# STC SA00162AT

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Whelen Aerospace Technologies, United States
- Description: Installation of flap gap seals
- Applied: January 22, 1993
- Status date: January 24, 2023
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A7SO](https://openairdocs.org/tcds/A7SO)
- Certificate PDF: https://openairdocs.org/files/sha256/d7/83/d783dd2398976640dcac19b88d63a79a336e37d951212356c75ab3fc23e79795
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID110811918320230206143826.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00162AT

## ADs that name it (0)

None.

## Approved models (3)

- Piper Aircraft Inc. PA-34-200 ([TCDS A7SO](https://openairdocs.org/tcds/A7SO))
- Piper Aircraft Inc. PA-34-200T ([TCDS A7SO](https://openairdocs.org/tcds/A7SO))
- Piper Aircraft Inc. PA-34-220T ([TCDS A7SO](https://openairdocs.org/tcds/A7SO))

## 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.

SA00162AT Whelen Aerospace Technologies 51 Winthrop Road Chester, CT 06412 Part 23 Federal Aviation Regulations A7SO Piper PA-34 Series Installation of flap gap seals in accordance with LoPresti ''Master Drawing List, Report No. 19, dated January 18, 1993, 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 and any of those other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. (See continuation sheet 3 of 3) January 22, 1993 January 16, 2019; January 24, 2023 March 23, 1993 (for) Robert P. Capezzuto Acting Manager, Atlanta ACO Branch 3

SA00162AT 3

SA00162AT Date Reissued: January 24, 2023

Limitations & Conditions (Continued):

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 (1)

- January 24, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d7/83/d783dd2398976640dcac19b88d63a79a336e37d951212356c75ab3fc23e79795)

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From OpenAirDocs.org, an independent open copy of FAA and NTSB data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.