Cessna 206 Series | Type Acceptance Report - CAA

registered ZK-OAY. Type Acceptance was granted on 26 February 1999. The application for type acceptance of the 1978 Model TU206G was from Mr Keith Hubber dated 6 May 1997. The first-of-type example was serial number U206-04075, registered ZK-KMH. Type Acceptance was granted on 27 May 1997. Revision 2 was issued to add 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 October 2007. This report was raised to Revision 3 to include the TU206C model. The first-of-type example was serial number U206-1218 registered ZK-JAO. Type Acceptance was granted on 6 November 2009. Revision 4 to this report added all the other variants and model years of the Model 206 Series not previously included. This was at the request of the type certificate holder, who has provided access to all technical publications. The Cessna 206 was developed from the Model 205 by installation of the more powerful IO-520 engine and a larger tail, with various changes to the flaps and ailerons. A 42 inch double door was fitted on the right rear cabin to facilitate loading of cargo. The P206 Model was a “personal” version without the double doors and a more luxurious interior. Turbocharged engines and an increase in gross weight to 3600 lb were introduced in 1966. 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 and a cambered leading edge was adopted. 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 Type Acceptance Report Rev.4 : 25 January 2019 TAR 98/01 – Cessna 206 Series 5 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. Type Acceptance Report TAR 98/01 – Cessna 206 Series Rev.4 : 25 January 2019 6 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: (1) State-of-Design type certificate: FAA Type Certificate Number A4CE issued July 19, 1963 FAA Type Certificate Data Sheet No. A4CE at Revision 47 dated July 29, 2015 – Model 206 approved July 19, 1963 – Models U206 and P206 approved October 8, 1964 – Models U206A and P206A approved September 24, 1965 – Models TU206A and TP206A approved December 20, 1965 – Models U206B, TU206B, P206B, and TP206B approved August 3, 1966 – Models U206C, P206C, TU206C and TP206C approved July 20, 1967 – Models U206D, P206D, TU206D and TP206D approved Sept. 18, 1968 – Models U206E, P206E, TU206E and TP206E approved July 28, 1969 – Models U206F and TU206F approved October 26, 1971 – Models U206G and 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, plus FAR §23.1559 effective March 1, 1978 for the 1979 U206G on, and FAR §23.1545 effective December 1, 1978 for the 1985 U206G on. 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 re- start models.) For 206H 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.23-150-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 CAR 3 is the predecessor of FAR Part 23, which is the basic standard for Normal Category Airplanes called up under Part 21 Appendix C. Type Acceptance Report Rev.4 : 25 January 2019 TAR 98/01 – Cessna 206 Series 7 There are no non-compliances and no additional special conditions have been prescribed by the Director under §21.23. (ii) Special Conditions: 23-150-SC Cessna Aircraft Company; EFIS on the Cessna 206H and T206H; Protection of Systems for High Intensity Radiated Fields (HIRF) – Defines the HIRF environment for which no adverse effect on critical function performance must be demonstrated. This may be by test, analysis, models or similarity, or any combination of these. (iii) Equivalent Level of Safety Findings: 1976 T/U206F and up: CAR 3.757 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. T/206H: Throttle and Mixture Controls – FAR §23.1143(g) and §23.1147(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-02-03 §23.971 Fuel Tank Sump – For fuel system changes in ECR 046069 (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-02-02 §23.1401(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) Aircraft Noise and Engine Emission Standards: (i) Environmental Standard: The Models