# STC SA2826CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Teledyne Controls, United States
- Description: Installation of optional set of B&D Instruments & Avionics, Inc. Electronic Exhaust Gas Temperature (EFT) Indicators.
- Applied: February 14, 1992
- Status date: November 3, 2011
- Product: Aircraft, Large Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 4A25](https://openairdocs.org/tcds/4A25)
- Certificate PDF: https://openairdocs.org/files/sha256/ac/91/ac9196fb9d3aaca23d631957b96319c02e4684b0e7d564d162cee14e11e52370
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D499F637B85BE04C86257B3C005DB2D6.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2826CE

## ADs that name it (0)

None.

## Approved models (6)

- The Boeing Company DC-8-71 ([TCDS 4A25](https://openairdocs.org/tcds/4A25))
- The Boeing Company DC-8-71F ([TCDS 4A25](https://openairdocs.org/tcds/4A25))
- The Boeing Company DC-8-72 ([TCDS 4A25](https://openairdocs.org/tcds/4A25))
- The Boeing Company DC-8-72F ([TCDS 4A25](https://openairdocs.org/tcds/4A25))
- The Boeing Company DC-8-73 ([TCDS 4A25](https://openairdocs.org/tcds/4A25))
- The Boeing Company DC-8-73F ([TCDS 4A25](https://openairdocs.org/tcds/4A25))

## 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: SA2826CE This certificate issued to: Teledyne Controls 501 Continental Blvd El Segundo, CA 90245 Part 25 of the Federal Aviation Regulations.

Original Product -Type Berlificate Number: 4A25 McDonnell Douglas Model DC-8-71, -71F, -72, -72F, -73, -73F Description of Type Design Change:

Installation of optional set of B&D Instruments & Avionics, Inc. Electronic Exhaust Gas Temperature (EFT) Indicators.

Data required: (1) B&D Instruments & Avionics, Inc. Installation and Operation Manual No. 65016-003-011, Ist Edition, Revision " , and/or Installation Manual No. 65003-003-011, I" Edition, Revision B, or later "FAA Approved" revision; and (2) copy of this certificate.

Eligible on airplanes that have been modified in accordance with Douglas Aircraft Service Bulletin No. 77-26, Revision 1, dated December 13, 1985. This approval should not be extended to other specific airplanes of these models on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of these other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane. 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.

recked or a termination date is otherwise established by the Administrator of the Irteral Aviation Administration.

Date of Application: February 14, 1992 Lieute reided: January 5, 1998; October 2, 2000;

June 30, 2003; November 3, 2011 Late of issunses: April 23, 1992 Date Amended: April 28, 1992; January 8, 1996;

February 3, 1997 By dirrelion of the Aulninistrater FEDERAL AVIATION Original signed by Raymond Johnston (Signature) Raymond N. Johnston TOMINSTRATOT Program Manager Wichita Aircraft Certification Office (Title)

## Every issue (1)

- November 3, 2011: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ac/91/ac9196fb9d3aaca23d631957b96319c02e4684b0e7d564d162cee14e11e52370)

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