Type Acceptance Report TAR 20/21B/8 – Piper J3L Series
Piper J-3 Cub · Other Documents
Overview
This Type Acceptance Report provides details regarding the Piper J3L Series aircraft, which has been granted Type Acceptance in New Zealand based on validation of the FAA Type Certificate A-698. The report outlines the certification details, application background, and compliance with New Zealand operational requirements. It serves as a reference for operators and regulatory bodies to ensure that the aircraft meets the necessary standards for airworthiness and operation in New Zealand. The report confirms that there are no special import requirements for the J3L Series, making it eligible for an Airworthiness Certificate in the Standard Category.
- MCTOW for J3L: 1100 lb (499 kg); J3L-65: 1170 lb (530 kg)
- Engine: Lycoming O-145-A1, A2, or A3 for J3L; O-145-B1, B2, or B3 for J3L-65
- Maximum seating capacity: 2
- Type Acceptance Certificate No. 20/21B/8 granted on December 23, 2019
- No special import requirements for the J3L Series 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
- Other Documents
- Year
- 2019
- Pages
- 12
- File size
- 256 KB
- Publisher
- www.aviation.govt.nz
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Most owners only have the POH. Here's the essential set for the Piper J-3 Cub.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
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In this document
Executive Summary
The Piper J3L Series has received New Zealand Type Acceptance based on validation of FAA Type Certificate A-698. All models covered by this certificate are eligible for an Airworthiness Certificate in the Standard Category, provided they meet New Zealand operational requirements.
Aircraft Certification Details
The J3L Series is certified under FAA Type Certificate A-698, with a maximum certified takeoff weight (MCTOW) of 1100 lb (499 kg) for the J3L and 1170 lb (530 kg) for the J3L-65. It features a Lycoming O-145 engine and can accommodate two seats.
Application Details and Background Information
The application for type acceptance was submitted by Mr. David Johnson on December 3, 2019. The first example registered in New Zealand was serial number 6615. The J3L is a tandem two-seat high-wing light aircraft with a fixed undercarriage.
NZCAR §21.43 Data Requirements
The report details the data requirements satisfied for type acceptance, including the FAA Type Certificate and airworthiness design standards. It confirms that no special conditions or non-compliances were identified.
New Zealand Operational Rule Compliance
The report assesses compliance with New Zealand operational rules, confirming that the J3L meets the necessary requirements for airworthiness and operation without any special conditions.
Full document text
Aircraft Certification Unit Type Acceptance Report TAR 20/21B/8 PIPER J3L Series Type Acceptance Report Rev.0 : 23 December 2019 TAR 20/21B/8 – Piper J3L Series i TABLE OF CONTENTS EXECUTIVE SUMMARY 1 1. INTRODUCTION 1 2. AIRCRAFT CERTIFICATION DETAILS 2 3. APPLICATION DETAILS AND BACKGROUND INFORMATION 3 4. NZCAR §21.43 DATA REQUIREMENTS 4 5. NEW ZEALAND OPERATIONAL RULE REQUIREMENTS 6 ATTACHMENTS 7 Type Acceptance Report Rev.0 : 23 December 2019 TAR 20/21B/8 – Piper J3L Series 1 Executive Summary New Zealand Type Acceptance has been granted to the Piper Model J3L Series based on validation of FAA Type Certificate number A-698. There are no special requirements for import. Applicability is to all aircraft covered by the type certificate, which are now eligible for the issue of an Airworthiness Certificate in the Standard Category in accordance with NZCAR §21.191, 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. 20/21B/8 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 covers all models included on the State-of-Design type certificate which have been granted type acceptance in New Zealand in accordance with the provisions of CAR Part 21B. Type Acceptance Report TAR 20/21B/8 – Piper J3L Series Rev.0 : 23 December 2019 2 2. Aircraft Certification Details (a) State-of-Design Type and Production Certificates: Manufacturer: Piper Aircraft Corporation Type Certificate: A-698 Issued by: Federal Aviation Administration Production Approval: Not applicable (b) Models Covered by the Part 21B Type Acceptance Certificate: (i) Models: J3L, J3L-65 (Army L-4C) MCTOW: 1100 lb. [499 kg] 1170 lb. [530 kg] – J3L-65 per Note 4 on TCDS Max. No. of Seats: 2 Noise Standard: Not Applicable Engine: Lycoming O-145-A1, A2 or A3 [J3L] Lycoming O-145-B1, B2 or B3 [J3L-65] Type Certificate: 210 Issued by: Federal Aviation Administration Propeller: Sensenich M74CX-2 Type Certificate: 1P2 Issued by: Federal Aviation Administration Hartzell HA-12U/7414 to 6814 or 7214M to 6814M Type Certificate: P-824 Issued by: Federal Aviation Administration Any fixed or adjustable pitch type certificated wooden propeller Note: Refer to Advisory Circular 21-1 Appendix 2 for the New Zealand type acceptance status of any engines and propellers listed above. Type Acceptance Report Rev.0 : 23 December 2019 TAR 20/21B/8 – Piper J3L