# STC SA01111SE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Raisbeck Engineering, United States - Description: Installation of engine plenum seal.` - Applied: January 2, 2002 - Status date: September 1, 2023 - Product: Aircraft, Small Multi-Engine - Certification basis: Part 23 - Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) - Certificate PDF: https://openairdocs.org/files/sha256/68/c6/68c6017976aab755fc004aba37b26536d333b6d98b1c2fc5bf464d32746d310d - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151649585920230925141255.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA01111SE ## ADs that name it (0) None. ## Approved models (5) - 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 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. FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: Page 1 of 2 SA01111SE Raisbeck Engineering Inc. 2811 South 102nd Street, Suite 100 Tukwila, WA 98168 Part 23 the Federal Aviation Regulations A24CE Raytheon Aircraft Company 300, B300, 300LW, and B300C Installation of engine plenum seal manufactured in accordance with Master Drawing List 201-7120, Revision IR, dated July 12, 2002, or later Federal Aviation Administration (FAA) approved revision, and installed in accordance with Installation Instructions 201-7123, Revision IR, dated July 2002, or later FAA approved revision. Maintain in accordance with Component Maintenance Manual 201-7127, Revision IR, dated July 2002, or later FAA approved revision. January 2, 2002 September 1, 2023 August 12, 2002 for Manager, West Certification Branch Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship 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. 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. FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: Page 2 of 2 SA01111SE ## Every issue (2) - September 1, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/68/c6/68c6017976aab755fc004aba37b26536d333b6d98b1c2fc5bf464d32746d310d) - August 12, 2002: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/cd/50/cd50afc279a95f9368502516e098a2ebaddc000ce79c25cdf87540f08dc4d694) --- 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.