# STC SR01459LA - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Dart Aerospace ULC, Canada - Description: Installation of Apical Industries, Inc Emergency Mid-Float with 10-man Life Raft kits - Applied: February 18, 2003 - Status date: January 14, 2022 - Product: Aircraft, Rotorcraft - Certification basis: Part 29 - Data sheets: [TCDS H4SW](https://openairdocs.org/tcds/H4SW) - Certificate PDF: https://openairdocs.org/files/sha256/0f/cc/0fcc532893596593aa26b4c714f2ba9ef492571c45af3c85da6dc1b53acd443c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142101511020230324150801.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SR01459LA ## ADs that name it (1) - [AD 2024-20-07](https://openairdocs.org/ad/2024-20-07): Emergency Equipment; Emergency Flotation Section · Apical Emergency Float Kit, P/N 20498 (STC SR00780LA or 12 others). Effective Dec 5, 2024. Named in the applicability ## Approved models (3) - Bell Helicopter Textron Inc. 412 ([TCDS H4SW](https://openairdocs.org/tcds/H4SW)) - Bell Helicopter Textron Inc. 412CF ([TCDS H4SW](https://openairdocs.org/tcds/H4SW)) - Bell Helicopter Textron Inc. 412EP ([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. United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number: SR01459LA 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 Apical Industries, Inc. Emergency Mid-Float with 10-man Life Raft Kits in accordance with FAA approved Apical Industries, Inc., Master Document List MD 412- 31, Revision B, dated May 29, 2003, or later FAA approved revision. Apical Industries, Inc. Rotorcraft Flight Manual Supplement FMS -412-31, Revision N/C, FAA approved on June 11, 2003, or later FAA approved revision is required as part of this modification. 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 Administrator 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: H4SW Make: Bell Model: 412, 412EP, 412CF Date of Application: February 18, 2003 Date Reissued: Aug. 19, 2014; Jan. 14, 2022 Date of Issuance: June 17, 2003 Date Amended: March 8, 2005 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: SR01459LA The STC’ s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC holder. 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: SR01459LA The STC’ s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC holder. FAA Form 8110-2 (4/22) SUPERSEDES PREVIOUS EDITION Page 3 of 3 (Continuation Sheet) 1. Bell Helicopter Textron, Inc., Emergency Float Kit Part Number 412-706-004-137, or 412-706-004- 143, or 412-706-004-149 or Apical Industries, Inc. Emergency Float Kit, Part Number 604.9601 per STC SR01648LA must be installed prior to the installation of this STC. 2. This approval requires the inspections and overhaul schedules to be performed as mandated by the Instructions for Continued Airworthiness, ICA 412-31, Revision I/R, dated March 3, 2003, or later FAA approved revision. 3. 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 that permission. -END- ## Every issue (2) - January 14, 2022: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/0f/cc/0fcc532893596593aa26b4c714f2ba9ef492571c45af3c85da6dc1b53acd443c) - March 8, 2005: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/d8/7e/d87e316828c872dfbcdbafdf77d23307ba76e4bb0781e4535301b7ff641bc136) --- 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.