# STC SA1002CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Relocation of warning cancel switch from instrument panel to #1 engine power lever.
- Applied: January 16, 1974
- Status date: December 1, 2016
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A3EU](https://openairdocs.org/tcds/A3EU)
- Certificate PDF: https://openairdocs.org/files/sha256/50/08/500898b82dcf2da205e8ca78c11cdb16c2c607ab6323cacdcb5cb87419927cec
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E456AC889A69AAE8862581480059A489.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1002CE

## ADs that name it (0)

None.

## Approved models (5)

- Raytheon Aircraft Company BH.125 Series 400A ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))
- Raytheon Aircraft Company DH.125 Series 1A ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))
- Raytheon Aircraft Company DH.125 Series 3A ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))
- Raytheon Aircraft Company DH.125 Series 3A/RA ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))
- Raytheon Aircraft Company DH.125 Series 400A ([TCDS A3EU](https://openairdocs.org/tcds/A3EU))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title SA1002CE Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 2 Civil Air Regulations.

4b Relocation of warning cancel switch from instrument panel to #1 engine power lever. Data required:

1. Beech Aircraft Corporation Drawing No. 125-3005, Revision "A".

Hawker Siddeley DH-125-1A; DH125-3A; DH125-3ARA; DH125-400A;

BH125-400A This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those 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.

April 15, 1996; March 26, 2007;

December 1, 2016 January 16, 1974 March 4, 1974 A3EU Mark Fuller STC ODA administrator ODA-100129-CE

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

## Every issue (2)

- December 1, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/50/08/500898b82dcf2da205e8ca78c11cdb16c2c607ab6323cacdcb5cb87419927cec)
- March 26, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/7b/5f/7b5fa7a09004a1d9a09ef73e1fab2e46f14d947bc1ae0fcc7314b74fc8f8e738)

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