# STC SA1094CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Airplane Equipment Installation.
- Status date: December 12, 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/a7/d5/a7d52220e2907ffca90a2b08ecd3f70d37463bbcb820f6208c2e947ef29a3bbc
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DD3CFF3E4467E06D8625814800665F9B.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1094CE

## ADs that name it (0)

None.

## Approved models (1)

- Raytheon Aircraft Company BH.125 Series 600A ([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 Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 3 SA1094CE Civil Air Regulations.

4b Airplane Equipment Installation per FAA approved Beech Aircraft Corporation Drawing No. 125-001154 and Supplements Nos. 1 and 2, thereto. FAA approved Airplane Flight Manual Supplement, Part No. 131303, dated August 21, 1974, required.

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.

(see continuation sheet 3 of 3) Hawker Siddeley BH125-600A April 15, 1996; March 26, 2007;

December 12, 2016 June 19, 1974 August 21, 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)

FAA Form 8110-2 (5/14) Page 3 of

Date of Issuance: August 21, 1974 Date Reissued: December 12, 2016

Parts manufactured under this STC may have been produced without an FAA approved quality control procedure. Prior to installation, such parts must be inspected for conformity and airworthiness in accordance with FARs 21 and 43. 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.

-- END -- SA1094CE 3

## Every issue (2)

- December 12, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a7/d5/a7d52220e2907ffca90a2b08ecd3f70d37463bbcb820f6208c2e947ef29a3bbc)
- March 26, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/b7/9c/b79c4a51b8ad89cd0359ad6caf11aed353c7947575520105e8da33c069f964f7)

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