Type Acceptance Report TAR 8/21B/8 – Cessna 404
Cessna 404 Titan · Other Documents
Overview
This Type Acceptance Report provides detailed information on the Cessna Model 404, which has been granted type acceptance in New Zealand based on validation of FAA Type Certificate number A25CE. The report outlines the aircraft's certification details, operational requirements, and compliance with New Zealand regulations. It serves as a reference for operators and regulatory bodies, ensuring that the Cessna 404 meets the necessary standards for airworthiness and operational safety. The document includes specifications for the aircraft, including its maximum takeoff weight, seating capacity, and engine details, as well as information on the certification process and any applicable requirements for operation in New Zealand.
- Maximum Certificated Takeoff Weight (MCTOW): 8,400 lb (3,810 kg)
- Maximum seating capacity: 11
- Engine: Continental GTSIO-520-M
- Type Certificate: A25CE
- First registered example: 404-0693, ZK-NDY, in 2007
Document
Source
Originally published by www.aviation.govt.nz. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Other Documents
- Year
- 2018
- Pages
- 11
- File size
- 48 KB
- Publisher
- www.aviation.govt.nz
Common. Rarer than 5% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna 404 Titan.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Executive Summary
The Cessna Model 404 has received New Zealand Type Acceptance based on FAA Type Certificate A25CE. All serial numbers under this certificate are accepted, except for the Model 406. The report confirms that the Model 404 is eligible for an Airworthiness Certificate in the Standard Category, pending compliance with New Zealand operational requirements.
Aircraft Certification Details
The Cessna 404 is certified under FAA Type Certificate A25CE, with a maximum certificated takeoff weight (MCTOW) of 8,400 lb (3,810 kg) and a maximum seating capacity of 11. It is powered by a Continental GTSIO-520-M engine and features a McCauley propeller.
Application Details and Background Information
The report details the application for type acceptance of the Cessna 404, initiated by Dennis Thompson International Ltd in 2007. The aircraft is described as an unpressurized low-wing light twin-engine piston aircraft, accommodating two crew and nine passengers. The first example was registered in New Zealand in 1977.
NZCAR §21.43 Data Requirements
The report outlines the data requirements satisfied under NZCAR Part 21B, including the FAA Type Certificate and airworthiness design standards. The certification basis for the Model 404 is FAR Part 23, with no non-compliances noted.
New Zealand Operational Rule Compliance
The report reviews compliance with New Zealand operational requirements, confirming that the Cessna 404 meets the necessary standards for airworthiness and operational safety. Specific requirements for seating, restraints, and emergency equipment are addressed.
Safety notes
- Ensure compliance with New Zealand operational requirements before flight.
- Refer to the latest revision of the State-of-Design Type Certificate Data Sheet for current technical data.
Full document text
Aircraft Certification Unit Type Acceptance Report TAR 8/21B/8 – Revision 1 CESSNA 404 Type Acceptance Report Rev.1 : 22 May 2018 TAR 8/21B/8 – Cessna 404 i TABLE OF CONTENTS EXECUTIVE SUMMARY 1 1. INTRODUCTION 1 2. AIRCRAFT CERTIFICATION DETAILS 2 3. APPLICATION DETAILS AND BACKGROUND INFORMATION 3 4. NZCAR §21.43 DATA REQUIREMENTS 4 5. NEW ZEALAND OPERATIONAL RULE REQUIREMENTS 6 ATTACHMENTS 7 APPENDIX 1 7 Type Acceptance Report Rev.1 : 22 May 2018 TAR 8/21B/8 – Cessna 404 1 Executive Summary New Zealand Type Acceptance has been granted to the Cessna Model 404 based on validation of FAA Type Certificate number A25CE. There are no special requirements for import. All serial numbers listed under the FAA type certificate have been type accepted in New Zealand, except for the Model 406, which was only produced in France by Reims Aviation. The Model 404 is now eligible for the issue of an Airworthiness Certificate in the Standard Category in accordance with NZCAR §21.177, subject to any outstanding New Zealand operational requirements being met. (See Section 5 of this report for a review of compliance of the basic type design with the operating Rules.) NOTE: The information in this report was correct as at the date of issue. The report is generally only updated when an application is received to revise the Type Acceptance Certificate. For details on the current type certificate holder and any specific technical data, refer to the latest revision of the State-of-Design Type Certificate Data Sheet referenced herein. 