# STC SA1126EA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: DeVore Aviation Corporation of America, a New Mexico Corporation, United States
- Description: Installation of DeVore vertical tail floodlights on upper surface of stabilator
- Applied: May 16, 1978
- Status date: January 31, 2000
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 1A10](https://openairdocs.org/tcds/1A10)
- Certificate PDF: https://openairdocs.org/files/sha256/e6/ad/e6adc781ef494c10a754dbde811bafdafbc0235744f3dc86942f7b685fbdf55b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/72719291C92C514486257D41004F6298.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1126EA

## ADs that name it (0)

None.

## Approved models (3)

- Piper Aircraft Inc. PA-23-235 ([TCDS 1A10](https://openairdocs.org/tcds/1A10))
- Piper Aircraft Inc. PA-23-250 ([TCDS 1A10](https://openairdocs.org/tcds/1A10))
- Piper Aircraft Inc. PA-E23-250 ([TCDS 1A10](https://openairdocs.org/tcds/1A10))

## 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: SA1126EA 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 Civi1 Aix Fegulations.

Original Product Type Certificate Number: 1A10 Make: Piper Model: PA-23-235, PA-23-250 S/N 27-1 thru 27-7554172, PA-E23-250 S/N 27-2505 thru 27-7554172, PA-23-250 (model "F") S/N Description of Type Design Change: 27-7654001 and up Installation of DeVore Vertical Tail Floodlights on upper surface of stabilator in accordance with data listed on DeVore Drawing No. 92300001 Revision C, dated August 21, 1978, "Top Drawing Tail Floodlight Installation Piper PA-23 Series" or later FAA approved revisions.

The approval of this change in type design applies to the PA-23 series aircraft 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 effect upon the airworthiness of that aircraft. This determination should include consideration of significant change in weight distribution such as an increase in the fixed disposable weight of the fuselage.

Date of Application: May 16, 1978 Date Reissued: 9/28/78; 1/31/00 Date of Issuance: August 08, 1978 Date Amended: 8/25/78; 8/31/79 FEDERAL AVIATION By Direction of the Administrator Michele MAuster (Signature) Michele M. Owsley, Manager TOMINISTRATO Airplane Certification Office, Southwest Region (Title) 47

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 and street) (City, State, and Z1P code) Exent of Authority (if licensing agreement) :

Signature of grantor (In ink) :

## Every issue (1)

- January 31, 2000: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e6/ad/e6adc781ef494c10a754dbde811bafdafbc0235744f3dc86942f7b685fbdf55b)

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