# STC SR00077IB - Type: Supplemental type certificate - Status: Current, Issued - Holder: Ascent Aerospace Ltd., Canada - Description: Installation of the Two Place Seat Assembly - Applied: November 22, 2022 - Status date: November 18, 2022 - Product: Aircraft, Rotorcraft - Certification basis: Part 29 - Foreign approvals: TCCA SH22-34 Issue 1 - Data sheets: [TCDS H1SW](https://openairdocs.org/tcds/H1SW), [TCDS H4SW](https://openairdocs.org/tcds/H4SW) - Certificate PDF: https://openairdocs.org/files/sha256/f4/06/f40671af550fcf64ac05db57de9e7c2e5f646f95b594fb7b8257c265cde94485 - Approved model list and other attachments: [SR00077IB AML.pdf](https://openairdocs.org/files/sha256/cc/75/cc75ecd5b05c0a684f204b082cd0ad646c7f1cb8e94cd0c6b59305f0637bea70) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143305570820221122125520.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR00077IB ## ADs that name it (0) None. ## Approved models (2) - Bell Textron Inc. 205A-1 ([TCDS H1SW](https://openairdocs.org/tcds/H1SW)) - Bell Textron Inc. 212 ([TCDS H4SW](https://openairdocs.org/tcds/H4SW)) ## 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. IMPORT SR00077IB Ascent Aerospace Ltd. 1550 Springhill Road Parksville, British Columbia Canada V9P 2T2 Part 29 Title 14 Code of Federal Regulations *See attached FAA Approved Model List (AML) SR00077IB *See attached FAA AML No. SR00077IB *See attached FAA AML No. SR00077IB 1. Installation of the Two Place Seat Assembly must be done in accordance with Avio Design Group Inc. (Avio dg) Modification Instructions as shown on the attached FAA Approved Model List (AML) No. SR00077IB. 2. Definition of the Type Design Change is found in Avio dg Master Data List as shown on the attached FAA AML No. SR00077IB. 1. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. (Limitations and Conditions Continued on Page 3 of 3) November 1, 2022 November 18, 2022 Anthony E. Gallo Manager, International Validation Branch (AIR-730) Compliance & Airworthiness Division Aircraft Certification Service (AIR) 3 **IMPORT SR00077IB SR00077IB 3** IMPORT SR00077IB Date of Issuance: November 18, 2022 2. The installer must determine whether this design change is compatible with previously approved modifications. 3. This STC is applicable to all serial numbers for the Make and Models as shown on the attached FAA AML No. SR00077IB. 4. A copy of this certificate and the FAA AML No. SR00077IB, issued November 18, 2022, must be maintained as part of the permanent records for the modified aircraft. ----------END---------- 3 3 ### SR00077IB AML.pdf FAA APPROVED MODEL LIST (AML) No. SR00077IB ASCENT AEROSPACE LTD. For Two Place Seat Assembly Installation Page 1 of 1 Issue Date: November 18, 2022 **CONFIG MAKE MODEL CERT BASIS** **TCDS REQUIRED DOCUMENTATION INITIAL** **APPROVAL DATE** **AMENDED** **DATE MODIFICATION** **INSTRUCTIONS** **MASTER DATA LIST** 1. Bell 205A-1 * H1SW Rev. 27 4/20/2020 Installation of Two Place Seat Assembly must be done in accordance with Avio Design Group Inc. (Avio dg) Modification Instructions 2220-Ml-001, Revision --, Transport Canada Civil Aviation (TCCA) approved October 25, 2022, or later TCCA approved revision. Definition of Type Design Change is found in Avio dg Master Data List 2220- MD-001, Revision --, TCCA approved October 25, 2022, or later TCCA approved revision. 11/18/2022 N/A 2. * H4SW Rev. 39 10/21/2022 * Certification Basis for Configuration 1 and Configuration 2: Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for design changes that are identified as not significant in FAA Order 8110.48, the certification basis for the modification is as follows: a. The type certification basis for the Bell Model 205A-1 as shown on TCDS H1SW and for the Bell Model 212 as shown on TCDS H4SW for parts not changed or not affected by the change. b. The type certification basis for the Bell Model 205A-1 as shown on TCDS H1SW and for the Bell Model 212 as shown on TCDS H4SW for parts changed or affected by the change, the STC holder has elected to comply with the certification basis as shown on TCDS H4SW with the following exceptions: • 14 CFR Part 29.29, 29.301, 29.303, 29.305, 29.307, 29.337, 29.561, 29.601, 29.603, 29.605, 29.609, 29.613, 29.619, 29.785, and 29.1541 at Amendment 29-0. FAA Approved: Anthony E. Gallo Manager, International Validation Branch (AIR-730) Compliance & Airworthiness Division Aircraft Certification Service (AIR) ## Every issue (1) - November 18, 2022: Issued, Current. [certificate](https://openairdocs.org/files/sha256/f4/06/f40671af550fcf64ac05db57de9e7c2e5f646f95b594fb7b8257c265cde94485), [SR00077IB AML.pdf](https://openairdocs.org/files/sha256/cc/75/cc75ecd5b05c0a684f204b082cd0ad646c7f1cb8e94cd0c6b59305f0637bea70) --- 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.