# STC SA3736WE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aircraft Metal Products Corporation, United States
- Description: Installation of an engine oil cooler hose.
- Status date: September 22, 1978
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A3SO](https://openairdocs.org/tcds/A3SO)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4670B2A8099521CA85256CC2000C5A16.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3736WE

## ADs that name it (1)

- [AD 78-16-08](https://openairdocs.org/ad/78-16-08): Loss of Engine Oil · Piper PA-32R-300 and PA-32RT-300. Effective Jun 25, 1979. Cited in the text

## Approved models (3)

- The New Piper Aircraft Inc. PA-32-260 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- The New Piper Aircraft Inc. PA-32-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))
- The New Piper Aircraft Inc. PA-32R-300 ([TCDS A3SO](https://openairdocs.org/tcds/A3SO))

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