Type Acceptance Report

Transcription

1 TAR 98/01 Revision 3 Cessna 206 Series Aircraft Certification Unit

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3 TABLE OF CONTENTS EXECUTIVE SUMMARY 1 1. INTRODUCTION 1 2. ICAO TYPE CERTIFICATE DETAILS 1 3. TYPE ACCEPTANCE CERTIFICATE 3 4. TYPE DATA 3 5. ADDITIONAL NEW ZEALAND REQUIREMENTS 8 ATTACHMENTS 9 APPENDIX 1 9 i TAR 98/01 Cessna 206 Series

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5 Executive Summary New Zealand Type Acceptance has been granted to the Cessna Model 206 Series based on validation of FAA Type Certificate A4CE. There are no special requirements for import. Applicability is currently limited to the Models and/or serial numbers detailed in Appendix 1, which are now eligible for the issue of an Airworthiness Certificate in the Standard Category in accordance with NZCAR , 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.) Additional variants or serial numbers approved under the foreign type certificate can become type accepted after supply of the applicable documentation, in accordance with the provisions of NZCAR 21.43(b). 1. Introduction This report details the basis on which Type Acceptance Certificate No. 98/01 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 also notes the status of all models included under the foreign type certificate which have been granted type acceptance in New Zealand. Models covered by the type acceptance certificate issued under Part 21B are listed in Section 2 of this report. Models which were accepted prior to that under NZCAR Section B.9 are listed in Appendix ICAO Type Certificate Details Manufacturer: Type Certificate: Issued by: Model: MCTOW: Noise Standard: Engine: Cessna Aircraft Company A4CE Federal Aviation Administration TU206C, TU206F 3600 lb. (1633 kg) Not applicable Continental TSIO-520-C Type Certificate: E8CE 1 TAR 98/01 Cessna 206 Series

6 Propeller: McCauley D2A34C78/90AT-8 or E2A34C70/90AT-8 Type Certificate: P3EA McCauley D3A32C79/82NK-2 or D3A32C90/82NC-2 or D3A32C88/82NC-2 Type Certificate: P21EA Model: MCTOW: TU206G 3600 lb. (1633 kg) Max. No. of Seats: 6 Noise Standard: Engine: Propeller: Model(s): MCTOW: FAR 36 including Amendments 1 through 6 (1978 Model up) Continental TSIO-520-M Type Certificate: E8CE McCauley D3A34C402/90DFA-10 Type Certificate: P47GL 206H, T206H 3600 lb. (1633 kg) Max. No. of Seats: 6 Noise Standard: FAR 36 at Amendment Engine: Lycoming IO-540-AC1A5 (206H) Type Certificate: 1E4 Lycoming TIO-540-AJ1A (T206H) Type Certificate: E14EA Propeller: McCauley B3D36C432/80VSA-1 Type Certificate: P58GL TAR 98/01 Cessna 206 Series 2

7 3. Type Acceptance Certificate The application for type acceptance of the Cessna T/206H was from the manufacturer by CAA Form 24021/02 dated 8 th July The 206H was originally certificated with the IO-580-A1A engine. However after a failure of the engine during a 500-hour endurance test Cessna decided to revert to the previous IO-540 engine. Type acceptance was then placed on hold while the engine change was embodied and the models re-certificated. The Cessna 206 is a six-seat high-wing all-metal single-piston-engine utility aircraft. Type Acceptance Certificate No.98/01 covering the Cessna Models 206H and T206H was granted on 12 May 1999, based on validation of FAA Type Certificate A4CE. There are no special requirements for import into New Zealand. This report was raised to Revision 1 under CAA Work Request 4/21B/24 to include the new NAV III avionics option (Garmin G1000 EFIS installation), which requires a new Flight Manual. The opportunity was also taken to re-issue the report in the latest format, and to include all 206 models previously type accepted under the foreign type certificate and covered in individual reports. The application was from Cessna dated 2 March 2004 and type acceptance was granted on 15 November The application for type acceptance of the TU206F was from the owner dated 4 th February The first-of-type example was a 1974 model serial no. U , registered as ZK-OAY. Type Acceptance Certificate No.99/27 was granted on 26 February The application for type acceptance of the TU206G was from Mr Keith Hubber dated 6th May This covers the addition of the 1978 TU206G with the serial number range U through U Type Acceptance was granted on 27th May The report was raised to Revision 2 to include the T/206H Models which under Block Point Change 2007 have replaced the KAP140 autopilot with the Garmin GFC 700 AFCS and use a different Flight Manual. Type acceptance was granted on 26 th October This report was raised to Revision 3 to include the TU206C model. The first-of-type example was serial number U registered ZK-JAO. The Cessna 206 was developed from the Model 205 by installation of the IO-520 engine and other detail changes. The T/U206F is a modification of the 206E with emphasis on improved low speed flight performance. The 207 wing structure and strut ends were used with the aerofoil section changed to provide an under-cambered leading edge shape. Structural alterations include use of bonded skin on the new wing leading edge and aft extension of the baggage shelf. The T/U206G was very similar to the F model, except the turbocharged Continental TSIO-520-M engine was re-rated for takeoff (5 min.) to 310 hp. The 206H, production of which was re-started in 1998, is similar to the previous G model. The main difference is the use of the Lycoming IO-540 Series engine. Larger seat rails are used and there is an all-new interior with modernised instrumentation and avionics. 3 TAR 98/01 Cessna 206 Series

