TECNAM P2010tdi - Aircraft Flight Manual

Section 9 - SUPPLEMENTS S01 - GTS 800 TAS UNIT ®TEcTOl»P2010tdi - Aircraft Flight Manual pagesoi-4 2. LIMITATIONS Refer to the basic AFM. Section 2 - Limitations. EASA Approved 2"° Edition - Rev. 0 Section 9 - SUPPLEMENTS S01 -GTS800TASUNIT ^ ^^^ p2oi otdi - Aircraft Flight Manual Page 301-5 3. EMERGENCY PROCEDURES If a TAS Computer failure occurs or the "TAS System Test Failed" aural annunciation occurs, the System must be tumed OFF through the dedicated CB. 2"d&A'bon - Rev. 0 Section 9 - SUPPLEMENTS S01 - GTS 800 TAS UNIT W£CNAMP2010tdi - Aircraft Flight Manual pagesoi-e 4. NORMAL PROCEDURES INITIALIZATION 1. After engine starting verify that the TAS circuit breakeris engaged. 2. The TAS System automatically cycles through a power-on. On ground: ^The System goes automatically in Stand-by mode (no traffic surveillance functions are performed.). ^To switch to Operate mode, select it manually via System controls. Inflight: ^The System goes automatically in Operate mode. SYSTEM SELF-TEST 1. Prior to initiate the TAS self-test, ensure that all avionics are turned ON and operational. 2. With the TAS in standby mode perform the TAS l self-test (manually select). It takes approximately ten seconds to complete. 3. After the completion of the lest the aural "TAS System Test Failed / Passed " is annunciated. ^Edition - Rev. 0 Section 9 - SUPPLEMENTS S01 . GTS 800 TAS UNIT ^TECNAMP20^töi - Aircraft Flight Manual pagesoi-7 5. PERFORMANCE Refer to the basic AFM. Section 5 - Performance. 2"dEdition - Rev. 0 Section 9 - SUPPLEMENTS S01 - GTS 800 TAS UNIT (SjAlß^&W.8Ang!NCE1W»^<»<»^ A,- •• • • <«d »W. ?TECÄÄP2010tdi - Aircraft Flight Manual pagesoi -s 6. WEIGHT AND BALANCE Refer to the basic AFM, Section 6 - Weight and Balance. 2") Edition - Rev. 0 Section 9 - SUPPLEMENTS S01 - GTS 800 TAS UNIT r£civJu»P2010tdi - Aircraft Flight Manual pagesoi-9 7. AIRFRAME AND SYSTEMS DESCRIPTION 7.1. GTS 800 TAS UNIT The Garmin GTS 800 is a microprocessor based Line Replaceable Unit (LRU) (hat uses active interrogations of Mode S and Mode C transponders to provide Traffic Advisories to the pilot. When installed with a 1090 MHz ADS-B transmit class of equipment the GTS 800 also utilizes passive surveillance. Traffic is displayed on an external MFD via Ethernet High Speed Data Bus (HSDB), (linked to PFD#1 but displayed to MFD). An aural alert is also provided to inform the crew a traffic advisory (TA) will be displayed. The remote LRU is installed on a dedicated mount located in the nose baggage compartment. Two directional antennas (GA58) are installed on the top and bottom of the fuselage, on the front LH side. A 5 Amps circuit breaker, tied to the "LH BUS"and labelled "TAS", is installed on the circuit breaker panel to protect the System from over current. Figure S01 -1 - GTS 800 Connection Scheme 7.1.1. OPERATING MODES The system typically powers up in Standby mode. In Standby mode, the System is powered on, but no traffic surveillance functions are performed. Operate mode is the normal mode for operations. All active and ADS-B Intraffic surveillance functions are performed in Operate mode. The system can automatically switch between Operate and Standby modes based on whether the own ship is in the air or on the ground. The System will automatically select Operate mode 8 seconds after becoming airborne. Standby mode will automatically be selected 24 seconds after landing. Self-test mode is a manually selected mode that briefly performs a test of the System. If the System detects a fault fhat will prevent normal Operation, the System will enter and remain in Fail mode. 7.1.1.1. CONTROL OF MODES Standby, Operate, and Self-test modes may be manually selected via System contrpls. When the ADS-B In function is installed and the unit is in Operate mode, the ADS-B in feature can be turned on and off. The controls are either integrated with the traffic display(s) or installed äs external control switches. For display(s) that integrate control of ADS-B In and GTS Modes configuration can^be set to allo'w ADS-B IrTfeature to be turned on or off while GTS is in Standby. This feature requires display(s) support. 