Type Acceptance Report TAR 98/08 – Cessna 150/152
Cessna 152 Aerobat · Maintenance Manual
Overview
This Type Acceptance Report provides an overview of the Cessna 150 and 152 series aircraft, including the Aerobat variant, as accepted for operation in New Zealand. It outlines the certification details, operational requirements, and compliance with local regulations. The report confirms that all models under FAA Type Certificate number 3A19 are eligible for an Airworthiness Certificate in New Zealand, provided they meet specific operational requirements. This document is essential for operators and maintenance personnel to understand the regulatory framework and compliance necessary for the Cessna 150/152 series aircraft.
- Cessna 152 MCTOW: 1670 lb (757 kg)
- Cessna 150 MCTOW: 1500 lb (680 kg)
- Cessna 152 engine: Lycoming O-235-L2C or -N2C
- Cessna 150 series engine: Continental O-200-A
- All models under FAA Type Certificate 3A19 are accepted in New Zealand.
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
- Maintenance Manual
- Year
- 2018
- Pages
- 14
- File size
- 54 KB
- Publisher
- www.aviation.govt.nz
Common. Rarer than 4% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Cessna 152 Aerobat.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the A152 Aerobat to your watchlist and track it in one place.
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In this document
Executive Summary
The report grants New Zealand Type Acceptance to the Cessna 150/152 and Aerobat Series based on FAA Type Certificate validation. It states that all models listed under this certificate are eligible for Airworthiness Certificates in New Zealand, subject to compliance with local operational requirements.
Aircraft Certification Details
The Cessna 150/152 series includes multiple models with a maximum certified takeoff weight (MCTOW) of 1500 lb for the 150 series and 1670 lb for the 152 series. The 152 is powered by a Lycoming O-235 engine, while the 150 series uses a Continental O-200 engine.
Application Details and Background Information
The report details the history of the Cessna 150 and 152 series, including their development and certification process in New Zealand. It highlights the major design changes from the 150 to the 152, including engine upgrades and weight increases.
NZCAR §21.43 Data Requirements
This section outlines the data requirements for type acceptance under New Zealand Civil Aviation Rules, including the necessary documentation and compliance with airworthiness standards.
Operating Data for Aircraft
The report lists maintenance manuals and parts catalogs for the Cessna 150 and 152 series, providing essential references for maintenance personnel.
Safety notes
- Ensure compliance with local operational requirements for airworthiness certification.
Full document text
Aircraft Certification Unit Type Acceptance Report TAR 98/08 – Revision 2 CESSNA 150/152 Series Type Acceptance Report Rev.2 : 19 September 2018 TAR 98/08 – Cessna 150/152 i TABLE OF CONTENTS EXECUTIVE SUMMARY 1 1. INTRODUCTION 1 2. AIRCRAFT CERTIFICATION DETAILS 2 3. APPLICATION DETAILS AND BACKGROUND INFORMATION 4 4. NZCAR §21.43 DATA REQUIREMENTS 5 5. NEW ZEALAND OPERATIONAL RULE REQUIREMENTS 9 ATTACHMENTS 10 APPENDIX 1 10 Type Acceptance Report Rev.2 : 19 September 2018 TAR 98/08 – Cessna 150/152 1 Executive Summary New Zealand Type Acceptance has been granted to the Cessna 150/152 and Aerobat Series based on validation of FAA Type Certificate number 3A19. There are no special requirements for import. All models listed under the FAA type certificate have been type accepted in New Zealand, which are 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. 