# STC SA1747CE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Anderson Clinton
- Description: Installation of 300 hp. Lycoming IO-540-K1G5 engine and Hartzell HC-C3YR-1()F/8468A or HC-C2YK-( )F/F8475R propeller.
- Status date: June 21, 1982
- Data sheets: A10SO
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6B4BF647CF7BBC2485256CC10083CFCD.0001
- Page: https://openairdocs.org/stc/SA1747CE

## ADs that name it

- [AD 2002-19-03](https://openairdocs.org/ad/2002-19-03): Crankshaft · Lycoming Engines IO-540-A1A5, IO-540-AA1A5, IO-540-AA1B5 and 81 more. Effective Sep 20, 2002. Named in the applicability

## Approved models (1)

- The New Piper Aircraft Inc. PA-36-285 (Restricted Cat.) (TCDS A10SO)

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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.