# STC SA1763SO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: James D. McArthur, United States
- Description: Installation of Lycoming O-235-L2C engine derated and McCauley 1A103/ TCM6958 propeller.
- Applied: January 3, 1984
- Status date: February 14, 1997
- Product: Aircraft, Small Airplane
- Data sheets: [TCDS A-691](https://openairdocs.org/tcds/A-691)
- Certificate PDF: https://openairdocs.org/files/sha256/c6/0d/c60d8ef3b5a90df22b0f1fdce580fd57e8c1fb1faac59f906c63db3cd0328070
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136230671720230608201118.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1763SO

## ADs that name it (1)

- [AD 2010-04-05](https://openairdocs.org/ad/2010-04-05): Hub Fatique Cracking · McCauley Propeller Systems 1A103/TCM. Effective Mar 10, 2010. Named in the applicability

## Approved models (1)

- The New Piper Aircraft Inc. PA-11 ([TCDS A-691](https://openairdocs.org/tcds/A-691))

## What the certificate says

The certificate is a scan without a text layer; open the PDF to read it.

## Every issue (1)

- February 14, 1997: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c6/0d/c60d8ef3b5a90df22b0f1fdce580fd57e8c1fb1faac59f906c63db3cd0328070)

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