# STC SA1075SO

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Stephenson William J, United States
- Description: Wing-Ding door stop to be installed using existing screws(Piper P/N 415 309, MS27039-0809) on leading edge of right wing at inboard side of fuel cell(W.S. 57.00).
- Status date: May 18, 1979
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/37BD171DB3BB2FC885256CC10080DD76.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1075SO

## ADs that name it (0)

None.

## Approved models (7)

- The New Piper Aircraft Inc. PA-28-151 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- The New Piper Aircraft Inc. PA-28-161 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- The New Piper Aircraft Inc. PA-28-181 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))
- The New Piper Aircraft Inc. PA-28-235 ([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-28R-201T ([TCDS 2A13](https://openairdocs.org/tcds/2A13))

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