8 4. Type Data The type data requirements of NZCAR Part 21B Para have been satisfied by supply of the following documents: (1) Type certificate: FAA Type Certificate Number A4CE issued July 19, 1963 FAA TCDS No. A4CE at Revision 47 dated February 25, 2009 Model TU206C approved July 20, 1967 Model TU206F approved October 26, 1971 Model TU206G approved June 21, 1976 Model 206H approved November 26, 1997 Models T206H approved October 1, 1998 Engine: FAA TC No.1E4 - Model IO-540-AC1A5 Approved May 27, 1998 FAA TCDS No.1E4 at Revision 17 dated August 1, 1998 TC No.E14EA - Model TIO-540-AJ1A Approved April 30, 1998 FAA TCDS No.E14EA at Revision 15 dated May 18, 1998 Propeller: FAA TC No. P58GL Model B3D36C Approved June 30, 1988 FAA TCDS No.P58GL at Revision 10 dated March 23, 1998 (2) Airworthiness design requirements: (i) Airworthiness Design Standards: The certification basis of the Cessna 206 Series up to the Model 206G is Part 3 of the Civil Air Regulations effective May 15, 1956, as amended by 3-1 through 3-8. For the Model 206H this was updated to FAR Part 23 effective February 1, 1965, including Amendments 23-1 through 23-6, plus later amendment dates for individual paragraphs as detailed on the TCDS. (As was done for the earlier restart singles.) For aircraft with the Garmin G1000 Integrated Cockpit System (ICS) the certification basis was further updated for specific paragraphs, again as detailed on the TCDS, and Special Condition No SC was applied for Protection from HIRF. Some further additions were made for aircraft fitted with the GFC-700, again as detailed on the TCDS. 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, and CAR 3 is an acceptable alternative as noted in Advisory Circular There are no non-compliances and no additional special conditions have been prescribed by the Director under (ii) Special Conditions: SC Cessna Aircraft Company; EFIS on the Cessna 206H and T206H; Protection of Systems for High Intensity Radiated Fields (HIRF). (iii) Equivalent Level of Safety Findings: Two Equivalent Safety Item findings were made for the 1976 T/U206F and up, as follows: CAR Airspeed Indicator; CAR 3.778(a) 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. TAR 98/01 Cessna 206 Series 4

