Type Acceptance Report TAR 99/21B/31 – Piper PA-28 Cherokee Series

Hartzell HC-C2YK-1( )F/F7666A FAA Type Certificate: P-920 McCauley B2D34C213/90DHA-16 [with -C1C6 engine only] McCauley 2D34C215/90DJA-14E [PA-28RT-201] FAA Type Certificate: P7EA (vi) Model: PA-28R-201T, PA-28RT-201T, PA-28-201T MCTOW: 2900 lb. [1315 kg] Noise Standard: FAR Part 36 Engine: Continental TSIO-360-F or -FB FAA Type Certificate: E16EA Propeller: Hartzell BHC-C2YF-1( )F/F8459A-8R FAA Type Certificate: P-920 Hartzell PHC-C3YF-1( )F/F7663-2R [PA-28RT-201T] FAA Type Certificate: P25EA Notes: 1. Refer to FAA TCDS 2A13 for specific applicability of engine and propeller combinations to individual aircraft models. 2. 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.2 : 8 July 2019 TAR 99/21B/31 – Piper PA-28 Series 5 3. Application Details and Background Information There have been many examples of the Piper PA-28 Cherokee in New Zealand prior to 1995 when Part 21 was introduced, and those particular model years or serial number ranges were therefore deemed to have a type acceptance certificate under the transitional arrangements of Part 21 Appendix A(c). The first application for New Zealand type acceptance under Part 21B was for the Model PA-28-181 Archer III from the NZ agent and importer, Airwork (NZ) Ltd, dated 24 February 1999. A new production aircraft serial number 2843213 had been ordered as a demonstrator, registered as ZK-NEW. The PA-28 Cherokee Series is a four-seat low-wing all-metal unpressurised light aircraft. There have been subsequent imports of later production aircraft equipped with the Avidyne FlightMax Entegra EFIS system under an STC, for which New Piper supplied a certification package. Type acceptance was not required because the same manuals are used with Supplements. Type Acceptance Certificate No. 99/21B/31 was granted on 30 March 1999 to the Piper Model PA-28-181 Archer III based on validation of FAA Type Certificate 2A13. Specific applicability is limited to the coverage provided by the operating documentation supplied. There are no special requirements for import into New Zealand. The application for type acceptance of the Model PA-28R-201T was from the owner dated 26 November 2001. The first-of-type example was serial number 28R-7803237, registered ZK-REC. (Although there have been three examples of the Arrow III on the NZ register, the first being ZK-EIF in 1978, and four examples of the later Turbo Arrow IV, there have been no Turbo Arrow III.) Type acceptance was granted on 20 December 2001. The application for New Zealand type acceptance of the most recent production Model PA-28-161 Warrior III was from the aircraft manufacturer dated 14 August 2002. The first- of-type example was serial number 2842165, which was registered as ZK-EBW for the Canterbury Aero Club. Type acceptance was granted on 3 September 2002. This report was raised to Revision 1 to include the 1969/71 Model PA-28R-200 Arrow. The opportunity was also taken to consolidate all the previous (separate) PA-28 Reports and update to the latest format. The applicant was Flight Care Ltd and the first-of-type was serial no.28-35725, registered ZK-RTE. Type acceptance was granted on 20 October 2008. Revision 2 was raised to add the two latest PA-28-181 production versions, the “Archer DX” with the G1000 and the later “Archer TX” with the G1000NXi EFIS displays. The first-of-type examples were serial numbers 2843918 and 2843919 registered