# STC SA2627CE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Aviation Fabricators Inc, United States
- Description: Installation of a two-place side facing divan.
- Applied: August 7, 1989
- Status date: January 28, 2003
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A31CE](https://openairdocs.org/tcds/A31CE)
- Certificate PDF: https://openairdocs.org/files/sha256/96/40/964034a5c239dab554b2c87f3d17f999e04d1af410482e8e83747a3eaa5c7300
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0865B47CF7796B2186256F7E0057C847.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2627CE

## ADs that name it (0)

None.

## Approved models (1)

- Raytheon Aircraft Company F90 ([TCDS A31CE](https://openairdocs.org/tcds/A31CE))

## 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.

Number SA2627CE This certificate issued to Aviation Fabricators 805 North Fourth Street Clinton, MO 64735

Part 23 of the Federal Aviation Regulations. effective February 1, 1965, plus amendments listed in the Type Certificate data Sheet.

Original Product--Type Certificate Number : A31CE Make : Beech F-90 Model :

Description of Type Design Change: Installation of a two-place side facing divan according to (1) Aviation Fabricators Drawing Number D10002B, stamped “FAA Approved” with a date of May 30, 1990, or later; or (2) Aviation Fabricators STC Data Package AF-112, Rev. (D), dated 07/21/98, stamped “FAA Approved”, with an approval date of October 28, 1998, or later FAA approved revision.

1. This STC must be installed per Aviation Fabricators Drawing D-10265, no revision, dated 07/21/98 or later FAA approved revision on airplanes manufactured after December 12, 1986 with nine or fewer passenger seats, including the divan. For other divan installations, Aviation Fabricators Drawing AF-155, Revision C, dated 05/30/97 or later FAA approved revision may be used.

2. Compatibility of this design change with previously approved modifications must be determined by the installer.

3. 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.

4. This STC approves only the installation of the parts contained in the above section “Description of Type Design Change.” The requirements for the aisle width, passenger oxygen system, Seats and Safety belts, and upholstery coverings will require a separate FAA approval to verify compatibility with installation of this STC.

Date of application : August 07, 1989

Date of issuance : May 30, 1990 Date reissued :

Date amended : October 28, 1998; January 28, 2003

( Signature) Joel M. Ligon Program Manager Wichita Aircraft Certification Office

(Title)

## Every issue (1)

- January 28, 2003: Amended, Current. [certificate](https://openairdocs.org/files/sha256/96/40/964034a5c239dab554b2c87f3d17f999e04d1af410482e8e83747a3eaa5c7300)

---
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.