1. Introduction This report details the basis on which Type Acceptance Certificate No.8/21B/8 was granted in the Standard Category in accordance with NZCAR Part 21 Subpart B. Specifically, the report aims to: (a) Specify the foreign type certificate and associated airworthiness design standard used for type acceptance of the model(s) in New Zealand; and (b) Identify any special conditions for import applicable to any model(s) covered by the Type Acceptance Certificate; and (c) Identify any additional requirements which must be complied with prior to the issue of a NZ Airworthiness Certificate or for any subsequent operations. The report covers all models included on the State-of-Design type certificate which have been granted type acceptance in New Zealand. Appendix 1 details which models have been type accepted in accordance with the provisions of CAR Part 21B and which were certificated prior to that under NZCAR Section B.9 and are now type accepted under the transitional arrangements of Part 21 Appendix A(c). Type Acceptance Report TAR 8/21B/8 – Cessna 404 Rev.1 : 22 May 2018 2 2. Aircraft Certification Details (a) State-of-Design Type and Production Certificates: Manufacturer: Cessna Aircraft Company Type Certificate Holder: Textron Aviation Inc. (since July 29, 2015) Type Certificate: A25CE Issued by: Federal Aviation Administration Production Approval: Delegation Option Manufacturer No. CE-3 FAA Production Certificate 312 (b) Models Covered by the Part 21B Type Acceptance Certificate: (i) Model: 404 MCTOW: 8400 lb. [3810 kg] Max. No. of Seats: 11 Noise Standard: FAR Part 36 Engine: Continental GTSIO-520-M Type Certificate: E7CE Issued by: Federal Aviation Administration Propeller: McCauley 3FF32C501/90UMB-0 Type Certificate: P45GL Issued by: Federal Aviation Administration Type Acceptance Report Rev.1 : 22 May 2018 TAR 8/21B/8 – Cessna 404 3 3. Application Details and Background Information The application for New Zealand type acceptance of the 1980 Model 404 was from Dennis Thompson International Ltd, dated 14 August 2007. The first-of-type example was serial number 404-0693, registered ZK-NDY. The Cessna 404 is an unpressurised low-wing light twin-engine piston aircraft with accommodation for two crew and nine passengers. Type Acceptance Certificate Number 8/21B/8 was granted on 24 September 2007 to the 1980 Model 404 based on validation of FAA Type Certificate A25CE. Specific applicability is limited to the coverage provided by the operating documentation supplied. There are no special requirements for import into New Zealand. Revision 1 to this report added all the other model years of the 404 not previously included. This was at the request of the type certificate holder, who has provided access to all technical publications. The Model 404 was conceived as a growth version of the Model 402B, with a larger wing and 35-inch fuselage stretch similar to the 441 and incorporating large fowler flaps, new trailing link main landing gear and a new bonded metal “wet wing”. The basic hydraulic system is taken from the 421C. There have been four previous examples of the 404 on the New Zealand Register including a 1980 model serial number 404-0603 ZK-TNT, but this was de-registered in 1984 and was not current in 1995. The type is therefore not covered by the Transitional Arrangements provisions of Part 21 Appendix A(c). The first example was serial number 404-0067 registered ZK-TAS in April 1977. Type Acceptance Report TAR 8/21B/8 – Cessna 404 Rev.1 : 22 May 2018 4 4. NZCAR §21.43 Data Requirements The type data requirements of NZCAR Part 21B Para §21.43 have been satisfied by supply of the following documents, or were already held by the CAA: (1) State-of-Design Type certificate: FAA Type Certificate Number A25CE FAA Type Certificate Data Sheet A25CE at Revision 13 dated October 29, 2015 – Model 404 approved July 21, 1976 (2) Airworthiness design requirements: (i) Airworthiness Design Standards: The certification basis of the Model 404 is FAR Part 23 effective February 1, 1965, including Amendments 23-1 through 23-13, except Subpart B at Amendment 23- 14; FAR Part 23 paragraph §23.1385(c) at Amendment 23-21 and FAR §23.1327 at Amendment 23-23. This is an acceptable certification basis in accordance with NZCAR Part 21B Para §21.41 and Advisory Circular 21-1A, as FAR 23 is the basic standard for Normal
