What it approves
Installation of Landing Gear Sleeve
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 Aviation Tech Associates LLC 2769 Panepoo Street Kihei, Hawaii 96753 Part 27 * of the Federal Aviation Regulations *Certification basis set forth in Type Certificate Data Sheet Original Product Type Certificate Number :
H9EU
Airbus Helicopters
EC130B4, EC130T2 Description of Type Design Change: Installation of Landing Gear Sleeve in accordance with FAA approved Master Drawing List ATA-130-110, Revision “C” Dated August 5, 2016 or later FAA approved revision.
Limitations and Conditions: The approval of this modification applies to the above noted helicopter model series only. This installation should not be incorporated in any rotorcraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the rotorcraft. A copy of this STC must be included in the permanent records of the modified rotorcraft. 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. This installation must be maintained using FAA accepted Aviation Tech Associates Instructions for Continued Airworthiness (ICA) document ATA-109, Revision 2, dated July 30, 2016 or other FAA accepted ICA.
Date of application : July 20, 2015
Date of issuance : August 31, 2016
(Signature) Manager, Airframe Branch Los Angeles Aircraft Certification Office (Title)
NOTE:
DO NOT DELETE THIS PAGE.
DO NOT ADD ANY DATA TO THIS PAGE.
THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.
Number SR02601LA
ADs that name this STC · 0
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