9 Four Equivalent Safety Item findings were made for the T/206H, as follows: Throttle and Mixture Controls FAR (g) and (b) at Amendment 43 specifies that attachments must be designed so that the flight can continue and land if the controls separate, to account for poor reliability. (Usually a spring device is used.) The same criteria as accepted for the 172R were used: compensating elements included engine control attachment features, which are not likely to separate in flight; establishment of mandatory inspection intervals; and replacement criteria. ACE Fuel Tank Sump For fuel system changes in ECR (introduced under Blockpoint 2002) Cessna proposed substantiation similar to that used for the 182T. Instead of fixed specified capacities the means of compliance involved tank fluid retention measurements and an evaluation of sump and strainer size to ensure water could not be introduced into the system if Flight Manual procedures were followed. The FAA requested an ELOS for transparency. ACE (d) Anti-collision Lights An ELOS was granted for the use of white strobe lights which meet all the requirements of the rule except for colour. The strobe light has been previously accepted under STC and PMA, and later amendments of the Rule allow red or white. (iv) Airworthiness Limitations: See the Aircraft Maintenance Manual. (3) Environmental Certification: Cessna Structural Dynamics Report D-206H H Take Off Noise Structural Dynamics Rpt D-T206H-31 Model T206H Take Off Noise (4) Certification Compliance Listing: Cessna Delegation Option Manufacturer Flight Test Report DM-TP/U206C-0 Certification of the 1968 Model Changes by Rational Analysis June 21, 1967 Cessna Report DM TU206F-0 Certification of Model TU206F 20 September 1971 DM-TU206F-0 ADD. #4 Certification of the 1974 Model Changes Aug 8, 1973 Cessna Report S-206F-35(72) Fatigue Analysis T/U206F 11 September 1971 Cessna Report S-206F-33(72) Substantiation, Critical Loads and Structural Materials Summary Model U206F 26 August 1971 Loading and Centre of Gravity Charts/Equipment List U206F/TU206F (1974) DM-TU206G-0 ADD.#1 Rational Analysis Certification of 1978 Model TU206G Cessna Airworthiness Report No Master Compliance Checklist Model 206H Stationair Superseded by: Cessna Airworthiness Report No Master Compliance Checklist Model 206H Stationair with IO-540 Engine Cessna Airworthiness Report No. T Master Compliance Checklist T206H Turbo Stationair Superseded by: Cessna Airworthiness Report No. T Master Compliance Checklist T206H Turbo Stationair with TIO-540 Engine Cessna Airworthiness Report No Master Compliance Checklist Nav III (G1000 EFIS) Model 206H/T206H Stationair dated 30 June 2004 DOA Manufacturer Flight Test Rpt. DMT206H-29 Addendum No Approval of the Garmin G1000 Integrated Cockpit System in the Model T206H 5 TAR 98/01 Cessna 206 Series

10 DOA Manufacturer Flight Test Report DM206H-29 Addendum No Approval of the Garmin G1000 Integrated Cockpit System in the Model 206H Certification Plan CP Model 206H/T206H Garmin GFC-700 AFCS Propeller: Compliance Check Sheet Report B2D34C432/80VSA Statement of Compliance TC No.P58GL dated 16/5/97 Statement of Compliance PC No.P3 dated 16/5/97 FAA Addition of B2D34C432/80VS FAA dated 16/5/97 (Vibration Approval 206H) FAA dated 16/5/97 (Vibration Approval T206H) dated 8/4/98 (Vibration Approval 206H/IO-540) dated 8/4/98 (Vibration Approval T206H/TIO-540) (5) Flight Manual: 1978 Model TU206G Turbo Stationair 6 Pilot s Operating Handbook Part Number D CAA Accepted as AIR 2586 Model 206H POH and FAA Approved AFM P/N 206HPHUS00 dated 5 October 1998 CAA Accepted as AIR Turbo Stationair Owner s Manual Part Number D CAA Accepted as AIR Turbo Stationair Owner s Manual Part Number D CAA Accepted as AIR Turbo Stationair Owner s Manual Part Number D CAA Accepted as AIR Turbo Stationair Owner s Manual Part Number D CAA Accepted as AIR Turbo Stationair Pilot's Operating Handbook Part Number D CAA Accepted as AIR 2657 Model T206H POH and FAA Approved AFM P/N T206HPHUS00 dated 9 November 1998 CAA Accepted as AIR 2664 Model 206H Nav III Avionics Option POH and FAA Approved AFM P/N 206HPHAUS00 dated 4 Oct CAA Accepted as AIR 2880 Model T206H Nav III Avionics Option POH and FAA Approved AFM P/N T206HPHAUS00 dated 3 Sep CAA Accepted as AIR 2879 POH and FAA Approved Airplane Flight Manual 206H NAV III Avionics Option GFC 700 AFCS Serials and and On Part No.206HPHBUS CAA Accepted as AIR 3017 TAR 98/01 Cessna 206 Series 6

