# STC SA02164LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Certified Aeronautical Products, United States
- Description: Removal of Teledyne Continental Motors A-65-8 engine and installing one of the following Teledyne Continental Model engines: C85-8, C85-8F, C85-12, C85-12F, C85 (Modified per STC # SE00979AT), C90-8F, C90-12F OR 0-200A.
- Applied: December 19, 2008
- Status date: December 19, 2008
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-746](https://openairdocs.org/tcds/A-746)
- Certificate PDF: https://openairdocs.org/files/sha256/1f/18/1f18c0379f2fb74714d440046d57207b7e68d47c096e52a58a5c1a985e1cbd7e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A05AD89C7325E975862575760055E3AA.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02164LA

## ADs that name it (0)

None.

## Approved models (2)

- Arizona Aerospace Foundation DC-65 ([TCDS A-746](https://openairdocs.org/tcds/A-746))
- Arizona Aerospace Foundation DCO-65 ([TCDS A-746](https://openairdocs.org/tcds/A-746))

## 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 SAO2164LA This certificate issued to: CERTIFIED AERONAUTICAL PRODUCTS MAILING ADDRESS 9864 GLENOAKS BLVD 2457 TEXAS HIGHWAY 236 SUN VALLEY, CA 91352 MOODY, TX 76557 Part 4a of the Civil Air Poegulations Original Product Type Certificate Number: A-746 Make: Arizona Aerospace Foundation (Taylorcraft) Model: DC-65 (Army L-2) and DCO-65 (Army L-2A, -2B, -2M) Description of Type Design Change: Removal of the Teledyne Continental Motors A-65-8 engine and installing one of the following Teledyne Continental Model engines: C85-8, C85-8F, C85-12, C83-12F, C85 (Modified per STC # SE00979AT), C90-8F, C90-12F or O-200A, in accordance with Certificated Aeronautical Products Master Drawing List 1026, Revision B, dated October 13, 2008 or later FAA- approved revision. See continuation sheet.

Limitations and Conditions: The installation should not be incorporated in any airplanes unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the airplane. The installer must determine whether this design change is compatible with previously approved modifications. The approval of this modification applies to the above-noted airplane model series only. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. See continuation sheet.

This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration Date of Application: August 15, 2008 Date Reissued: December 19, 2008 Date of Issuance: November 28, 2008 Date Amended:

FEDERAL AVIATION By Direction of the Administrator (Signature) Manager, Propulsion Branch TOMINSTRATIO Los Angeles Aircraft Certification Office (Title)

## Every issue (1)

- December 19, 2008: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/1f/18/1f18c0379f2fb74714d440046d57207b7e68d47c096e52a58a5c1a985e1cbd7e)

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