U206G and TU206G have been certificated for noise under FAR Part 36, including Amendments 36-1 through 36-6. For the 206H and T206H this was updated to Amendment 36-21. (ii) Compliance Listing: See Advisory Circular 36-1H Appendix 7 and Flight Manuals (Section 4). Model: MTOW: Engine: Propeller: RPM: Noise Levels MdbA CdbA U206G 3600 IO-520-F D3A34C404 2700 77.9 77.5 TU206G 3600 TSIO-520-M D3A34C402 2600 78.5 75.4 Cessna Structural Dynamics Report D-206H-31 – 206H Take Off Noise Structural Dynamics Report D-T206H-31 – Model T206H Take Off Noise Type Acceptance Report TAR 98/01 – Cessna 206 Series Rev.4 : 25 January 2019 8 Cessna 206H – certificated noise level at 3600 lb is 79.7 dB(A) with 2-bladed propeller and 77.7 dB(A) with 3-bladed propeller – See AFM Section 4 Cessna T206H – certificated noise level at 3600 lb is 77.7 dB(A) per FAR Part 36 Appendix G, or 81.1 dB(A) per ICAO Annex 16 Chapter 10 – See AFM Section 4 (4) Certification Compliance Listing: Cessna Report S-206A-0: Basic Data (Model 206A) Cessna Report S-206A-33: Structures Substantiation Summary (Model 206A) Cessna Report S-U206-31: Equipment Weight Report (Model U206) Cessna Report SP206-0: Basic Data (Model P206) 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 1978 Model TU206G Cessna Airworthiness Report No. 206-96-001 – 26.6.97 Master Compliance Checklist – Model 206H Stationair – Superseded by: Cessna Airworthiness Report No. 206-98-001 – 26.6.98 Master Compliance Checklist – Model 206H Stationair with IO-540 Engine Cessna Airworthiness Report No. T206-96-001 – 26.6.97 Master Compliance Checklist – T206H Turbo Stationair – Superseded by: Cessna Airworthiness Report No. T206-96-001 – 26.6.97 Master Compliance Checklist – T206H Turbo Stationair with TIO-540 Engine Cessna Airworthiness Report No. 206-04-001 – Master Compliance Checklist Nav III (G1000 EFIS) Model 206H/T206H Stationair – dated 30 June 2004 DOA Manufacturer Flight Test Rpt. DMT206H-29 Addendum No.1 – 30-7-04 Approval of the Garmin G1000 Integrated Cockpit System in the Model T206H DOA Manufacturer Flight Test Report DM206H-29 Addendum No.1 – 29-9-04 Approval of the Garmin G1000 Integrated Cockpit System in the Model 206H Certification Plan CP-058070 – 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 8110-12 - Addition of B2D34C432/80VS FAA 8110-3 dated 16/5/97 (Vibration Approval 206H) FAA 8110-3 dated 16/5/97 (Vibration Approval T206H) 8110-3 dated 8/4/98 (Vibration Approval 206H/IO-540) 8110-3 dated 8/4/98 (Vibration Approval T206H/TIO-540) Type Acceptance Report Rev.4 : 25 January 2019 TAR 98/01 – Cessna 206 Series 9 (5) Flight Manual: CAA AIR Cessna Number: Publication: Title: AIR 2777 D207-13 Model 206 (1965) Owner's Manual AIR 3033 D283-13 Model P206 (1965) Owner's Manual AIR 3714 D366-13 Model P206A (1966) Owner's Manual AIR 3715 D440-13 Model P206B (1967) Owner's Manual AIR 3716 D549-13 Model P206C (1968) Owner's Manual AIR 3717 D664-13 Model P206D (1969) Owner's Manual AIR 2241 D755-13 Model P206E (1970) Owner's Manual AIR 3718 D370-13 Model TP206A (1966) Owner's Manual AIR 3719 D441-13 Model TP206B (1967) Owner's Manual AIR 3720 D550-13 Model TP206C (1968) Owner's Manual AIR 3721 D665-13 Model TP206D (1969) Owner's Manual AIR 3722 D756-13 Model TP206E (1970) Owner's Manual AIR 2564 D266-13 Model U206 (1965) Owner's Manual AIR 2887 D347-13 Model U206A (1966) Owner's Manual AIR 2017 D417-13 Model U206B (1967) Owner's Manual AIR 2720 D523-13 Model U206C (1968) Owner's Manual AIR 2721 D685-13 Model U206D (1969) Owner's Manual AIR 2722 D766-13 Model U206E (1970) Owner's Manual AIR 2723 D876-13 Model U206E (1971) Owner's Manual AIR 2724 D916-13 Model U206F (1972) Owner's Manual AIR 2725 D1004-13 Model U206F (1973) Owner's Manual AIR 2726 D1024-13 Model U206F (1974) Owner's Manual AIR 2727 D1044-13 Model U206F (1975) Owner's Manual AIR 2728 D1065-13 Model U206F (1976) Pilot's Operating Handbook AIR 2729 D1090-13 Model U206G (1977) Pilot's Operating Handbook AIR 2730 D1118-13 