98/08 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 models in New Zealand; and (b) Identify any special conditions for import applicable to any models 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 98/08 – Cessna 150/152 Rev.2 : 19 September 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: 3A19 Issued by: Federal Aviation Administration Production Approval: Delegation Option Manufacturer No. CE-1 FAA Production Certificate No.4 (b) Models Covered by the Part 21B Type Acceptance Certificate: (i) Models: 150, 150A, 150B, 150C, 150D 150E, 150F, 150G, 150H, 150J 150K, A150K, 150L, A150L 150M, A150M MCTOW: 1500 lb. [680 kg] 1600 lb. [726 kg] – Model 150D on Max. No. of Seats: 2 Noise Standard: Not Applicable Engine: Continental O-200-A Type Certificate: E-252 Issued by: Federal Aviation Administration Propeller: Sensenich 69CK Type Certificate: P-904 Issued by: Federal Aviation Administration McCauley 1A100/MCM or 1A101/DCM McCauley 1A101/GCM, /HCM, /PCM McCauley 1A102/OCM Type Certificate: P-918 Issued by: Federal Aviation Administration Type Acceptance Report Rev.2 : 19 September 2018 TAR 98/08 – Cessna 150/152 3 (ii) Models: 152, A152 MCTOW: 1670 lb. [757 kg] Max. No. of Seats: 2 Noise Standard: FAR Part 36 Engine: Lycoming O-235-L2C or -N2C Type Certificate: E-223 Issued by: Federal Aviation Administration Propeller: McCauley 1A103/TCM Type Certificate: P50GL Issued by: Federal Aviation Administration Type Acceptance Report TAR 98/08 – Cessna 150/152 Rev.2 : 19 September 2018 4 3. Application Details and Background Information The application for New Zealand type acceptance of the Model 150J was from Messrs P R & C M McGregor, dated 1 December 1997. The first-of-type aircraft was serial number 15069904 registered ZK-SUM. The Cessna 150/152 series is a two-seat high-wing all- metal single-engine light training aircraft. Type Acceptance Certificate No. 98/08 was granted on 10 December 1997 to the Cessna 150J based on validation of FAA Type Certificate 3A19. There are no special requirements for import into New Zealand. This report was raised to Revision 1 to include the 1985 Model 152 serial numbers 15285940 through 15286033, and to update the report to the latest format. The applicant was the Manawatu Districts Aero Club, and the first-of-type was serial number 15286015 registered ZK-JDC. Type acceptance was granted on 26 June 2008. Revision 2 to this report added all the other variants and serial number ranges of the 150/152 Series not previously included. This was at the request of the type certificate holder, who has provided access to all technical publications. The Cessna 150 was developed as a successor to the popular Cessna 140B which finished production in 1951. The main changes were the use of tricycle landing gear, and replacing the rounded wingtips and horizontal and vertical stabilizers with more modern, squared-off profiles. In addition, the narrow, hinged wing flaps of the 140 were replaced by larger, more effective Fowler flaps. The 150 Series followed the usual Cessna practice of annual model changes with incremental improvements. The omnivision rear window was introduced on the 1964 150D, while the swept rear vertical fin was fitted from the 1967 150F onwards. In 1961, the main gear struts were moved aft two inches to improve tail- heavy tendencies on the ground, and tubular gear legs with a wider track were added in
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1971. The gross weight was increased from 1500 pounds to 1600 pounds in 1964. Electric flaps of 40 degrees were installed in 1966, but travel was later limited to 30 degrees. The A150 Aerobat had a strengthened airframe with jettisonable doors. The 150J is identical to the previous 150G/H except for minor cosmetic changes to the doors, window seals, instrument panel, control yoke, compass relocation and other miscellaneous items of equipment, plus new nose wheel fairings. The Cessna 152 was a development of the Model 150, the major design change being the substitution of the 