Series 3 3. Application Details and Background Information The application for New Zealand type acceptance of the Piper J3L Series was from the importer Mr David Johnson, dated 3 December 2019. The first-of-type example was serial number 6615, registered ZK-AND. The J3L is a single-engine tandem two-seat high-wing light aircraft with fixed undercarriage and conventional steel-tube and fabric construction. Type Acceptance Certificate No. 20/21B/8 was granted on 23 December 2019 to the Piper Model J3L Series based on validation of FAA Type Certificate A-698. There are no special requirements for import into New Zealand. The J3L is the Lycoming-powered version of the J3C Cub, the first examples of which were registered in New Zealand in 1939 (ZK-AHC). Many examples of the J3L have had the Lycoming engine changed to a Continental, although there is no Service Bulletin available to cover this or to formally re-designate the aircraft model. Type Acceptance Report TAR 20/21B/8 – Piper J3L Series Rev.0 : 23 December 2019 4 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 A-698 FAA Aircraft Specification number A-698 at Revision 14 dated August 7, 2006 – Model J3L approved September 17, 1938 – Model J3L-65 approved May 27, 1940 (2) Airworthiness design requirements: (i) Airworthiness Design Standards: The certification basis of the J3L Series is CAR 4a. This is an acceptable certification basis in accordance with NZCAR Part 21B paragraph §21.41, as CAR 4a is the predecessor to CAR 3 and FAR 23, which is the basic standard for Normal Category Airplanes specified under NZCAR Part 21 Appendix C and Advisory Circular 21-1. 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: Nil (iv) Airworthiness Limitations: Nil (3) Aircraft Noise and Engine Emission Standards: (i) Environmental Standard: Not Applicable. (4) Certification Compliance Listing: "Cub" Model J3: Basic Drawing List Under Type Certificate Stress Summary: J3 Series Airplanes (5) Flight Manual: Piper advises no Flight Manual was required under CAR 4a. The Regulations did require an “Operations Limitations Certificate”, which could be obtained
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from the local FAA Regional Office. The Operations Limitations for N35846 dated July 14, 1944 was adopted as the Flight Manual in New Zealand as AIR 3958 Type Acceptance Report Rev.0 : 23 December 2019 TAR 20/21B/8 – Piper J3L Series 5 (6) Operating Data for Aircraft: (i) Maintenance Manual: (There is no published Maintenance Manual. Piper recommends FAA AC 43.13- 1 for standard repair procedures.) Inspection intervals are found in Report 230 3000. (ii) Current service Information: Service Bulletins and Service Letters (iii) Illustrated Parts Catalogue: Not Published for J-3 (7) Agreement from manufacturer to supply updates of data in (5), and (6): Piper provides CAANZ access to all publications through the Piper Fileshare Server Type Acceptance Report TAR 20/21B/8 – Piper J3L Series Rev.0 : 23 December 2019 6 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 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 N/A – 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 §4.655(a)(1) CAR §4.655(a)(2) CAR §4.655(a)(3) CAR §4.655(b)(1)(i) CAR §4.655(b)(1)(iv) CAR §4.655(b)(1)(ii) CAR §4.655(b)(1)(v) (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 CAR §4.655(b)(1)(iii) N/A – Normally aspirated N/A – Less than 250 h.p. N/A – Not fitted to the J3 N/A – Fixed undercarriage CAR §4.687 [Optional equipment] 91.511 Night VFR Instruments and Equipment Operating Rule – Compliance to be determined by operator 91.513 VFR Communication Equipment Operating Rule – Compliance to be determined by operator 91.517 IFR Instruments and Equipment Operating Rule – Compliance to be determined by operator 91.519 IFR Communication and Navigation Equipment Operating Rule – Compliance to be determined by operator 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 Operating Rule – Compliance to be determined by operator 91.531 Oxygen Indicators – Volume/Pressure/Delivery Operating Rule – Compliance to be determined by operator 91.533 Oxygen for non-Pressurised Aircraft Not Fitted as Standard 91.541 SSR Transponder and Altitude Reporting Equipment Operating Rule – Compliance to be determined by operator 91.543 Altitude Alerting Device – Turbojet or Turbofan Not Applicable – Not turbo jet or turbofan powered 91.545 Assigned Altitude Indicator Operating Rule – Compliance to be determined by operator A.15 ELT Installation Requirements To be determined on an individual aircraft basis 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. Type Acceptance Report Rev.0 : 23 December 2019 TAR 20/21B/8 – Piper J3L Series 7 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 20/21B/8 – Piper J3L Series Rev.0 : 23 December 2019 8 Attachments The following documents form attachments to this report: Three-view drawing Piper Model J3L Copy of FAA Aircraft Specification Number A-698 Sign off …………………………………….. ……………………………............... David Gill Checked – Greg Baum Team Leader Airworthiness Acting Team Leader Product Certification









