# STC SR09240RC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Bell Helicopter Textron Inc., United States
- Description: Installation of FADEC mode switch relocation per Premier Aviation, Inc. master drawing list F00-15003, Rev D dtd 8/17/00 or later FAA approved revision.
- Applied: December 19, 1996
- Status date: April 15, 2011
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS H2SW](https://openairdocs.org/tcds/H2SW)
- Certificate PDF: https://openairdocs.org/files/sha256/8a/e2/8ae2e0b7829400fd3eb08a078024d60e45dd45d847b6410fa349656a3130e1dc
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C1F5E5374D2FC6D7862578B8006D51C9.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SR09240RC

## ADs that name it (0)

None.

## Approved models (1)

- Bell Helicopter Textron (Canada) 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.

Number SR09240RC This certificate issued to

Part 27 of the Federal Aviation Regulations.

Installation of FADEC Mode Switch Relocation in accordance with Premier Aviation, Inc.

Master Drawing List F00-15003, Revision D, dated August 17, 2000, or later FAA approved revision.

Bell Helicopter Textron, Inc.

441 Industrial Park Road Piney Flats, TN 37686 H2SW Make : Bell Helicopter Textron Model : 407 Date of application : December 19, 1996

Date of issuance : March 16, 2000

Date reissued : April 15, 2011;

January 17, 2002

( Signature) James A. Richmond, Acting Manager Rotorcraft Certification Office, Southwest Region

( Title)

FAA Form 8110-2-1(10-69) Page 2 of 3

FAA Form 8110-2-1(10-69) Page 3 of 3

Number SR09240RC Date of Issuance: March 16, 2000 Date of Reissuance: April 15, 2011

FAA approved Rotorcraft Flight Manual Supplement (RFMS) F09-62002 dated March 16, 2000, or later FAA approved RFMS is required.

Instructions for Continued Airworthiness, Premier Aviation, Inc., Document F08-72004, Revision - , dated May 11, 2000, or later FAA accepted revision is required for this installation.

If the helicopter configuration includes equipment(either previously installed or installed concurrently with this STC) for which a FADEC EMC Test is required (see BHTI Document 407-099-096) a FADEC EMC test is required after the installation of this STC.

The installer must determine whether this design change is compatible with previously approved modifications. The standard EMC test for intra-system compatibility between on-board electrical/electronic systems is the responsibility of the installer.

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.

## Every issue (1)

- April 15, 2011: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/8a/e2/8ae2e0b7829400fd3eb08a078024d60e45dd45d847b6410fa349656a3130e1dc)

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