# STC SA01085SE - Type: Supplemental type certificate - Status: Current, Amended - Holder: BAS Inc, United States - Description: Installation of BAS, Inc. of Shoulder Harness per the appropriate BAS Report listed on FAA AML SA01085SE, dated May 13, 2002, or later FAA approved revision. - Applied: May 13, 2002 - Status date: December 2, 2010 - Product: Aircraft, Single-Engine - Certification basis: Part 21 - Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15), [TCDS 3A16](https://openairdocs.org/tcds/3A16), [TCDS A-777](https://openairdocs.org/tcds/A-777) - Certificate PDF: https://openairdocs.org/files/sha256/f2/35/f235fa7e3d215154e72c6bde147d6dfc9ecc25d7ea20bc26539a6bded6bf41e4 - Approved model list and other attachments: [SA01085SE.pdf](https://openairdocs.org/files/sha256/b6/aa/b6aab60e10f5e2a96cd89aa059c5035105c598a0d384d8e00c1a644d4b7edce3) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D6CF7834948EAEA9862577FB005EC16F.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA01085SE ## ADs that name it (0) None. ## Approved models (55, first 50) - Hawker Beechcraft Corporation 35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation 35-33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 35-A33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 35-B33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 35-C33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 35-C33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 35R ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation 56TC ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation 58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation 58A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation 95 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation 95-55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation 95-A55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation 95-B55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation 95-B55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation 95-B55B ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation 95-C55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation 95-C55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation A35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation A36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation A56TC ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation B35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation B36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation B95 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation B95A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation C35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation D35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation D55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation D55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation D95A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation E33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation E33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation E33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation E35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation E55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation E55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation E95 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Hawker Beechcraft Corporation F33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation F33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation F33C ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation F35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation G33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation G35 ([TCDS A-777](https://openairdocs.org/tcds/A-777)) - Hawker Beechcraft Corporation H35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation J35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation K35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation M35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Hawker Beechcraft Corporation N35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) All 55: https://openairdocs.org/stc/SA01085SE/models.md ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. FAA APPROVED MODEL LIST (AML) No. SA01085SE BAS, Inc. SHOULDER HARNESS INSTALLATION ORIGINAL ISSUE DATE: May 13, 2002 **ORIGINAL FAA APPROVED DRAWING / DRAWING LIST** ITEM AIRCRAFT MAKE AIRCRAFT MODEL TYPE CERTIFICATION BASIS FOR AML AMENDMENT DATE CERTIFICATE ALTERATION REVISION NO. AND DATE NUMBER NUMBER Or Later FAA-Approved Revision 1 Hawker-Beechcraft 35, A35, B35, C35, D35, E35, F35, G35, 