# STC SA02026AK

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: F Atlee Dodge Aircraft Service, United States
- Description: Fabrication and installation of wing front spart lift strut fitting reinforcing brackets
- Applied: December 20, 1992
- Status date: September 1, 1994
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 1A2](https://openairdocs.org/tcds/1A2)
- Certificate PDF: https://openairdocs.org/files/sha256/e0/51/e05105afe2a5e04ff810929bf8cc3e7a31ce75d9e230b338087c3ba67c448df5
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/301D51112CEF1C12862582F6006793A8.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02026AK

## ADs that name it (0)

None.

## Approved models (18)

- 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-19 (Army L-18C) ([TCDS 1A2](https://openairdocs.org/tcds/1A2))
- Piper Aircraft Inc. PA-19S ([TCDS 1A2](https://openairdocs.org/tcds/1A2))

## 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 SA02026AK This certificate issued to: F. Atlee Dodge P.O. Box 190409 Anchorage, Alaska 99519-0409 Purt 3* the Civil Air *Complete certification basis is specified in Aircraft Specification Regulations: No. 1A2, Revision 34.

Original Product -Type Certificate Number: 1A2 Make: Piper Model: PA-18, PA-18S, PA-18 "105" (Special), PA-18S "105" (Special), PA-18A, PA-18 "125" (Army L-21A), Description of Type Design Change: (See Continuation Sheet, Page 3 of 3) 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. 3192-18DL, Original Issue dated November 15, 1993, or later FAA approved revision.

The approval of this change in type design applies to the basic Piper PA-19'"125" (Army L-21A), PA-18S "125", PA-18AS "125", PA-18S, PA-18 "105" (Special), PA-18S "105" (Special), PA-18A, PA-18 "135" PA-18A "150" (A-T 2501, PA-185 "135", PA-184 "1150, PA-19 (my 1-PA) "150", PA-19S airplanes only.

Date of Application: December 20, 1992 Date Reissued:

Date of Issuance: . September 1, 1994 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Gordon K. Mandell FOR Robert L. Miller, (Signature) Manager TAMIN STRA TO Anchorage Aircraft Certification Office (Title)

47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA02026AK Model: (Continued) ВA-168 150, 8N-30 (Аtну (Any 580) am 9A.-15- 195-104 150, 2A-108 71504, Limitations and Conditions: (Continued) 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.

- END -

**FAA FORM 8110-2-1 (10-69) PAGE 3OF 3 PAGES C FAA AC 82-03578**

## Every issue (1)

- September 1, 1994: Issued, Current. [certificate](https://openairdocs.org/files/sha256/e0/51/e05105afe2a5e04ff810929bf8cc3e7a31ce75d9e230b338087c3ba67c448df5)

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