STC SR00102RD

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title H13EU Airwork (NZ) Limited 487 Airfield Road Ardmore Papakura, New Zealand 2582 3 SR00102RD Federal Air Regulation 29 Installation of dual torque indicator in accordance with Master Document List STC.AW.0017 revision 3 dated 11 November 2016, or later FAA approved revision.

Continuation on page 3 of 3 Airbus Helicopters Deutschland MBB-BK117 B-2

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

2) A copy of this certificate must be maintained as part of the permanent records for the modified aircraft.

3) Aircraft with this STC embodied must be maintained in accordance with the Instructions for Continued Airworthiness STC.AW.0017 ICA Revision 3 dated 11 November 2016, or later FAA accepted revision.

4) Aircraft installing this STC must have incorporated Airbus Helicopter Service Bulletin MBB-BK117-60-113, Upgrade of OEI Torque Limits, Rev 1, dated May 13, 1995

January 18, 2016 January 13, 2017 IMPORT Larry Kelly Manager, Rotorcraft Standard Staff Southwest Region

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

3 SR00102RD

FAA Form 8110-2 (5/14) Page 3 of

3 Date of issuance: January 13, 2017

Certification Basis

Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this STC is as follows:

a. 14 CFR § 29 including up to amendment number 29-55 with the exception of 29.561 at amendment 0, 29.1305 at amendment 10, 29.1351 at amendment 14, and excluding 29.1316 and 29.1317.

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