ZK-LJT and ZK-LJX respectively. The opportunity was also taken to add all the other PA-28 variants on the current type certificate which were not previously covered. This was on the basis that the type certificate holder had provided CAA with access to all technical publications. The very first Model PA-28-160 Cherokee introduced in 1960 was an all-new entry-level training and touring aircraft from Piper. It has since been developed into a large family of variants with a range of powerplant options, including the Arrow Series with retractable undercarriage and constant-speed propeller. All variants have four seats with a single entry door on the right hand side, while an extra fuselage window was added in the late 1960s. The first Cherokees had a constant-chord rectangular planform wing, but starting in 1974 Piper introduced a new wing with tapered outer section and an extra two feet of span. This was progressively fitted to the new PA-28-151/161/181/201 variants. Type Acceptance Report TAR 99/21B/31 – Piper PA-28 Series Rev.2 : 8 July 2019 6 The Archer III is a derivative of the PA-28-181 Archer II which was first type accepted in NZ in 1978 with ZK-EIP. The Archer III is a new sub-model on the Type Certificate, and the modifications include: 28 volt electrical system; a restyled flat single-piece metal instrument panel with post lights; new style control wheel; an overhead switch panel with internally lit rocker switches; a redesigned engine cowling with NACA scoop air induction system and axisymmetric engine cooling inlets; and a modified muffler exhaust exit pipe. The taxi and landing lights are now mounted in the wing tips and there is an electric engine primer system. A propeller with an extended hub was also incorporated. The first example of the original 180 hp Arrow in New Zealand was ZK-CUI, which was imported in 1969. The PA-28R-200 was the first development, with an uprated engine, and the first-of-type example was ZK-RTE. The PA-28R-200 Arrow II introduced for the 1972 model year had a five inch fuselage extension, to allow more rear seat room, a larger horizontal tail, and small wingspan and gross weight increases. The first example here was registered ZK-DIU in 1973. The Arrow III was a major re-development incorporating the new increased-span semi-tapered wing first introduced on the PA-28-151 Warrior. This uses the same wing section, but it permits an increase in MCTOW. The first example of the Model PA-28R-201 Arrow III in New Zealand was ZK-EIF, which was registered in 1978. The Warrior III is an updated version of the PA-28-161 Warrior II, which was a 160 hp development of the PA-28-151 Warrior. A simplified version with reduced trim standard was sold as the Cadet. There have been fifteen examples of the Warrior in NZ, the first being ZK-DIX and ZK-DOU registered in January 1974, and twenty six examples of the Warrior II, starting with ZK-EID in October 1977. For the Warrior III the electrical system was uprated from 14 to 28 volts, and a new two-piece panel fitted with modernised engine instrumentation, lighted rocker switches and post lights. The only aerodynamic change is the deletion of wheel pants and the use of the small-chord strut fairings from the Cadet. The Commercial Model Names for the various Cherokee models are as follows: PA-28-150, PA-28-160 Cherokee, Cherokee B/C PA-28-140 Cherokee Cruiser PA-28-151 Cherokee Warrior PA-28-161 Warrior II/III PA-28-180 Cherokee / Archer