Dados objetivos obtidos de ensaio traditional aircraft testing or anothe r approved em voo da aeronave ou outra fonte de dados source; aprovada; (2) The results of FTD objective tests; (2) Os resultados dos testes objetivos do FTD; (3) The results of FTD subjective tests; (3) Os resultados dos testes subjetivos and do FTD; e (4) A description of the equipment (4) Uma descrição do equipamento necessary to perform the evaluation for initial necessário para executar as avaliações para qualification and the continuing qualification qualificação inicial e para qualificação evaluations. recorrente.

Origem: S P O 98 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Table D1 – General technical requirements for FTD levels – Helicopter General technical requirements FTD Level A Level 4 device is one that may have an open helicopter - specific flight deck area, or an enclosed helicopter - specific flight deck and at least one operating system.

Air/ground logic is required (no aerodynamic programming required). All displays may be flat/LCD panel representations or actual representations of displays in the aircraft.

All controls, switches, and knobs may be touch sensitive activation (not capable of manual manipulation of the flight controls) or may physically replicate the aircraft in control operation.

See table D2 for more FTD requirements.

A Level 5 device is one that may have an open helicopter - specific flight deck area, or an enclosed helicopter - specific flight deck and a generic aerodynamic program ming with at least one operating system and control loading representative of the simulated helicopter.

The control loading need only represent the helicopter at an approach speed a nd configuration.

All displays may be flat/LCD panel representations or actual representations of displays in the aircraft. Primary and secondary flight controls (e.g., rudder, aileron, elevator, flaps, spoilers/speed brakes, engine controls, landing gear , nosewheel steering, trim, brakes) must be physical controls.

All other controls, switches, and knobs may be touch sensitive activation.

See table D2 for more FTD requirements.

A Level 6 device is one that has an enclosed helicopter - specific flight deck and aerodynamic program with all applicable helicopter systems operating and control loading that is representative of the simulated helicopter throughout its ground and flight en velope and significant sound representation.

All displays may be flat/LCD panel representations or actual representations of displays in the aircraft, but all controls, switches, and knobs must physically replicate the aircraft in control operation.

See t able D2 for more FTD requirements.

A Level 7 device is one that has an enclosed helicopter - specific flight deck and aerodynamic program with all applicable helicopter systems operating and control loading that is representative of the simulated helicopter throughout its ground and flight en velope and significant sound representation.

All displays may be flat/LCD panel representations or actual representations of displays in the aircraft, but all controls, switches, and knobs must physically replicate the aircraft in control operation. It al so has a visual system that provides an out - of - the - flight deck view, providing cross - flight deck viewing (for both pilots simultaneously) of a field - of - view of at least 146° horizontally and 36° vertically as well as a vibration cueing system for character istic helicopter vibrations noted at the pilot station(s).

See table D2 for more FTD requirements.

Origem: S P O 99 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Table D 2 – General FTD Requirements Entry FTD General FTD Requirements Notes/Information Number Level 1. General Flight deck Configuration. See next None 1.a. The FTD must have a flight deck that is a replica of the helicopter, or set of 6,7 For FTD purposes, the flight deck consists of helicopters simulated with controls, equipment, observable flight deck all that space forward of a cross section of the indicators, circuit breakers, and bulkheads properly located, functionally flight deck at the most extreme aft setting of accurate and replicating the helicopter or set of helicopters. The direct ion of the pilots ’ seats including additional, required movement of controls and switches must be identical to that in the helicopter crewmember duty stations and those required or set of helicopters. bulkheads aft of the pilot seats.

Crewmember seats must afford the capability for the occupant to be able to Bulkheads containing only items such as achieve the design “eye position.” Equipment for the operation of the fli ght la nding gear pin storage compartments, fire deck windows must be included, but the actual windows need not be axes and extinguishers, spare light bulbs, and operable. Those circuit breakers that affect procedures or result in observable aircraft documents pouches are not considered flight deck indications must be properly located and functionally accurate. essential and may be omitted. If omitted, these Fire axes, extinguishers, land ing gear pins, and spare light bulbs must be items, or the silhouettes of these items, may be available, and may be represented in silhouette, in the flight simulator. This placed on the wall of th e simulator, or in any equipment must be present as near as practical to the original position. other location as near as practical to the original position of these items.

