# STC SA3234WE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Aircraft Maintenance Service, United States
- Description: Installation of Piper oil cooler and associated installation components.
- Applied: July 8, 1976
- Status date: July 8, 1976
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A11EA](https://openairdocs.org/tcds/A11EA)
- Certificate PDF: https://openairdocs.org/files/sha256/26/ef/26efbfee691be99a56724e7c6782476088ba9e3511bedcc486c6e45f3e5ea616
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/78235ABF6B65F0D985256CC2000A95A7.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA3234WE

## ADs that name it (0)

None.

## Approved models (3)

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

MAIL Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number: SA3234WE This certificate issued to: Aircraft Maintenance Service 7950B Joe Crosson Drive Santee, CA 92071 Part 23 the Federal Aviation Fugulalions. effective February 1, 1965 and Amendments 23-1 and 23-2.

Original Product -Type bertificate Number: ALTEA Make: Grumman-American Aviation Model: AA-1, AA-IA, AA-1B Description of Type Design Change:

Installation of Piper oil cooler and associated installation components in accordance with Aircraft Maintenance Service Drawing No. lAM0001 dated July 7, 1976.

The approval of this change in type design applies to the basic aircraft of the specified models that are otherwise unmodified. This approval should not be extended to other aircraft of these models 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.

Date of Application: July 8, 1976 Date Reissued:

Date of Issuance: July 8, 1976 Date Amended:

FEDERAL AVIATION By direlin of the l rinistrate неко Signature )

## Every issue (1)

- July 8, 1976: Issued, Current. [certificate](https://openairdocs.org/files/sha256/26/ef/26efbfee691be99a56724e7c6782476088ba9e3511bedcc486c6e45f3e5ea616)

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