# STC SA02483AK - Type: Supplemental type certificate - Status: Current, Issued - Holder: Trimmer Marvin E/Trimmer Aviation LLC, United States - Description: Installation of : (1) Cleveland 199-62 or 199-62A wheel and brake kit or ABI LLC AB-199-62 or ABI-199-62A wheel and brake kit on aircraft with 1.5" axles, OR (2) Cleveland wheel and brake kit 199-71 or ABI LLC ABI-199-71 kit on aircraft with 1.25" axles. - Applied: November 5, 2014 - Status date: March 1, 2017 - Product: Aircraft, Small Airplane - Certification basis: Part 3, Part 21 - Data sheets: [TCDS A-780](https://openairdocs.org/tcds/A-780), [TCDS 1A1](https://openairdocs.org/tcds/1A1), [TCDS 1A2](https://openairdocs.org/tcds/1A2), [TCDS 1A4](https://openairdocs.org/tcds/1A4), [TCDS 1A6](https://openairdocs.org/tcds/1A6) - Certificate PDF: https://openairdocs.org/files/sha256/0f/f9/0ff9094e666dc7e410bb50ac3d49ec712128b39e26604165efc70be5dceeaf78 - Approved model list and other attachments: [SA02483AK_AML.pdf](https://openairdocs.org/files/sha256/bc/c0/bcc0afad350cc01b5d6334e37fc1d761a30e6a997bef31d51e7e3ddd091c3fc1) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4777DB195332B2A6862580DE005D6EBA.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02483AK ## ADs that name it (0) None. ## Approved models (34) - FS 2003 Corp. PA-12 ([TCDS A-780](https://openairdocs.org/tcds/A-780)) - FS 2003 Corp. PA-12S ([TCDS A-780](https://openairdocs.org/tcds/A-780)) - Piper Aircraft Inc. PA-16 ([TCDS 1A1](https://openairdocs.org/tcds/1A1)) - Piper Aircraft Inc. PA-16S ([TCDS 1A1](https://openairdocs.org/tcds/1A1)) - Piper Aircraft Inc. PA-18 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-105 (Special) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-125 (Army L-21A) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18A ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18A-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18A-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18AS-125 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18AS-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18AS-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-105 (Special) ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-125 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-135 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-18S-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) - Piper Aircraft Inc. PA-20 ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-20-115 ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-20-135 ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-20S ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-20S-115 ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-20S-135 ([TCDS 1A4](https://openairdocs.org/tcds/1A4)) - Piper Aircraft Inc. PA-22 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22-108 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22-135 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22-150 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22-160 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22S-135 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22S-150 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) - Piper Aircraft Inc. PA-22S-160 ([TCDS 1A6](https://openairdocs.org/tcds/1A6)) ## 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. This Certificate issued to Part 3 of the Civil Air Regulations. Description of Type Design Change: Installation of : (1) Cleveland 199-62 or 199-62A wheel and brake kit or ABI LLC AB-199-62 or ABI-199-62A wheel and brake kit on aircraft with 1.5" axles, OR (2) Cleveland wheel and brake kit 199-71 or ABI LLC ABI-199-71 kit on aircraft with 1.25" axles. 1) The installer must determine whether this design change is compatible with previously approved modifications. 2) 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. 3) Existing Instructions for Continued Airworthiness are considered adequate for this modification. Date of application: November 5, 2014 Date of issuance: March 1, 2017 Date reissued: (Signature) August A. Asay Manager, Anchorage Aircraft Certification Office (Title) *Refer to FAA Approved Model List (AML), Number SA02483AK, dated March 1, 2017, or later FAA approved revision, for airplane makes and models, corresponding Type Certificate numbers, and applicable airworthiness regulations. Marvin E. Trimmer P. O. Box 361 Willow, AK 99688-0361 ### SA02483AK_AML.pdf United States Of America Department of Transportation - Federal Aviation Administration Marvin E. Trimmer Approved Model List (AML) Number SA02483AK P. O. Box 361 Date of Issuance: March 1, 2017 Willow, AK 99688-0361 AML for the Installation of Wheels and Brakes. Page 1 of 2 **AIRPLANE MAKE** **AIRPLANE MODEL TYPE** **CERTIFICATE NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **REQUIRED INSTALLATION** INSTRUCTIONS FS 2003 Corporation PA-12 PA-12S A-780 CAR 3 II-010, Revision A, dated December 23, 2016 Piper Aircraft, Inc. PA-16 PA-16S 1A1 CAR 3 II-010, Revision A, dated December 23, 2016 Piper Aircraft, Inc. PA-18 PA-18S PA18 ”105” (Special) PA-18S “105” (Special) PA-18A PA-18 “125” (Army L-21A) PA-18S “125” PA-18AS “125” PA-18 “135” (Army L-21B) PA-18A “135” PA-18S “135” PA-18AS “135” PA-18 “150” PA-18A “150” PA-18S “150” PA-18AS “150” 1A2 CAR 3 II-010, Revision A, dated December 23, 2016 United States Of America Department of Transportation - Federal Aviation Administration Marvin E. Trimmer Approved Model List (AML) Number SA02483AK P. O. Box 361 Date of Issuance: March 1, 2017 Willow, AK 99688-0361 AML for the Installation of Wheels and Brakes. Page 2 of 2 **AIRPLANE MAKE** **AIRPLANE MODEL TYPE** **CERTIFICATE NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **REQUIRED INSTALLATION** INSTRUCTIONS Piper Aircraft, Inc. PA-20 PA-20S PA-20 “115” PA-20S “115” PA-20 “135” PA-20S “135” 1A4 CAR 3 II-010, Revision A, dated December 23, 2016 Piper PA-22 PA-22-108 PA-22-135 PA-22S-135 PA-22-150 PA-22S-150 PA-22-160 PA-22S-160 1A6 CAR 3 II-010, Revision A, dated December 23, 2016 ## Every issue (1) - March 1, 2017: Issued, Current. [certificate](https://openairdocs.org/files/sha256/0f/f9/0ff9094e666dc7e410bb50ac3d49ec712128b39e26604165efc70be5dceeaf78), [SA02483AK_AML.pdf](https://openairdocs.org/files/sha256/bc/c0/bcc0afad350cc01b5d6334e37fc1d761a30e6a997bef31d51e7e3ddd091c3fc1) --- 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.