# STC SA2943WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: DeVore Aviation Corporation of America, a New Mexico Corporation, United States
- Description: Installation of recognition lights on horizontal stabilizer upper surface.
- Applied: August 5, 1974
- Status date: January 31, 2000
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 2A15](https://openairdocs.org/tcds/2A15)
- Certificate PDF: https://openairdocs.org/files/sha256/c0/e5/c0e5544a09ab12e34e5002afbb886794570c1d8722e18df6c5cdf345b49010e1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FDC691FCB8CFD7B886257D7F00575E04.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2943WE

## ADs that name it (0)

None.

## Approved models (4)

- Lockheed Martin Corporation 1329-23A ([TCDS 2A15](https://openairdocs.org/tcds/2A15))
- Lockheed Martin Corporation 1329-23D ([TCDS 2A15](https://openairdocs.org/tcds/2A15))
- Lockheed Martin Corporation 1329-23E ([TCDS 2A15](https://openairdocs.org/tcds/2A15))
- Lockheed Martin Corporation 1329-25 ([TCDS 2A15](https://openairdocs.org/tcds/2A15))

## 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: SA2943WE This certificate issued to: DeVore Aviation Corporation of America, a New Mexico Corporation 6104-B Jefferson, N.E.

Albuquerque, NM 87109-3410 Purt Ab of the Civil Air Regulalions CAR 4b dated Dec. 31, 1953 and Amdt's. 4b-1 thru 4b-9 together with revised Jan. 10, 1961. SR-422B and special conditions in FAA letter to Lockheed dated Dec. 19, 1958 and Original Product Type Certificate Number : 2A15 Make: Lockheed Model: 1329-23A, 1329-23D, 1329-23E, 1329-25 Description of Type Design Change:

Installation of recognition lights on horizontal stabilizer upper surface in accordance with installation drawings listed on FAA sealed Top Drawing 32900001, Rev. "C" or later FAA sealed revisions.

The approval of this change in type design applies basically to the Lockheed Model 1329 aircraft only. This approval should not be extended to aircraft of these models 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 effect upon the airworthiness of that 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: August 05, 1974 Date Reissued: January 31, 2000 Date of Issuance: October 20, 1974 Date Amended: 1/23/76; 3/11177 FEDERAL AVIATION By Direction of the Administrator Michel MOurlen (Signature) Michele M. Owsley, Manager TOMINSTRATOR Airplane Certification Office, Southwest Region (Title)

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number & street) (City, State, and ZIP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- January 31, 2000: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c0/e5/c0e5544a09ab12e34e5002afbb886794570c1d8722e18df6c5cdf345b49010e1)

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