11 POH and FAA Approved Airplane Flight Manual T206H NAV III Avionics Option GFC 700 AFCS Serials T and T and On Part No.T206HPHBUS CAA Accepted as AIR Turbo-System Super Skywagon Owner s Manual Part Number D CAA Accepted as AIR 3105 (6) Operating Data for Aircraft, Engine and Propeller: (i) Maintenance Manual: Cessna 200 Series Maintenance Manual Part Number D470-13AF Cessna 200 Series Maintenance Manual Part Number D606-13AF Model U/206/P206 Maintenance Manual Part Number D AF 206H/T206H Series 1998 and on Maint. Manual 206HMM01AF 3 Aug 1998 Model 206H/T206H Wiring Diagram Manual 206HWD01AF 26 Oct 1998 IO-580-A1A Wide Cylinder Flange Crankcase Parts Catalog PC--10 IO-580 and TIO-580 Operator s Manual P/N rd Ed. Revised up to Jan 1997 Overhaul Manual Revisions supplied as part of 172R Type Acceptance Service Manual for McCauley C400 Constant Speed Propellers Parts List PL-7352 for E-7345-B Propeller Model B3D34C432-X/H-80VSA-X Drawing E-7345 Propeller Assembly - 3 Blade Constant - Oil Filled Drawing D-7463 Hub Assembly - 3 Blade Constant Speed - Oil Filled MPC-11 Operator s Manual for C200 (2 blade) and C400 (3 Blade) CS Props -Sept 81 (ii) Current service Information: McCauley Service Bulletins 137K, 154E, 172B, 176C, 177B, 192A McCauley Service Letters through (iii) Illustrated Parts Catalogue: Model P206/U206 series Parts Catalog Part Number P516-12AF Model 206 and T206 series Parts Catalog P664-12AF Model 206H/T206H 206HPC01AF 3 Aug 1998 (7) Agreement from manufacturer to supply updates of data in (5) and (6): Cessna now provides CAA access to their website for all additional manuals and revisions. McCauley letter dated August 15, 1997 stated updates to all submitted data would automatically be provided at no cost. (8) Other information: Cessna Letters with Overview of Model Changes Models 206H and T206H: Reference L , and Reference L Cessna Letter Reference L Block Point Change 2007 (BP2007) 7 TAR 98/01 Cessna 206 Series

