# STC SA00149BO - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Aircraft Components Inc, United States - Description: Installation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1 - Applied: October 18, 2001 - Status date: February 29, 2016 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A17WE](https://openairdocs.org/tcds/A17WE), [TCDS 1A3](https://openairdocs.org/tcds/1A3), [TCDS A18CE](https://openairdocs.org/tcds/A18CE), [TCDS A1CE](https://openairdocs.org/tcds/A1CE), [TCDS 3A15](https://openairdocs.org/tcds/3A15), [TCDS A-777](https://openairdocs.org/tcds/A-777), [TCDS 3A16](https://openairdocs.org/tcds/3A16), [TCDS A23CE](https://openairdocs.org/tcds/A23CE), [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A12SO](https://openairdocs.org/tcds/A12SO), [TCDS A11SO](https://openairdocs.org/tcds/A11SO), [TCDS 2A8](https://openairdocs.org/tcds/2A8), [TCDS 3A23](https://openairdocs.org/tcds/3A23), [TCDS 2A3](https://openairdocs.org/tcds/2A3), [TCDS 1A6](https://openairdocs.org/tcds/1A6), [TCDS 1A10](https://openairdocs.org/tcds/1A10), [TCDS 1A15](https://openairdocs.org/tcds/1A15), [TCDS 2A13](https://openairdocs.org/tcds/2A13), [TCDS A1EA](https://openairdocs.org/tcds/A1EA), [TCDS A20SO](https://openairdocs.org/tcds/A20SO) and 25 more - Certificate PDF: https://openairdocs.org/files/sha256/8c/28/8c289ed9cb0ce18806c6ddf2d01b4b2e7acc72f3b3b22a284337abee098f1d77 - Approved model list and other attachments: [AML_SA00149BO.pdf](https://openairdocs.org/files/sha256/cd/f4/cdf4bb0b93d8a6214d020a50dc05d8d4c7a539f1be099617bf569f6d59d76854) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CF1E56D4F6DE479686257F68007099C5.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00149BO ## ADs that name it (0) None. ## Approved models (475, 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 17-30A ([TCDS A18CE](https://openairdocs.org/tcds/A18CE)) - Alexandria Aircraft LLC 17-31 ([TCDS 1A3](https://openairdocs.org/tcds/1A3)) - Alexandria Aircraft LLC 17-31A ([TCDS A18CE](https://openairdocs.org/tcds/A18CE)) - Alexandria Aircraft LLC 17-31ATC ([TCDS A18CE](https://openairdocs.org/tcds/A18CE)) - Alexandria Aircraft LLC 17-31TC ([TCDS 1A3](https://openairdocs.org/tcds/1A3)) - Beechcraft Corporation 19A ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - Beechcraft Corporation 23 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - Beechcraft Corporation 35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Beechcraft Corporation 35-33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation 35-A33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation 35-B33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation 35-C33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation 35-C33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation 35R ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Beechcraft Corporation 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Beechcraft Corporation 56TC ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Beechcraft Corporation 58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Beechcraft Corporation 58A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Beechcraft Corporation 58P ([TCDS A23CE](https://openairdocs.org/tcds/A23CE)) - Beechcraft Corporation 58PA ([TCDS A23CE](https://openairdocs.org/tcds/A23CE)) - Beechcraft Corporation 58TC ([TCDS A23CE](https://openairdocs.org/tcds/A23CE)) - Beechcraft Corporation 58TCA ([TCDS A23CE](https://openairdocs.org/tcds/A23CE)) - Beechcraft Corporation 65 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation 65-80 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation 65-88 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation 65-90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation 65-A80 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation 65-A90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation 65-B80 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation 70 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation 95 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Beechcraft Corporation 95-55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Beechcraft Corporation 