# STC SA00161BO - Type: Supplemental type certificate - Status: Current, Amended - Holder: Avidyne Corporation, United States - Description: Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display. - Applied: September 10, 2002 - Status date: February 8, 2005 - Product: Aircraft, Single-Engine - Certification basis: Part 5, Part 14, Part 21, Part 23, Part 25, Part 27, Part 29, Part 50, Part 65, Part 140, Part 185 - Data sheets: [TCDS A17WE](https://openairdocs.org/tcds/A17WE), [TCDS 1A3](https://openairdocs.org/tcds/1A3), [TCDS 3A10](https://openairdocs.org/tcds/3A10), [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 3A17](https://openairdocs.org/tcds/3A17), [TCDS 3A19](https://openairdocs.org/tcds/3A19), [TCDS 3A21](https://openairdocs.org/tcds/3A21), [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS 3A25](https://openairdocs.org/tcds/3A25), [TCDS 5A2](https://openairdocs.org/tcds/5A2), [TCDS 5A6](https://openairdocs.org/tcds/5A6), [TCDS A-790](https://openairdocs.org/tcds/A-790), [TCDS A-799](https://openairdocs.org/tcds/A-799), [TCDS A13CE](https://openairdocs.org/tcds/A13CE), [TCDS A16CE](https://openairdocs.org/tcds/A16CE), [TCDS A1WI](https://openairdocs.org/tcds/A1WI), [TCDS A20CE](https://openairdocs.org/tcds/A20CE), [TCDS A2CE](https://openairdocs.org/tcds/A2CE), [TCDS A34CE](https://openairdocs.org/tcds/A34CE) and 48 more - Certificate PDF: https://openairdocs.org/files/sha256/b5/28/b528c676e8319c728ca1aeae487107104cb9f7851f1f84daf7b4b17f5e9bb9dd - Approved model list and other attachments: [SA00161BOAML.pdf](https://openairdocs.org/files/sha256/ee/26/ee2638add3cd77eef87339e55c2d385ccb8d0da1065788e951f9227308e94082) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7AFE614651F15E70862570530051A046.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00161BO ## ADs that name it (0) None. ## Approved models (562, first 50) - Aerostar Aircraft Corporation PA-60-600 (Aerostar 600) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE)) - Aerostar Aircraft Corporation PA-60-601 (Aerostar 601) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE)) - Aerostar Aircraft Corporation PA-60-601P (Aerostar 601P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE)) - Aerostar Aircraft Corporation PA-60-602P (Aerostar 602P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE)) - Aerostar Aircraft Corporation PA-60-700P (Aerostar 700P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE)) - Alexandria Aircraft LLC 14-19 ([TCDS 1A3](https://openairdocs.org/tcds/1A3)) - Alexandria Aircraft LLC 14-19-2 ([TCDS 1A3](https://openairdocs.org/tcds/1A3)) - Alexandria Aircraft LLC 14-19-3 ([TCDS 1A3](https://openairdocs.org/tcds/1A3)) - Alexandria Aircraft LLC 14-19-3A ([TCDS 1A3](https://openairdocs.org/tcds/1A3)) - Alexandria Aircraft LLC 17-30 ([TCDS 1A3](https://openairdocs.org/tcds/1A3)) - Alexandria Aircraft LLC 17-31 ([TCDS 1A3](https://openairdocs.org/tcds/1A3)) - Alexandria Aircraft LLC 17-31TC ([TCDS 1A3](https://openairdocs.org/tcds/1A3)) - Bombardier Inc. DHC-6-1 ([TCDS A9EA](https://openairdocs.org/tcds/A9EA)) - Bombardier Inc. DHC-6-100 ([TCDS A9EA](https://openairdocs.org/tcds/A9EA)) - Bombardier Inc. DHC-6-200 ([TCDS A9EA](https://openairdocs.org/tcds/A9EA)) - Bombardier