PA-28-181 Archer II/III PA-28-235 Cherokee Pathfinder PA-28-236 Dakota PA-28R-180 Arrow PA-28R-200 Arrow II PA-28R-201 Arrow III PA-28R-201T Turbo Arrow III PA-28RT-201 Arrow IV PA-28RT-201T Turbo Arrow IV PA-28-201T Turbo Dakota Type Acceptance Report Rev.2 : 8 July 2019 TAR 99/21B/31 – Piper PA-28 Series 7 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 2A13 FAA Type Certificate Data Sheet no. 2A13 at Revision 59 dated 27 August, 2018 – Model PA-28-160 approved October 31, 1960 – Model PA-28-150 approved June 2, 1961 – Model PA-28-180 approved August 3, 1962 – Model PA-28-235 approved July 15, 1963 – Model PA-28-140 approved February 14, 1964 – Model PA-28R-180 approved June 8, 1967 – Model PA-28R-200 approved January 16, 1969 – Model PA-28-151 approved August 9, 1973 – Model PA-28-181 approved July 8, 1975 – Model PA-28-161 approved November 2, 1976 – Model PA-28R-201 approved November 2, 1976 – Model PA-28R-201T approved November 2, 1976 – Model PA-28-236 approved June 1, 1978 – Model PA-28RT-201 approved November 13, 1978 – Model PA-28RT-201T approved November 13, 1978 – Model PA-28-201T approved December 14, 1978 (2) Airworthiness design requirements: (i) Airworthiness Design Standards: The original certification basis of the first Cherokee Model PA-28-160 was CAR 3 effective May 15, 1956, including Amendments 3-1, 3-2 and 3-4. For subsequent variants of the PA-28 this was upgraded to include paragraphs of Amendment 3-7, plus specific paragraphs of FAR Part 23, as noted individually on the TCDS. This is an acceptable certification basis in accordance with NZCAR Part 21B paragraph §21.41 and Advisory Circular 21-1A, because CAR 3 is the predecessor of FAR 23, which is the basic standard for Normal Category Airplanes called up under 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: Special Condition (Docket #CE207) for HIRF was applied to later production versions of the PA-28 Series when fitted with electronic flight instrument systems. (iii) Equivalent Level of Safety Findings: Piper Models PA-28-161, PA-28R-201, PA-28R-201T, PA-28-236, PA-28RT-201, PA-28RT-201T, and PA-28-201T – CAR 3.757(a) Airspeed Indicator – Piper advised this addressed “calibrated airspeed shall be used”, while these later Models used an ASI which displayed indicated airspeed. Type Acceptance Report TAR 99/21B/31 – Piper PA-28 Series Rev.2 : 8 July 2019 8 (iv) Airworthiness Limitations: See Maintenance Manual. (3) Aircraft Noise and Engine Emission Standards: (i) Environmental Standard: The PA-28-161 and later versions have been certificated under FAR Part 36, including Amendments 36-1 through 36-4, and later as applicable. (ii) Compliance Listing: Report VB-1610 – PA-28-161 Warrior III noise level is 72.9 dB(A). Report VB-1611 – PA-28-181 Archer III FAR 36G noise level is 73.1 dB(A) with standard exhaust, and 71.9 dB(A) with optional exhaust system. Report VB-1612 – PA-28R-201 Arrow III noise level is 75.5 dB(A). Report VB-800 – PA-28R-201T noise level is 68.8 dB(A). Report VB-910 – PA-28-236 noise level is 72.9 dB(A). Report VB-930 – PA-28RT-201 noise level is 75.5 dB(A). Report VB-940 – PA-28RT-201T noise level is 69.4 dB(A). Report VB-920 – PA-28-201T noise level is 69.6 dB(A). (4) Certification Compliance Listing: Piper Report VB-2 Model PA-28 Section 2 Basic Data Piper Report VB-15 PA-28 Land Plane Equipment List Piper Report FT-183 – Model PA-28-181 Archer III Certification dated 19 Aug 94 Piper Report