# STC SA3719SW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Mexia Systems, Inc
- Description: Installation of Lycoming IO-540-AA1A5 engines, Hartzell HC-CY-2UF/FC-8468/8R propellers and two Ray-Jay 103599-02 turbochargers on each engine to maintain maximum continuous cruise power. (PA-60-601 (AEROSTAR 601) B)
- Status date: January 6, 1987
- Data sheets: A17WE
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/29FCF6E6A46C12B785256CC2000C59F7.0001
- Page: https://openairdocs.org/stc/SA3719SW

## 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)

- Aerostar Aircraft Corporation PA-60-601 (Aerostar 601) (TCDS A17WE)

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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.