Inc. DHC-6-300 ([TCDS A9EA](https://openairdocs.org/tcds/A9EA)) - Fairchild Aircraft Corporation SA226-AT ([TCDS A5SW](https://openairdocs.org/tcds/A5SW)) - Fairchild Aircraft Corporation SA226-T ([TCDS A5SW](https://openairdocs.org/tcds/A5SW)) - Fairchild Aircraft Corporation SA226-T(B) ([TCDS A5SW](https://openairdocs.org/tcds/A5SW)) - Fairchild Aircraft Corporation SA226-TC ([TCDS A8SW](https://openairdocs.org/tcds/A8SW)) - Fairchild Aircraft Corporation SA227-AC (C-26A) ([TCDS A8SW](https://openairdocs.org/tcds/A8SW)) - Fairchild Aircraft Corporation SA227-AT ([TCDS A5SW](https://openairdocs.org/tcds/A5SW)) - Fairchild Aircraft Corporation SA227-BC (C-26A) ([TCDS A8SW](https://openairdocs.org/tcds/A8SW)) - Fairchild Aircraft Corporation SA227-CC ([TCDS A18SW](https://openairdocs.org/tcds/A18SW)) - Fairchild Aircraft Corporation SA227-DC (C-26B) ([TCDS A18SW](https://openairdocs.org/tcds/A18SW)) - Fairchild Aircraft Corporation SA227-PC ([TCDS A8SW](https://openairdocs.org/tcds/A8SW)) - Fairchild Aircraft Corporation SA227-TT ([TCDS A5SW](https://openairdocs.org/tcds/A5SW)) - Fairchild Aircraft Corporation SA26-AT ([TCDS A5SW](https://openairdocs.org/tcds/A5SW)) - Fairchild Aircraft Corporation SA26-T ([TCDS A5SW](https://openairdocs.org/tcds/A5SW)) - Learjet Inc. 23 ([TCDS A5CE](https://openairdocs.org/tcds/A5CE)) - Mitsubishi Heavy Industries Ltd. MU-2B ([TCDS A2PC](https://openairdocs.org/tcds/A2PC)) - Mitsubishi Heavy Industries Ltd. MU-2B-10 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC)) - Mitsubishi Heavy Industries Ltd. MU-2B-15 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC)) - Mitsubishi Heavy Industries Ltd. MU-2B-20 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC)) - Mitsubishi Heavy Industries Ltd. MU-2B-25 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-25 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC)) - Mitsubishi Heavy Industries Ltd. MU-2B-26 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-26 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC)) - Mitsubishi Heavy Industries Ltd. MU-2B-26A ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-30 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC)) - Mitsubishi Heavy Industries Ltd. MU-2B-35 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-35 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC)) - Mitsubishi Heavy Industries Ltd. MU-2B-36 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-36 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC)) - Mitsubishi Heavy Industries Ltd. MU-2B-36A ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-40 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mitsubishi Heavy Industries Ltd. MU-2B-60 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW)) - Mooney Aircraft Corporation M20 ([TCDS 2A3](https://openairdocs.org/tcds/2A3)) - Mooney Aircraft Corporation M20A ([TCDS 2A3](https://openairdocs.org/tcds/2A3)) - Mooney Aircraft Corporation M20B ([TCDS 2A3](https://openairdocs.org/tcds/2A3)) All 562: https://openairdocs.org/stc/SA00161BO/models.md ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. FAA Form 8110-2(10-68) Page 1 of 1 Number SA00161BO This Certificate issued to Avidyne Corporation 55 Old Bedford Road