110 hp Lycoming O-235 engine, along with associated changes to the engine cowl, exhaust system, propeller, engine mount and baffles. The electrical system was changed to 28 volts and the maximum all-up weight increased to 1670 lb. The first Model 150 on the New Zealand Civil Aircraft Register was serial number 17688 registered ZK-BPO in November 1959. The first Model 152 was serial number 152-80954 registered ZK-EKM in March 1978. Type Acceptance Report Rev.2 : 19 September 2018 TAR 98/08 – Cessna 150/152 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 3A19 FAA Type Certificate Data Sheet no. 3A19 at Revision 50 dated July 21, 2017 – Model 150 approved July 10, 1958 – Model 150A approved June 14, 1960 – Model 150B approved June 20, 1961 – Model 150C approved June 15, 1962 – Model 150D approved July 19, 1963 – Model 150E approved June 18, 1964 – Model 150F approved May 27, 1965 – Model 150G approved May 5, 1966 – Model 150H approved August 12, 1966 – Model 150J approved May 2, 1968 – Models 150K and A150K approved June 5, 1969 – Models 150L and A150L approved June 8, 1970 – Models 150M and A150M approved May 6, 1974 – Models 152 and A152 approved March 16, 1977 (2) Airworthiness design requirements: (i) Airworthiness Design Standards: The certification basis of the Cessna Model 150/152 Series is Part 3 of the Civil Air Regulations dated May 15, 1956, as amended by 3-4. In addition for 1979 Models 152 and A152 and on, FAR paragraph §23.1559 effective 1 March 1978 was added, and for 1985 Models 152 and A152 and on, FAR paragraph §23.1545(a) at amendment 23-23 dated 1 December 1978 was added. This is an acceptable certification basis in accordance with NZCAR Part 21B Para §21.41 and Advisory Circular 21-1A, because CAR 3 was the predecessor to FAR 23 which is the basic standard for Normal Category Airplanes called up under Appendix C. There are no non-compliances and no special conditions have been prescribed by the Director under §21.23. (ii) Special Conditions: Nil (iii) Equivalent Level of Safety Findings: 1977 Model 150 and 152: 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 presented in the Pilot’s Operating Handbook is available to the pilot. ASI calibration data must be predicated on flight test. Type Acceptance Report TAR 98/08 – Cessna 150/152 Rev.2 : 19 September 2018 6 (iv) Airworthiness Limitations: Nil (3) Aircraft Noise and Engine Emission Standards: (i) Environmental Standard: The Models 152 and A152 have been certificated under FAR Part 36, including Amendments 36-1 through 36-5. (ii) Compliance Listing: Report ET-78-131 – Noise Level Certification for Light Propeller Driven Aircraft per FAR 36 (Amdt. 1-10)/Model 152/A152 – Corrected Noise Level 66.3 dB(A) Report ET-82-12 – Flyover Noise Analysis for FAA Certification Model 152/A152 See Advisory Circular 36-1H Appendix 7 and Flight Manuals (Section 4). Model: MTOW: Engine: Propeller: RPM: Noise Levels MdbA CdbA 152 1670 O-235-L2C 1A102/TCM6955 2550 65.8 64.8 152/A152 1670 O-235-L2C 1A103/TCM6958 2550 66.7 66.3 (4) Certification Compliance Listing: Cessna Report DM 150A-0 – Type Inspection Report Model 150A Cessna Report S-150B-0: Model 150B – Basic Data Cessna Report S-150B-33: Model 150B – Structures Substantiation Summary Cessna Report S-150C-0: Model 150C – Basic Data Cessna Report S-150C-33: Model 150C – Structures Substantiation Summary Cessna Report DM 150C-0: - Type Inspection Report Model 150C Cessna Report S-150D-0: Model 150D – Basic Data Cessna Report DM 150F-0: Engineering Flight Test Report Model 150F Cessna Report DM 150G-0: Type Inspection Report Model 150G Cessna Report DM 150H-0: 1968 Model 150 Changes Report S-150J-33 – Substantiation, Critical Loads & Structural Materials Summary Cessna Report DM 150J-0 – 1969 Model Changes Cessna Report S-150L-35(71): Model 150L – Fatigue Analysis Cessna Report DM 150M-0: Certification