# STC SA00082SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Flight Shop, United States
- Description: Installation of a baggage door strut.
- Applied: February 7, 1994
- Status date: April 29, 1994
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A17WE](https://openairdocs.org/tcds/A17WE)
- Certificate PDF: https://openairdocs.org/files/sha256/38/c8/38c876490412fa5146924dd76fa9218af3829cd41086530e184a1bf33176196d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127637768620231103131048.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00082SE

## ADs that name it (0)

None.

## Approved models (5)

- Aerostar Aircraft Corporation PA-60-600 (Aerostar 600) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-601 (Aerostar 601) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-601P (Aerostar 601P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-602P (Aerostar 602P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-700P (Aerostar 700P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA000825E This certificate issued to: The Flight Shop Puri 23 of the Federal Aviation Regulations.

Original Product -Type bertificate Number: * AITWE Make: * Aerostar Model: * PA-60-600, -601, -601P, -602P, and -700P Shop Daving is ye a face 19, 1 3a, olate FAA sproved rev stout in accordance with The Flight Limitations and Conditions: Approval of this change in type design applies to the model aircraft listed above only. This approval should not be extended to aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate, dated April 29, 1994, or later FAA approved revision, must be maintained as part of the permanent records for the

## Every issue (1)

- April 29, 1994: Issued, Current. [certificate](https://openairdocs.org/files/sha256/38/c8/38c876490412fa5146924dd76fa9218af3829cd41086530e184a1bf33176196d)

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