STC SA2626CE

Supplemental type certificate · Aviation Fabricators Inc

Holder
Aviation Fabricators Inc · United States
Status
Current · Amended
Status date
January 28, 2003
Applied
August 7, 1989
Product
Aircraft · Small Multi-Engine
Certification basis
Part 3, Part 21
Data sheet
TCDS3A20

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of a two-place facing divan.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

Number SA2626CE This certificate issued to Aviation Fabricators 805 N. 4th Street Clinton, MO 64735

Part 3 of the Civil Air Regulations. effective May 15, 1956, plus amendments listed in the Type Certificate Data Sheet.

Original Product--Type Certificate Number : 3A20 Make : Beech 65, A65, 65-80, 65-A80, 65-88, 65-90, 65-A80-8800, 65-A90, B90, C90, E90, 65-B80, A65-8200, C90A, H90, 70 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-156, Rev. (C), 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)

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 16

MakeModelData sheet
Raytheon Aircraft Company65 (L-23F)3A20
Raytheon Aircraft Company65-803A20
Raytheon Aircraft Company65-883A20
See all 16 models