95-A55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Beechcraft Corporation 95-B55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Beechcraft Corporation 95-B55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Beechcraft Corporation 95-B55B ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Beechcraft Corporation 95-C55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Beechcraft Corporation 95-C55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Beechcraft Corporation A23 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) - Beechcraft Corporation A23-19 ([TCDS A1CE](https://openairdocs.org/tcds/A1CE)) All 475: https://openairdocs.org/stc/SA00149BO/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. Number SA00149BO FAA Form 8110-2 (8/13) Page 1 of 3 This certificate issued to: Aircraft Components, Inc. 1700 Fostoria Avenue, Suite 300 Findlay, Ohio 45840 Part 23 of the Federal; Aviation Regulations. Installation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1, in accordance with Aircraft Components, Inc. Master Document List (MDL), Document Number MDL-2044, Revision 2, dated March 17, 2003, or later FAA approved revision. 1. Operation must be in accordance with the Aircraft Components, Inc. Aircraft Flight Manual Supplement (AFMS), Document Number AFMS-2044, Revision 1, FAA approved on May 15, 2003, or later FAA approved revision. The AFMS must be carried in the aircraft during all flights. (continued on Page 3 of 3) Date of Application: October 18, 2001 Date reissued: February 29, 2016 Date of Issuance: June 11, 2002 Date amended: May 15, 2003 Signature Robert G. Mann Manager, Boston Aircraft Certification Office Title See attached FAA Approved Model List (AML), Document No. 2044AML, Revision 0, dated May 15, 2003, or later FAA approved revision, for the list of approved airplane models, applicable installation data requirements, and specific limitations. **SUPPLEMENTAL TYPE CERTIFICATE, FAA FORM 8110-2 (CONTINUED)** FAA Form 8110-2 (8/13) Page 2 of 3 **TRANSFER** **ENDORSEMENT** To (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP Code) From (Name of grantor) (Address of grantor) (Number and street) (City, State, and ZIP Code) Number SA00149BO February 29, 2016 FAA Form 8110-2 (8/13) Page 3 of 3 Limitations and Conditions: (continued from Page 1 of 3) 2. Maintenance must be in accordance with Aircraft Components, Inc. Instructions for Continued Airworthiness (ICA), Document Number ICA-2044, Revision 1, dated May 10, 2003, or later FAA accepted revision. The ICA must 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. ------------------------------------------------------------END------------------------------------------------------- ### AML_SA00149BO.pdf FAA Approved Model List (AML) For Installation of P/N 2044-1 Volt & Vac Alert System per **STC SA00149BO** Specification 2044AML Rev 0 FAA Aproved _______________ Robert G. Mann, Manager Boston Aircraft Certification Office Burlington MA Date _________ Page 1 of 6 TABLE OF REVISIONS Rev No. Date Description of Revision and pages changed Approval FAA Approved _____________ Page 2 of 6 Item TC Holder Aircraft Model Type Certificate 1 Raytheon Aircraft Co. 19A, B19, M19A, 23, A23, A23A, A23-19, A23-24, B23, C23, A24, A24R, B24R, C24R A1CE 2 Raytheon Aircraft Co. 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 36, A36, A36TC, B36TC, See Note 1 3A15 3 Raytheon Aircraft Co. 58P, 58PA, 58TC, 58TCA See Note 1 A23CE 4 Raytheon Aircraft Co. 35, A35, B35, C35, D35, E35, F35, G35, 35R See Note 1 A-777 5 Raytheon Aircraft Co. B95A, D95A, E95, 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, D55A, E55, E55A, 56TC, A56TC, 58, 58A, 95, B95 See Note 1 3A16 6 Raytheon Aircraft Co. 65, A65, A65-8200, 65-80, 65-A80, 65-B80, 65-88, 65-90, 65-A90, 70, B90, C90, C90A, E90, H90 3A20 7 Bellanca Inc. 14-19, 14-19-2,14-19-3, 14-19-3A, 17-30, 17-31, 17-31TC 1A3 8 Bellanca Inc. 17-30A, 17-31A, 17-31ATC A18CE 9 The Cessna Aircraft Co. 172, 172A, 172B, 172C, 172D, 172E, 172F, 172G, 172H, 172I, 172K, 172L, 172M, 172N, 172P, 172Q, 172R 3A12 10 The Cessna Aircraft Co. 