# STC SA118GL

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Pampe Robert E, United States
- Description: Installation of Huron Aviation Products alternator, P/N 10346 and regulator, P/N 10316.
- Status date: March 23, 1978
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 1A4](https://openairdocs.org/tcds/1A4)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A2801B22B4625CE785256CC10080DFA1.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA118GL

## ADs that name it (0)

None.

## Approved models (2)

- The New Piper Aircraft Inc. PA-20-"115" ([TCDS 1A4](https://openairdocs.org/tcds/1A4))
- The New Piper Aircraft Inc. PA-20S ([TCDS 1A4](https://openairdocs.org/tcds/1A4))

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.