# STC SA00872SE - Type: Supplemental type certificate - Status: Current, Amended - Holder: American Aviation Inc, United States - Description: Installation of modified ram air engine induction system (Option I or Option II). - Applied: January 20, 1999 - Status date: February 24, 2009 - Product: Aircraft, Small Multi-Engine - Certification basis: Part 21 - Data sheets: [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A14CE](https://openairdocs.org/tcds/A14CE), [TCDS A31CE](https://openairdocs.org/tcds/A31CE) - Certificate PDF: https://openairdocs.org/files/sha256/5a/bb/5abb330782ea10e1af5f49a3e1e688c1da33a4e5b90a8c39b471f44b065cb277 - Approved model list and other attachments: [sa00872se aml.pdf](https://openairdocs.org/files/sha256/02/72/0272ead09ecf521261bb3c1410f00f689ba7d5fae02852396ad61e9ffb0eb98f) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D0EDCFF546D0D2008625757500605EC5.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00872SE ## ADs that name it (0) None. ## Approved models (10) - Hawker Beechcraft Corporation 100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE)) - Hawker Beechcraft Corporation 65-90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Hawker Beechcraft Corporation 65-A90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Hawker Beechcraft Corporation 65-A90-1 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Hawker Beechcraft Corporation 65-A90-4 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Hawker Beechcraft Corporation A100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE)) - Hawker Beechcraft Corporation B90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Hawker Beechcraft Corporation C90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Hawker Beechcraft Corporation E90 ([TCDS 3A20](https://openairdocs.org/tcds/3A20)) - Hawker Beechcraft Corporation F90 ([TCDS A31CE](https://openairdocs.org/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. Number SA00872SE This certificate, issued to: American Aviation, Inc. 10555 Airport Drive Coeur d'Alene Airport Hayden Lake, ID 83835 Part * of the * Regulations. Original Product⎯Type Certificate Number: *See attached Approved Model List (AML) Make: No. SA00872SE for list of approved aircraft Model: models and applicable airworthiness regulations Description of the Type Design Change : Installation of modified ram air engine induction system (Option I or Option II) in accordance with American Aviation data referenced on Approved Model List (AML) SA00872SE dated February 24, 2009, or later FAA approved revision. Limitations and Conditions: 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. Aircraft modified per this STC must be operated in accordance with the appropriate Airplane Flight Manual Supplement (AFMS) given in AML SA00872SE. A copy of this certificate, the appropriate AFMS and AML SA00872SE 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: January 20, 1999 Date reissued: Date of issuance: March 25, 1999 Date amended: November 30, 1999; August 31, 2000, February 24, 2009 (Signature) Manager, Seattle Aircraft Certification Office (Title) ### sa00872se aml.pdf FAA APPROVED MODEL LIST (AML) NO. SA00872SE FOR INSTALLATION OF AMERICAN AVIATION INC. INDUCTION SYSTEM Issue Date : July 12, 2001 **ITEM AIRPLANE MAKE** **AIRPLANE MODEL TYPE** **CERTIFICATE NUMBER** **CERTIFICATION BASIS FOR** **ALTERATION** DRAWING LIST _______________ **NUMBER DATE** **AIRPLANE FLIGHT MANUAL** **SUPPLEMENT** **OPTION** 1. Beech 65-90, 65-A90, B90, C90, E90 3A20 CAR 3 200-TDL January 19, 2009 A200-1 or A200-2 dated 2/24/09 Option I & II 2. Beech F90 A31CE FAR 23 200-TDL January 19, 2009 A200-1 dated 2/24/09 Option I & II 3. Beech 100 A14CE FAR 23 200-TDL January 19, 2009 A200-1 dated 2/24/09 Option I & II 4. Beech A100 A14CE FAR 23 200-TDL January 19, 2009 A200-1 dated 2/24/09 Option I & II 5. Beech 65-A90-1 3A20 CAR 3 200-TDL January 19, 2009 A200-1 dated 2/24/09 Option I & II 6. Beech 65-A90-4 3A20 CAR 3 200-TDL January 19, 2009 A200-1 dated 2/24/09 Option I & II Note: Option I includes both the installation of the internal vanes, associated mechanism and the American Aviation “pitot inlet”. Option II includes only the installation of the internal vanes a nd associated mechanism installed in the original cowling. Approved:______________________________ M a n a g e r Seattle Aircraft Certification Office Amendend August 3, 2001, February 24, 2009 ## Every issue (1) - February 24, 2009: Amended, Current. [certificate](https://openairdocs.org/files/sha256/5a/bb/5abb330782ea10e1af5f49a3e1e688c1da33a4e5b90a8c39b471f44b065cb277), [sa00872se aml.pdf](https://openairdocs.org/files/sha256/02/72/0272ead09ecf521261bb3c1410f00f689ba7d5fae02852396ad61e9ffb0eb98f) --- 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.