The FTD must have equipment (i.e., instruments, panels, systems, circuit 1.b. 4,5 None breakers, and controls) simulated sufficiently for the authorized training/ch ecking events to be accomplished. The installed equipment, must be located in a spatially correct configuration, and may be in a flight deck or an open flight deck area. Those circuit breakers that affect procedures or result in observable flight deck indi cations must be properly located and functionally accurate. Additional equipment required for the authorized training and checking events must be available in the FTD but may be located in a suitable location as near as practical to the spatially correct p osition. Actuation of this equipment must replicate the appropriate function in the helicopter.

Origem: S P O 100 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry FTD General FTD Requirements Notes/Information Number Level Fire axes, landing gear pins, and any similar purpose instruments need only be represented in silhouette.

2. Programming. See next None 2.a. The FTD must provide the proper effect of aerodynamic changes for the 5,6,7 None combinations of drag and thrust normally encountered in flight. This must include the effect of change in helicopter attitude, thrust, drag, altitude, temperature, and configuration.

Levels 6 and 7 additionally require the effects of changes in gross weight and center of gravity.

Level 5 requires only generic aerodynamic programming. An SOC is required.

The FTD must have the computer (analog or digital) capability (i.e ., 2.b. 4,5,6,7 None capacity, accuracy, resolution, and dynamic response) needed to meet the qualification level sought.

An SOC is required.

2.c. Relative responses of the flight deck instruments must be measured by 5,6,7 The intent is to verify that the FTD provides latency tests or transport delay tests, and may not exceed 150 milliseconds. instrument cues that are, within the stated The instruments must respond to abrupt input at the pilot ’ s position within time delays, like the helicopter responses.

the allotted time, but not before the time that the helicopter or set of For helicopter response, acceleration in the helicopters respond under the same conditions.

appropriate, corresponding rotational axis is preferred.

● Latency: The FTD instrument and, if applicable, the motion system and the visual system response must not be prior to that time when the helicopter responds and may resp ond up to 150 milliseconds after that time under the same conditions.

● Transport Delay: As an alternative to the Latency requirement, a transport delay objective test may be used to demonstrate that the FTD system does Origem: S P O 101 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry FTD General FTD Requirements Notes/Information Number Level not exceed the specified limit. The sponsor must measure all the delay encountered by a step signal migrating from the pilot’s control through all the simulation software modules in the correct order, using a handshaking protocol, finally through the normal output interfaces to the instrument display and, if applicable, the motion system, and the visual system.

3. Equipment Operation. See next None All relevant instrument indications involved in the simulation of the 3.a. 4(a),5,6,7 None helicopter must automatically respond to control movement or external disturbances to the simulated helicopter or set of helicopters; e.g., turbu lence or winds.

Navigation equipment must be installed and operate within the tolerances 3.b. 4(a),5,6,7 None applicable for the helicopter or set of helicopters.

Levels 6 and 7 must also include communication equipment (inter - phone and air/ground) like that in the helicopter.

Level 5 only needs that navigation equipment necessary to fly an instrument approach.

Installed systems must simulate the applicable helicopter system operation 3.c. 4(a),5,6,7 None both on the ground and in flight . At least one helicopter system must be represented. Systems must be operative to the extent that applicable normal, abnormal, and emergency operating procedures included in the sponsor’s training programs can be accomplished.

Levels 6 and 7 must simulate all applicable helicopter flight, navigation, and systems operation.

Level 5 must have functional flight and navigational controls, displays, and instrumentation.

Origem: S P O 102 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry FTD General FTD Requirements Notes/Information Number Level 3.d. The lighting environment for panels and instruments must be su fficient for 4,5,6,7 Back - lighted panels and instruments may be the operation being conducted. installed but are not required.

The FTD must provide control forces and control travel that correspond to 3.e. 6,7 None the replicated helicopter or set of helicopters. Control forces must react in the same manner as in the helicopter or set of helicopters under the same flight conditions.