of the 1975 Model Changes Cessna Report S-152-33 (78) – Model 152 – Substantiation, Critical Loads & Structural Materials Summary – Revision L (Includes Memo 80M2/7-4 which lists the various Cessna 152 structural reports) Cessna Report DM-152-0 – Revision B – Certification of the 1978 Model 152 DM-152-0 Addendum #2 – Approval of the 1979 Model Changes to the 152 DM-152-0 Addendum #4 – Approval of the 1980 Model Changes DM-152-0 Addendum #5 – Approval of the 1981 Model Changes DM-152-0 Addendum #6 – Approval of the 1982 Model Changes DM-152-0 Addendum #7 – Approval of the 1983 Model Changes DM-152-0 Addendum #10 – Approval of the 1984 Model Changes DM-152-0 Addendum #11 – Approval of the 1985 Model Changes Type Acceptance Report Rev.2 : 19 September 2018 TAR 98/08 – Cessna 150/152 7 (5) Flight Manual: CAA AIR Cessna Number: Publication: Title: AIR 2757 P187-13 Model 150 (1959-60) Owner's Manual AIR 139 P220-13 Model 150A (1961) Owner's Manual AIR 3671 D123-13 Model 150B (1962) Owner's Manual AIR 3672 D156-13 Model 150C (1963) Owner's Manual AIR 2424 D208-13 Model 150D (1964) Owner's Manual AIR 2425 D251-13 Model 150E (1965) Owner's Manual AIR 2426 D326-13 Model 150F (1966) Owner's Manual AIR 2427 D397-13 Model 150G (1967) Owner's Manual AIR 2428 D518-13 Model 150H (1968) Owner's Manual AIR 2600 D624-13 Model 150J (1969) Owner's Manual AIR 3663 D727-13 Model 150K (1970) Owner's Manual AIR 3664 D836-13 Model 150L (1971) Owner's Manual AIR 3665 D901-13 Model 150L (1972) Owner's Manual AIR 238 D962-13 Model 150L (1973) Owner's Manual AIR 3666 D1013-13 Model 150M (1974) Owner's Manual AIR 254 D1033-13 Model 150M (1975) Owner's Manual AIR 2621 D1055-13 Model 150M (1976) Pilot's Operating Handbook AIR 2622 D1080-13 Model 150M (1977) Pilot's Operating Handbook AIR 3056 D740-13 Model A150K (1970) Owner's Manual AIR 3667 D839-13 Model A150L (1971) Owner's Manual AIR 3668 D900-13 Model A150L (1972) Owner's Manual AIR 2497 D963-13 Model A150L (1973) Owner's Manual AIR 2579 D1014-13 Model A150M (1974) Owner's Manual AIR 286 D1034-13 Model A150M (1975) Owner's Manual AIR 2623 D1056-13 Model A150M (1976) Pilot's Operating Handbook AIR 2624 D1081-13 Model A150M (1977) Pilot's Operating Handbook AIR 2049 D1107-13 Model 152 (1978) Pilot's Operating Handbook AIR 2745 D1136-13PH Model 152 (1979) Pilot's Operating Handbook AIR 2746 D1170-13PH Model 152 (1980) Pilot's Operating Handbook AIR 2156 D1190-13PH Model 152 (1981) Pilot's Operating Handbook AIR 2180 D1210-13PH Model 152 (1982) Pilot's Operating Handbook AIR 2197 D1229-13PH Model 152 (1983) Pilot's Operating Handbook AIR 2246 D1249-13PH Model 152 (1984) Pilot's Operating Handbook AIR 3040 D1270-13PH Model 152 (1985) Pilot's Operating Handbook AIR 2032 D1108-13 Model A152 (1978) Pilot's Operating Handbook AIR 2684 D1137-13PH Model A152 (1979) Pilot's Operating Handbook AIR 2685 D1171-13PH Model A152 (1980) Pilot's Operating Handbook AIR 2148 D1191-13PH Model A152 (1981) Pilot's Operating Handbook AIR 2181 D1211-13PH Model A152 (1982) Pilot's Operating Handbook AIR 2329 D1230-13PH Model A152 (1983) Pilot's Operating Handbook AIR 3669 D1250-13PH Model A152 (1984) Pilot's Operating Handbook AIR 3670 D1271-13PH Model A152 (1985) Pilot's Operating Handbook Type Acceptance Report TAR 98/08 – Cessna 150/152 Rev.2 : 19 September 2018 8 (6) Operating Data for Aircraft: (i) Maintenance Manual: Cessna 100 Series (1953-1962) Service Manual – Publication D138-13 Cessna 100 Series (1963-1968) Service Manual – Publication D637-13 Cessna Model 150 (1969-1976) Service Manual – Publication D971-13 Cessna Model 150 (1977) Service Manual – Publication D2011-13 Cessna Model 152 (1978-1985) Service Manual – Publication D2064-13 Cessna 100 Series Continued Airworthiness Program – Publication D5133-13 (ii) Current service Information: Service Bulletins/Service Letters (iii) Illustrated Parts