STC SR02672NY

This certificate issued to

Part 7 of the Civil Air Regulations.

Original Product -- Type Certificate Number: 1H15

The installation of the dual Garmin GNS-430 COM/NAV/GPS, dual GAD-42 Adapter, GTX 330 Transponder, Skywatch 497 Traffic Advisory, Artex 406HM ELT, and Garmin GMX-200 MFD must be performed in accordance with VIH Aerospace Master Drawing List 250-50176-00, Revision 02, dated October 13, 2008, or later Transport Canada approved revision.

1. Maintenance must be in accordance with VIH Aerospace Instructions for Continued Airworthiness VIHA-0628-AV1-ICA, Revision 01, dated October 13, 2008, or later Transport Canada accepted revision.

2. Operation must be in accordance with the following VIH Aerospace Rotorcraft Flight Manual Supplements or later Transport Canada approved revisions:

i. Dual GNS-430; VIHA-0628-GNS-FMS, Revision 01, dated October 13, 2008; Transport Canada approved November 20, 2008.

ii. King KRA-405B Rad Alt and Gear Up Warning; VIHA-0628-KRA-FMS, Revision 01, dated October 13, 2008;

Transport Canada approved November 20, 2008.

iii. GMX-200 MFD; VIHA-0628-MFD-FMS, Revision 01, dated October 13, 2008; Transport Canada approved November 20, 2008.

iv. SKY497 Skywatch Traffic Advisory; VIHA-0628-TAS-FMS, Revision 01, dated October 13, 2008; Transport Canada approved November 20, 2008.

VIH Aerospace Inc.

1962 Canso Road North Saanich, British Columbia V8L 5V5 Canada Make: Sikorsky Aircraft Model: S-61L, N Date reissued:

( Signature) Anthony Socias Manager New York Aircraft Certification Office

( Title)

Date of application: November 12, 2008

Date of issuance: January 14, 2009

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

Number SR02672NY Date of Issuance: January 14, 2009 Limitations and Conditions (Continued):

3. A placard stating “NAVIGATION NOT TO BE PREDICATED ON THE GMX-200 MFD MOVING MAP” must be installed adjacent to the GMX-200 multi-function display.

4. A placard stating “TAS IS BLIND AFT AND LOW” must be installed adjacent to the GMX-200 multi-function display.

5. Other cockpit labels shall be in accordance with drawings:

i. VS61-0628IP-001, Revision 0, dated June 27, 2006 DWG, S61 Instrument Panel Layout ii. VS61-CB-61761, Revision IR1, dated July 20, 2006 DWG, AUX & AC CB Panel Layout

6. The installer must determine whether this design change is compatible with previously approved modifications.

7. If the holder agrees to permit another person to use the certificate to alter a product, the holder must give the other person written evidence of that permission.

---END---