# STC SA3695WE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aero Training Inc, United States
- Description: Installation of Lycoming O-235-C2C engine and McCauley1A105/SCM7154 propeller. No installation data required. Placards required with this installation: At the fuel filler caps - 80/87 MIN OCTANE AVGAS (AA-1C UTILITY CATEGORY)
- Status date: July 7, 1978
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A11EA](https://openairdocs.org/tcds/A11EA)
- Certificate PDF: https://openairdocs.org/files/sha256/f4/c8/f4c8b106d1454cb2ba6155182680061a38f6f6e03998d02becf53355d10824ca
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1D2180E04F98B0BD85256CC2000C59BC.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3695WE

## ADs that name it (0)

None.

## Approved models (1)

- Tiger Aircraft LLC AA-1C ([TCDS A11EA](https://openairdocs.org/tcds/A11EA))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA3695WE This certificate issued to: Aero-TraininE, InC.

Purt 23 of the Federal Aviation Regulalions. See I.C. Data Sheet No. AlIFA for complete certification basis.

Original Product -Type Certificate Number: A11EA Make: Grumman American Model: AA-1C, Utility Category Description of Type Design Change: Installation of Lycoming 0-235-C2C engine and McCauley 1A105/SCM7154 propeller. No installation data required. Placards required with this installation:

At the fuel filler caps - "80/87 MIN OCTANE AVGAS".

Limitations and Conditions: The approval of this change in type design applies to the basic aircraft of the specified model that is otherwise unmodified. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

C. Stratel TAIVISTRAIO At chief, Aircraft Modification Branch

47.

**FAA FORM 8110-2/10-691**

## Every issue (1)

- July 7, 1978: Issued, Current. [certificate](https://openairdocs.org/files/sha256/f4/c8/f4c8b106d1454cb2ba6155182680061a38f6f6e03998d02becf53355d10824ca)

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