Type Acceptance Report - TAR 17/21B/26 - CESSNA F337 Series

(Avions à Atterissage et Décollage Court) and the type designation was changed by changing the model prefix to FA or FTA. The ADAC kit consisted of a recontoured wing leading edge cuff (with optional de-ice boots), wing stall fences, conical cambered wing tips, aileron centering springs, an interconnect mechanism to droop the ailerons when flaps are selected, an Automatic Trim spring connect to the elevator, vortex generators on the rear fuselage, vertical fin fairings, and a new heated pitot system with recalibrated ASI. The FA and FTA versions are not listed on the FAA TCDS, because the re-designation is authorised under the STC. All other Reims-Cessna F337 models are covered under the FAA Type Certificate, with the exception of the FTB337G and GA, which are covered by EASA Specific Airworthiness Specification SAS.A.115 (these were the “milirole” versions with four underwing hardpoints, used by the Portugese and some other Air Forces.) Type Acceptance Report Rev.0 : 30 August 2017 TAR 17/21B/26 – Cessna F337 Series 5 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 A23EU FAA Type Certificate Data Sheet number A23EU at Revision 7 dated July 31, 2012 – Models F337E and FT337E approved March 24, 1970 – Models F337F and FT337F approved April 28, 1971 – Model F337G approved May 11, 1973 – Model FT337GP approved June 22, 1973 – Models F337H and FT337HP approved May 22, 1978 These supersede the original type certificate: DGAC Certificat de Navigabilité de Type Numéro 50 – Reims/Cessna 337 DGAC Fiche de Navigabilité No. 124 – Reims-Cessna F337 et dérivés FAA STC SA11EU issued to Reims Aviation S.A. June 4, 1973 Addendum to STC SA11EU dated 4 June 1973 (2) Airworthiness design requirements: (i) Airworthiness Design Standards: The certification basis of the F337 Series is FAR Part 23 effective February 1, 1965, including Amendments 23-1 through 23-6. This is an acceptable certification basis in accordance with NZCAR Part 21B Para §21.41, because FAR Part 23 is the basic standard for Normal 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 and Exemptions: Nil (iii) Equivalent Level of Safety Findings: (1976 Models onwards) FAR §23.1545 and §23.1583(a)(1) Operating Limitations – The use of indicated airspeed instead of calibrated airspeed was accepted provided the approved calibration data presented in the POH is available to the pilot. ASI calibration data must be predicated on flight test. (iv) Airworthiness Limitations: See TCDS Note 4. (3) Aircraft Noise and Engine Emission Standards: Not Applicable Type Acceptance Report TAR 17/21B/26 – Cessna F337 Series Rev.0 : 30 August 2017 6 (4) Certification Compliance Listing: The DGAC type certificate was issued on the basis of the FAA type certificate for the identical type design, so no separate certification process was followed. (5) Flight Manual: AIR No: Reims Model: Cessna P/N: Publication Title: AIR 3433 F 337E D759-13 1970 Skymaster Owner’s Manual AIR 3434 F T337E D760-13 1970 Turbocharged Skymaster OM AIR 3435 F 337F D859-13 1971 Skymaster Owner’s Manual AIR 3436 F 337F D910-13 1972 Skymaster Owner’s Manual AIR 3437 FT 337F D861-13 1971 Turbocharged Skymaster OM AIR 3438 F 337G D1500-13 1973 Skymaster Owner’s Manual AIR 3439 F 337G D1512-13 1974 Skymaster Owner’s Manual AIR 3440 F 337G D1516-13 1975 Skymaster Owner’s Manual AIR 3441 F 337G D1534-13 1976 337G Pilots Operating Handbook AIR 3442 F 337G D1538-13 1977 337G Pilots Operating Handbook AIR 3443 FT 337GP D911-13 1973 Pressurised Skymaster Owners Manual AIR 3444 FT 337GP D1513-13 1974 Pressurised Skymaster Owners Manual AIR 3445 FT 337GP D1517-13 1975 Pressurised Skymaster Owners Manual AIR 3446 FT 337GP D1535-13 1976 T337G Pilots Operating Handbook AIR 3447 FT 337GP D1539-13 1977 T337G Pilots Operating Handbook AIR 3448 F 337H D1554-13 1978 337H Pilots Operating Handbook AIR 3449 FT 337HP D1556-13 1978 P337H Pilot’s Operating Handbook (6) Operating Data for Aircraft: (i) Maintenance Manual: Cessna 337 (1965-1973) Service Manual – Publication D2500-13 Cessna 337/T337 (1974-1980) Service Manual – Publication D2506-13 Cessna P337 (1973-1980) Service Manual – Publication D2516-13 (ii) Current service Information: Service Bulletins (iii) Illustrated Parts Catalogue: Cessna 337/T337 (1965-1969) Parts Catalog – Publication P443-12 Cessna 337/T337 (1970-1972) Parts Catalog – Publication P492-12 Cessna 337 (1973-1980) Parts Catalog – Publication P607-12 (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 some older manuals at http://techpubs.cessna.com/ Type Acceptance Report Rev.0 : 30 August 2017 TAR 17/21B/26 – Cessna F337 Series 7 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. Civil Aviation Rules 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 Civil Aviation Rules 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(d) 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 fitted FAR §23.1305(c) FAR §23.1305(h) FAR §23.1305(f) FAR §23.699(a)(2) FAR §23.729(e) FAR §23.1351 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: Operational requirement – Compliance as applicable 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 Civil Aviation Rules Part 135 Subpart F – Instrument and Equipment Requirements PARA: REQUIREMENT: MEANS OF COMPLIANCE: 135.355 Seating and 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 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 that date and should be checked individually. Type Acceptance Report TAR 17/21B/26 – Cessna F337 Series Rev.0 : 30 August 2017 8 Attachments The following documents form attachments to this report: Three-view drawing Reims Cessna Model F337 Copy of FAA Type Certificate Data Sheet Number A23EU Copy of FAA STC and Addendum SA11EU 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: F337 Series Twenty Twenty Four Limited 17/21B/26 30 August 2017