Lincoln, Massachusetts 01773 Part 23 of the Federal Aviation Regulations. Original Product Type Certificate Number : See attached FAA Approved Model List (AML), Document No. AVMFC-076, Rev (D), dated February 08, 2005, or later FAA ed revisions for the list of approved airplane models and applicable regulations. Make : approv Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display in accordance with Avidyne Corporation Master Document List, Document No. AVMFD-088, Revision 09, dated February 4, 2005, or later FAA-approved revisions. 1. The FlightMax EX500 Multi-Function Display integrates with separately approved system installations. Adherence to the limitations in the appropriate Aircraft Flight Manual Supplements for those systems is mandatory. 2. Instructions for Continued Airworthiness (ICA), Avidyne Corporation Document AVMFD-083, Revision 05, dated October 15, 2004 or later FAA accepted revision shall be made available to the operator at the time of installation. 3. Compatibility of this design with previously approved modifications must be determined by the installer. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. Date of application : September 10, 2002 Date of issuance : February 6, 2003 Date reissued : Date amended : February 8, 2005 ( Signature) Robert G. Mann Manager Boston Aircraft Certification Office ( Title) ### SA00161BOAML.pdf Avidyne 700-00007-XXX-() MFD Approved Model List STC No. SA00161BO AVIDYNE CORPORATION 55 Old Bedford Road Lincoln, MA 01773 FAA Approved: ______________________ Robert G Mann, Manager Boston Aircraft Certification Office Federal Aviation Administration Burlington, MA AVMFC-076 Avidyne 700-00007-XXX-() MFD Approved Model List STC No. SA00161BO Page 1 of 10 FAA Approved Date: __ _____ AVMFC-076 Avidyne 700-00007-XXX-() MFD Approved Model List STC No. SA00161BO Log Of Revisions Revision Number Revised Pages Description of Revisions FAA Approval Date (-) ALL Initial Release See Page 1 for Signature Feb. 06, 2003 (A) 7 Addition of New Piper Aircraft model PA-46-500TP R. G. Mann March 18, 2003 (B) 5 Addition of PA-60-602P (Aerostar 602P) R. G. Mann April 4, 2003 (C) ALL Addition of Diamond DA-40, Lancair LC40-550FG, LC42- 550FG, Class III aircraft w/ associated Notice changes. R. G. Mann September 5, 2003 (D) 4 5, 6 Update AFMS reference Addition of Cessna 182T, T182T, P206-series, TP206- series, T303; correction of miscellaneous typographical errors Page 2 of 10 FAA Approved Date: __ _____ AVMFC-076 Avidyne 700-00007-XXX-() MFD Approved Model List STC No. SA00161BO Table of Contents 1. Introduction … 4 2. Approved Model List – Part 23 Class I and Class II … 5 3. Approved Model List – Part 23 Class III … 9 Page 3 of 10 FAA Approved Date: __ _____ AVMFC-076 Avidyne 700-00007-XXX-() MFD Approved Model List STC No. SA00161BO 1. Introduct ion This document is the FAA Approved Model List for STC No. SA00161BO for the installation of the Avidyne 700-00007-XXX-() Multi-Function Display into eligible aircraft. Revisions to the AML must be coordinated through the STC holder, and require FAA approval. IMPORTANT NOTICE This STC is only applicable to the 14 CFR Part 23 Class I, II, and III aircraft, as defined in Advisory Circular AC 23.1309-1C, which are listed in this