VB-712 Sect. II – PA-28-181 III 28V Electrical System Substantiation Piper Report FT107 – Flight Test Certification PA-28R-201T Piper Report FT108 – Flight Test Report PA-28R-201/T Piper Report VB-751 – Structural Substantiation PA-28R-201/T Piper Report FT-184 – PA-28-161 Warrior III Type Inspection Report – Rev C Piper Report VB-814 – Appendix 7 – 28 Volt Electrical System – PA-28-161 III Project 28-079-34 – Compliance Checklist PA28-161 – Optional 28V Elec. System Project 28-118-18 – Compliance Checklist PA28-161 – 2000 Yearly Model Change Project 28-069-03 – Compliance Checklist PA28-161 – Model Year 2001 Warrior Report VB-1892 – PSCP – Avidyne Entegra Integrated Flight Deck Option PA-28 Report VB-1898 – Electrical Substantiation Report – Avidyne Entegra Integrated Flight Deck System (PFD and MFD) Installation in PA28R-201; PA-28-181 and PA-28-161 (FAA project TD7644AT-A). Report VB-1901 – PA-28 Series Powerplant Substantiation – Optional Avidyne Report VB-1901 – PA-28 Series Mechanical Systems Substantiation – Optional AE Piper Report VB-59 – Structural Substantiation PA-28R-180/200 Piper Report FT67 – Model PA-28R-200 Flight Test Report Piper Report VB-176: Equipment List, Model PA-28R-200 Type Acceptance Report Rev.2 : 8 July 2019 TAR 99/21B/31 – Piper PA-28 Series 9 (5) Flight Manual: CAA AIR Report Number: Number: Piper Model and Serial Number Range: AIR 3858 VB-160 PA-28-140 S/N 28-20001 through 28-26946, and 28-7125001 through 28-7125641 AIR 3859 VB-339 PA-28-140 S/N 28-7225001 through 28-7325674 AIR 225 VB-557 PA-28-140 S/N 28-7425001 through 28-7625275 AIR 2400 VB-770 PA-28-140 S/N 28-7725001 through 28-7725290 AIR 3860 VB-166 PA-28-150 S/N 28-1 through 28-4377 AIR 2048 VB-573 PA-28-151 S/N 28-7415001 through 28-7615435 AIR 2022 VB-780 PA-28-151 S/N 28-7715001 through 28-7715314 AIR 2770 VB-168 PA-28-160 S/N 28-1 through 28-4377, and 28-1760A AIR 2024 VB-880 PA-28-161 S/N 28-7716001 through 28-8216300 AIR 2387 VB-1180 PA-28-161 S/N 28-8316001 through 28-8616057, and 2816001 through 2816119 AIR 3861 VB-1360 PA-28-161 S/N 2841001 through 2841365 AIR 3862 VB-1565 PA-28-161 S/N 2816110 through 2816119 AIR 2793 VB-1610 PA-28-161 Warrior III Serial Number 2842001 and Up AIR 2103 VB-163 PA-28-180 S/N 28-671 through 28-5600 AIR 2773 VB-210 PA-28-180 S/N 28-5601 through 28-5859, and 28-7105001 through 28-7205091 AIR 2863 VB-355 PA-28-180 S/N 28-7205092 through 28-7205318 AIR 203 VB-437 PA-28-180 S/N 28-7305001 through 28-7305601 AIR 2850 VB-558 PA-28-180 S/N 28-7405001 through 28-7505260 AIR 2009 VB-760 PA-28-181 S/N 28-7690001 through 28-7690467 AIR 2438 VB-790 PA-28-181 S/N 28-7790001 through 28-7990589 AIR 2128 VB-1120 PA-28-181 S/N 28-8090001 through 28-8690056, 28-8690061, 28-8690062, and 2890001 through 2890205 AIR 2650 VB-1611 PA-28-181 Archer III Serial Number 2843001 and Up AIR 3863 VB-1563 PA-28-181 Archer III S/N 2890206 through 2890231 AIR 3845 VB-2266 PA-28-181 Archer III S/N 2843701, 03 and up G1000 AIR 3916 VB-2596 PA-28-181 Archer III S/N 2843852, 54 and up G1000NXi AIR 3864 VB-2749 PA-28-181 S/N 2843823, 2881001 and up G1000NXi-GFC AIR 2313 VB-173 PA-28R-180 S/N 28R-30001 through 28R-31270, and 28R-7130001 through 28R-7130013 AIR 3055 VB-175 PA-28R-200 S/N 28R-35001 through 28R-35820, and 28R-7135001 through 28R-7135229 AIR 3054 VB-343 PA-28R-200 S/N 28R-7235001 through 28R-7335446 AIR 2905 VB-560 PA-28R-200 S/N 28R-7435001 through 28R-7635545 AIR 2042 VB-870 PA-28R-201 S/N 28R-7737001 