What it approves
Installation of a Replacement Caution Warning Panel in accordance with Heli-Lynx Installation Manual IM-HL-08-001-91-02, Revision A, dated June 29, 2010, and Master Drawing List MDL HL-08-001-91-02, Revision A, dated June 30, 2010, both Transport Canada approved July 05, 2010, or later Transport Canada 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.
This certificate issued to
Part 27 of the Federal Aviation Regulations.
Original Product Type Certificate Number: H11EU
Installation of a Replacement Caution Warning Panel in accordance with Heli-Lynx Installation Manual IM-HL-08-001-91-02, Revision A, dated June 29, 2010, and Master Drawing List MDL HL-08-001-91-02, Revision A, dated June 30, 2010, both Transport Canada approved July 05, 2010, or later Transport Canada approved revision.
1. Maintenance must be performed in accordance with Heli-Lynx Instructions for Continued Airworthiness Document ICA-HL- 08-001-05-02, Revision A, dated June 28, 2010, Transport Canada accepted June 28, 2010, or later Transport Canada accepted revision. Compliance with Airworthiness Limitations Section 4, Transport Canada approved June 28, 2010, or later Transport Canada approved Airworthiness Limitation is mandatory.
2. Aircraft is to be operated in accordance with Heli-Lynx Rotorcraft Flight Manual Supplement Report No. FMS-HL-08-001-91- 02, Revision Orig, dated July 05, 2010, Transport Canada approved July 05, 2010, or later Transport Canada approved revision.
Heli-Lynx Helicopter Services Inc.
Stoney Creek Airport, 684 Mud Street E, Hangar 1 Stoney Creek, ON Canada L8J 3C9 Make: Eurocopter France Model: AS 355F1, AS 355F2
( Signature) Anthony Socias Manager New York Aircraft Certification Office
( Title) Date of application: August 17, 2010
Date of issuance: March 9, 2011
FAA Form 8110-2-1(10-69) Page 2 of 2
Number SR02936NY Date of Issuance: March 9, 2011
Limitations and Conditions(Con’t):
3. Heli-Lynx System Modifications must be installed in accordance with FAA STC SR02015NY prior to incorporation of this modification.
4. Installation of this modification in conjunction with Full Authority Digital Engine Control (FADEC), Vehicle and Engine Multifunctional Display (VEMD), and/or Multi-Function Display/Primary Flight Display (MFD/PFD) will require additional FAA approval.
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.
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