# STC SR02405LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Bell Helicopter Textron Inc., United States
- Description: Installation of an emergency life raft
- Applied: January 26, 2011
- Status date: August 1, 2013
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/d8/6c/d86c34b86403fc158e49e87793beb1ac0ccb8412061c8a33bc0561b3a38ae68b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C186139B15A89DE086257BC600682478.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SR02405LA

## ADs that name it (0)

None.

## Approved models (1)

- Bell Helicopter Textron Canada Limited 407 ([TCDS H2SW](https://openairdocs.org/tcds/H2SW))

## 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.

441 Industrial Park Road Piney Flats, TN 37686 Part 27* of the Federal Aviation Regulations. *Certification basis is set forth in TCDS H2SW

Original Product – Type Certificate Number : H2SW

Make: Bell Helicopter Textron Canada Limited Model: Bell 407 Description of Type Design Change:

Installation of an emergency life raft in accordance with Federal Aviation Administration approved Meeker Aviation Drawing and Documents List for Survivor Window Raft Kit, AA-10072, Revision C, dated January 10, 2012, or later FAA approved revision(s). Rotorcraft Flight Manual Supplement (RFMS), Meeker Aviation Document No. AA -10078, Revision N/A (Original Issue), dated December 6, 2011, or later FAA approved RFMS is required. Instructions for Continued Airworthiness, Meeker Aviation, Report No.AA-10074, Rev B, dated August 8, 2011, or later FAA accepted revision is required for this installation.

The 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. The approval of this modification applies to the above noted aircraft model only. A copy of this certificate 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 26, 2011 Date reissued: May 24, 2012; August 1, 2013 Date of issuance: March 28, 2012 Date amended:

(Signature) Scott A. Horn, Acting Manager Rotorcraft Certification Office Southwest Region (Title) PM JLK ASW-170

FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES

## Every issue (3)

- August 1, 2013: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d8/6c/d86c34b86403fc158e49e87793beb1ac0ccb8412061c8a33bc0561b3a38ae68b)
- May 24, 2012: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/24/eb/24eb1dcc5b3cb9b10b87eea6a79f01e4cafb7b625e05a404e65921ff10aa530f)
- March 28, 2012: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/35/25/35250647fc991669dd78e816c165a016b48b15a387b4cc8bc250c2daabdf0219)

---
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.