# STC SA01082AT

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Aire Comanche Performance, United States
- Description: Installation of new fiberglass cowling, full length gear doors, relocation of engine oil cooler and replacement of the exhaust system. S/N 24-1 and u
- Applied: October 2, 1995
- Status date: April 9, 2024
- Product: Aircraft, Small Airplane
- Data sheets: [TCDS 1A15](https://openairdocs.org/tcds/1A15)
- Certificate PDF: https://openairdocs.org/files/sha256/b1/28/b1282fcad65bc139c6a40843ab1ee2f60f5c6c8c40eb77d8b8dd01db4eecb8dc
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140796655920240531160055.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01082AT

## ADs that name it (0)

None.

## Approved models (1)

- The New Piper Aircraft Inc. PA-24 ([TCDS 1A15](https://openairdocs.org/tcds/1A15))

## 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.

Title: (for) Christina M. Underwood Manager, East Certification Branch Compliance and Airworthiness Division Aircraft Certification Service

SA01082AT Aire Comanche Performance 10215 Shoshone Ave Northridge, CA 91325 Part 3 the Civil Air Regulations 1A15 Piper PA-24, S/N 24-1 and up Installation of new fiberglass cowling, full length gear doors, relocation of engine oil cooler and replacement of the exhaust system in accordance with Aviation Performance Products, Inc. “Piper PA24-180 Cowling Modification Package”, dated 10/15/95, and Master Drawing – List MDL-95-01, Rev. B, dated 09/15/97 in Piper PA24-180 model aircrafts.

October 2, 1995 May 2, 2001, April 9, 2024 July 9, 1996 January 26, 1998 3

SA01082AT 3

SA01082AT Limitations and Conditions:

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. 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.

Note:

Model entry updated to PA-24 during re-issuance of this STC on 4/9/24 to make it consistent with Type Certificate Data Sheet (TCDS) entry. In prior versions of the STC, Model entry indicated PA-24-180.

## Every issue (1)

- April 9, 2024: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/b1/28/b1282fcad65bc139c6a40843ab1ee2f60f5c6c8c40eb77d8b8dd01db4eecb8dc)

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