AML. When installed in Class III aircraft, an independent lightning detection and display system complying to TSO-C110a must also be installed for operations in IMC and FAA Approved Flight Manual Supplement, Document 600-00083- 001 Rev (A), or later FAA approved revision is required and must be carried aboard the aircraft during all flights. Installation in 14 CFR Part 23 Class IV, Part 25, Part 27 and Part 29 aircraft are not authorized under this STC. Page 4 of 10 FAA Approved Date: __ _____ AVMFC-076 Avidyne 700-00007-XXX-() MFD Approved Model List STC No. SA00161BO 2. Approved Model List – Part 23 Class I and Class II Aircraft Make Aircraft Model(s) Type Certificate Number Certification Basis Aerostar Aircraft Corporation PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P), PA-60-602P (Aerostar 602P) A17WE 14 CFR Part 23 14-19,. 14-19-2, 14-19-3, 14-19-3A, 17-30, 17-31, 17-31TC 1A3 CAR 3 Alexandria Aircraft 17-30A, 17-31A, 17-31ATC A18CE 14 CFR Part 23 140A 5A2 CAR 3 Cessna Aircraft Company 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, 150L, A150L, 150M, A150K, A150M 152, A152 3A19 CAR 3 170, 170A, 170B A-799 CAR 3 172, 172A, 172B, 172C, 172D, 172E, 172F, 172G, 172H, 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S, 3A12 CAR 3, 14 CFR Part 23 172RG, P172D, R172E, R172F, R172G, R172H, R172J, R172K 175, 175A, 175B, 175C 3A17 CAR 3 177, 177A, 177B A13CE 14 CFR Part 23 177RG A20CE 14 CFR Part 23 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K 5A6 CAR 3 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, 182S, 182T, R182, T182, T182T, TR182 3A13 CAR 3, 14 CFR Part 23 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F 3A24 CAR 3 190 195, 195A, 195B A-790 CAR 3 206, 206H, P206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C, TP206D, TP206E, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, T206H, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G A4CE CAR 3, 14 CFR Part 23 Page 5 of 10 FAA Approved Date: __ _____ AVMFC-076 Avidyne 700-00007-XXX-() MFD Approved Model List STC No. SA00161BO Aircraft Make Aircraft Model(s) Type Certificate Number Certification Basis 207, 207A, T207, T207A A16CE 14 CFR Part 23 Cessna Continued 210, 210A, 210B, 210C, 210D, 210E, 210F, 210G, 210H, 210J, 210K, 210L, 210M, 210N, 210R, 210-5 (205), 210-5A (205A), P210N, P210R, T210F, T210G, T210H, T210J, T210K, T210L, T210M, T210N, T210R 3A21 CAR 3 T303 A34CE 14 CFR Part 23 310, 310A (USAF U-3A), 310B, 310C, 310D, 310E (USAF U-3B), 310F, 310G, 310H, 310I, 310J, 310J-1, 310K, 310L, 310N, 310P, E310H, E310J, T310P, 310Q, T310Q, 310R, T310R 3A10 CAR 3 320, 320-1, 320A, 320B, 320C, 320D, 320E, 320F 340, 340A, 335, 340, 340A 3A25 CAR 3 336 A2CE CAR 3 337, 337A (USAF O2B), 337B, 337C, 337D, 337E, 337F, 337G, 337H, M337B (USAF O2A), P337H, T337B, T337C, T337D, T337E, T337F, T337G, T337H, T337H-SP A6CE CAR 3, 14 CFR Part 23 Commander Aircraft 112, 114, 112TC, 112B, 112TCA, 114A, 114B, 114TC A12SO CAR 3 de Havilland Inc. DHC-2 Mk. I, DHC-2 Mk. II, DHC-2 Mk. III A-806 CAR 3 DA 20-A1, DA20-C1 TA4CH 14 CFR Part 23 Diamond Aircraft Industries DA40 A47CE 14 CFR Part 21, 14 CFR Part 23 Maule Aerospace Technology, Inc. Bee Dee