# STC SA02015CH - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Alpha Aviation Inc, United States - Description: Installation of Three-Point Torso Restraint System. - Applied: May 1, 2004 - Status date: December 20, 2016 - Product: Aircraft, Small Airplane - Certification basis: Part 21 - Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13), [TCDS A3SO](https://openairdocs.org/tcds/A3SO) - Certificate PDF: https://openairdocs.org/files/sha256/72/9f/729f8d84b5bf2fba85ba8bf1a8812a066bedc092a360fdfcbc79c480bdc91dcb - Approved model list and other attachments: [SA02015CH_AML.pdf](https://openairdocs.org/files/sha256/21/36/2136564de3e8d125719de98070eae0852dc7715c9f7bd4ac82b5a5fb0cc2c71e) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/175D1A15C2BA28828625809900597333.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02015CH ## ADs that name it (0) None. ## Approved models (12) - Piper Aircraft Inc. PA-32-260 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - Piper Aircraft Inc. PA-32S-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO)) - The New Piper Aircraft Inc. PA-28-140 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - The New Piper Aircraft Inc. PA-28-150 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - The New Piper Aircraft Inc. PA-28-160 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - The New Piper Aircraft Inc. PA-28-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - The New Piper Aircraft Inc. PA-28-235 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - The New Piper Aircraft Inc. PA-28R-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - The New Piper Aircraft Inc. PA-28R-200 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - The New Piper Aircraft Inc. PA-28S-160 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) - The New Piper Aircraft Inc. PA-28S-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13)) ## 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. Part * of the *Regulations Installation of a Three Point Torso Restraint System in accordance with Alpha Aviation Inc. Installation and Maintenance Manual as listed on AML SA02015CH, reissued December 20, 2016, or later FAA Approved revisions. 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. A copy of this Certificate and FAA Approved Model List (AML) No. SA02015CH, reissued December 20, 2016, or later FAA approved revisions, must be maintained as part of the permanent records for the modified aircraft. 3. The Three Point Torso Restraint System installation is to be inspected and maintained in accordance with Alpha Aviation Inc. Installation and Maintenance Manual as listed on AML SA02015CH, reissued December 20, 2016, or later FAA Approved revisions 4. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. Alpha Aviation, Inc. 1500 E Main St Owatonna, MN 55060 * (see attached FAA Approved Model Make :* List (AML) No. SA02015CH for list of Model :* Approved models and applicable airworthiness regulations) Date of application : May 01, 2004 Date of issuance : July 30, 2004 Date reissued :December 20, 2016 Date amended : October 05, 2005 (Signature) Karol Mordasiewicz Manager, Airframe & Administrative Branch Chicago Aircraft Certification Office (Title) Original signed by: Gregory J. Michalik FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES Number ### SA02015CH_AML.pdf **FAA APPROVED MODEL LIST (AML) NO. SA02015CH ALPHA AVIATION INC.** FOR INSTALLING THREE POINT TORSO RESTRAINT SYSTEM ISSUE DATE: 10/5/05 **ITEM** **AIRCRAFT** **AIRCRAFT** **ORIGINAL TYPE** **CERTIFICATION BASIS** **INSTALLATION** **INSTRUCTIONS** AFM AML **MAKE MODEL CERTIFICATE NUMBER FOR** **ALTERATION** **NUMBER** **REVISION NO. & DATE** **SUPPLEMENT** **NUMBER/DATE** **AMENDMENT DATE** Page 1 of 1 1 Piper PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-28R-180, PA-28R-200, PA-28S-160, PA-28S-180 2A13 CAR 3 Installation and Maintenance Manual No. PA285001 Revision B, dated 5/14/04* N/A -- 2 Piper PA-32-260, PA-32-300, PA-32S-300 A3SO CAR 3 Installation and Maintenance Manual No. PA285001 Revision D, dated 9/1/05* N/A -- * or latter FAA Approved Revisions. FAA APPROVED: Karol Mordasiewicz Manager, Airframe & Administrative Branch Chicago Aircraft Certification Office Reissued: 12/20/16 Original signed by: Gregory J. Michalik ## Every issue (2) - December 20, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/72/9f/729f8d84b5bf2fba85ba8bf1a8812a066bedc092a360fdfcbc79c480bdc91dcb), [SA02015CH_AML.pdf](https://openairdocs.org/files/sha256/21/36/2136564de3e8d125719de98070eae0852dc7715c9f7bd4ac82b5a5fb0cc2c71e) - July 30, 2004: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/cb/13/cb13888987f576a4bef2aeaf888193280d73c088b74cea2c8e84bf767337d1ea) --- 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.