# STC SA01319AT

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Whelen Aerospace Technologies, United States
- Description: Installation of new composite engine cowling with cowl flap and large inspection access doors on both sides of cowling.
- Applied: January 16, 2019
- Status date: January 24, 2023
- Product: Aircraft, Small Airplane
- Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13)
- Certificate PDF: https://openairdocs.org/files/sha256/55/3a/553a5876dcf92fd6d836bc3cc3b1ca0ddf99756b39a146813429352ed9632a58
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107813713920230206153938.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01319AT

## ADs that name it (0)

None.

## Approved models (4)

- The New Piper Aircraft Inc. PA-28R-180 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- The New Piper Aircraft Inc. PA-28R-200 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- The New Piper Aircraft Inc. PA-28R-201 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- The New Piper Aircraft Inc. PA-28RT-201 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))

## 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.

SA01319AT Whelen Aerospace Technologies 51 Winthrop Road Chester, CT 06412 Part 3 the Civil Aviation Regulatons 2A13 Piper PA-28R-180, -200, -201. PA-28RT-201 Installation of a new composite engine cowling with cowl flap and large inspection access doors on both sides of the cowling in accordance with LoPresti Speed Merchants Master Drawing List, Report No. 39, Arrow Cowling Installation, Revision "A", dated February 28, 1997 or later FAA Approved revision.

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 a11d any of those other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. (See continuation sheet 3 of 3) November 12, 1996 January 16, 2019; January 24, 2023 March 25, 1997 May 20, 1997 (for) Robert P. Capezzuto Acting Manager, Atlanta ACO Branch 3

SA01319AT 3

SA01319AT Date Reissued: January 24, 2023

Limitations and Conditions: Continued from Page 1

This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage.

-----------------------END------------------- 3 3

## Every issue (2)

- January 24, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/55/3a/553a5876dcf92fd6d836bc3cc3b1ca0ddf99756b39a146813429352ed9632a58)
- January 16, 2019: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/26/35/2635518d427d5fe7a2e0a28035afbb26c6447e407338bb08c890c704d68a876f)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.