Catalogue: Cessna Model 150 (1959-1969) Parts Catalog – Publication P438-12 Cessna Model 150 (1970-1977) Parts Catalog – Publication P691-12 Cessna Model 152 (1978-1985) Parts Catalog – Publication P692-12 (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 Type Acceptance Report Rev.2 : 19 September 2018 TAR 98/08 – Cessna 150/152 9 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 – 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 Rules Part 91 Subpart F – Instrument and Equipment Requirements PARA: REQUIREMENT: MEANS OF COMPLIANCE: 91.505 Seating and Restraints – Safety belt/Shoulder Harness To be determined on an individual aircraft basis 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 (8) Coolant Temp CAR3 §3.655(a)(1) N/A – No mach limitation CAR3 §3.655(a)(2) CAR3 §3.655(a)(3) CAR3 §3.655(b)(1) CAR3 §3.655(b)(4) CAR3 §3.655(b)(2) N/A – Air cooled (9) Oil Temperature (10) Manifold Pressure (11) Cylinder Head Temp. (12) Flap Position (13) U/c Position (14) Ammeter/Voltmeter (15) CO indicator N/A – less than 250 hp N/A – not turbo, not CSP N/A – less than 250 hp CAR 3 §3.338 N/A – fixed gear CAR §3.681 To be determined for each individual aircraft 91.511 Night VFR Instruments and Equipment To be determined on an individual aircraft basis 91.513 VFR Communication Equipment To be determined on an individual aircraft basis 91.517 IFR Instruments and Equipment To be determined on an individual aircraft basis 91.519 IFR Communication and Navigation Equipment To be determined on an individual aircraft basis 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 9 Passengers Not Applicable – less than 9 Passengers Not Applicable – less than 20 Passengers Not Applicable – less than 61 Passengers 91.529 ELT - TSO C126 406 MHz after 22/11/2007 To be determined on an individual aircraft basis 91.531 Oxygen Indicators - Volume/Pressure/Delivery To be determined on an individual aircraft basis 91.533 Oxygen for Non-Pressurised Aircraft To be determined on an individual aircraft basis 91.541 SSR Transponder and Altitude Reporting Equipment To be determined on an individual aircraft basis 91.543 Altitude Alerting Device - Turbojet or Turbofan Not Applicable – Not turbojet or turbofan 91.545 Assigned Altitude Indicator To be determined on an individual aircraft basis 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 / Restraints – Shoulder harness flight-crew seats To be determined on an individual aircraft basis 135.357 Additional Instruments (Powerplant and Propeller) To be determined on an individual aircraft basis 135.359 Night Flight Landing light, Pax compartment To be determined on an individual aircraft basis 135.361 IFR Operations Speed, Alt, spare bulbs/fuses To be determined on an individual aircraft basis 135.363 Emergency Equipment (Part 91.523 (a) and (b)) To be determined on an individual aircraft basis 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 TAR 98/08 – Cessna 150/152 Rev.2 : 19 September 2018 10 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. 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 91/135 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 150J Three-view drawing Cessna Model 152 Copy of FAA Type Certificate Data Sheet Number 3A19 Sign off …………………………………….. ……………………………............... David Gill Checked – Kavita Vanmari Team Leader Airworthiness Airworthiness Engineer Appendix 1 List of Type Accepted Variants: Model: Applicant: CAA Work Request: Date Granted: 150, 150A, 150D, 150F, 150G, 150H AC 21-1.2/NZCAR Part 21 Appendix A(c) 150L, A150L (1972-1974), 150M, A150M AC 21-1.2/NZCAR Part 21 Appendix A(c) 152 (1978-1984), A152 (1978-1983) AC 21-1.2/NZCAR Part 21 Appendix A(c) 150J P R & C M McGregor 98/21H/8 10 December 1997 152 (1985) Manawatu Districts Aero Club 8/21B/30 26 June 2008 All 150/152 Textron Aviation Inc. 18/21B/10 19 September 2018