# STC SR02244LA - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Dart Aerospace ULC, Canada - Description: Installation of Emergency Float Kits. - Applied: May 29, 2008 - Status date: January 14, 2022 - Product: Aircraft, Rotorcraft - Certification basis: Part 29 - Data sheets: [TCDS H13EU](https://openairdocs.org/tcds/H13EU) - Certificate PDF: https://openairdocs.org/files/sha256/12/bc/12bc66b9e165631df25229814dce40fdd9f390f7faee63c8375dfbb881a0bd30 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176112411820230324151606.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR02244LA ## ADs that name it (1) - [AD 2024-20-07](https://openairdocs.org/ad/2024-20-07): Emergency Equipment; Emergency Flotation Section ยท Apical Emergency Float Kit, P/N 20498 (STC SR00780LA or 12 others). Effective Dec 5, 2024. Named in the applicability ## Approved models (2) - Airbus Helicopters Deutschland GmbH MBB-BK 117 C-2 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU)) - Airbus Helicopters Deutschland GmbH MBB-BK 117 D-2 ([TCDS H13EU](https://openairdocs.org/tcds/H13EU)) ## 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. United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number: SR02244LA FAA Form 8110-2 (4/22) SUPERSEDES PREVIOUS EDITION Page 1 of 3 C ertifies 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 29* of the Federal Aviation Regulations. *Certification basis is set forth in Type Certificate Data Sheet. D escription of Type Design Change: Installation of Emergency Float Kits in accordance with FAA approved Apical Industries, Inc. Master Document List MD145-1, Revision B, dated June 29, 2009, or later FAA approved revision. Rotorcraft Flight Manual Supplement RFMS145-1, Revision N/C, approved on July 20, 2009 or later FAA approved revision is required as part of this modification. L imitations and Conditions: See Continuation Sheet. T his 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 Administra tor of the Federal Aviation Administration. This certificate issued to: Dart Aerospace ULC 1055 West Georgia Street Suite 2100 Vancouver, BC, V6E 3P3, Canada Original Product Type Certificate Number: R00002RD Make: Airbus Helicopters Deutschland GmbH Model: MBB-BK 117 C-2, MBB-BK 117 D-2 Date of Application: May 29, 2008 Date Reissued: Aug. 19, 2014; Apr. 24, 2017; Jan. 14, 2022 Date of Issuance: July 21, 2009 Date Amended: April 24, 2017 By Direction of the Administrator Si gnature: Title: Aviation Safety Manager, Technical & Administrative Section, Los Angeles ACO Branch United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number: SR02244LA FAA Form 8110-2 (4/22) SUPERSEDES PREVIOUS EDITION Page 2 of 3 United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number: SR02244LA FAA Form 8110-2 (4/22) SUPERSEDES PREVIOUS EDITION Page 3 of 3 (Continuation Sheet) This approval requires the inspections and overhaul schedules to be performed as mandated by Apical Industries, Inc. dba Dart Aerospace's Instructions for Continued Airworthiness as follows: MBB-BK 117 C-2 with PIN 646.4100 series installed: Use document ICA145-l Instructions for Continued Airworthiness, Revision N/C, dated May 11, 2009 or later FAA accepted revision. MBB-BK 117 C-2 and D-2 with PIN 651.3400 series installed: Use document ICA145-4 Instructions for Continued Airworthiness, Revision N/C, dated October 19, 2016 or later FAA accepted revision. This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the 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 this permission. -END- ## Every issue (4) - January 14, 2022: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/12/bc/12bc66b9e165631df25229814dce40fdd9f390f7faee63c8375dfbb881a0bd30) - April 24, 2017: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/59/96/5996c9925089702c273ba8723c9ebcd9347e29b0d91c324acde86333082e6d17) - August 19, 2014: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/2d/15/2d152763cf86d3b28d4c6c06d9bf7ad2e844dcf7c47352535cfae4c1981fe92a) - July 21, 2009: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/8c/6b/8c6bd6ed613c6dbe41a25aa9da472dd36903fae46845a5e341a4ce7b9d389f38) --- 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.