What it approves
Installation of a Landing Gear Warning System to incorporate a stall warning interface
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
FAA Form 8110-2 (5/14) Page 1 of 3
Number: SA01644AT
This certificate issued to: Aircraft Components, Inc.
1700 Fostoria Avenue, Ste 300 Findlay, OH 45840
Part * of the * Regulations.
Original Product – Type Certificate Number: * See Attached Make: FAA Approved Model List (AML) Model: Document 2037- AML for a list of Approved Airplane Models
Description of Type Design Change: Installation of a Landing Gear Warning System to incorporate a stall warning interface in accordance with Master Document List ML-2037, Revision 7, dated July 14, 2003, or later FAA Approved Revision.
Limitations and Conditions: 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 other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane.
Date of Application: June 30, 2003 Date Reissued: January 22, 2016
Date of Issuance: March 15, 2000 Date Amended: August 10, 2000, January 09, 2001, September 12, 2003
Signature Rick Jones, Acting Manager Atlanta Aircraft Certification Office Title
FAA Form 8110-2 (5/14) Page 2 of 3
Transfer the ownership of Supplemental Type Certificate Number: SA01644AT
To (Name and address of transferee)
From (Name and address of grantor)
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01644AT
FAA Form 8110-2 (5/14) Page 3 of 3
Limitations and Conditions: (Continued):
The FAA Approved Flight Manual Supplement, dated September 12, 2003, or later FAA approved revision is a required part of this STC. 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.
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ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 14
| Make | Model | Data sheet |
|---|---|---|
| Mooney Aircraft Corporation | M20 | 2A3 |
| Mooney Aircraft Corporation | M20A | 2A3 |
| Mooney Aircraft Corporation | M20B | 2A3 |
| Mooney Aircraft Corporation | M20C | 2A3 |
| Mooney Aircraft Corporation | M20D | 2A3 |
| Mooney Aircraft Corporation | M20E | 2A3 |
| Mooney Aircraft Corporation | M20F | 2A3 |
| Mooney Aircraft Corporation | M20G | 2A3 |
| Mooney Aircraft Corporation | M20J | 2A3 |
| Mooney Aircraft Corporation | M20K | 2A3 |
| Mooney Aircraft Corporation | M20L | 2A3 |
| Mooney Aircraft Corporation | M20M | 2A3 |
| Mooney Aircraft Corporation | M20R | 2A3 |
| Mooney Aircraft Corporation | M20S | 2A3 |