35R A-777 Type Certificate A-777 CAR 3, and Report No. 1003 August 29, 2002 December 02, 2010 35-33, 35-А33, 35-B33, 35-C33, 35-C3ЗА, Е33, E33A, E33C, F33, 2 Hawker-Beechcraft J35, K35, M35, N35, F33A, F33C, G33, H35, ЗА15 Type Certificate 3A15 CAR 3, and Report No. 1003 August 29, 2002 December 02, 2010 P35, S35, V35, V35A V35B, 36, A36, A36TC, B36TC 95, B95, B95A, B95A, D95A, E95, 95-55, 95-A55, 95-B55, Hawker-Beechcraft (T-42A), 95-C55, 95-B55A, 95-B55B ЗА16 Type Certificate 3A16 CAR 3, and Report No. 1003 August 29, 2002 December 02, 2010 95-C55A, D55, D55A, E55, E55A, 56TC, A56TC, 58, 58A FAA Approved: Acting Manager, Seattle Aircraft Certification Office Reissued: Amended: December 02, 2010 Page 1 of 1 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01085SE This certificate issued to: BAS, Inc. 411 Super Cub Drive North PO Box 190 Eatonville, WA 98328 Part * of the * Regulations. Original Product -Type Certificate Number: * See Attached FAA Approved Model List SA01085SE Make: for List of Approved Airplane Models Model: and Applicable Airworthiness Regulations Description of Type Design Change: Installation of BAS, Inc. Shoulder Harness in accordance with the appropriate BAS Report listed on FAA Approved Model List (AML) SA01085SE, dated May 13, 2002, 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. A copy of this certificate and FAA Approved Model List SA01085SE 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: August 06, 2001 Date Reissued: Date of Issuance: May 13, 2002 Date Amended: December 02, 2010 FEDERAL AVIATION By Direction of the Administrator HOMINIST RATION (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ### SA01085SE.pdf This is OCR from the scanned FAA attachment. OCR can misread letters and numbers. United States of America Department of Oransportation Federal Auiation Administration Supplemental Ogpe Certificate Number SA01085SE This certificate, issued to: BAS, Inc. 411 Super Cub Drive North PO Box 190 Eatonville, WA 98328 certifies that the change in the type design for the following product with the limitations and conditions therefore as specified hereon meets the airworthiness requirements of Part * of the * Regulations. Original Product-Type Certificate Number: * See Attached FAA Approved Model List SA01085SE Make: for List of Approved Airplane Models Model: and Applicable Airworthiness Regulations Description of the Type Design. Change: Installation of BAS, Inc. Shoulder Harness in accordance with the appropriate BAS Report listed on FAA Approved Model List (AML) SA01085SE, dated May 13, 2002, 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. A copy of this certificate and FAA Approved Model List SA01085SE 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. 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: August 06, 2001 Date reissued: Date of issuance: May 13, 2002 Date amended: December 02, 2010 FEDERAL AVIATION By divection of the Administrator HOMINIST RATION (Signature) Acting Manager, Seattle 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. This certificate may be transferred in accordance with FAR 21.47. **FAA FORM 8110-2 (10-68)** FAA APPROVED MODEL LIST (AML) No. SA01085SE BAS, Inc. for SHOULDER HARNESS INSTALLATION ORIGINAL ISSUE DATE: May 13, 2002 **ORIGINAL FAA APPROVED DRAWING / DRAWING LIST** ITEM AIRCRAFT MAKE AIRCRAFT MODEL TYPE CERTIFICATION BASIS FOR AML AMENDMENT DATE CERTIFICATE ALTERATION REVISION NO. AND DATE NUMBER NUMBER Or Later FAA-Approved Revision 1 Hawker-Beechcraft 35, A35, B35, C35, D35, E35, F35, G35, 35R A-777 Type Certificate A-777 CAR 3, and Report No. 1003 August 29, 2002 December 02, 2010 35-33, 35-А33, 35-B33, 35-C33, 35-C3ЗА, Е33, E33A, E33C, F33, 2 Hawker-Beechcraft J35, K35, M35, N35, F33A, F33C, G33, H35, ЗА15 Type Certificate 3A15 CAR 3, and Report No. 1003 August 29, 2002 December 02, 2010 P35, S35, V35, V35A V35B, 36, A36, A36TC, B36TC 95, B95, B95A, B95A, D95A, E95, 95-55, 95-A55, 95-B55, Hawker-Beechcraft (T-42A), 95-C55, 95-B55A, 95-B55B ЗА16 Type Certificate 3A16 CAR 3, and Report No. 1003 August 29, 2002 December 02, 2010 95-C55A, D55, D55A, E55, E55A, 56TC, A56TC, 58, 58A FAA Approved: Acting Manager, Seattle Aircraft Certification Office Reissued: Amended: December 02, 2010 Page 1 of 1 ## Every issue (1) - December 2, 2010: Amended, Current. [certificate](https://openairdocs.org/files/sha256/f2/35/f235fa7e3d215154e72c6bde147d6dfc9ecc25d7ea20bc26539a6bded6bf41e4), [SA01085SE.pdf](https://openairdocs.org/files/sha256/b6/aa/b6aab60e10f5e2a96cd89aa059c5035105c598a0d384d8e00c1a644d4b7edce3) --- 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.