3.f. The FTD must provide control forces and control travel of sufficient 5 None precision to manually fly an instrume nt approach. The control forces must react in the same manner as in the helicopter or set of helicopters under the same flight conditions.

4. Instructor or Evaluator Facilities. See next None In addition to the flight crewmember stations, suitable seating arrangements These seats need not be a replica of an aircraft 4.a. 4,5,6,7 for an instructor/check airman and ANAC Inspector must be available. seat and may be as simple as an office chair These seats must provide adequate view of crewmember ’ s panel(s). placed in an appropriate position.

The FTD must have instructor controls that permit activation of normal, 4.b. 4,5,6,7 None abnormal, and emergency conditions, as appropriate. Once activated, proper system operation must result from system management by the crew and not require input from the instructor controls.

5. Motion System. See next None A motion system may be installed in an FTD. If installed, the motion system None 5.a. 4,5,6,7 operation must not be distracting. If a motion system is installed and additional training, testing, or checking credits are being sought, sensory cues must also be integrated. The motion system must respond to abrupt input at the pilot ’ s position within t he allotted time, but not before the time when the helicopter responds under the same conditions. The motion system must be measured by latency tests or transport delay tests and may not exceed 150 milliseconds. Instrument response must not occur prior to motion Origem: S P O 103 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry FTD General FTD Requirements Notes/Information Number Level onset.

The FTD must have at least a vibration cueing system for characteristic May be accomplished by a “seat shaker” or a 5.b. 7 bass speaker sufficient to provide the necessary helicopter vibrations noted at the pilot station(s).

cueing.

6. Visual System. See next None 6.a. The FTD may have a visual system, if desired, although it is not required. If See next None a visual system is installed, it must meet the following criteria: The visual system must respond to abrupt input at the pilot ’ s position.

6.a.1. 4,5,6 None An SOC is required.

The visual system must be at least a single channel, non - collimated display.

6.a.2. 4,5,6 None An SOC is required.

The visual system must provide at least a field - of - view of 18° vertical / 24° 6.a.3. 4,5,6 None horizontal for the pilot flying.

An SOC is required.

6.a.4. The visual system must provide for a maximum parallax of 10° per pilot. 4,5,6 None An SOC is required.

The visual scene content may not be distracting.

6.a.5. 4,5,6 None An SOC is required.

The minimum distance from the pilot’s eye position to the surface of a direct 6.a.6. 4,5,6 None view display may not be less than the distance to any front panel instrument.

An SOC is required.

The visual system must provide for a minimum resolution of 5 arc - minutes 6.a.7. 4,5,6 None Origem: S P O 104 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry FTD General FTD Requirements Notes/Information Number Level for both computed and displayed pixel size.

An SOC is required.

If a visual system is installed and additional training, testing, or checking 6.b. 4,5,6 None credits are being sought on the basis of having a visual system, a visual system meeting the standards set out for at least a Level A FFS (see Appendix A of this RBAC ) will be required. A “direct - view,” non - collimated visual system (with the other requirements for a Level A visual system met) may be considered satisfactory for those installations where the visual system design “eye point” is appropriate ly adjusted for each pilot’s position such that the parallax error is at or less than 10º simultaneously for each pilot.

An SOC is required.

The FTD must provide a continuous visual field - of - view of at least 146° Optimization of the vertical field - of - view may 6.c. 7 horizontally and 36° vertically for both pilot seats, simultaneously. The be considered with respec t to the specific minimum horizontal field - of - view coverage must be plus and minus one - half helicopter flight deck cut - off angle. When (½) of the minimum continuous field - of - view requirement, centered on the considering the installation/use of augmented zero degree azimuth line relative to the aircraft fuselage. Additional fields of view, as described here, it will be the horizontal field - of - view capability may be added at the sponsor’s discretion responsibility of the sponsor to meet with the provided the minimum field - of - view is retained. Capability for a fiel d - of - ANAC to determine the training, testing, view in excess of these minima is not required for qualification at Level 7. checking, o r experience tasks for which the However, where specific tasks require extended fields of view beyond the augmented field - of - view capability may be 146° by 36° (e.g., to accommodate the use of “chin windows” where the critical to that approval.

accommodation is either integra l with or separate from the primary visual system display), then such extended fields of view must be provided.

