STC SR09244RC

Number SR09244RC This certificate issued to

Part 27 of the Federal Aviation Regulations.

Description of Type Design Change: Installation of a Single Pilot IFR Configuration, Silver Crown or Gold Crown on Bell Model 407 Helicopter Serial numbers 53019 and 53358 in accordance with the following:

Gold Crown Configuration: Premier Aviation, Inc. Master Drawing List F00-01000, Revision C, dated December 1, 2000, or later FAA approved revision.

Silver Crown Configuration: Premier Aviation, Inc. Master Drawing List F00-01001, Revision A, dated December 1, 2000, or later FAA approved revision.

(See continuation sheets 3 & 4 of 4)

Mountain Pacific Aviation, L.L.C.

10801 Main Street, Suite 200 Bellevue, WA 98004 H2SW Make : Bell Helicopter Textron (Canada) Limited Model : 407

Date of application : March 13, 1996

Date of issuance : April 27, 2000

Date reissued : April 30, 2003;

January 31, 2008

( Signature) Lance T. Gant, Manager Rotorcraft Certification Office, Southwest Region

( Title)

FAA Form 8110-2-1(10-69) Page 2 of 4

FAA Form 8110-2-1(10-69) Page 3 of 4

Number SR09244RC Date of Issuance: April 27, 2000 Reissuance Date: January 31, 2008

FAA approved Rotorcraft Flight Manual Supplements (RFMS) Premier Aviation, Inc.

Document F09-64001, Revision -, dated April 27, 2000, and Premier Aviation, Inc, Document F09-64002, Revision -, dated April 27, 2000, and Premier Aviation, Inc.

Document F09-64003, Revision -, dated April 27, 2000, or later FAA approved RFMs are required.

The following Supplemental Type Certificates (STCs) must be installed with this STC:

• SR09239RC, BHT407 Steerable Landing Light Installation

• SR09088RC, BHT407 Enlarged Instrument Panel or SR09250RC, BHT Law Enforcement Instrument Panel Installation

The data was not substantiated for multiple installations therefore this approval is limited to only the installations made in the Bell Model Helicopter Serial Numbers 53019 and 53358.

Airworthiness Directive (AD) 2000-14-16 is not compatible with this STC. Bell Helicopter Textron Alert Service Bulletin (ASB) 407-99-33, Revision A, dated March 10, 2000, or later dated, is not compatible with this installation. Additionally, BHT407 serial numbers 53397, 53400 and subsequent, which have the intent of ASB 407-99-33 incorporated, are not compatible with this STC.

Bell Helicopter Textron Alert Service Bulletin (ASB) 407-99-31, FADEC Direct Reversion to Manual Mode, dated September 10, 1999 is not compatible with this installation.

The following Premier Aviation, Inc. Instructions for continued Airworthiness (ICA) are required for this installation:

Gold Crown Configuration:

• F08-72002, Instrument Lighting System, Revision -, dated July 7, 1998, or later FAA accepted revision.

• F08-74000, Avionics and EFIS Systems, Revision A, dated January 28, 1999, or later FAA accepted revision.

• F08-74001, Pitot/Static and Flight Instruments Systems, Revision A, dated February 3, 1999, or later FAA accepted revision.

• F08-75000, Automatic Flight Control and Flight Director Systems, Revision A, dated March 17, 1999, or later FAA accepted revision.

FAA Form 8110-2-1(10-69) Page 4 of 4

Number SR09244RC Date of Issuance: April 27, 2000 Reissuance Date: January 31, 2008

Silver Crown Configuration:

• F08-72003, Instrument Lighting System, Revision -, dated March 12, 2000, or later FAA accepted revision.

• F08-74002, Avionics and EFIS Systems, Revision -, dated March 10, 2000, or later FAA accepted revision.

• F08-74003, Pitot/Static and Flight Instruments Systems, Revision -, dated March 12, 2000, or later FAA accepted revision.

• F08-75002, Automatic Flight Control and Flight Director Systems, Revision -, dated March 13, 2000, or later FAA accepted revision.

Both Configurations:

• F08-72001, IFR Electrical System, Revision B, dated May 8, 2000, or later FAA accepted revision.

• F08-73003, Secondary Hydraulic System, Revision C, dated May 8, 2000, or later FAA accepted revision.

The following optional equipment is approved for use with this STC:

• Cargo Hook Kit, BHT P/N 206-706-341 (without external loads attached)

• Low Skid Gear, BHT P/N 407-706-006

• Standard Gear Fairings, BHT P/N 407-706-010

• High Skid Gear, BHT P/N 407-706-007

• STC SR09240RC, FADEC Mode Switch Relocation

• STC SR09241RC, Adjustable Crew Seat Installation

The certification basis for this STC is the same as that identified on Type Certificate Data Sheet H2SW, FAR 27 with the addition of Equivalent Safety Finding made in accordance with 14 CFR § 21.21(b)(1) and 27.695.

Compatibility of this design change with previously approved modifications must be determined by the installer. 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.

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