# STC SA00343AT

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Air Comanche Performance, United States
- Description: Installation of engine cowl and full length gear doors and relocation of engine oil cooler and replacement exhaust system. For PA-24-250, S/N 24-103 and up; for PA-24-260, S/N 24-3642, 24-4000 to 24-4782 and 24-4784 to 24-4803.
- Applied: March 29, 1992
- 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/bf/fc/bffc6557a7363c30a9a3210acbdb2c39f8a5237c2a1726f23c72273b88b106a0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173998735920240522194100.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00343AT

## ADs that name it (0)

None.

## Approved models (2)

- Piper Aircraft Inc. PA-24-250 ([TCDS 1A15](https://openairdocs.org/tcds/1A15))
- Piper Aircraft Inc. PA-24-260 ([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.

FAA Form 8110-2 (03/21) Page 1 of ___ SA00343AT Aire Comanche Performance 10215 Shoshone Ave Northridge, CA 91325 Civil Air Regulations 3 Piper See Page 3 1A15 Installation of engine cowl and full length gear doors and relocation of engine oil cooler and replacement exhaust system in accordance with Aviation Performance Products, Inc. Master Drawing List No. MDL­92­01, Revision B, dated April 1, 1993 or later FAA approved revision.

See Page 3 3/29/92 5/2/01, 4/9/24 9/21/93 (for) Christina M. Underwood 3 (for) Christina M. Underwood Manager, East Certification Branch Compliance and Airworthiness Division Aircraft Certification Service

FAA Form 8110-2 (03/21) Page ___ of ___ SA00343AT Model: PA­24­250, S/N 24­103 and up; PA­24­260, S/N 24­3642, 24­4000 to 24­4782 and 24­4784 to 24­4803

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: This STC was originally, erroneously assigned the number ST00343AT. Installations completed under this number are still valid.

## Every issue (1)

- April 9, 2024: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/bf/fc/bffc6557a7363c30a9a3210acbdb2c39f8a5237c2a1726f23c72273b88b106a0)

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