# STC SA3229SO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Whelen Aerospace Technologies
- Description: Installation of main landing gear fairings.
- Status date: January 24, 2023
- Data sheets: 2A13, 2A13, 2A13, 2A13, 2A13, 2A13
- Certificate PDF: https://openairdocs.org/files/sha256/f7/a4/f7a42de0d1795485d2d7ec912453b545a676cfdaa1884c71715cbe52bea02f5c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193508936120230203204117.0001
- Page: https://openairdocs.org/stc/SA3229SO

## ADs that name it

None.

## Approved models (6)

- The New Piper Aircraft Inc. PA-28R-180 (TCDS 2A13)
- The New Piper Aircraft Inc. PA-28R-200 (TCDS 2A13)
- The New Piper Aircraft Inc. PA-28R-201 (TCDS 2A13)
- The New Piper Aircraft Inc. PA-28R-201T (TCDS 2A13)
- The New Piper Aircraft Inc. PA-28RT-201 (TCDS 2A13)
- The New Piper Aircraft Inc. PA-28RT-201T (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.

SA3229SO Whelen Aerospace Technologies 51 Winthrop Road Chester, CT 06412 Part 3 the Civil Aviation Regulations 2A13 Piper PA-28R-180/200/201/201T PA28RT-201/201T Installation of main landing gear fairings in accordance with LoPresti Master Drawing List, Report No. 4, dated March 24, 1992, 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) April 14, 1992 January 16, 2019; January 24, 2023 May 14, 1992 (for) Robert P. Capezzuto Acting Manager, Atlanta ACO Branch 3

SA3229SO 3

SA3229SO 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/f7/a4/f7a42de0d1795485d2d7ec912453b545a676cfdaa1884c71715cbe52bea02f5c)
- January 16, 2019: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f9/8f/f98ffe0c176a1a2c0b8ecd9d9a2d59cb6357e81dca02f96856b70de3211ee81f)

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