# STC SA02231AK

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: F Atlee Dodge Aircraft Service, United States
- Description: Installation of Cleveland Main Wheels and Brakes.
- Applied: October 15, 2004
- Status date: March 17, 2008
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 3A17](https://openairdocs.org/tcds/3A17), [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS 5A6](https://openairdocs.org/tcds/5A6), [TCDS A-799](https://openairdocs.org/tcds/A-799), [TCDS ATC 660](https://openairdocs.org/tcds/ATC%20660)
- Certificate PDF: https://openairdocs.org/files/sha256/4d/59/4d59e92fabd63263de93bae4ac28fe9b72fd4cb962ce16f6f15dd694ea7693a1
- Approved model list and other attachments: [SA02231AK amdt 1.pdf](https://openairdocs.org/files/sha256/1e/ee/1eee0061234d0eb26afc792e963fcb784356d0825db3da9af45deede5d7a3058)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BF9159CC78197A418625741D004F161F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02231AK

## ADs that name it (0)

None.

## Approved models (58, first 50)

- Cessna Aircraft Company 170 ([TCDS A-799](https://openairdocs.org/tcds/A-799))
- Cessna Aircraft Company 170A ([TCDS A-799](https://openairdocs.org/tcds/A-799))
- Cessna Aircraft Company 170B ([TCDS A-799](https://openairdocs.org/tcds/A-799))
- Cessna Aircraft Company 172 ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172A ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172B ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172C ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172D ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172E ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172F (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172G ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172H (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172I ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172K ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172L ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172M ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172N ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172P ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172Q ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 175 ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company 175A ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company 175B ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company 175C ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180A ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180B ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180C ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180D ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180E ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180F ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180G ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180H ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180J ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180K ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 182 ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182A ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182B ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182C ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182D ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182J ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182N ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182P ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182Q ([TCDS 3A13](https://openairdocs.org/tcds/3A13))

All 58: https://openairdocs.org/stc/SA02231AK/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.

F. Atlee Dodge Aircraft Services, LLC. Revision: A 6672 Wes Way Date: March 3, 2008 Anchorage, AK 99518 Page 1 of 1

FAA Approved Model List (AML) No. SA02231AK For the Installation of Cleveland Main Wheels and Brakes in accordance with F. A. Dodge “Installation Instructions for Cleveland Wheel & Brake Kits, 199-62 and 199-62A”

Aircraft Make and Model Designation Original Type Certificate Number Certification Basis Cessna 170, 170A A-799 CAR 03 170B A-799 CAR 3 172, 172A, 172B, 172C, 172D, 172E, 172F (USAF T-41A), 172G, 172H (USAF T-41A), 172I, 172K, 172L, 172M, 172N, 172P, 172Q 3A12 CAR 3 175, 175A, 175B, 175C 3A17 CAR 3 180, 180A, 180B, 180C, 180D, 180E, 180E, 180F, 180G, 180H, 180J, 180K 5A6 CAR 3 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182S, 182K, 182L, 182M, 182N, 182P, 182Q 3A13 CAR 3 185, 185A, 185B, 185C, 185D, 185E 3A24 CAR 3 Piper J-3 ATC 660 CAR 04 J3C Series A-691 CAR 4a PA-11, PA-11S A-691 CAR 4a PA-12, PA-12S A-780 CAR 3 PA-14 A-797 CAR 3 PA-16, PA-16S 1A1 CAR 3 PA-18 Series 1A2 CAR 3 END

FAA APPROVED:

Manager, Anchor age Aircraft Certification Office Federal Aviation Administration Anchorage, Alaska

Date: March 17, 2008

### SA02231AK amdt 1.pdf

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate

_____________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.

_____________________________________________________________________________________________________________________________________ FAA Form 8110-2(10-68) Page 1 of 1 This certificate may be transferred in accordance with FAR 21.47.

Number SA02231AK This Certificate issued to F. Atlee Dodge Aircraft Services, LLC 6672 Wes Way Anchorage, AK 99518

certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part * of the * Regulations.

*See attached FAA Approved Model List (AML) No. SA02231AK, Revision A, dated March 3, 2008, for list of approved airplane models and applicable airworthiness regulations.

Original Product Type Certificate Number:

Make:

Model:

Description of Type Design Change: Installation of Cleveland Main Wheels and Brakes in accordance with F. A. Dodge “Installation Instructions, Cleveland Wheel & Brake Kits, 199-62 and 199-62A”, Document No: IM-02231, revision A, dated March 3, 2008, or later FAA approved revisions.

Limitations and Conditions:

1. Piper aircraft must be equipped with a previously FAA approved installation of a PA-18 landing gear with 1½-inch axles.

2. Compatibility of this design change with previously approved modifications must be determined by the installer.

3. Refer to “Cleveland Wheels and Brakes, Technician’s Service Guide”, PRM64, Rev H or later revision, and Piper Service Manual for Instructions for Continued Airworthiness.

4. 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.

This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: October 15, 2004

Date of issuance: December 9, 2004 Date reissued: March 17, 2008

Date amended: March 17, 2008

By direction of the Administrator

______________________________________________ ( Signature) Gregory J. Holt Manager Anchorage Aircraft Certification Office ______________________________________________ ( Title)

## Every issue (1)

- March 17, 2008: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/4d/59/4d59e92fabd63263de93bae4ac28fe9b72fd4cb962ce16f6f15dd694ea7693a1), [SA02231AK amdt 1.pdf](https://openairdocs.org/files/sha256/1e/ee/1eee0061234d0eb26afc792e963fcb784356d0825db3da9af45deede5d7a3058)

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