M-4, M-5-180C, MXT-7-160, M-4, M-5-200, MX-7-180A, M-4C, M-5-210C, MXT-7-180, M-4S, M-5-210TC, MX-7-180B, M-4T, M-5-220C, MXT-7-420, M-4-180C, M- 5-235C, M-7-235B, M-4-180S, M-6-180, M- 7-235A, M-4-180T, M-6-235, M-7-235C M- 4-210 M-7-235 MX-7-180C, M-4-210C, MX- 7-235, M-7-260, M-4-210S MX-7-180 MT-7- 260, M-4-210T, MX-7-420, M-7-260C, M-4-220, MXT-7-180, M-7-420AC, M-4- 220C, MT-7-235, MX-7-160C, M-4-220S, M- 8-235, MX-7-180AC, M-4-220T, MX-7-160 3A23 CAR 3 Page 6 of 10 FAA Approved Date: __ _____ AVMFC-076 Avidyne 700-00007-XXX-() MFD Approved Model List STC No. SA00161BO Aircraft Make Aircraft Model(s) Type Certificate Number Certification Basis Mooney Aircraft Corp. M20, M20A, M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, M20R, M20S 2A3 CAR 3 M22 A6SW CAR 3 Partenavia Costruzioni Aeronauticas S.p.A. P 68, P 68B, P 68C, P 68C-TC, P 68 "OBSERVER", AP68 TP series 300, P68TC "OBSERVER", AP68TP 600, P68 "OBSERVER 2" A31EU 14 CFR Part 23 The Lancair Company LC40-550FG, LC42-550FG A00003SE 14 CFR Part 23 The New Piper Aircraft, Inc. PA-28-160, PA-28-150, PA-28-180, PA- 28S-160, PA-28S-180, PA-28-235, PA-28- 140 2 PCLM, PA-28-140 4 PCLM, PA-28R- 180, PA-28R-200, PA-28R-200, PA-28-180, PA-28-235, PA-28-151, PA-28-181, PA-28- 181, PA-28-161, PA-28-161, PA-28-161, PA-28R-201, PA-28R-201T, PA-28-236, PA-28RT-201, PA-28RT-201, PA-28RT- 201T, PA-28-201T 2A13 CAR 3 PA-32-260, PA-32-300, PA-32S-300, PA- 32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301, PA-32R-301, PA-32R-301T, PA-32-301, PA-32-301T, PA-32R-301T A3SO CAR 3 PA-23, PA-23-160, PA-23-250 (Navy UO-1), PA-23-235, PA-E23-250, PA-23-250 1A10 CAR 3 PA-30, PA-39, PA-40 A1EA CAR 3 PA-24-250, PA-24-260, PA-24-400 1A15 CAR 3 PA-34-200, PA-34-200T, PA-34-220T, PA- 34-220T, PA-34-220T A7SO CAR 3 PA-44-180, PA-44-180, PA-44-180T A19SO 14 CFR Part 23 PA-38-112 A18SO 14 CFR Part 23 PA-46-310P, PA-46-350P, PA-46-500TP A25SO 14 CFR Part 23 Page 7 of 10 FAA Approved Date: __ _____ AVMFC-076 Avidyne 700-00007-XXX-() MFD Approved Model List STC No. SA00161BO Aircraft Make Aircraft Model(s) Type Certificate Number Certification Basis Raytheon Aircraft Company 19A, B23, B19, C23, M19A, A24, 23 A24R, A23, B24R, A23A, C24R, A23-19, A23-24 A1CE CAR 3 H35, J35, K35, M35, 35-33, N35, 35-A355, 35-B33, P35, S35, 35-C33, E33, F33, V35, V35A, V35B, 35-C33A, E33A, E33C, 36, A36, F33A, F33C, G33, A36TC, B36TC 3A15 CAR 3 95, B95, 95-55 and 95-A55, B95A, D95A and E95, 95-B55 and 95-B55A, 95-B55B, 95-C55, D55, 95-C55A, D55A, E55 and E55A, 56TC and A56TC, 58 and 58A 3A16 CAR 3 58P and 58PA, 58TC and 58TCA A23CE 14 CFR Part 23 50 (L-23A), B50 (L-23B) 5A4 CAR 3 REVO, Incorporated Colonial C-1, Colonial C-2, Lake LA-4, LA- 4A, LA-4P, Lake LA-4-200, Lake 250 1A13 CAR 3, 14 CFR Part 23 SOCATA - Groupe AEROSPATIALE TB 20, TB 10, TB 21, TB9, TB 200 A51EU 14 CFR Part 23 Tiger Aircraft (American General) AA-1, AA-1A, AA-1B, AA-1C A11EA 14 CFR Part 23 AA-5, AA-5A, AA-5B, AG-5B A16EA 14 CFR Part 23 Twin Commander 500, 520, 560, 560-A 6A1 CAR 3 Page 8 of 10 FAA Approved Date: __ _____ AVMFC-076 Avidyne 700-00007-XXX-() MFD Approved Model List STC No. SA00161BO 3. Approved Model List – Part 23 Class III Aircraft Make Aircraft Model(s) Type Certificate Number Certification Basis Aerostar Aircraft Corporation PA-60-700P (Aerostar 700P) A17WE 14 