# STC SA4740NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Fletchair Inc., United States - Description: Installation of a landing light in the left wing tip or in both wing tips. - Applied: December 1, 1988 - Status date: April 9, 2012 - Product: Aircraft, Single-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A11EA](https://openairdocs.org/tcds/A11EA), [TCDS A16EA](https://openairdocs.org/tcds/A16EA) - Certificate PDF: https://openairdocs.org/files/sha256/09/3b/093b67636b3a364f10a5d798846b731ac8f2caebb91437b401e6dc5efee8fd72 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/33AE590342C22438862579E500543E6A.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA4740NM ## ADs that name it (0) None. ## Approved models (6) - 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)) - True Flight Holdings LLC AA-5 ([TCDS A16EA](https://openairdocs.org/tcds/A16EA)) - True Flight Holdings LLC AA-5A ([TCDS A16EA](https://openairdocs.org/tcds/A16EA)) - True Flight Holdings LLC AA-5B ([TCDS A16EA](https://openairdocs.org/tcds/A16EA)) ## 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. Number SA4740NM This certificate, issued to Fletchair Inc. 103 Turkey Run Lane Comfort, TX 78013 Part 23 of the Federal Air Regulations. Original ProductType Certificate Number: A11EA I A16EA Make: Gulfstream Aerospace I Gulfstream Aerospace Model: AA-1A, AA-1B, and AA-1C I AA-5, AA-5A, and AA-5B Description of the Type Design Change: Installation of a landing light in the left wing tip or both wing tips, in accordance with Josef G. Breuer Drawing List Number DL-200, dated November 18, 1988, revised November 22, 1989, or later Federal Aviation Administration (FAA) approved revision. Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously incorporated approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate must be maintained as part of the permanent records for the modified aircraft. 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. Date of application: December 1, 1988 Date reissued: April 9, 2012 Date of issuance: August 24, 1989 Date amended: March 1, 1990 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (2) - April 9, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/09/3b/093b67636b3a364f10a5d798846b731ac8f2caebb91437b401e6dc5efee8fd72) - March 1, 1990: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/9a/0a/9a0aa8f237e2c3fa09385c771ffcbe9c5d11a7fa79a3b2bda0e815cc7a01573d) --- 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.