Model U206G (1978) Pilot's Operating Handbook AIR 2731 D1147-13PH Model U206G (1979) Pilot's Operating Handbook AIR 2124 D1182-13PH Model U206G (1980) Pilot's Operating Handbook AIR 2204 D1203-13PH Model U206G (1981) Pilot's Operating Handbook AIR 2186 D1222-13PH Model U206G (1982) Pilot's Operating Handbook AIR 3723 D1240-13PH Model U206G (1983) Pilot's Operating Handbook AIR 3724 D1261-13PH Model U206G (1984) Pilot's Operating Handbook AIR 3725 D1282-13PH Model U206G (1985) Pilot's Operating Handbook AIR 3726 D1302-13PH Model U206G (1986) Pilot's Operating Handbook AIR 2114 D371-13 Model TU206A (1966) Owner's Manual AIR 3727 D418-13 Model TU206B (1967) Owner's Manual AIR 3105 D524-13 Model TU206C (1968) Owner's Manual AIR 3728 D686-13 Model TU206D (1969) Owner's Manual AIR 3729 D767-13 Model TU206E (1970) Owner's Manual AIR 3730 D877-13 Model TU206E (1971) Owner's Manual AIR 2654 D917-13 Model TU206F (1972) Owner's Manual Type Acceptance Report TAR 98/01 – Cessna 206 Series Rev.4 : 25 January 2019 10 AIR 2655 D1005-13 Model TU206F (1973) Owner's Manual AIR 2651 D1025-13 Model TU206F (1974) Owner's Manual AIR 2656 D1045-13 Model TU206F (1975) Owner's Manual AIR 2657 D1066-13 Model TU206F (1976) Pilot's Operating Handbook AIR 2585 D1091-13 Model TU206G (1977) Pilot's Operating Handbook AIR 2586 D1119-13 Model TU206G (1978) Pilot's Operating Handbook AIR 3731 D1148-13PH Model TU206G (1979) Pilot's Operating Handbook AIR 3732 D1183-13PH Model TU206G (1980) Pilot's Operating Handbook AIR 3733 D1204-13PH Model TU206G (1981) Pilot's Operating Handbook AIR 3734 D1223-13PH Model TU206G (1982) Pilot's Operating Handbook AIR 3735 D1241-13PH Model TU206G (1983) Pilot's Operating Handbook AIR 3736 D1262-13PH Model TU206G (1984) Pilot's Operating Handbook AIR 3737 D1283-13PH Model TU206G (1985) Pilot's Operating Handbook AIR 3738 D1303-13PH Model TU206G (1986) Pilot's Operating Handbook Model 206H POH and FAA Approved AFM – Part No. 206HPHUS00 dated 5 October 1998 – CAA Accepted as AIR 2649 Model T206H POH and FAA Approved AFM – Part No. T206HPHUS00 dated 9 November 1998 – CAA Accepted as AIR 2664 Model 206H NAV III Avionics Option POH and FAA Approved AFM Part No. 206HPHAUS00 dated 4 Oct. 2004 – CAA Accepted as AIR 2880 Model T206H NAV III Avionics Option POH and FAA Approved AFM Part No. T206HPHAUS00 dated 3 Sep. 2004 – CAA Accepted as AIR 2879 POH and FAA Approved Airplane Flight Manual 206H NAV III Avionics Option – GFC 700 AFCS – Serials 20608279 and 20608284 and On – Part No. 206HPHBUS – CAA Accepted as AIR 3017 POH and FAA Approved Airplane Flight Manual T206H NAV III Avionics Option – GFC 700 AFCS – Serials T20608682 and T20608705 and On – Part No. T206HPHBUS – CAA Accepted as AIR 3018 (6) Operating Data for Aircraft, Engine and Propeller: (i) Maintenance Manual: Cessna 200 Series (1960-65) Service Manual – Publication D470-13 Cessna 200 Series (1966-68) Service Manual – Publication D606-13 Cessna U/206/P206 (1969-76) Service Manual – Publication D2007-13 Cessna U206 Series (1977-86) Service Manual – Publication D2070-13 Cessna 206H/T206H Series 1998 and on – Maint. Manual – 206HMM Cessna 206H/T206H Wiring Diagram Manual – 206HWD IO-580-A1A Wide Cylinder Flange Crankcase Parts Catalog PC--10 IO-580 and TIO-580 Operator’s Manual P/N 60297-10 3rd Edition Overhaul Manual Revisions supplied as part of 172R Type Acceptance Type Acceptance Report Rev.4 : 25 January 2019 TAR 98/01 – Cessna 206 Series 11 Service Manual 761001 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 (ii) Current service Information: McCauley Service Bulletins 137K, 154E, 172B, 176C, 177B, 192A McCauley Service Letters 1973-9 through 1996-11 (iii) Illustrated Parts Catalogue: Cessna P206/U206 Series (1964-1973) Parts Catalog – Publication P516-12 Cessna 206 and T206 Series (1974-1984) Parts Catalog – P664-12 Cessna 206H/T206H Parts Catalog – 206HPC (7) Agreement from manufacturer to supply updates of data in (5) and (6): Textron Aviation Publications are now