# STC SA736CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Installation aerial camera supporting structure and related modifications.
- Applied: July 6, 1970
- Status date: December 14, 2016
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A14CE](https://openairdocs.org/tcds/A14CE)
- Certificate PDF: https://openairdocs.org/files/sha256/55/de/55de1ec023981c839b65a0b601cc908c8df1f2f72a995369e30aac3a17d2f785
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6DEABD3B06D553798625814D0070258A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA736CE

## ADs that name it (0)

None.

## Approved models (1)

- Raytheon Aircraft Company 99A ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))

## 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 SA736CE Federal Aviation Regulations.

23 Installation aerial camera supporting structure and related modifications as follows (Ref. Drawing List PDG 4042):

1. Install aerial camera supporting structure and opening in bottom of fuselage between Bulkhead Stations 227.0 and

266.50.

(see continuation sheet 3 of 3) Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation made in Beech Model 99A, Serial No. 134 only.

Beech 99A May 29, 2007; December 14, 2016 November 6, 1970 July 6, 1970 October 19, 1970 A14CE 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: October 19, 1970 Date Amended: November 6, 1970 Date Reissued: December 14, 2016

Description of Type Design Change (continued):

2. Install external door to cover camera opening when camera is not in use. Door to be operational in flight.

3. Relocate air conditioning evaporator coil and blower, relocate de-icing control valve without change to system arrangement and schematic. Reroute cabin air conditioning and heating ducts.

4. Provide cover for camera hole to support seat in standard configuration when camera is not installed.

-- END -- SA736CE 3

## Every issue (2)

- December 14, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/55/de/55de1ec023981c839b65a0b601cc908c8df1f2f72a995369e30aac3a17d2f785)
- May 29, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/9d/f3/9df3e4a8da3c87ec1257df14a0d2cb6cedea7a83dbbda7be1c10fa9dcbf7c6ed)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.