An SOC is required and must explain the geometry of the installation.

A minimum of one (1) representative airport and one (1) representative Each model must be acceptable to the ANAC, 6.d. 7 helicopter landing area model. selectable from the IOS, and listed on the SOQ Origem: S P O 105 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry FTD General FTD Requirements Notes/Information Number Level The airport and the helicopter landing area may be contained within the same visual model. If this option is selected, the approach path to the airport runway(s) and the approach path to the helicopter landing area must be different. The model(s) used to m eet the following requirements may be demonstrated at either a fictional or a real - world airport or helicopter landing area.

7. Sound System See next None The FTD must simulate significant flight deck sounds resulting from 7.a. 6,7 None pilot actions that correspond to those heard in the helicopter.

Origem: S P O 106 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Table D 3 - Minimum FTD Requirements – Subjective Requirements The FTD must be able to perform the tasks associated with the level of qualification sought.

Entry FTD Level Notes/Information Number Subjective Requirements 1. 1. Preflight Procedures. See next None 1.a. Preflight Inspection (Flight deck Only) switches, indicators, systems, and equipment. 4(a),5(a),6,7 None 1.b. APU/Engine start and run - up. See next None 1.b.1. Normal start procedures. 4(a),5(a),6,7 None 1.b.2. Alternate start procedures. 4(a),5(a),6,7 None 1.b.3. Abnormal starts and shutdowns (hot start, hung start). 4(a),5(a),6,7 None 1.c. Taxiing – Ground. 7 None 1.d. Taxiing – Hover. 7 None 1.e. Pre - takeoff Checks. 4(a),5(a),6,7 None 2. 2. Takeoff and Departure Phase. See next None 2.a. Normal takeoff. See next None 2.a.1. From ground. 7 None 2.a.2. From hover. 7 None 2.a.3 Running. 7 None 2.b. Instrument. 6,7 None 2.c. Powerplant Failure During Takeoff. 6,7 None 2.d. Rejected Takeoff. 7 None 2.e. Instrument Departure. 6,7 None 3. 3. Climb. See next None Origem: S P O 107 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry FTD Level Notes/Information Number Subjective Requirements 3.a. Normal. 6,7 None 3.b. Obstacle clearance. 7 None 3.c. Vertical. 6,7 None 3.d. One engine inoperative. 6,7 None 4. 4. In - flight Maneuvers. See next None 4.a. Turns (timed, normal, steep). 5,6,7 None 4.b. Powerplant Failure - Multiengine Helicopters. 6,7 None 4.c. Powerplant Failure - Single - Engine Helicopters. 6,7 None 4.d. Recovery From Unusual Attitudes. 7 None 4.e. Settling with Power. 7 None 5. 5. Instrument Procedures. See next None 5.a. Instrument Arrival. 6,7 None 5.b. Holding. 6,7 None 5.c. Precision Instrument Approach. See next None 5.c.1. Normal - All engines operating. 5,6,7 None 5.c.2. Manually controlled - One or more engines inoperative. 6,7 None 5.d. Non - precision Instrument Approach. 5,6,7 None 5.e. Missed Approach. See next None 5.e.1. All engines operating. 6,7 None 5.e.2. One or more engines inoperative. 6,7 None 5.e.3. Stability augmentation system failure. 6,7 None Origem: S P O 108 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry FTD Level Notes/Information Number Subjective Requirements 6. 6. Landings and Approaches to Landings See next None 6.a. Visual Approaches (normal, steep, shallow). 5,6,7 None 6.b. Landings. See next None 6.b.1. Normal/crosswind. See next None 6.b.1.a. Running. 7 None 6.b.1.b. From Hover. 7 None 6.b.2. One or more engines inoperative. 7 None 6.b.3. Rejected Landing. 7 None 7. 7. Normal and Abnormal Procedures. See next None 7.a. Powerplant. 4(a),5(a),6,7 None 7.b. Fuel System. 4(a),5(a),6,7 None 7.c. Electrical System. 4(a),5(a),6,7 None 7.d. Hydraulic System. 4(a),5(a),6,7 None 7.e. Environmental System(s). 4(a),5(a),6,7 None 7.f. Fire Detection and Extinguisher Systems. 4(a),5(a),6,7 None 7.g. Navigation and Aviation Systems. 4(a),5(a),6,7 None 7.h. Automatic Flight Control System, Electronic Flight Instrument System, and Related 4(a),5(a),6,7 None Subsystems.