12 5. Additional New Zealand Requirements Compliance with the retrospective airworthiness requirements of NZCAR Part 26 is a prerequisite for the grant of a type acceptance 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 - Agricultural Aircraft CAM 8 Appendix B Section.35 Not Applicable Compliance with the following additional NZ operating requirements has been reviewed for the Model T/206H and were found to be covered by either the original certification requirements or the basic build standard of the aircraft, except as noted: Civil Aviation Rules Part 91 Subpart F - Instrument and Equipment Requirements PARA: REQUIREMENT: MEANS OF COMPLIANCE: Shoulder Harness if Aerobatic; >10 pax; Flight Training Integrated seat belt/shoulder harness fitted - POH page Pax Information Signs - Smoking, safety belts fastened N/A - Less than 10 passenger seats Min. VFR (1) ASI (8) Coolant Temp (9) Oil Temperature (2) Machmeter (3) Altimeter (4) Magnetic Compass (5) Fuel Contents (6) Engine RPM (7) Oil Pressure FAR (a) Fitted as Std See POH Fig.7-2 Item 7 N/A FAR (b) Fitted as Std See POH Fig.7-2 Item 12 FAR (c) Fitted as Std FAR (a) Fitted as Std See POH Fig.7-2 Item 2 FAR (d) Fitted as Std See POH Fig.7-2 Item 10 FAR (b) Fitted as Std See POH Fig.7-2 Item 1 (10) Manifold Pressure (11) Cylinder Head Temp. (12) Flap Position (13) U/c Position (14) Ammeter/Voltmeter N/A Air cooled engine fitted FAR (c) Fitted as Std See POH Fig.7-2 Item 1 FAR (h) Fitted as Std See POH Fig.7-2 Item 36 FAR (f) Fitted as Std See POH Fig.7-2 Item 5 See POH Fig.7-2 Item 28 N/A Fixed Undercarriage FAR Fitted as Std See POH Fig.7-2 Item Night (1)Turn and Slip (2) Position Lights See POH Fig.7-2 Item 6 Standard - See POH page 7-43 (3) Anti-collision Lights (4) Instrument Lighting Standard - See POH page 7-43 Standard - See POH page VFR Communication Equipment Standard Avionics includes Dual KX-155 TSO Radios IFR (1) Gyroscopic AH (2) Gyroscopic DI (3) Gyro Power Supply (4) Sensitive Altimeter Standard - See POH page 7-49 Standard - See POH page 7-49 Standard - See POH page 7-51 Standard - See POH page 7-49 (5) OAT (6) Time in hr/min/sec (7) ASI/Heated Pitot (8) Rate of Climb/Descent See POH Fig.7-2 Item 4 See POH Fig.7-2 Item 4 Standard - See POH page 7-47 See POH Fig.7-2 Item IFR Communication and Navigation Equipment KX-155 TSO Nav/Comm plus KLN89 GPS fitted as std The G1000S has 2 GIA 63 Integrated Avionics Units, which contain a GPS receiver, VHF Nav and Comm receivers Emrgcy Eqpmt. (a) More Than 10 pax - First Aid Kits per Table 7 - Fire Extinguishers per Table 8 (b) More than 20 pax - Axe readily acceptable 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 ELT - TSO C91a after 1/4/97 (or replacement) Pointer fitted as standard POH Page 7-55/Supp Oxygen Indicators - Volume/Pressure/Delivery Operational requirement compliance as applicable Unpress. A/c >30 min above FL100 - Supplemental for crew, 10% Pax - Therapeutic for 3% of Pax Above FL100 - Supplemental for all Crew, Passengers - Therapeutic for 1% of Pax - 120l PBE for each crew member The T206H has a six-place oxygen system supplied from a 76 cu. ft. cylinder. Pressure is indicated by a gauge in the overhead console. A permanent microphone-equipped mask is provided for the pilot and five partial-breathing disposable masks for the pax, with vinyl hoses and flow indicators SSR Transponder and Altitude Reporting Equipment KT-76C TSO Transponder fitted as Standard GTX-33 Mode S Transponder Standard with NAV III Altitude Alerting Device - Turbojet or Turbofan Not Applicable reciprocating engine Assigned Altitude Indicator Operational requirement compliance as applicable A.15 ELT Installation Requirements To be determined on an individual aircraft basis NOTE: Page and Figure references are based on the Model 206H Pilot s Operating Handbook 206HPHUS. TAR 98/01 Cessna 206 Series 8

13 Civil Aviation Rules Part 135 Subpart F - Instrument and Equipment Requirements PARA: REQUIREMENT: MEANS OF COMPLIANCE: Seating and Restraints Shoulder harness for flight-crew seats FAR Additional Instruments (Powerplant and Propeller) FAR 23 is a Part 21 Appendix C design standard Night Flight Landing light, Pax compartment Operational requirement compliance as applicable IFR Operations Speed, Alt, spare bulbs/fuses Operational requirement compliance as applicable Emergency Equipment (Part (a) and (b)) Operational requirement compliance as applicable Cockpit Voice Recorder Not Applicable Helicopters only Flight Data Recorder Not Applicable Helicopters only Additional Attitude Indicator Not Applicable Not turbo jet or turbofan powered Attachments The following documents form attachments to this report: Three-view drawing Cessna Model T206H Turbo Stationair Copy of FAA Type Certificate Data Sheet No. 4ACE Sign off.. David Gill Team Leader Airworthiness... Checked Dave Selby Airworthiness Engineer Appendix 1 List of Type Accepted Variants: Model: Applicant: CAA Work Request: Date Granted: 206, P206, U206A, TU206A AC /NZCAR Part 21 Appendix A(c) U206B, U206C, U206D, P206E AC /NZCAR Part 21 Appendix A(c) U206F, U206G, TU206G AC /NZCAR Part 21 Appendix A(c) TU206G (1978) Invercargill Holdings Ltd 97/21B/18 27 May H/T206H Cessna Aircraft Company 98/21B/1 12 May 1999 TU206F M S Delport 99/21B/27 1 March /T206H Nav III Cessna Aircraft Company 4/21B/24 15 November 2004 T/206H NAV III/GFC700 Cessna Aircraft Company 8/21B/6 26 October 2007 TU206C Hawker Pacific NZ Ltd 10/21B/7 6 November TAR 98/01 Cessna 206 Series