# STC SA02569SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Steve's Aircraft, United States
- Description: Installation of disk brakes
- Applied: April 23, 2017
- Status date: October 17, 2017
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS 1A6](https://openairdocs.org/tcds/1A6)
- Certificate PDF: https://openairdocs.org/files/sha256/80/8b/808bc2e85df1e42059c8e1b440f4693bb2ef3a9da8f9e1732e99b9a509b860cd
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1D8401A91EBC29D3862581BD004E3F3A.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA02569SE

## ADs that name it (0)

None.

## Approved models (8)

- 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.

Un ited S tates of Am erica Department of Transportation - Federal Aviation Administration Supplemental Type Certificate

Number SA02569SE

This certificate, issued to Steve’s Aircraft 15373 Jones Rd.

White City, OR 97503

Part 23 of the Federal Aviation Regulations.

Original ProductType Certificate Number: 1A6 Make: Piper Model: PA-22, PA-22-108, PA-22-135, PA-22S-135, PA-22-150, PA-22S-150, PA-22-160, PA-22S-160

Description of the Type Design Change: Installation of disk brakes in accordance with Bill of Materials Document No. 3200-11-2, Revision I.R., dated April 14, 2017, and Installation Instructions Document No.

3200-11-3, Revision I.R., dated April 14, 2017, or later Federal Aviation Administration (FAA) approved revision.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only.

This approval should not be extended to other aircraft of these model unless the installer determines that the relationship between this change and any other previously incorporated approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. Modified aircraft must be maintained in accordance with Instructions for Continued Airworthiness (ICA) 3200-11-1, Revision I.R., dated April 14, 2017, or later FAA-accepted revision.

A copy of this certificate and the ICA must be maintained as part of the permanent records for the modified aircraft.

Date of application: April 23, 2017 Date reissued:

Date of issuance: October 17, 2017 Date amended:

FAA FORM 8110-2 (5/14) PAGE 1 OF 2 PAGES By direction of the Administrator

(Signature)

Manager, Seattle ACO Branch (Title)

## Every issue (1)

- October 17, 2017: Issued, Current. [certificate](https://openairdocs.org/files/sha256/80/8b/808bc2e85df1e42059c8e1b440f4693bb2ef3a9da8f9e1732e99b9a509b860cd)

---
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.