Type Acceptance Report TAR 99/11 — Cessna 180 Series

180E based on validation of FAA Type Certificate 5A6. Specific applicability is limited to the coverage provided by the operating documentation supplied. There are no special requirements for import into New Zealand. This report was raised to Revision 1 under CAA Work Request 12/21B/22 to include the 1978 180K model, and the opportunity was also taken to update to the latest format. The application was from Sunair Aviation Ltd dated 25 May 2012. The first-of-type example was ZK-DKP serial number 18052966, and type acceptance was granted on 4 July 2012. This report was raised to Revision 2 to add all the other variants and model years of the 180 Series not previously included in the existing type acceptance. This was at the request of the type certificate holder, who has provided access to all technical publications. The Cessna Model 180 was developed as a high-performance version of the 170 with six- cylinder engine and increased size vertical and horizontal tails. The 1952 prototype was a modified 170B, with a new engine, a rectangular fin with a dorsal fairing, and reshaped side windows. Other changes included improvements to the steering, cowling, optional wheel fairings, and a new wing tip design. The usual Cessna annual Model changes followed. A revised instrument panel was adopted for the 1959 180B. The 180E is the 1961 model 180 with minor changes from the previous 180D. These were mostly cosmetic but included dual-outlet ports in the fuel tanks and optional 84-gallon capacity tanks. The 1964 180G and on used the Model 185 fuselage, wings, landing gear and utility seat to offer 6-place seating with an additional cabin window on each side. The camber-lift wing with bonded leading edges was introduced on the 1973 180J. The 180K, the last production version, is largely similar to preceding models but introduced the O-470-U engine (no power increase) and was the first model certificated against noise requirements. The first example of the Cessna Model 180 in New Zealand was serial number 30537, which was registered ZK-AZZ as one of a batch of six in August 1953. Type Acceptance Report Rev.2 : 12 March 2019 TAR 99/11 — Cessna 180 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: (1) State-of-Design Type certificate: FAA Type Certificate Number 5A6 FAA Type Certificate Data Sheet No. 5A6 at Revision 68 dated Sept. 11, 2015 – Model 180 approved December 23, 1952 – Model 180A approved December 17, 1956 – Model 180B approved August 22, 1958 – Model 180C approved July 8, 1959 – Model 180D approved June 14, 1960 – Model 180E approved September 21, 1961 – Model 180F approved June 25, 1962 – Model 180G approved July 19, 1963 – Model 180H approved June 17, 1964 – Model 180J approved October 13, 1972 – Model 180K approved August 19, 1976 (2) Airworthiness design requirements: (i) Airworthiness Design Standards: The certification basis of the Model 180 Series up to the Model 180B is Part 3 of the Civil Air Regulations dated November 1, 1949, as amended by 3-1 through 3-8, except paragraphs §3.265 and §3.668 of 3-7. For the Models 180C through 180H this was updated to CAR 3 at Amendment 3-12, except again paragraphs §3.265 of 3-7 and §3.668 of 3-3. For the Models 180J and 180K CAR 3 subpart B was at Amendment 3-5. For the 1979 Model 180K and on FAR 23 paragraph §23.1559 effective March 1, 1978 was added. This is an acceptable certification basis in accordance with NZCAR Part 21B Para §21.41 because CAR 3 was the predecessor of FAR 23, which is the basic standard for Normal Category aircraft called up under CAR 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: 1976 180J and 180K: CAR 3.757 Airspeed Indicator; CAR 3.778(a) Operating Limitations – The use of indicated instead of calibrated airspeed was accepted provided the approved calibration data given in the POH is available to the pilot. ASI calibration data must be predicated on flight test. (iv) Airworthiness Limitations: See the Aircraft Maintenance Manual. Type Acceptance Report TAR 99/11 — Cessna 180 Series Rev.2 : 12 March 2019 6 (3) Aircraft Noise and Engine Emission Standards: (i) Environmental Standard: The Model 180K has been certificated for noise under FAR Part 36 including Amendments 36-1 through 36-6. (ii) Compliance Listing: See Advisory Circular 36-1H Appendix 7 and Flight Manual (Section 4). Model: MTOW: Engine: Propeller: RPM: Noise Levels MdbA CdbA 180K 2950 O-470-U C2A34C204 2400 73.0 70.0 (4) Certification Compliance Listing: Cessna Report No. 700 – Type Record for: Model 180 Cessna Report No. 722: Weight & Balance (Models 180, Landplane & Seaplane) Cessna Report No. 723: Flutter Survey Report S-107: Investigation of 3/4" Spring for Australian Agricultural Model 180 Report No. 754: Take-Off, Landing and Level Flight Performance (180 Seaplane) Report 755: Take-Off, Landing and Level Flight Performance (Model 180) Cessna 180B – Type Record Cessna Report No. 702: Type Record – Fuselage Analysis (Cessna 180C) Cessna DM 180D-0: Type Inspection Report Model 180D Report No. S-180E-33: Structures Substantiation Summary (Model 180E) Report No. S-180G-0: Basic Data (Model 180G) Report No: S-180G-33: Structures Substantiation Summary (Model 180G) Cessna Report No: S-180H-33: Structures Substantiation Summary (Model 180H) Report No. S-180J-33: Substantiation, Critical Loads, Structural Materials Summary, Model 180J Report No. DM-180J-0: Certification of the 1975 Model Changes (Model 180J) (5) Flight Manual: CAA AIR Cessna Number: Publication: Title: AIR 3068 P131-13 Model 180 (1953-1954) Owner's Manual AIR 3069 P132-13 Model 180 (1955) Owner's Manual AIR 3070 P133-13 Model 180 (1956) Owner's Manual AIR 2991 P136-13 Model 180A (1957-1958) Owner's Manual AIR 3037 P170-13 Model 180B (1959) Owner's Manual AIR 3071 P198-13 Model 180C (1960) Owner's Manual AIR 3039 P231-13 Model 180D (1961) Owner's Manual AIR 2634 D127-13 Model 180E (1962) Owner's Manual AIR 3705 D158-13 Model 180F (1963) Owner's Manual AIR 3706 D210-13 Model 180G (1964) Owner's Manual AIR 3036 D264-13 Model 180H (1965) Owner's Manual AIR 3707 D335-13 Model 180H (1966) Owner's Manual AIR 3049 D413-13 Model 180H (1967) Owner's Manual AIR 3048 D521-13 Model 180H (1968) Owner's Manual AIR 3708 D692-13 Model 180H (1969) Owner's Manual Type Acceptance Report Rev.2 : 12 March 2019 TAR 99/11 — Cessna 180 Series 7 AIR 3709 D765-13 Model 180H (1970) Owner's Manual AIR 3710 D946-13 Model 180H (1971-1972) Owner's Manual AIR 2760 D1000-13 Model 180J (1973) Owner's Manual AIR 2761 D1020-13 Model 180J (1974) Owner's Manual AIR 2764 D1040-13 Model 180J (1975) Owner's Manual AIR 2002 D1061-13 Model 180J (1976) Pilot's Operating Handbook AIR 2629 D1086-13 Model 180K (1977) Pilot's Operating Handbook AIR 3221 D1113-13 Model 180K (1978) Pilot's Operating Handbook AIR 2092 D1140-13PH Model 180K (1979) Pilot's Operating Handbook AIR 3711 D1175-13PH Model 180K (1980) Pilot's Operating Handbook AIR 2509 D1195-13PH Model 180K (1981) Pilot's Operating Handbook (6) Operating Data for Aircraft, Engine and Propeller: (i) Maintenance Manual: Cessna 100 Series (1953-1962) Service Manual – Publication D138-13 Cessna 100 Series (1963-1968) Service Manual – Publication D637-13 Cessna 180/185 (1969-1980) Service Manual – Publication D2000-13 Cessna 180/185 (1981-1985) Service Manual – Publication D2067-13 (ii) Current service Information: Cessna Service Bulletins (iii) Illustrated Parts Catalogue: Cessna 180 (1953-62) and 182 (1956-61) Parts Catalog – Publication P259-12 Cessna 180/185 (1961-1973) Parts Catalog – Publication P527-12 Cessna 180/185 (1974-1985) Parts Catalog – Publication P699-12 (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 (8) Other information: Equipment List, Model 180H Equipment List, Model 180J Type Acceptance Report TAR 99/11 — Cessna 180 Series Rev.2 : 12 March 2019 8 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 Rule 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: Civil Aviation Rule Part 91 Subpart F – Instrument and Equipment Requirements PARA: REQUIREMENT: MEANS OF COMPLIANCE: 91.505 Seating and Restraints – Safety belt/Shoulder Harness CAR §3.715 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 CAR §3.655(a)(1) Not Applicable CAR §3.655(a)(2) CAR §3.655(a)(3) CAR §3.672 CAR §3.655(b)(1)(iv) CAR §3.655(b)(1)(ii) (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 CAR §3.655(b)(1)(iii) N/A – Fixed-Pitch N/A – less than 250 hp CAR §3.338 N/A – Fixed undercarriage CAR §3.681 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 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 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 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 Civil Aviation Rule Part 135 Subpart F – Instrument and Equipment Requirements PARA: REQUIREMENT: MEANS OF COMPLIANCE: 135.355 Seating / Restraints – Shoulder harness flight-crew seats Operational requirement – Compliance as applicable 135.357 Additional Instruments (Powerplant and Propeller) Has all instruments required under 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.2 : 12 March 2019 TAR 99/11 — Cessna 180 Series 9 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 drawings Cessna Model 180 Skywagon Copy of FAA Type Certificate Data Sheet 5A6 Sign off …………………………………….. ……………………………............... David Gill Checked – Jason Ashworth Team Leader Airworthiness Team Leader Product Certification Appendix 1 List of Type Accepted Variants: Model: Applicant: CAA Work Request: Date Granted: 180, A, B, C, D, H, J AC 21-1.2/NZCAR Part 21 App. A(c) 180K (1977, 1979, 1981) AC 21-1.2/NZCAR Part 21 App. A(c) 180E K Christophers 99/21B/11 21 September 1998 180K (1978) Sunair Aviation Ltd 12/21B/22 9 July 2012 180F, 180G Textron Aviation Inc 18/21B/12 12 March 2019