7.i. Flight Control Systems. 4(a),5(a),6,7 None 7.j. Anti - ice and Deice Systems. 4(a),5(a),6,7 None 7.k. Aircraft and Personal Emergency Equipment. 4(a),5(a),6,7 None Origem: S P O 109 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Entry FTD Level Notes/Information Number Subjective Requirements 7.l. Special Missions tasks (e.g., Night Vision goggles, Forward Looking Infrared System, 7 None External Loads and as listed on the SOQ.)

8. 8. Emergency procedures (as applicable). See next None 8.a. Emergency Descent. 6,7 None 8.b. Inflight Fire and Smoke Removal. 6,7 None 8.c. Emergency Evacuation. 6,7 None 8.d. Ditching. 7 None 8.e. Autorotative Landing. 7 None 8.f. Retreating blade stall recovery. 7 None 8.g. Mast bumping. 7 None 8.h. Loss of tail rotor effectiveness. 6,7 None 9. 9. Postflight Procedures. See next None 9.a After - Landing Procedures. 4(a),5(a),6,7 None 9.b. Parking and Securing. See next None 9.b.1. Rotor brake operation. 4(a),5(a),6,7 None 9.b.2. Abnormal/emergency procedures. 4(a),5(a),6,7 None Note: An “(a)” in the table indicates that the system, task, or procedure may be examined if the appropriate aircraft system or control is simulated in the FTD and is working properly.

Origem: S P O 110 / 113 Data da emissão: 20 de março de 2020. RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 Table D 4 - Table of FTD System Tasks – Subjective Requirements In order to be qualified at the FTD qualification level indicated, the FTD must be able to perform at least the tasks associa te with that level of qualification.

Entry FT D Subjective Requirements Notes/Information Number Level 1. Instructor Operating Station (IOS). See next None 1.a.

Power switch(es). 4(a),5,6,7 None 1.b. Helicopter conditions. e.g., GW, CG, Fuel 4(a),5(a),6,7 loading, Systems, Ground. Crew 1.c.

Airports / Heliports / Helicopter Landing Areas 4(a),5,6,7 e.g., Selection, Surface, Presets, Lighting controls.

1.d. Environmental controls. 4(a),5,6,7 e.g., Temp and Wind.

1.e.

Helicopter system malfunctions (Insertion / deletion) 4(a),5(a),6,7 None 1.f.

Locks, Freezes, and Repositioning (as appropriate). 4(a),5,6,7 None 1.g.

Sound Controls. (On / off / adjustment) 5,6,7 None 1.fh Motion / Control Loading System, as appropriate. On / off / emergency stop 5(a),6,7 None 2. Observer Seats / Stations. See next None Position / Adjustment / Positive restraint system.

2.a. 4(a),5,6,7 None Note: An “A” in the table indicates that the system, task, or procedure may be examined if the appropriate simulator system o r control is in the FTD and is working properly.

Origem: S P O 111 / 113 Data da emissão: 20 de março de 2020 RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 APÊNDICE E ( APPENDIX E ) QUALIFICATION PERFORMANCE REQUISITOS PARA O SISTEMA DE STANDARDS FOR QUALITY GERENCIAMENTO DA QUALIDADE MANAGEMENT SYSTEMS (QMS) FOR (QMS) PARA FSTD FSTD ( a ) Cada operador de FSTD deve enviar à (a) E ach current sponsor of an FSTD must ANAC uma proposta para o Programa de submit to the ANAC a proposed Quality Gerenciamento da Qualidade (QMS). A Management System (QMS) program. The ANAC notificará o operador sobre a ANAC will notify the sponsor of the aceitação do programa, incluindo quaisquer acceptability of the program, including any ajustes que forem necessários. Dentro de 6 required adjustments. Within 6 months of the meses da notificação de ac eitação, o operador notification of acceptability, the sponsor must deve implantar o programa, conduzir implement the program, conduct internal auditorias internas, ajustar o programa como audits, make required program adjustments as resultados dessas auditorias, e agendar a a result of any internal audit, and schedule the inspeção inicial com a ANAC.

