# STC SA1367SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc
- Description: Installation of Collins AP104 Autopilot and single FD108N Flight Director.
- Status date: December 1, 2016
- Data sheets: A3EU
- Certificate PDF: https://openairdocs.org/files/sha256/2c/24/2c2453ba6920d35c2b12cbdb5a150d8feaa683b9edb8daaccd73c8f6d4a9dd77
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A1863E30CED75F8E862581480059A9E3.0001
- Page: https://openairdocs.org/stc/SA1367SW

## ADs that name it

None.

## Approved models (1)

- Raytheon Aircraft Company BH.125 Series 600A (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 SA1367SW Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 3 Civil Air Regulations 10/4b Installation of Collins AP104 Autopilot and single FD108N Flight Director according to Beech Aircraft Corporation Drawing 125-001111 original issue date 09/15/71, Specification 21928A revised 03/17/71, R-84182-NA761, COD14289, DO 7984, COD 15787, D16311.

Beechcraft Hawker BH125-400A

1. Equipment mounting racks must be installed per STCs SA764CE and SA757CE.

2. FAA approved Airplane Flight Manual Supplement dated September 17, 1971, required.

(see continuation sheet 3 of 3) February 18, 1972; April 15, 1996;

March 26, 2007; December 1, 2016 July 27, 1971 September 17, 1971 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

SA1367SW Date of Issuance: September 17, 1971 Date Reissued: December 1, 2016

3. 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.

4. 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 -- 3

## Every issue (2)

- December 1, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/2c/24/2c2453ba6920d35c2b12cbdb5a150d8feaa683b9edb8daaccd73c8f6d4a9dd77)
- March 26, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/78/1d/781ddd46ba67e386e8b2ff7798dfde62831f9359366e5e97d675e2d9017b9787)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.