STC SR02863NY

Part * of the Civil Air Regulations.

Installation of “Torrentula” Valve, Power Fill & Control System in accordance with SEI Industries Ltd. Master Drawing List BXSK107MDL, Revision Original, dated February 19, 2010, Transport Canada approved February 25, 2010, and Installation Instructions Document BXSK107INSTL, Revision Original, dated December 30, 2009, Transport Canada approved February 25, 2010, or later Transport Canada approved revisions.

1. Maintenance must be in accordance with TCCA accepted Instructions for Continued Airworthiness specified in the attached aircraft Approved Model List.

SEI Industries Ltd.

7400 Wilson Avenue Delta, British Columbia V4G 1H3 Canada

Date of application: April 26, 2010

Date of issuance: November 19, 2010

Date reissued: January 26, 2012

( Signature) Timothy Hadsall Acting Manager New York Aircraft Certification Office

( Title) *See attached FAA Approved Model List (AML) No.

SR02863NY for the list of approved aircraft models and applicable airworthiness regulations.

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

Number SR02863NY Date of Re-issue: January 26, 2012

2. Aircraft is to be operated in accordance with SEI Industries Ltd. Rotorcraft Flight Manual Supplement, Report No.

BXSK107FMS, Revision Original, dated May 25, 2009, Transport Canada approved February 25, 2010.

3. Operation is limited to day/night VFR only.

4. The following equipment is required:

i. C07E2123 Utility Power & Control System Installation (TCCA accepted FAA STC SR01276SE) ii. C07X0030 Mounting Provisions, Utility Equipment (TCCA accepted FAA STC SR01642SE)

5. 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.

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

7. A copy of this certificate and the FAA Approved Model List (AML) No. SR02863NY, issued November 19, 2010, or later FAA approved revisions, must be maintained as part of the permanent records for the modified aircraft.

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for changes that are not significant in FAA Order 8110.48, the certification basis for this modification is as follows:

a. The existing type certification basis for Columbia model CHI 107-II series helicopter as shown on FAA type certificate data sheet 1H16 with the following exceptions:

29.865 Amendment 12

29.1322 Amendment 3

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