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Category Airplanes called up under Part 21 Appendix C. There are no non- compliances and no additional special conditions have been prescribed by the Director under §21.23. (ii) Special Conditions: Nil (iii) Equivalent Level of Safety Findings: FAR §23.1189(a) – Engine compartment shutoff means were not required provided hydraulic lines were fireproof hoses with steel fittings which met demonstrated fire resistance criteria. FAR §23.1545 and 23.1583(a) – IAS permitted instead of CAS provided both values are given in the POH/AFM and all placards to meet certification requirements are consistent with instrument markings. ASI calibration data must cover the full operating range and be predicated on flight tests. (iv) Airworthiness Limitations: See the aircraft Maintenance Manual. (3) Environmental Certification: (i) Environmental Standard: The 1980 Model 404 and on has been certificated for noise under FAR Part 36, including Amendments 36-1 through 36-4. (ii) Compliance Listing: Flyover noise, established in compliance with FAR 36 at maximum continuous power is 78.9 dB(A) – See Flight Manual Section 4. (4) Certification Compliance Listing: DM Report 404-0 Type Inspection Report – Basic Aircraft Configuration Cessna Report S-404-110 – Cessna 404 – Structures Data Summary Type Acceptance Report Rev.1 : 22 May 2018 TAR 8/21B/8 – Cessna 404 5 (5) Flight Manual: CAA AIR Cessna Number: Publication: Title: AIR 2025 D1540-13 Model 404 Titan (1977) Pilot’s Operating Handbook AIR 3450 D1563-13 Model 404 Titan (1978) Pilot’s Operating Handbook AIR 2027 D1572-13PH Model 404 Titan (1979) Pilot’s Operating Handbook AIR 3011 D1583-13PH Model 404 Titan (1980) Pilot’s Operating Handbook AIR 2505 D1593-13PH Model 404 Titan (1981) Pilot’s Operating Handbook (6) Operating Data for Aircraft: (i) Maintenance Manual: Cessna 404 (1977-1981) Maintenance Manual – Publication D2517-13 Cessna 400 Series Continued Airworthiness Program – Publication D5305-13 (ii) Current service Information: Service Bulletins (iii) Illustrated Parts Catalogue: Cessna 404 Titan (1977-1981) Parts Catalog – Publication P559-12 (7) Agreement from manufacturer to supply updates of data in (5), and (6): Cessna publications are now available through the Textron 1View website at https://ww2.txtav.com or for older manuals at http://techpubs.cessna.com/ (8) Other information: Cessna Model 404 Titan Ambassador Equipment List – 14 July 1976 Cessna Model 404 Titan Freighter Equipment List – 15 August 1977 Cessna Model 404 Titan Courier Equipment List – 15 August 1978 Cessna Model 404 Titan Ambassador Equipment List – 6 July 1979 Cessna Model 404 Titan Freighter Equipment List – 7 August 1980 Type Acceptance Report TAR 8/21B/8 – Cessna 404 Rev.1 : 22 May 2018 6 5. New Zealand Operational Rule Compliance Compliance with the retrospective airworthiness requirements of NZCAR Part 26 has been assessed as they are a prerequisite for the grant of an airworthiness certificate. CAR Part 26 – Subpart B – Additional Airworthiness Requirements Appendix B – All Aircraft PARA: REQUIREMENT: MEANS OF COMPLIANCE: B.1 Marking of Doors and Emergency Exits To be determined on an individual aircraft basis B.2 Crew Protection Requirements – CAM 8 Appdx. B # .35 Not Applicable – Agricultural Aircraft only Compliance with the following additional NZ operating requirements has been reviewed and were found to be covered by either the original certification requirements or the basic build standard of the aircraft, except as noted: CAR Part 91 – Subpart F – Instrument and Equipment Requirements PARA: REQUIREMENT: MEANS OF COMPLIANCE: 91.505 Seating and Restraints – Safety belt/Shoulder Harness FAR §23.785 91.507 Pax Information Signs – Smoking, safety belts fastened Not Applicable – Less than 10 passenger seats 91.509 Min. VFR (1) ASI (2) Machmeter (3) Altimeter (4) Magnetic Compass (5) Fuel Contents (6) Engine RPM (7) Oil Pressure FAR §23.1303(a) N/A – No mach limitations FAR §23.1303(b) FAR §23.1303(c FAR §23.1305(a) FAR §23.1305(e) FAR §23.1305(b) (8) Coolant Temp (9) Oil Temperature (10) Manifold Pressure (11) Cylinder Head Temp. (12) Flap Position (13) U/c Position (14) Ammeter/Voltmeter