# STC SA01051SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Enflite Inc., United States - Description: Installation of an interior sidewall folding table, part numbers 56300-144-03 or 53600-144-04 - Applied: July 13, 1999 - Status date: May 10, 2019 - Product: Aircraft, Large Airplane - Certification basis: Part 21, Part 23, Part 43 - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) - Certificate PDF: https://openairdocs.org/files/sha256/a2/e9/a2e9cb525b90e1f89b38ebaa55a097301b6293fbeec78f5aaa2740dac1f62edc - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A1C683F23B54E8D8862585D00043751B.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA01051SE ## ADs that name it (0) None. ## Approved models (19) - 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 A200 (C-12A) ([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 B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE)) - Hawker Beechcraft Corporation B200T ([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. Number SA01051SE This certificate, issued to EnFlite, LLC. 105 Cooperative Way Georgetown, TX 78626 Part 23 of the Federal Aviation Regulations. Original ProductType Certificate Number: A24CE Make: Raytheon (Beech) Model: 200, 200C, 200CT, 200T, A200, A200C, A200CT, B200, B200C, B200CT, B200T Description of the Type Design Change: Installation of an interior sidewall folding table, part numbers 56300- 144-03 or 53600-144-04, in accordance with EnFlite Master Drawing List MDL53600, Revision T, dated January 24, 2002, or later FAA approved revision. Limitations and Conditions: Approval of this change in type design applies to the model aircraft listed above only. This approval should not be extended to aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer that the re lationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. 14 CFR Part 43 is adequate to insure continued Airworthiness of this modification. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft. 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: July 13, 1999 Date reissued: January 24, 2006; May 10, 2019 Date of issuance: February 14, 2002 Date amended: FAA FORM 8110-2 (5/14) PAGE 1 OF 2 PAGES By direction of the Administrator (Signature) Acting Manager, Seattle ACO Branch (Title) Transfer the ownership of Supplemental Type Certificate Number to (Name of Transferee) (Address of Transferee) (Number and Street) (City, State, and ZIP Code) from (Name of Grantor) (Print or Type) (Address of Grantor) (Number and Street) (City, State, and ZIP Code) Signature of Grantor (In Ink): U.S. GPO: 1987-763-289 ## Every issue (2) - May 10, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a2/e9/a2e9cb525b90e1f89b38ebaa55a097301b6293fbeec78f5aaa2740dac1f62edc) - January 24, 2006: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/59/b7/59b75f0466956203c3f042b0964dd2c77fb121081383433926a49a398ad8eec9) --- 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.