# STC SA4157SW

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Aviation Fabricators Inc
- Description: Install one, two, or three place side facing seat (frame only).
- Status date: August 25, 2010
- Data sheets: 3A20, 3A20, 3A20, 3A20, 3A20, 3A20, 3A20, 3A20, 3A20, 3A20, 3A20, 3A20, 3A20, 3A20, 3A20, 3A20, 3A20, 3A20, 3A20, A14CE, A14CE, A14CE, A14CE, A14CE, A14CE, A14CE, A14CE, A14CE, A14CE, A14CE, A14CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A24CE, A31CE
- Certificate PDF: https://openairdocs.org/files/sha256/16/b0/16b037863bf60dc05373754f4fc1a9f033a965dde26882b1e9b21296ccbd1abd
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/11CF1FD2CAD270BE862577D700585101.0001
- Page: https://openairdocs.org/stc/SA4157SW

## ADs that name it

None.

## Approved models (62)

- Hawker Beechcraft Corporation 100 (TCDS A14CE)
- Hawker Beechcraft Corporation 200 (TCDS A24CE)
- Hawker Beechcraft Corporation 200C (TCDS A24CE)
- Hawker Beechcraft Corporation 200CT (TCDS A24CE)
- Hawker Beechcraft Corporation 200T (TCDS A24CE)
- Hawker Beechcraft Corporation 300 (TCDS A24CE)
- Hawker Beechcraft Corporation 300LW (TCDS A24CE)
- Hawker Beechcraft Corporation 65 (TCDS 3A20)
- Hawker Beechcraft Corporation 65-80 (TCDS 3A20)
- Hawker Beechcraft Corporation 65-88 (TCDS 3A20)
- Hawker Beechcraft Corporation 65-90 (TCDS 3A20)
- Hawker Beechcraft Corporation 65-A80 (TCDS 3A20)
- Hawker Beechcraft Corporation 65-A80-8800 (TCDS 3A20)
- Hawker Beechcraft Corporation 65-A90 (TCDS 3A20)
- Hawker Beechcraft Corporation 65-A90-1 (TCDS 3A20)
- Hawker Beechcraft Corporation 65-A90-2 (TCDS 3A20)
- Hawker Beechcraft Corporation 65-A90-3 (TCDS 3A20)
- Hawker Beechcraft Corporation 65-A90-4 (TCDS 3A20)
- Hawker Beechcraft Corporation 65-B80 (TCDS 3A20)
- Hawker Beechcraft Corporation 99 (TCDS A14CE)
- Hawker Beechcraft Corporation 99A (TCDS A14CE)
- Hawker Beechcraft Corporation 99A (FACH) (TCDS A14CE)
- Hawker Beechcraft Corporation A100 (TCDS A14CE)
- Hawker Beechcraft Corporation A100A (TCDS A14CE)
- Hawker Beechcraft Corporation A100C (TCDS A14CE)
- Hawker Beechcraft Corporation A200 (C-12A) (TCDS A24CE)
- Hawker Beechcraft Corporation A200 (C-12C) (TCDS A24CE)
- Hawker Beechcraft Corporation A200C (UC-12B) (TCDS A24CE)
- Hawker Beechcraft Corporation A200CT (C-12D) (TCDS A24CE)
- Hawker Beechcraft Corporation A200CT (C-12F) (TCDS A24CE)
- Hawker Beechcraft Corporation A200CT (FWC-12D) (TCDS A24CE)
- Hawker Beechcraft Corporation A200CT (RC-12D) (TCDS A24CE)
- Hawker Beechcraft Corporation A200CT (RC-12G) (TCDS A24CE)
- Hawker Beechcraft Corporation A200CT (RC-12H) (TCDS A24CE)
- Hawker Beechcraft Corporation A200CT (RC-12K) (TCDS A24CE)
- Hawker Beechcraft Corporation A200CT (RC-12P) (TCDS A24CE)
- Hawker Beechcraft Corporation A200CT (RC-12Q) (TCDS A24CE)
- Hawker Beechcraft Corporation A65 (TCDS 3A20)
- Hawker Beechcraft Corporation A65-8200 (TCDS 3A20)
- Hawker Beechcraft Corporation A99 (TCDS A14CE)
- Hawker Beechcraft Corporation A99A (TCDS A14CE)
- Hawker Beechcraft Corporation B100 (TCDS A14CE)
- Hawker Beechcraft Corporation B200 (TCDS A24CE)
- Hawker Beechcraft Corporation B200C (TCDS A24CE)
- Hawker Beechcraft Corporation B200C (C-12F) (TCDS A24CE)
- Hawker Beechcraft Corporation B200C (C-12R) (TCDS A24CE)
- Hawker Beechcraft Corporation B200C (UC-12F) (TCDS A24CE)
- Hawker Beechcraft Corporation B200C (UC-12M) (TCDS A24CE)
- Hawker Beechcraft Corporation B200CGT (TCDS A24CE)
- Hawker Beechcraft Corporation B200CT (TCDS A24CE)
- Hawker Beechcraft Corporation B200GT (TCDS A24CE)
- Hawker Beechcraft Corporation B200T (TCDS A24CE)
- Hawker Beechcraft Corporation B300 (TCDS A24CE)
- Hawker Beechcraft Corporation B300C (C-12W) (TCDS A24CE)
- Hawker Beechcraft Corporation B90 (TCDS 3A20)
- Hawker Beechcraft Corporation B99 (TCDS A14CE)
- Hawker Beechcraft Corporation C90 (TCDS 3A20)
- Hawker Beechcraft Corporation C90A (TCDS 3A20)
- Hawker Beechcraft Corporation C90GT (TCDS 3A20)
- Hawker Beechcraft Corporation C99 (TCDS A14CE)
- Hawker Beechcraft Corporation E90 (TCDS 3A20)
- Hawker Beechcraft Corporation F90 (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.