2"" Edition - Rev. 0 Section 9 - SUPPLEMENTS S01 - GTS 800 TAS UNIT ^clT£CJVAMP2010tdi - Aircraft Flight Manual pagesono 7.1.2. TRAFFIC INFORMATION The function of the GTS Traffic System is to provide Information regarding nearby traffic to the crew. For each traffic target that is tracked by the GTS, the System computes the bearing, ränge, relative altitude, and vertical trend for the target. Relative altitude and vertical trend are available for targets with altitude reporting capability. When ADS-B data is received for a traffic target, additional information is available such äs directionality, ground track, and other identifying information (ICAO address, flight ID, tail number). Traffic information may be available from several sources such äs active surveillance, ADS-B, ADS-R, and TIS-B. The GTS correlates data from multiple sources to create a single, fused traffic picture for the flight crew. This traffic Information is displayed to the crew on an interfaced display. Figure S01-1 shows an example traffic display showing ränge, bearing, relative altitude, and vertical trend. Figure S01-2 shows an example traffic display capable of showing additional data received via ADS-B. Figure S01-2 - Example of Traffic displayed on MFD •INDICATES MULTIPLE TARGETS TOUCH THE TARGET TO SHOW ALL TARGETS THEN TOUCH NEXT TO GET INFO ON EACH OF THE TARGETS Figure S01-3 - Example of Traffic displayed on MFD (via ADS-B) 2"° Edition - Rev. 0 Section 9 - SUPPLEMENTS S01 - GTS 800 TAS UNIT CHJAUTTAUICAUTSlNCElW n^»A ^ ^ ^ •- m. - ^- ^••" l«jr"EcivÄ)wP2010tdi - Aircraft Flight Manual pagesoi-n 7.1.2.1. TRAFFIC ADVISORY INFORMATION Targets may become a TA (Traffic Advisory) based on closure rate (time until collision) or if they encroach within a minimum distance. The criteria used depends on the current sensitivity level and whether the target has altitude reporting capability. Once a TA is generated, it will remain a TA for at least 8 seconds, even if the target no langer satisfies the criteria for a TA. Table S01-1 summarizes the criteria used for TAs. To prevent nuisance TAs in the airport environment, there are two sensitivity levels available: Sensitivity Level A (SLA) and Sensitivity Level B (SL B). The Sensitivity Level determines what criteria will be used for TAs. SL A is less sensitive and traffic must be closer before it will generate an alert. SL B is more sensitive and traffic may be farther away to generate an alert. The logic for choosing the sensitivity level is based on available System inputs. Table S01-1 - TA Alerting Cntena Seiulüvlty intruder Ablüde ^ ^„rt„g condltlons Level Avallable Intruder closing rate provides less than 20 second ofvertical and honzontal separation. Or Intruder closing rate provides less than 20 A Yes second of horizontal separation and vertlcal separation is within 600 feet. Or Intruder ränge is within 0.2 NM and vertical separatem is within 600 feet. Intruder closing rate provides less than 15 No second ofseparation or intruder ränge is within 0.2 NM. Intruder closing rate provides less than 30 second ofvertical and horizontal separation. Or Intruder closing rate provides less than 30 Yes second of horizontal separation and vertical separation is within 800 feet. Or Intruder ränge iswiüiin 0-55 NM and vertical separation is within 800 feet. Intmder closmg rate provides less than 20 No second of separation or intruder ränge is mithin 0.55 NM. 7.1.2.2. NOBEARINGTAS If the bearing of a TA target cannot be determined, a No-Bearing TA will be issued :igure S01-1)_No-Bearing TAs are typically displayed äs a yellpw text banner pn the fraffic display. The text typically includes "TA" followed by the distance, relative altitude, and vertical trend arrow. Relative altitude and vertical trend arrow are not available for targets that da not report altitude. 2"° Edition - Rev. 0 Section 9 - SUPPLEMENTS S01 - GTS 800 TAS UNIT ;«lrECNAMP2010tdi - Aircraft Flight Manual Page 301-12 8. AIRCRAFT CARE AND MAINTENANCE Refer to the basic AFM, Section 8 - Aircraft Care and Maintenance. 2"" Edition - Rev. 0 Section 9 - SUPPLEMENTS S01 - GTS 800 TAS UNIT QiMiJiYAiROWTSmK1Si!i TECNÄM P2010tdi - Aircraft Flight Manualpageso2-o S02 GIOOONxi Synthetic Vision Technology (SVT) 2"" Edition - Rev. 0 Section 9 - SUPPLEMENTS S02 - GIOOOxi Synthetic Vision Technology (SVT) QUUJTf AfflCXW 31NCE •Wt [^t~ECNÄM P2010tdi - Aircraft FIight Manual pagei 1. RECORD OF REVISION W Rev Ed. 2 Rev.O Revised pages Description of Revision First issue Approval See note (*) Previous version was issued and approved accordingto MOD2010/198.210121. 