through 28R-7837317 AIR 3865 VB-1365 PA-28R-201 S/N 2837001 through 2837061 AIR 3866 VB-1612 PA-28R-201 S/N 2844001 and up Type Acceptance Report TAR 99/21B/31 – Piper PA-28 Series Rev.2 : 8 July 2019 10 AIR 2765 VB-800 PA-28R-201T S/N 28R-7703001 through 28R-7803373 AIR 3867 VB-1370 PA-28R-201T S/N 2803001 through 2803012 AIR 3868 VB-930 PA-28RT-201 S/N 28R-7918001 through 28R-7918267 AIR 3869 VB-1130 PA-28RT-201 S/N 28R-8018001 through 28R-8218026 AIR 2195 VB-940 PA-28RT-201T S/N 28R-7931001 through 28R-8631005, and 2831001 through 2831013 AIR 3870 VB-920 PA-28-201T S/N 28-7921001 through 28-7921095 AIR 2040 VB-170 PA-28-235 S/N 28-10001 through 28-11378, and 28-7110001 through 28-7210023 AIR 204 VB-442 PA-28-235 S/N 28-7310001 through 28-7310176 AIR 2469 VB-559 PA-28-235 S/N 28-7410001 through 28-7610202 AIR 3871 VB-810 PA-28-235 S/N 28-7710001 through 28-7710089 AIR 2123 VB-910 PA-28-236 S/N 28-7911001 through 28-8611008, and 2811001 through 2811050 AIR 3872 VB-1613 PA-28-236 S/N 2845001 and up (6) Operating Data for Aircraft: (i) Maintenance Manual: P/N 761-539 – PA-28-151 & PA-28-161 Warrior I, Warrior II, & Warrior III (III ending Serial Number 2816119) P/N 761-882 – PA-28-161 Warrior III (Serial Number 2842001 & up) P/N 761-829 – PA-28-161 Cadet P/N 753-586 – PA-28-140, PA-28-150, PA-28-160, PA-28-180, & PA-28-235 Cherokee, PA-28R-180, & PA-28R-200 Cherokee Arrow & Arrow II P/N 761-679 – PA-28-181 Archer II and Archer III P/N 761-883 – PA-28-181 Archer III (Serial Number 2843001 & up) P/N 761-702 – PA-28-201T Turbo Dakota P/N 761-681 – PA-28-236 Dakota P/N 761-639 – PA-28R-201 Arrow III & PA-28R-201T Turbo Arrow III (Serial numbers 28R-7737001 thru 28R-7837317 and 2837001 thru 2837061) P/N 761-895 – PA-28R-201 Arrow (Serial No.s 2844001 & up, 2881001 & up) P/N 761-694 – PA-28RT-201 & PA-28R-201T Arrow IV & Turbo Arrow IV (ii) Current service Information: Service Bulletins and Service Letters – P/N 1762-331 (iii) Illustrated Parts Catalogue: P/N 761-538 – PA-28-151 & PA-28-161 Warrior I, Warrior II, & Warrior III P/N 761-897 – PA-28-161 Warrior III (Serial Number 2842001 & up) P/N 761-828 – PA-28-161 Cadet P/N 753-582 – PA-28-140, PA-28-150, PA-28-160, PA-28-180 & PA-28-235 Cherokee, PA-28R-180 & PA-28R-200 Cherokee Arrow & Arrow II P/N 761-678 – PA-28-181 Archer, Archer II, Archer III (III ending S/N 2890231) P/N 761-898 – PA-28-181 Archer III (Serial Number 2843001 & up) P/N 761-701 – PA-28-201T Turbo Dakota P/N 761-680 – PA-28-236 Dakota Type Acceptance Report Rev.2 : 8 July 2019 TAR 99/21B/31 – Piper PA-28 Series 11 P/N 761-638 – PA-28R-201 & PA-28R-201T Arrow III & Turbo Arrow III P/N 761-894 – PA-28R-201 Arrow III (Serial Number 2844001 & up) P/N 761-693 – PA-28RT-201 & -201T Arrow IV & Turbo Arrow IV (7) Agreement from manufacturer to supply updates of data in (5), and (6): Letter from New Piper Inc. FAA/DOA Coordinator dated 10 December 1998 CAA 2171 – New Piper Director of Aircraft Certification Services dated 14-8-02 Piper now provides CAA access to publications through the NAA portal (8) Other information: PA-28-181 Archer III Equipment List – S/N 2843112 and Up. Engineering Order 101311 – Installation Nav & Comm Antenna PA-28-181 Report VB-712 Section II – PA-28-181 III 28V Electrical System Substantiation Type Acceptance Report TAR 99/21B/31 – Piper PA-28 Series Rev.2 : 8 July 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. CAR 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: