# STC SA3465WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: DeVore Aviation Corporation of America, a New Mexico Corporation, United States
- Description: Installation of recognition light assembly on the horizontal stabilizer
- Applied: June 14, 1977
- Status date: January 31, 2000
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A5SW](https://openairdocs.org/tcds/A5SW)
- Certificate PDF: https://openairdocs.org/files/sha256/77/47/77474409a97b9c52c10439ede329e0b7202cfd4d2f92b41d3b835bd0f2a67142
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2A133117754D1F9486257DC1005A3B7F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA3465WE

## ADs that name it (0)

None.

## Approved models (2)

- M7 Aerospace LLC SA26-AT ([TCDS A5SW](https://openairdocs.org/tcds/A5SW))
- M7 Aerospace LLC SA26-T ([TCDS A5SW](https://openairdocs.org/tcds/A5SW))

## 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: SA3465WE This certificate issued to: DeVore Aviation Corporation of America, a New Mexico Corporation 6104-B Jefferson, N.E.

Albuquerque, NM 87109-3410 Part 3* of the Civil Air A5SW, Revision 10 Vegulations. *Certification basis is set forth in Type Certificate Data Sheet Original Product Typo Certificate Number: ASSW Make: Swearingen Model: SA26-T and SA26-AT Description of Type Design Change:

Installation of recognition light assembly on the horizontal stabilizer in accordance with FAA sealed Drawing List 02600001, Revision C, or later FAA approved revision.

The approval of this change in type design applies to the basic models listed 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 of those other previously approved modifications will introduce no adverse efiect upon the airworthiness of the aircraft. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage.

Date of Application: June 14, 1977 Date Reissued: January 31, 2000 Date of Issuance: August 08, 1977 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Michel MOwskey (Signature) Michele M. Owsley, Manager TOMINISTRATIO Airplane Certification Office, Southwest Region (Title)

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) _ (Address of transferee) (23015s pico sequins') from (Name of grantor) (Prinl or type) (Address of grantor) (po26t5 paro sequen,") (City, Stake, and ZIP code) Extent of Authority (if licensing agreement):.

Date of Transier: - Signature of grantor (In ink): - + 11 = r. 0~. 1090-242-180

## Every issue (1)

- January 31, 2000: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/77/47/77474409a97b9c52c10439ede329e0b7202cfd4d2f92b41d3b835bd0f2a67142)

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