N/A – Air cooled engine FAR §23.1305(c) FAR §23.1305(h) FAR §23.1305(f) FAR §23.699(a)(2) FAR §23.729(e) FAR §23.1351 (d) 91.511 Night (1) Turn and Slip (2) Position Lights Fitted as std – See AFM/POH FAR §23.1385 (3) Anti-collision Lights (4) Instrument Lighting FAR §23.1401 FAR §23.1381 91.511 Night VFR Instruments and Equipment Operational requirement – Compliance as applicable 91.513 VFR Communication Equipment Operational requirement – Compliance as applicable 91.517 IFR Instruments and Equipment Operational requirement – Compliance as applicable 91.519 IFR Communication and Navigation Equipment Operational requirement – Compliance as applicable 91.523 Emergency Equipment: (a) More Than 9 pax – First Aid Kits per Table 7 – Fire Extinguishers per Table 8 (b) More than 20 pax – Axe readily accessible to crew (c) More than 61 pax – Portable Megaphones per Table 9 Operational Requirement – Compliance as applicable Operational Requirement – Compliance as applicable Not Applicable – Less than 20 passenger seats Not Applicable – Less than 61 passenger seats 91.529 ELT – TSO C126 406 MHz after 22/11/2007 Operational requirement – Compliance as applicable 91.531 Oxygen Indicators – Volume/Pressure/Delivery Operational requirement – Compliance as applicable 91.533 Oxygen for Non-Pressurised Aircraft >30 min above FL100 – Supplemental for crew, 10% Pax – Therapeutic for 3% of Pax Above FL100 – Supplemental for all Crew, Pax – Therapeutic for 1% of Pax – 120l PBE for each crew member Maximum Operating Altitude Limit in Flight Manual (with oxygen equipment) is 30,000 ft The standard oxygen system is either a 22 cu.ft. bottle or a 114.9 cu.ft. bottle in the nose compartment, with plumbed outlets for each occupant. The oxygen control, pressure gauge, bottle, regulator and plumbing are optional. 91.533 Oxygen for non-Pressurised Aircraft Not fitted as standard 91.541 SSR Transponder and Altitude Reporting Equipment Operational requirement – Compliance as applicable 91.543 Altitude Alerting Device – Turbojet or Turbofan Not Applicable – Not turbo jet or turbofan powered 91.545 Assigned Altitude Indicator Operational requirement – Compliance as applicable A.15 ELT Installation Requirements To be determined on an individual aircraft basis CAR Part 135 – Subpart F – Instrument and Equipment Requirements PARA: REQUIREMENT: MEANS OF COMPLIANCE: 135.355 Seating / Restraints – Shoulder harness flight-crew seats FAR §23.785 135.357 Additional Instruments (Powerplant and Propeller) FAR §23.1305 135.359 Night Flight Landing light, Pax compartment Operational requirement – Compliance as applicable 135.361 IFR Operations Speed, Alt, spare bulbs/fuses Operational requirement – Compliance as applicable 135.363 Emergency Equipment (Part 91.523 (a) and (b)) Operational requirement – Compliance as applicable 135.367 Cockpit Voice Recorder N/A – Only for 2-crew helicopters with more than 10 pax 135.369 Flight Data Recorder Not Applicable – Less than 10 passenger seats 135.371 Additional Attitude Indicator Not Applicable – Not turbo jet or turbofan powered Type Acceptance Report Rev.1 : 22 May 2018 TAR 8/21B/8 – Cessna 404 7 NOTES: 1. A Design Rule reference in the Means of Compliance column indicates the Design Rule was directly equivalent to the CAR requirement, and compliance is achieved for the basic aircraft type design by certification against the original Design Rule. 2. The CAR Compliance Tables above were correct at the time of issue of the Type Acceptance Report. The Rules may have changed since then and compliance should be checked individually. 3. Some means of compliance above are specific to a particular model/configuration. Compliance with Part 91/119 operating requirements should be checked in each case, particularly oxygen system capacity and emergency equipment. Attachments The following documents form attachments to this report: Photographs first-of-type example 1980 Cessna 404 ZK-NDY Three-view drawing Cessna Model 404 Titan Copy of FAA Type Certificate Data Sheet Number A25CE Sign off …………………………………….. ……………………………............... David Gill Checked – Gaetano Settineri Team Leader Airworthiness Airworthiness Engineer Appendix 1 List of Type Accepted Variants: Model: Applicant: CAA Work Request: Date Granted: 404 (1981) AC 21-1.2/NZCAR Part 21 Appendix A(c) 404 (1980) Dennis Thompson International Ltd 8/21B/8 24 September 2007 404 (1977-79) Textron Aviation Inc. 18/21B/17 22 May 2018