# STC SA2906WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: DeVore Aviation Corporation of America, a New Mexico Corporation, United States
- Description: Installation of vertical tail floodlights on horizontal stabilizer.
- Applied: April 19, 1974
- Status date: January 31, 2000
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A22CE](https://openairdocs.org/tcds/A22CE)
- Certificate PDF: https://openairdocs.org/files/sha256/02/79/0279c11295557115e9cb690ce14bf4d4a488f4696efd234c72aa227c1febdf4e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/123BE890E8CF2DFD86257D7E00715818.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2906WE

## ADs that name it (0)

None.

## Approved models (2)

- Cessna Aircraft Company 500 ([TCDS A22CE](https://openairdocs.org/tcds/A22CE))
- Cessna Aircraft Company 550 ([TCDS A22CE](https://openairdocs.org/tcds/A22CE))

## 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: SA2906WE This certificate issued to: DeVore Aviation Corporation of America, a New Mexico Corporation 6104-B Jefferson, N.E.

Albuquerque, NM 87109-3410 Furt 25 of the Federa). Aviation Regulalion (See T. C. Data Sheet A22CE for Certification Requirements) .

Original Product Type Certificate Number : A22CE Make: Cessna Model: 500, 550 Description of Type Design Change:

Installation of vertical tail flood lights on horizontal stabilizer per FAA sealed DeVore Top Drawing 50000001.

The approval of this change in type design applies basically to Cessna 500, 550 models. This approval should not be extended to other 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.

Owsley, Manager Nickel MAusler (Signature) TOMINSTRATO 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 (2)

- January 31, 2000: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/02/79/0279c11295557115e9cb690ce14bf4d4a488f4696efd234c72aa227c1febdf4e)
- February 28, 1980: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/02/79/0279c11295557115e9cb690ce14bf4d4a488f4696efd234c72aa227c1febdf4e)

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