available through the Textron Aviation Technical Publications website at https://ww2.txtav.com 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 L417-02-97-206, and Reference L417-02-97-282 Cessna Letter Reference L390-06-3010 – Block Point Change 2007 (BP2007) Type Acceptance Report TAR 98/01 – Cessna 206 Series Rev.4 : 25 January 2019 12 5. New Zealand Operational Rule Compliance 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: 91.505 Shoulder Harness if Aerobatic; >10 pax; Flight Training Integrated seat belt/shoulder harness Std – POH page 7-16 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) Fitted as Std - See POH Fig.7-2 Item 7 N/A – No mach limitations FAR §23.1303(b) Fitted as Std - See POH Fig.7-2 Item 12 FAR §23.1303(c) Std Fit FAR §23.1305(a) Fitted as Std See POH Fig.7-2 Item 2 FAR §23.1305(d) Fitted as Std See POH Fig.7-2 Item 10 FAR §23.1305(b) Fitted as Std See POH Fig.7-2 Item 1 (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) Fitted as Std – See POH Fig.7-2 Item 1 FAR §23.1305(h) Fitted as Std – POH Fig.7-2 Item 36 FAR §23.1305(f) Fitted as Std See POH Fig.7-2 Item 5 See POH Fig.7-2 Item 28 N/A – Fixed Undercarriage FAR §23.1351 Fitted as Std See POH Fig.7-2 Item 3 91.511 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 – POH page 7-43 Standard – POH page 7-44 91.513 VFR Communication Equipment Standard Avionics includes Dual KX-155 TSO Radios 91.517 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 – POH page 7-47 See POH Fig.7-2 Item 11 91.519 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. 91.523 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 Not Applicable – Less than 10 passenger seats Not Applicable – Less than 10 passenger seats Not Applicable – Less than 20 passenger seats Not Applicable – Less than 61 passenger seats 91.529 ELT - TSO C91a after 1/4/97 (or replacement) Pointer 3000-11 fitted as Std – POH Page 7-55/Supp.4 91.531 Oxygen Indicators - Volume/Pressure/Delivery Operational requirement – compliance as applicable 91.533 Unpress A/c >30 min above FL100 – Supplemental 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 6-place oxygen system supplied from a 76 cu. ft. cylinder. Pressure is indicated by a gauge in the overhead console. A microphone-equipped mask is provided for the pilot and 5 partial-breathing disposable masks for the pax, with vinyl hoses and flow indicators. 91.541 SSR Transponder and Altitude Reporting Equipment KT-76C TSO Transponder fitted as Standard GTX-33 Mode S Transponder Standard with NAV III 91.543 Altitude Alerting Device – Turbojet or Turbofan Not Applicable – reciprocating engine 91.545 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. Type Acceptance Report Rev.4 : 25 January 2019 TAR 98/01 – Cessna 206 Series 13 Civil Aviation Rules 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 is a Part 21 Appendix C design standard 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 Not Applicable – Less than 10 passenger seats 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 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: Three-view drawing Cessna Model T206H Turbo Stationair Copy of FAA Type Certificate Data Sheet No. 4ACE Sign off …………………………………….. ……………………………............... David Gill Checked – Jason Ashworth Team Leader Airworthiness Team Leader Product Certification Type Acceptance Report TAR 98/01 – Cessna 206 Series Rev.4 : 25 January 2019 14 Appendix 1 List of Type Accepted Variants: Model: Applicant: CAA Work Request: Date Granted: 206, P206, U206A, TU206A AC 21-1.2/NZCAR Part 21 Appendix A(c) U206B, U206C, U206D, P206E AC 21-1.2/NZCAR Part 21 Appendix A(c) U206F, U206G, TU206G AC 21-1.2/NZCAR Part 21 Appendix A(c) TU206G (1978) Invercargill Holdings Ltd 97/21B/18 27 May 1997 206H/T206H Cessna Aircraft Company 98/21B/1 12 May 1999 TU206F M S Delport 99/21B/27 1 March 1999 206/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 2009 All other models Textron Aviation Inc 18/21B/14 25 January 2019