STC SR09439RC

Supplemental type certificate · Bell Helicopter Textron Inc.

Holder
Bell Helicopter Textron Inc. · United States
Status
Current · Reissued
Status date
February 9, 2011
Applied
October 29, 2003
Product
Aircraft · Rotorcraft
Certification basis
Part 21, Part 29, Part 135
Data sheet
TCDSH9SW

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Combined Cockpit Voice Recorder/Flight Data Recorder in accordance with Aeronautical Accessories, Inc. Report No. AA-05035, Revision D, dated July 13, 2005, or later FAA approved revision and installation per Aeronautical Accessories, Inc. Report No. AA-03103, Revision D, dated June 29, 2005, or later FAA approved revision.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

Number SR09439RC This certificate issued to

Part 29 of the Federal Aviation Regulations.

Combined Cockpit Voice Recorder/Flight Data Recorder in accordance with Aeronautical Accessories, Inc. Report No. AA-05035, Revision D, dated July 13, 2005, or later FAA approved revision and installation per Aeronautical Accessories, Inc. Report No. AA-03103, Revision D, dated June 29, 2005, or later FAA approved revision.

Bell Helicopter Textron, Inc.

441 Industrial Park Road Piney Flats, TN 37686 H9SW Make : Bell Helicopter Textron Model : 430 Date of application: October 29, 2003

Date of issuance : June 21, 2005

Date reissued: February 9, 2011

Date amended : August 15, 2005

( 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 SR09439RC Date of Issuance: June 21, 2005 Date Amended: August 15, 2005 Dare of Reissuance: February 9, 2011

Rotorcraft Flight Manual Supplement, Aeronautical Accessories, Inc., Document Number AA-03113, dated June 21, 2005, or later FAA approved revision is required for this installation. Instructions for Continued Airworthiness, Aeronautical Accessories, Inc., Report No. AA-03104, Revision -, dated June 8, 2005, or later FAA accepted revision is required. The following FDR parameters are not verified: Yaw Rate, Drift Angle, nor Vertical Speed Reference (FCC). Installation credit is not given for these listed parameters. Installation is limited to aircraft configured with single or dual autopilot systems and fixed skid landing gear only. The Cockpit Voice Recorder portion of the CV/FDR does not meet the operating requirements of FAR Part 135. The installer must determine whether this design change is compatible with previously approved modifications.

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.

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
Bell Helicopter Textron A Division of Textron Canada430H9SW