# STC SA01356SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Del-Air, United States
- Description: Installation of Instrument Panel and Y  Yoke Assembly.
- Applied: June 30, 2003
- Status date: December 22, 2003
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A17](https://openairdocs.org/tcds/3A17)
- Certificate PDF: https://openairdocs.org/files/sha256/36/4f/364f44e9feccd242db0072880e185ec493a9ef6fc11d8c931b3540b355abffbc
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2E7B0AE11C81C10B862576E10061CA8E.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01356SE

## ADs that name it (0)

None.

## Approved models (5)

- 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 P172D ([TCDS 3A17](https://openairdocs.org/tcds/3A17))

## 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.

Number SA01356SE

This certificate, issued to Del-Air 2121 S. Wildcat Way Porterville, CA 93257

Part 3 of the Civil Air Regulations.

Original Product⎯Type Certificate Number: 3A17 Make: Cessna Model: 175, 175A, 175B, 175C and PA172D

Description of the Type Design Change: Installation of Instrument Panel and “Y” Yoke Assembly.

Manufactured in accordance with Del-Air Fabrication Drawing List 13000-6, Revision New, dated June 30, 2003, or later FAA approved revision. Installed in accordance with Del-Air Installation Instructions 13000-2, Revision New, dated June 30, 2003, or later FAA approved revision. Maintained in accordance with DA Report No. 160 13000-7, Instructions for Continued Airworthiness, Revision New, dated June 30, 2003, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies to the above aircraft models only. This approval should not be extended to other aircraft on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.

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.

Date of application: June 30, 2003 Date reissued:

Date of issuance: December 22, 2003 Date amended:

(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- December 22, 2003: Issued, Current. [certificate](https://openairdocs.org/files/sha256/36/4f/364f44e9feccd242db0072880e185ec493a9ef6fc11d8c931b3540b355abffbc)

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