# STC SA02021AK

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: F Atlee Dodge Aircraft Service, United States
- Description: Fabrication and installation of wing front spar lift strut fitting reinforcing brackets
- Applied: December 20, 1992
- Status date: July 29, 1994
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A-797](https://openairdocs.org/tcds/A-797), [TCDS A-780](https://openairdocs.org/tcds/A-780)
- Certificate PDF: https://openairdocs.org/files/sha256/40/00/4000f365d4a4dc290f530832e3fbadec1fce93b689d9a97e60c98c128b668d05
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1E0D01CFCD221C04862582F600659095.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02021AK

## ADs that name it (0)

None.

## Approved models (3)

- FS 2002 Corp. PA-14 ([TCDS A-797](https://openairdocs.org/tcds/A-797))
- 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))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA02021AK This certificate issued to: F. Atlee Dodge P.O. Box 190409 Anchorage, Alaska 99519-0409 Certifies that the change in the type design for the following product with the limitations and conditions therefor as specified heron meets the sinushiness requirementified in Aircraft Specification Civil Air *Complete certification basis Requlations. No. A-780, Revision 7, and in Aircraft Specification No. A-797, Revision 8.

Original Product - TypeCertificate Number: A-780 and A-797 Make: Piper Model: PA-12, PA-125, and PA-14 Description of Type Design Change:

Fabrication and installation of wing front spar lift strut fitting reinforcing brackets in accordance with F. Atlee Dodge Aircraft Services, Inc., Master Drawing List No. 3192-12DL, Original Issue dated November 15, 1993, or later FAA approved revision.

approval of this change in type design applies to the basic Piper PA-12, PA-12S, and PA-14 airplanes only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the modifications will introduce no adverse effect on the airworthiness of such aircraft. This determination should include consideration of significant changes in weight distribution.

Date of Application: December 20, 1992 Date Reissued:

Date of Issuance: . July 29, 1994 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Sor ‹obert L. MIler, (Sig ature) Manage Heven AMangrapane T29/94 * MINISTRATO Anchorage Aircraft Certification Office (Title)

47.

## Every issue (1)

- July 29, 1994: Issued, Current. [certificate](https://openairdocs.org/files/sha256/40/00/4000f365d4a4dc290f530832e3fbadec1fce93b689d9a97e60c98c128b668d05)

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