What it approves
Installation of an External ITT and Torque Indicating System
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.
Part 27 of the Federal Aviation Regulations.
Original Product Type Certificate Number: H7EU
Installation of an External ITT and Torque Indicating System in accordance with Aero-Dyne Repair Services, Ltd., Engineering Order EO407001, Revision 1 dated February 03, 2010, Transport Canada approved April 07, 2010, or later Transport Canada approved revision.
1. Maintenance must be performed in accordance with Aero-Dyne Repair Services Ltd. Instructions for Continued Airworthiness Document MMS407001, Revision 2, dated October 20, 2011, Transport Canada accepted October 25, 2011, or later Transport Canada accepted revision.
2. Aircraft is to be operated in accordance with Aero-Dyne Repair Services Flight Manual Supplement Report FMS407001, Revision 1, dated February 03, 2010, Transport Canada approved April 07, 2010, or later Transport Canada approved revisions.
3. Rotorcraft eligible for modification on all model A119 rotorcraft listed in the TCDS that are equipped with an Integrated Display System. Non-Integrated Display System rotorcraft are not eligible.
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 change with previously approved modifications must be determined by the installer.
Aero-Dyne Repair Services, Ltd.
P.O. Box 3966 Olds, Alberta Canada T4H 1P6 Make: AGUSTA S.p.A.
Model: A119, AW119 MKII Date of application: November 2, 2010
Date of issuance: October 31, 2011 Date reissued:
( Signature) Anthony Gallo Acting Manager New York Aircraft Certification Office
( Title)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.