STC ST00011MC

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST00011MC This certificate issued to: Greenpoint Technologies Inc.

4600 Carillon Point Kirkland, WA 98033-7355 Part 25 of the Federal Aviation Regulations.

Original Product Typo Cortificate Number: A16WF Make: Boeing Model: 737-700 Series Description of Type Design Change: Installation of Provisions for a Self Defense System in accordance with Greenpoint Technologies Inc. (GTI) Master Drawing List, Document Number G7340-DL- 01, Revision V, dated July 20, 2009, or later FAA approved revision.

1. FAA approved Airplane Flight Manual Supplement, GTI Document Number G7340-FM-01, Revision D, dated February 27, 2008, or later FAA approved revision is required and must be carried in the aircraft during all flights.

(See continuation sheet 3 of 3 for additional limitations)

Date of Application: November 21, 2006 Date Reissued:

Date of Issuance: February 28, 2008 Date Amended: July 27, 2009 By Direction of the Administrator FEDERAL AVIATION Sor Last (Signature) Portion TOMINSTRATO Ronald K. Rathgeber Manager Military Certification Office (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST00011MC Limitations and Conditions:

2. Instruction for Continued Airworthiness GTI Document Number G7340-CA-01, Revision A, dated February 14, 2008, or later FAA approved revision, shall be made available to the operator at the time of installation.

3. Instruction for Continued Airworthiness GTI Document Number G7340-CA-02, Revision A, dated July 20, 2009, or later FAA approved revision, shall be made available to the operator at the time of installation.

4. 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.

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

6. This modification may not be installed after June 7, 2010 unless (1) previously approved electrical wiring interconnection system (EWIS) instructions for continued airworthiness (ICA) have been evaluated and determined to be adequate for this installation by the FAA, or (2) revised EWIS ICA have been approved by the FAA Oversight Office.

(Refer to14 CFR Part 26.11) END-

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