**FAA APPROVED MODEL LIST (AML) NO. SA4157SW AVIATION FABRICATORS, INC.**

FOR INSTALLATION OF SIDE FACING SEATS Aviation Fabricators, Inc.

805 North Fourth Street Clinton, MO 64735

Issue Date: July 28, 1980 Re-issued: November 15, 2004, October 24, 2007, August 25, 2010

FAA Approved: Original signed by Steve Litke Steven Litke, Program Manager Wichita Aircraft Certification Office

Note (1): Installation of one, tw o, or three place side facing seats (frame only) according to Drawing B6912 dated 7/4/80, or later FAA approved revision; or according to Aviation Fabricators Drawing list AF-291 dated August 14, 2002, “FAA approved August 14, 2002” or later FAA approved revision.

**ITEM AIRCRAFT MAKE AIRCRAFT MODEL ORIG.**

**TYPE CERT.**

**NUMBER**

**CERTIFICATION**

**BASIS FOR**

**ALTERATION MASTER**

**DRAWING LIST NUMBER REVISION LEV. DATE AFM**

**SUPPLEMENT**

**NUMBER/ DATE AML**

**AMENDMENT DATE**

1. Beechcraft 65, A65, A65-8200, 65-80, 65- A80, 65-A80-8800, 65-B80, 65- 88, 65-90, 65-A90-1, 65-A90-2, 65-A90-3, 65-A90-4, 65-A90, B90, C90, C90A, C90GT, E90 3A20 FAR 23, plus Amendments listed in the TCDS See Note (1) N/A AML updated at STC amendment date 10/24/07

2. Beechcraft F90 A31CE FAR 23, plus Amendments listed in the TCDS See Note (1) N/A AML updated at STC amendment date 10/24/07

3. Beechcraft 99, 99A, A99, A99A, B99, C99, 100, A100, A100A, A100C, B100 A14CE FAR 23, plus Amendments listed in the TCDS See Note (1) N/A AML updated at STC amendment date 10/24/07

4. Beechcraft 200, 200C, 200CT, 200T, A200, A200C, A200CT, B200, B200C, B200CT, B200T, B200GT, B200CGT, 300, B300, B300C, 300LW A24CE FAR 23, plus Amendments listed in the TCDS See Note (1) N/A AML updated at STC amendment date 08/25/2010

### SA4157SW.pdf

United States of America Department of Transportation -- Federal Aviation Administration Supplemental Type Certificate

Number SA4157SW RE-ISSUED ON NOVEMBER 15, 2004 TO SUPERSEDE THE ORIGINAL STC WHICH HAS BEEN LOST OR MISPLACED.

This certificate issued to: Aviation Fabricators 805 North Fourth Street Clinton, NO 64735

certifies that the change in the type design for the following product with the limitations and conditions therefor as specified hereon meets the airworthiness requirements of Part 3 of the Civil Air Regulations.

Original Product - Type Certificate Number :

Make: * See Approved Model List * Model:

Description of Type Design Change:

Installation of one, two, or three place side facing seat (frame only) according to Drawing B6912 dated 7/4/80, or later FAA approved revision; or Aviation Fabricators drawing list AF-291, no revision, dated August 14, 2002, or later FAA approved revision.

Limitations and Conditions:

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. Compatibility of this modification with previously approved modifications must be determined by the installer. 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.

This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application : July 15, 1980 Date of issuance : July 28, 1980 Date reissued : November 1, 1993; November 15, 2004

Date amended : February 11, 2003; March 31, 2004

By direction of the Administrator

Original signed by Joel M. Ligon

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

_____________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.

_____________________________________________________________________________________________________________________________________ FAA FORM 8110-2(10-68) PAGE 1 of 1 PAGES This certificate may be transferred in accordance with FAR 21.47.

## Every issue (2)

- August 25, 2010: Amended, Current. [certificate](https://openairdocs.org/files/sha256/16/b0/16b037863bf60dc05373754f4fc1a9f033a965dde26882b1e9b21296ccbd1abd), [SA4157SW.pdf](https://openairdocs.org/files/sha256/96/4a/964a631b34064368c1143c5ffa975d48ea78bacf5c8dd89ee034983a36559642)
- November 15, 2004: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/96/4a/964a631b34064368c1143c5ffa975d48ea78bacf5c8dd89ee034983a36559642), [SA4157SWAML.pdf](https://openairdocs.org/files/sha256/ff/69/ff69b3bd99d86efa6990130f32cac6349925ccbb94c3c0323fe8bbf8ed9322db)

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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.
