# STC SA00428SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Univair Aircraft Corporation, United States
- Description: Installation of a modified instrument panel
- Applied: January 30, 1997
- Status date: January 2, 2008
- Product: Aircraft, Single-Engine
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 1A6](https://openairdocs.org/tcds/1A6)
- Certificate PDF: https://openairdocs.org/files/sha256/1e/fb/1efb3da5040ee836931fa58f08cac42122a3f995a12a455634e154a181011859
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4EA98FFAF84BD5A4862573DA00551444.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00428SE

## ADs that name it (0)

None.

## Approved models (3)

- The New Piper Aircraft Inc. PA-22-108 ([TCDS 1A6](https://openairdocs.org/tcds/1A6))
- The New Piper Aircraft Inc. PA-22-150 ([TCDS 1A6](https://openairdocs.org/tcds/1A6))
- The New Piper Aircraft Inc. PA-22-160 ([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.

Number SA00428SE This certificate, issued to Univair Aircraft Corporation 2500 Himalaya Rd.

Aurora, CO 80011 Part 3 of the Civil Air Regulations.

Original Product⎯Type Certificate Number: 1A6 Make: Piper Model: PA-22-108, PA-22-150 and PA-22-160

Description of the Type Design Change: Installation of a modified instrument panel in accordance with Woolsey Design Master Drawing List 92WD005-D01, Revision C, dated November 9, 2001, or later FAA approved revision.

Note: This installation includes provisions for mounting instruments in an new instrument panel. Any additions or changes to the original equipment instruments will require separate FAA approval. The maximum weight of equipment installed in the panel should not exceed the specified by Note #3 on Sheet 1 of Drawing 92WD005000, Revision C, dated November 9, 2001, or later 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 this model 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: January 30, 1997 Date reissued: January 2, 2008 Date of issuance: April 10, 1997 Date amended: December 7, 2001; January 2, 2008

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

## Every issue (2)

- January 2, 2008: Amended, Current. [certificate](https://openairdocs.org/files/sha256/1e/fb/1efb3da5040ee836931fa58f08cac42122a3f995a12a455634e154a181011859)
- December 7, 2001: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/38/b9/38b9218f9f665e982947db93311f0bd52f9f56e8ce0f3cd14dbe140b91d4aefc)

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