# STC SA810NW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Fletchair Inc., United States
- Description: Installation of main landing gear fairings from the AA-5 series aircraft incorporating sheet metal covers over rubber in place of stock rubber parts.
- Applied: July 17, 1979
- Status date: June 9, 2022
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A11EA](https://openairdocs.org/tcds/A11EA)
- Certificate PDF: https://openairdocs.org/files/sha256/3e/9b/3e9bd7cf7465e05294d3afa2edc0b56440ec4467f045165d502559cf7f86fd2d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DD0281D4D84AC9E8862588940042B637.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA810NW

## ADs that name it (0)

None.

## Approved models (4)

- True Flight Holdings LLC AA-1 ([TCDS A11EA](https://openairdocs.org/tcds/A11EA))
- True Flight Holdings LLC AA-1A ([TCDS A11EA](https://openairdocs.org/tcds/A11EA))
- True Flight Holdings LLC AA-1B ([TCDS A11EA](https://openairdocs.org/tcds/A11EA))
- True Flight Holdings LLC AA-1C ([TCDS A11EA](https://openairdocs.org/tcds/A11EA))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

SA810NW FletchAir, Inc.

103 Turkey Run Lane Comfort, TX 78013 23 the Federal Aviation Regulations A11EA Gulfstream American (Grumman) AA-1, AA1-A, AA-1B, and AA-1C Installation of main landing gear fairings in accordance with Maynard C. Crosby Installation Instructions No. MC110, Revision A.

Approval of this change in type design applies basically to the above model aircraft only. This approval should not be extended to other aircraft o fthis model on which other previously approved modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate and Maynard C. Crosby Installation Instructions shall be maintained as part of the permanent records for the modified aircraft.

July 17, 1979 June 9, 2022 July 20, 1979 January 23, 1981 For Acting Manager, Seattle ACO Branch 2

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

SA810NW 2

## Every issue (2)

- June 9, 2022: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/3e/9b/3e9bd7cf7465e05294d3afa2edc0b56440ec4467f045165d502559cf7f86fd2d)
- January 23, 1981: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/63/24/6324d1f6030a4e4073641bf067cd496dbd4fe733add393ea61f52f391ff2cf85)

---
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.