2"" Edition - Rev. 0 Section 9 - SUPPLEMENTS S02 - GIOOOxi Synthetic Vision Technology (SVT) \^fECNÄM P2010tdi - Aircraft Flight Manual pagei Intentionally left blank 2"" Edition - Rev. 0 Section 9 - SUPPLEMENTS S02 - GIOOOxi Synthetic Vision Technology (SVT) OUAUTfAISCfEAFTSiNCE 1M6 ® TECNÄM P201 Otdi - Aircraft Flight Manual page i 2. LIST OF EFFECTIVE PAGES Edition 2, Rev 0 ..................... May 31, 2021 Section Section 0 Section 1 Section 2 Section 3 Section 4 Section 5 Section 6 Section 7 Section 8 Pages AU AU All AU All AU AU AU All Edition / Revision 2"" Edition - Rev. 0 2"d Edition - Rev. 0 2"d Edition - Rev. 0 2"" Edition - Rev. 0 2"s Edition - Rev. 0 2"d Edition - Rev. 0 2"" Edition - Rev. 0 2"d Edition - Rev. 0 2"d Edition - Rev. 0 2"d Edition - Rev. 0 Section 9 - SUPPLEMENTS S02 - GIOOOxi Synthetlc Vision Technology (SVT) ^TECNAM P2010tdi - Aircraft Flight Manual pageiv Intentionally left blank 2"" Edition - Reu. 0 Section 9 - SUPPLEMENTS S02 - GIOOOxi Synthetic Vision Technology (SVT) ) P201 Otdi - Aircraft Flight Manual Page 302-1 INDEX 1. GENERAL......................................................................................................... 3 1.1. INTRODUCTION.................................................................................. 3 2. LIMITATIONS .................................................................................................... 4 3. EMERGENCY PROCEDURES......................................................................... 5 4. NORMAL PROCEDURES................................................................................. 6 5. PERFORMANCE............................................................................................... 8 6. WEIGHTAND BALANCE ................................................................................. 9 7. AIRFRAME AND SYSTEMS DESCRIPTION .................................................... 10 7.1. GTS 800 TAS UNIT ....................................................................... 10 8. AIRCRAFT CARE AND MAINTENANCE ......................................................... 14 2"" Edition - Rev. 0 Section 9 - SUPPLEMENTS S02 - GIOOOxi Synthetlc Vision Technology (SVT) ®T£CÄÄP2010tdi - Aircraft Flight Manual Page 302-2 Intentionally left blank 2"d Edition - Rev. 0 Section 9 - SUPPLEMENTS S02 - GIOOOxl Synthetlc Vision Technology (SVT) ^JfEciVAMP2010tdi - Aircraft Flight Manual Page 302-3 1.GENERAL 1.1. INTRODUCTION This section contains supplemental information to operate, in a safe and efficient manner, the aircraft when equipped with Garmin G1000NXJ Avionics Suite and describes the Synthetic Vision Technology (SVT) (MOD2010/198) which is an optional part ofthe Garmin GIOOONxi Avionics System. This supplement must be attached to the Airplane Flight Manual; the Information contained herein supplements the basic Airplane Flight Manual. For limitations, procedures and performance information not contained in this supplement consult the basic approved Airplane Flight Manual. The Information contained in this Supplement must be considered to override the EASA approved Aircraft Flight Manual where there is any conflict between the supplement and the manual. The purpose of the SVT System is to assist the pilot in maintaining situational awareness with regard to the terrain and traffic surrounding the airplane and the navigational Situation relative to the programmed flight plan. The Synthetic Terrain display is intended to aid the pilot awareness of the terrain and obstacles in front of the airplane. It may not provide either the accuracy or fidelity, or both, on which to solely base decisions and plan maneuvers to avoid terrain or obstacles. The synthetic vision elements are not intended to be used for primary airplane control in place ofthe primary flight Instruments. •^ The pathway presentation is intended only to aid the I ' p/toCs awareness ofthe programmed flight path location • \ relative to the airplanes current position. No vertical CAUTION pathway Information is presented for climbs. The synthetic terrain depiction displays an area approximating the view from the pilot's eye position when looking directly ahead out of the windshield in front of the pilot. Terrain features outside this field of view are not shown on the display. 