CFR Part 23 Cessna Aircraft Company 208, 208A, 208B A37CE 14 CFR Part 23 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 425 A7CE CAR3 404, 406 A25CE 14 CFR Part 23 441 A28CE 14 CFR Part 23 501, 551 A27CE 14 CFR Part 23 525, 525A A1W1 14 CFR Part 23 De Havilland Inc. (Twin Otter) DHC-6-1, DHC-6-100, DHC-6- 200, DHC-6-300 A9EA CAR3 Fairchild SA26-T, SA26-AT, SA226-T, SA226-AT, SA226-T(B), SA227-AT, SA227-TT A5SW CAR3 SA-226-TC, SA227-AC (C-26A), SA227-BC (C-26A), SA227-PC A8SW 14 CFR Part 23 SA227-CC, SA227-DC A18SW 14 CFR Part 23 Learjet 23 A5CE CAR3 Mitsubishi Heavy Industries, Ltd. MU-2B, MU-2B-10, MU-2B-20, MU-2B-15, MU-2B-30, MU-2B-35, MU-2B-25, MU-2B- 36, MU-2B-26 A2PC CAR 3 MU-2B-25, MU-2B-35, MU-2B-26, MU-2B- 36, MU-2B-26A, MU-2B-36A, MU-2B-40, MU-2B-60 A10SW CAR 3 Partenavia Costruzioni Aeronauticas S.p.A. “SPARTACUS”, AP68TP 600 “VIATOR”, VA300 A31EU 14 CFR Part 23 Piaggio Aero Industries S.p.A. P-180 A59EU 14 CFR Part 23 Pilatus Aircraft Limited PC-12, PC-12/45 A78EU 14 CFR Part 23 Page 9 of 10 FAA Approved Date: __ _____ AVMFC-076 Avidyne 700-00007-XXX-() MFD Approved Model List STC No. SA00161BO Aircraft Make Aircraft Model(s) Type Certificate Number Certification Basis PC-6, PC-6-H1, PC-6-H2, PC-6/350, PC- 6/350-H1, PC-6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC- 6/B2-H2, PC-6/B2-H4, PC-6/C-H2, PC-6/C1- H2 7A15 CAR3 The New Piper Aircraft, Inc. PA-31, PA-31-300, PA-31-325, PA-31-350 A20SO CAR3 PA-31P, PA-31T, PA-31T1, PA-31T2, PA- 31T3, PA-31P-350 A8EA CAR3 PA-42, PA-42-720, PA-42-720R, PA-42- 1000 A23SO 14 CFR Part 23 Raytheon Aircraft Company 200 (A100-1 (U-21J)), 200C, 200CT, 200T, A200 (C-12A) or (C-12C), A200C (UC-12B), A200CT (C-12D) or (FWC-12D) or (RC-12D) or (C-12F) or (RC-12G) or (RC-12H) or (RC- 12K) or (RC-12P) B200, B200C (C-12F) or (UC-12F) or (UC-12M), or (C-12R), B200CT, B200T, 300, B300, B300C, 300LW, 1900, 1900C (C-12J), 1900D A24CE 14 CFR Part 23 A100 (U-21F), A100A, A100C, B100 A14CE 14 CFR Part 23 F90 A31CE 14 CFR Part 23 E50 (L-23D, RL-23D), C50, F50, D50 (L- 23E), G50, D50A H50, D50B, J50, D50C, D50E, D50E-5990 5A4 CAR 3 60, A60, B60 A12CE 14 CFR Part 23 65, 65-A90-1, A65, 65-A90-2, A65-8200, 65- A90-3, 65-80, 65-A90-4, 65-A80, 65-A80- 8800, 65-B80, 65-88, 65-90, 65-A90, 70, B90, C90, C90A, E90, H90 3A20 CAR3, 14 CFR Part 23 SOCATA - Groupe AEROSPATIALE TBM 700 A60EU 14 CFR Part 23 Twin Commander 560-F, 681, 680, 690, 680E, 685, 680F, 690A, 720, 690B, 680FL, 690C, 680FL(P), 690D, 680T, 695, 680V, 695A, 680W, 695B 2A4 CAR 3 500-A, 500-B, 500-U, 560-E, 500-S 6A1 CAR 3 700 A12SW 14 CFR Part 23 Page 10 of 10 ## Every issue (2) - February 8, 2005: Amended, Current. [certificate](https://openairdocs.org/files/sha256/b5/28/b528c676e8319c728ca1aeae487107104cb9f7851f1f84daf7b4b17f5e9bb9dd), [SA00161BOAML.pdf](https://openairdocs.org/files/sha256/ee/26/ee2638add3cd77eef87339e55c2d385ccb8d0da1065788e951f9227308e94082) - February 7, 2005: Amended, Current. [certificate](https://openairdocs.org/files/sha256/b5/28/b528c676e8319c728ca1aeae487107104cb9f7851f1f84daf7b4b17f5e9bb9dd), [SA00161BOAML.pdf](https://openairdocs.org/files/sha256/ee/26/ee2638add3cd77eef87339e55c2d385ccb8d0da1065788e951f9227308e94082) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.