CAR Part 91 – Subpart F – Instrument and Equipment Requirements PARA: REQUIREMENT: MEANS OF COMPLIANCE: 91.505 Shoulder Harness if Aerobatic; >10 pax; Flight Training CAR §3.715 91.507 Pax Information Signs - Smoking, safety belts fastened Not Applicable – Less than ten passenger seats 91.509 Minimum Instruments and Equipment (1) ASI (2) Machmeter (3) Altimeter (4) Magnetic Compass (5) Fuel Contents (6) Engine RPM (7) Oil Pressure CAR §3.655(a)(1) N/A – No mach no. limitations CAR §3.655(a)(2) CAR §3.655(a)(3) CAR §3.655(b)(1)(i) 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 engine CAR §3.655(b)(1)(iii) CAR §3.655(b)(2)(v) CAR §3.655(b)(2)(iii) Spring-loaded lever position CAR §3.359 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 Not Applicable – Less than 10 passenger seats 91.529 ELT – TSO C126 after 1 July 2008 Operational requirement – Compliance as applicable 91.531 Oxygen Indicators - Volume/Pressure/Delivery Operational requirement – Compliance as applicable 91.533 Oxygen for Non-Pressurised Aircraft Operational requirement – Compliance as applicable 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 Compliance of factory installation to be determined CAR Part 135 – Subpart F – Instrument and Equipment Requirements PARA: REQUIREMENT: MEANS OF COMPLIANCE: 135.355 Seating and Restraints – Shoulder harness flight-crew seats Operational requirement – Compliance as applicable 135.357 Additional Instruments (Powerplant and Propeller) Operational requirement – Compliance as applicable 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 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 that date and 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. Type Acceptance Report Rev.2 : 8 July 2019 TAR 99/21B/31 – Piper PA-28 Series 13 Attachments The following documents form attachments to this report: Photographs first-of-type example serial number 28-43213 ZK-NEW Three-view drawing Piper Model PA-28-181 Archer III Photographs first-of-type example serial number 28R-7803237 ZK-REC Three-view drawing Piper Model PA-28R-201T Turbo Arrow III Photographs first-of-type example serial number 2842165 ZK-EBW Three-view drawing The New Piper Model PA-28-161 Warrior III Photographs first-of-type example serial number 28R-35725 ZK-RTE Piper Drawing 76101B – General Arrangement PA28R-200 (Arrow II) Copy of FAA Type Certificate/Type Certificate Data Sheet No. 2A13 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: PA-28-140, PA-28-160 AC 21-1.2/NZCAR Part 21 Appendix A(c) PA-28-151, PA-28-180 AC 21-1.2/NZCAR Part 21 Appendix A(c) PA-28-161 (1976-93) AC 21-1.2/NZCAR Part 21 Appendix A(c) PA-28-181 (1975-93) AC 21-1.2/NZCAR Part 21 Appendix A(c) PA-28R-180 AC 21-1.2/NZCAR Part 21 Appendix A(c) PA-28R-200 (1972-76) AC 21-1.2/NZCAR Part 21 Appendix A(c) PA-28R-201 (1977-78) AC 21-1.2/NZCAR Part 21 Appendix A(c) PA-28RT-201T AC 21-1.2/NZCAR Part 21 Appendix A(c) PA-28-235 (1963-76) AC 21-1.2/NZCAR Part 21 Appendix A(c) PA-28-236 (1978-93) AC 21-1.2/NZCAR Part 21 Appendix A(c) PA-28-181 (1995 on) Airwork Holdings Limited 99/21B/31 30 March 1999 PA-28R-201T (1977-78) M J Newcombe 2/21B/6 20 December 2001 PA-28-161 (1995 on) The New Piper Aircraft Inc. 3/21B/3 3 September 2002 PA-28R-200 (1969-71) Flight Care Limited 9/21B/5 20 October 2008 PA-28-181 (G1000NXi) Piper Aircraft, Inc. 18/21B/40 30 May 2018 PA-28 all other variants Piper Aircraft, Inc. 18/21B/40 8 July 2019 except PA-28S versions