2"" Edition - Rev. 0 Section 9 - SUPPLEMENTS S02 - GIOOOxi Synthetic Vision Technology (SVT) ^rE'civ/lM'P2010tdi - Aircraft Flight Manual Page 302-4 2. LIMITATIONS Refer to the basic AFM, Section 2 - Limitations. EASA Approved fi Edition - Rev. 0 Section 9 - SUPPLEMENTS S02 - GIOOOxi Synthetic Vision Technology (SVT) @rEC?MMP2010tdi - Aircraft Flight Manual Page 302-5 3. EMERGENCY PROCEDURES SVT Displays information inconsistent with GIOOONxi primary flight instrumentation On the PFD: 1. PFDOptkey ....................................................................................... press 2. SYNVISkey ....................................................................................... press 3. TERRAIN key .......................................................................presstodisable 4. SVT is removed from the PFD .............................................................verify Use GIOOONxi primary displays for navigation and airplane control. 2"d Edition - Rev. 0 Section 9 - SUPPLEMENTS S02 - GIOOOxi Synthetic Vision Technology (SVT) ^T;ECNAM'P2010tdi - Aircraft Flight Manual Page 302-6 4. NORMAL PROCEDURES Turn Synthetic Vision on/off The SVT System may be turned on or off äs desired. To turn the synthetic Vision System on or off: OnthePFD: 1. PFDOptkey ........................................................................................... press 2.SYNVISkey ........................................................................................... press 3. TERRAIN key ...........................................................................................press The synthetic vision System will cycle on or off with each press of the SYN TERR key. Turn Pathways on/off To turn the pathway on or off: OnthePFD: 1. PFDOptkey ............................................................................................... press 2. SYNVIS Key ............................................................................................... press 3. TERRAIN key ...............................................................................................press 4.PATHWAYSkey............................................................................................press The pathway will cycle on or off with each press of the PATHWAYS key. f Edition - Rev. 0 Section 9 - SUPPLEMENTS S02 - GIOOOxi Synthetic Vision Technology (SVT) QUAUTrUHÜUTT&NCE-MI »^^»^ ^ ^ < •• »- ^„ ^-• • ^BCjf£cJVAMP2010tdi - Aircraft Flight Manual page 302-7 Turn Horizon Heading on/off The Horizon Heading may be turned on or off äs desired. To turn the horizon heading on or off: On the PFD: 1. PFDOptkey ......................................................................................... press 2. SYNVISkey ......................................................................................... press S.TERRAINkey .........................................................................................press 4.HDGLBLkey...........................................................................................press The horizon heading will cycle on or offwith each press ofthe HDG LBL key. Turn Airport Signs on/off To turn the airport signs on or off: On the PFD: 1. PFD Optkey ......................................................................................... press 2. SYNVISkey ........................................................................................ press 3. TERRAIN key ........................................................................................press 4. APT Sign...............................................................................................press Airport signs will cycle on or off with each press of the APT Sign key. 2"d Edition - Rev. 0 Section 9 - SUPPLEMENTS S02 - GIOOOxi Synthetic Vision Technology (SVT) ®r£C"?"P2010tdi - Aircraft Flight Manual pageso2-, 5.PERFORMANCE Refer to the basic AFM. Section 5 - Performance. 2"a Edition - Rev. 0 Section 9 - SUPPLEMENTS S02 - GIOOOxi Synthetic Vision Technology (SVT)