ANAC i nitial audit. .

(b) First - time FSTD sponsors must submit (b) Novos operadores de FSTD devem to the ANAC the proposed QMS program no enviar à ANAC uma proposta de QMS com l ater than 120 days before the initial FSTD no mínimo 120 dias de antecedência à data de evaluation. The ANAC will notify the sponsor avaliaç ão inicial do FSTD. A ANAC of the acceptability of the program, including notificará o operador sobre a aceitação do any required adjustments. Within 6 months of programa, incluindo quaisquer ajustes que the notification of acceptability, the sponsor forem necessários. Dentro de 6 meses da must implement the program, c onduct internal notificação de aceitação, o operador deve audits, make required program adjustments as implantar o programa, conduzir auditorias a result of any internal audit, and schedule the internas, ajustar o programa como resultados ANAC initial audit. dessas auditorias, e agendar a inspeção inicial com a ANAC.

(c) The Director of Operations for a RBAC ( c ) O diretor de operações de um detentor 119 certificate holder, the Chief Instructor for de certificado sob o RBAC 119, o instrutor a RBAC 141 certificate holder, or the chefe de um detentor de certificado sob o equivalent for a RBAC 142 sponsor must RBAC 141, ou o equivalente para um d esignate a Management Representative (MR) detentor sob o RBAC 142 ; deve designar um who has the authority to establish and modify Representante do Operador (MR) que possua the sponsor's policies, processes , and a autoridade para estabelecer e modif icar as procedures regarding the QMS program for the políticas, processos e procedimentos do recurring qualification and the daily use of programa de QMS para as qualificações each FSTD. recorrentes e o uso diário de cada FSTD.

(d) The QMS policies, processes, or (d) As políticas, processos ou procedures must be maintained in a Quality procedimentos devem ser mantidos em um Manual and will serve as the basis for the Manual de Qualidade, que servirá de base following: para: Origem: S P O 112 / 113 Data da emissão: 20 de março de 2020 RBAC nº 60 Data de vigência: 1º de abril de 2020. Emenda n º 00 (1) The sponsor - conducted initial and (1) As auditorias inicia l e periódicas recurring periodic assessments ; conduzidas pelo operador; (2) The ANAC - conducted initial and (2) As auditorias inicial e periódicas recurring periodic assessments; and conduzidas pela ANAC; (3) The continuing surveillance and (3) A vigilância continuada e o analysis by the ANAC of the sponsor's acompanhamento da ANAC acerca do performance and effectiveness in providing a desempenho e efetividade do operador em satisfactory FSTD for use on a regular basis. disponibilizar um FSTD satisfatório para uso frequente .

(e) The sponsor mu st conduct assessments ( e ) O operador deve conduzir as auditorias of its QMS program in segments. The do seu programa de QMS em segmentos. Os segments will be established by the ANAC at segmentos serão definidos pela ANAC na the initial assessment, and the interval for the avaliação inicial, e cada segmento deverá ser segment assessments will be every 6 months. avaliado a cada 6 meses. Esse intervalo The intervals for the segment assessments may poderá ser estendido além de 6 meses, a be extended be yond 6 months as the QMS medida que o programa de QMS amadurecer, program matures, but will not be extended mas não poderá exceder 12 meses. O beyond 12 months. The entire QMS program programa de QMS deverá ser inteiramente must be assessed every 24 months. audit ado a cada 24 meses.

(f) The periodic assessments conducted by (f) As avaliações periódicas conduzidas the ANAC will be conducted at intervals not pela ANAC deverão o correr, no mínimo, uma less than once every 24 months, and include a vez a cada intervalo de 24 meses, e incluirá comprehensive review of the QMS program. uma revisão completa do programa de QMS.

Origem: S P O 113 / 113