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, 182S, R182, 7182, TR182 3A13 11 The Cessna Aircraft Co. 172RG, 175, 175A, 175B, 175C, P172D, R172E, R172F, R172G, R172H, R172J, R172K 3A17 12 The Cessna Aircraft Co. 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H, 150J, 150K, A150K, 150L, A150L, 150M, 152, A152 3A19 13 The Cessna Aircraft Co. 210, 210A, 210B, 210C, 210D, 210E, 210F, T210F, 210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, T210M, 210N, P210N, T210N, 210R, P210R, T210R, 210-5, 210-5A 3A21 14 The Cessna Aircraft Co. 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F 3A24 15 The Cessna Aircraft Co. 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K 5A6 16 The Cessna Aircraft Co. 177, 177A, 177B A13CE FAA Approved ___________________ Page 3 of 6 Item TC Holder Aircraft Model Type Certificate 17 The Cessna Aircraft Co. 207, 207A, T207, T207A A16CE 18 The Cessna Aircraft Co. 177RG A20CE 19 The Cessna Aircraft Co. 208, 208A, 208B A37CE 20 The Cessna Aircraft Co. 206, P206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C, TP206D, TP206E, U206, U206A, U206B, U206C, U206D, U206E U206F U206G TU206A TU206B TU206C TU206D A4CE 21 The Cessna Aircraft Co. 310, 310A, 310B, 310C, 310D, 310E, 310F, 310G, 310H, E310H, 310I, 310J, 310K, 310L, 310N, 310P, T310P, 310Q, T310Q, 310R, T310R A310 22 The Cessna Aircraft Co. 320, 320-1, 320A, 320B, 320C, 320D, 320E, 320F, 335, 340, 340A 3A25 23 The Cessna Aircraft Co. 337, 337A, 337B, T337B, 337C, T337C, 337D, T337D, 337E, T337E, 337F, T337F, 337G, T337G, 337H, P337H, T337H A6CE 24 The Cessna Aircraft Co. 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 425 A7CE **25 COMMAND ER** **112, 114, 112TC, 112B, 112TCA, 114A, 114B, 114TC A12SO** 26 Tiger Aircraft LLC AA-5, AA-5A, AA-5B, AG-5B A16EA 27 Tiger Aircraft LLC 111 A11SO 28 Tiger Aircraft LLC AA-1, AA-1A, AA-1B, AA-1C A11EA 29 Maul Aerospace BEE DEE, M-4, M-4C, M-4S, M-4T, M-4-180C, M-4-180S, M-4-180T, M-4-210, M-4-210C, M-4-210S, M-4-210T, M-4-220, M-4-220C, M 4 220S M 4 220T M 5 180C M 5 200 M 5 210C M 5 210TC 3A23 30 Mooney Aircraft Corp. M-20, M-20A, M-20B, M-20C, M-20D, M-20E, M-20F, M-20G, M-20J, M-20K, M-20L, M-20M, M-20R, M-20S 2A3 FAA Approved _______________ Page 4 of 6 Item TC Holder Aircraft Model Type Certificate 31 The New Piper Aircraft Inc. PA-24, PA-24-250, PA-24-260, PA-24-400 1A15 32 The New Piper Aircraft Inc. PA-22, PA-22-108, PA-22-135, PA-22S-135, PA-22-150, PA-22S-150, PA-22-160, PA-22S-160 1A6 33 The New Piper Aircraft Inc. PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-28-151, PA-28-161, PA-28-181, PA-28R-201, PA-28R-201T, PA-28S-160, PA-28S-180, PA-28R-180, PA-28R-200, PA-28-201T, PA-28RT-201T, PA-28RT-201, PA-28-236 2A13 34 The New Piper Aircraft Inc. PA-25, PA-25-235, PA-25-260 2A8 35 The New Piper Aircraft Inc. PA-46-310P, PA-46-350P A25SO 36 The New Piper Aircraft Inc. PA-44-180, PA-44-180T A1960 37 The New Piper Aircraft Inc. PA-30, PA-39, PA-40 A1EA 38 The New Piper Aircraft Inc. PA-31, PA-31-300, PA-31-325, PA-31-350 A20SO 39 The New Piper Aircraft Inc. PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32R-301, PA-32R-301T, PA-32-301, PA-32-301T A3SO 40 The New Piper Aircraft Inc. PA-34-200, PA-34-200t, PA-34-220T A7SO 41 The New Piper Aircraft Inc. PA-23, PA-23-160, PA-23-235, PA-23-250 1A10 42 The New Piper Aircraft Inc. PA-60-600, PA-60-601, PA-60-601P, PA-60-602P, PA-60-700P A17WE 43 The New Piper Aircraft Inc. PA-31P, PA-31T, PA-31T1, PA-31T2, PA-31T3, PA-31P-350 A8EA FAA Approval __________________ Page 5of 6 Item TC Holder Aircraft Model Type Certificate 44 Twin Commander Aircraft Corp 560-F, 680, 680-E, 680-F, 720, 680FL, 680T, 680V, 680-W, 681, 690, 685, 690A, 690B, 690C, 690D, 695, 695A, 695B 2A4 45 Twin Commander Aircraft Corp 500, 500A, 500-B, 500-U, 520, 560, 560-A, 560-E, 500-S 6A1 Note 1: STC Applicable to aircraft with vacuum powered gyro instruments only. FAA Approval ________________ Page 6 of 6 ## Every issue (1) - February 29, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/8c/28/8c289ed9cb0ce18806c6ddf2d01b4b2e7acc72f3b3b22a284337abee098f1d77), [AML_SA00149BO.pdf](https://openairdocs.org/files/sha256/cd/f4/cdf4bb0b93d8a6214d020a50dc05d8d4c7a539f1be099617bf569f6d59d76854) --- 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.