# STC SA01252SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Fessler Aviation Inc., United States
- Description: Installation of engine mount heat shield modification in accordance with Oregon Aircraft Design Drawing List DLPA30, dated September 24, 1999, (PA-30, PA-39) or DLPA30T, dated August 28, 1999 (Turbocharged PA-30, PA-39) or later FAA approved revisions to either document.
- Applied: July 29, 2003
- Status date: January 20, 2004
- Product: Aircraft
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS A1EA](https://openairdocs.org/tcds/A1EA)
- Certificate PDF: https://openairdocs.org/files/sha256/3b/c7/3bc764371669b7ebc1fe9479db859888762030fb5af11e777e765b0757724668
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8E2BF8761DBCAA5A8625795E007157F6.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01252SE

## ADs that name it (0)

None.

## Approved models (2)

- Piper Aircraft Inc. PA-30 ([TCDS A1EA](https://openairdocs.org/tcds/A1EA))
- Piper Aircraft Inc. PA-39 ([TCDS A1EA](https://openairdocs.org/tcds/A1EA))

## 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 SA01252SE

This certificate, issued to Fessler Aviation, Inc.

13342 80th Terrace Live Oak, FL 32060

Part 3 of the Civil Air Regulations.

Original ProductType Certificate Number: A1EA Make: New Piper (Piper) Model: PA-30, PA-39, Turbo PA-30, PA-39

Description of the Type Design Change: Installation of engine mount heat shield modification in accordance with Oregon Aircraft Design Drawing List DLPA30, dated September 24, 1999, (PA-30, PA-

39) or DLPA30T, dated August 28, 1999 (Turbocharged PA-30, PA-39) or later FAA approved revisions to either document.

Limitations and Conditions: Approval of this change in type design applies to the aircraft models listed above 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: July 29, 2003 Date reissued: January 20, 2004 Date of issuance: August 13, 2003 Date amended:

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

## Every issue (1)

- January 20, 2004: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/3b/c7/3bc764371669b7ebc1fe9479db859888762030fb5af11e777e765b0757724668)

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