# STC SA2631CE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Aviation Fabricators Inc, United States
- Description: Installation of a four-place side facing divan.
- Applied: May 30, 1990
- Status date: March 13, 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/sha256/4a/38/4a381478ac2a727406045df29de18c56ad4a05962e0655cc2554e559df23679b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/13C8FBFE100699C086256D65006A8E8C.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA2631CE

## 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.

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

Description of Type Design Change: Installation of a four-place side facing divan according to: (1) Aviation Fabricators Drawing Number D10003A, stamped "FAA Approved" with a date of May 30, 1990, or later FAA approved revision, or (2) Aviation Fabricators STC Data Package AF-279, stamped "FAA Approved" with an approval date of November 9, 1999, or later FAA approved revision.

1. This STC may not be installed on airplanes manufactured after December 12, 1986, except for airplanes configured with ten or more passenger seats, including the divan.

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 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.

Aviation Fabricators 805 North Fourth Street Clinton, MO 64735 A31CE Make: Beech Model: F90 Date of application : August 07, 1989

Date of issuance : May 30, 1990

Date amended : November 09, 1999; March 13, 2003

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

( Title)

## Every issue (1)

- March 13, 2003: Amended, Current. [certificate](https://openairdocs.org/files/sha256/4a/38/4a381478ac2a727406045df29de18c56ad4a05962e0655cc2554e559df23679b)

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