# STC SA00635WI - Type: Supplemental type certificate - Status: Current, Amended - Holder: Aviation Fabricators Inc, United States - Description: Jump seat installation. - Applied: February 8, 1996 - Status date: July 30, 2013 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A14CE](https://openairdocs.org/tcds/A14CE), [TCDS A24CE](https://openairdocs.org/tcds/A24CE) - Certificate PDF: https://openairdocs.org/files/sha256/01/47/0147e24d7e9c05e0c5e4a3642e71ccfa5906e652027de60af8b56300b11685ef - Approved model list and other attachments: [SA00635WI_AML.pdf](https://openairdocs.org/files/sha256/2f/9b/2f9bdac321e38867f60c365aa9973d13950773b7d14e0cf6ef7036e07e358248) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D1B8FFC54196258686257BBB00525BDE.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00635WI ## ADs that name it (0) None. ## Approved models (41) - Beechcraft Corporation C90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation C90A ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation C90GT ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation C90GTi ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Beechcraft Corporation E90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Hawker Beechcraft Corporation 100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE)) - Hawker Beechcraft Corporation 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation 200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation 200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation 300LW ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE)) - Hawker Beechcraft Corporation A100A ([TCDS A14CE](https://openairdocs.org/tcds/A14CE)) - Hawker Beechcraft Corporation A100C ([TCDS A14CE](https://openairdocs.org/tcds/A14CE)) - Hawker Beechcraft Corporation A200 (C-12A) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200 (C-12C) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200C (UC-12B) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (C-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (FWC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (RC-12D) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (RC-12G) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (RC-12H) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (RC-12K) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (RC-12P) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation A200CT (RC-12Q) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE)) - Hawker Beechcraft Corporation B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C (C-12R) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C (UC-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C (UC-12M) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200CGT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200GT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B300C (MC-12W) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B300C (UC-12W) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) ## 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. This certificate issued to Aviation Fabricators 805 N. Fourth Street Clinton, MO 64735 Part 23 of the Federal Aviation Regulations. Make : See attached AML No. SA00635WI Model : Jump seat installation per Aviation Fabricators, Inc., Drawing Lists as described in the attached AML No. SA00635WI. Limitations and Conditions : Installation per STC Drawing List AF-209 limited to aircraft with Beech (Raytheon) factory installed oxygen system for jump seat locations. Aircraft configured for more than 14 total occupants must be equipped with a 49 cubic foot (or greater) oxygen system. Compatibility of this design change 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. Date of application: February 08, 1996 Date of issuance: March 02, 1998 Date amended: June 8, 2001, June 20, 2003, July 30, 2013 Original signed by Steve Litke (Signature) Steven C. Litke Program Manager Wichita Aircraft Certification Office (Titl ) ### SA00635WI_AML.pdf Page 1 of 1 FAA APPROVED MODEL LIST (AML) NO. SA00635WI AVIATION FABRICATORS, INC. **JUMP SEAT INSTALLATION** Issue Date: March 2, 1998 **ITEM AIRCRAFT MAKE AIRCRAFT MODEL ORIG.** **TYPE CERT.** **NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **MDL NUMBER** **REVISION LEVEL DATE AFM** **SUPPLEMENT** **NUMBER/DATE AML** AMENDMENT DATE 1 Beechcraft 100, A100, A100A, A100C, B100 A14CE FAR 23, dated 2/1/65 (See TCDS for Amendments and other certification basis) AF-209 Revision (B ) 7/30/97* N/A Original 2 Beechcraft 200, 200C, 200T, 200CT, A200, A200C, A200CT, B200, B200C, B200T, B200CT A24CE FAR 23, dated 2/1/65 (See TCDS for Amendments and other certification basis) AF-209 Revision (B ) 7/30/97* N/A Original 3 Beechcraft B200GT, B200CGT A24CE FAR 23, dated 2/1/65 (See TCDS for Amendments and other certification basis) AF-209 Revision (J ) 11/08/07* N/A 12/3/08 4 Beechcraft 300, 300LW, B300, B300C A24CE FAR 23, dated 2/1/65 (See TCDS for Amendments and other certification basis) AF-209 Revision (J ) 11/08/07* N/A 12/3/08 5 Beechcraft 100, A100, A100A, A100C, B100 A14CE FAR 23, dated 2/1/65 (See TCDS for Amendments and other certification basis) AF-251-1 Revision (B) 10/5/00* N/A 6/8/01 6 Beechcraft 200, 200C, 200T, 200CT, A200, A200C, A200CT, B200, B200C, B200T, B200CT, B200GT, B200CGT A24CE FAR 23, dated 2/1/65 (See TCDS for Amendments and other certification basis) AF-251-2 Revision (B) 10/5/00* N/A 4/3/08 7 Beechcraft 300, 300LW, B300, B300C A24CE FAR 23, dated 2/1/65 (See TCDS for Amendments and other certification basis) AF-251-3 Revision (-) 10/24/02* N/A 6/2/03 8 Beechcraft C90, C90A, C90GT, C90GTi, E90 3A20 FAR 23, dated 2/1/65 (See TCDS for Amendments and other certification basis) AF-251-4 Revision (A) 9/18/12* AF-525FMS Revision (IR) 4/17/13* 7/30/13 Notes: See STC for installation limitations. * or later FAA Approved Revision FAA Approved: Original signed by Steve Litke Steven C. Litke, Program Manager Wichita Aircraft Certification Office ## Every issue (4) - July 30, 2013: Amended, Current. [certificate](https://openairdocs.org/files/sha256/01/47/0147e24d7e9c05e0c5e4a3642e71ccfa5906e652027de60af8b56300b11685ef), [SA00635WI_AML.pdf](https://openairdocs.org/files/sha256/2f/9b/2f9bdac321e38867f60c365aa9973d13950773b7d14e0cf6ef7036e07e358248) - July 19, 2013: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/45/66/4566e9dc0628311e6a4b84fb76df5ff1964452bd8f1a3d4ae738b1e8c5b158cb) - April 3, 2008: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/87/95/87958caf67b9e675c5c31fecd538950df6bc8a4dbc2b10df21f773e1a862f26b) - June 20, 2003: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/ef/c6/efc6034e503859b4f412d6d2d29913134bf8e5a14e1e796579d3b83da2ae06a4) --- 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.