Airbus

Document ID: FAA-2010-0279-0004
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: May 17 2010, at 12:00 AM Eastern Daylight Time
Date Posted: May 18 2010, at 12:00 AM Eastern Standard Time
Comment Start Date: April 2 2010, at 12:00 AM Eastern Standard Time
Comment Due Date: May 17 2010, at 11:59 PM Eastern Standard Time
Tracking Number: 80aeeeaa
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Comments for docket n°. FAA-2010-0279 Directorate Identifier 2009-NM-148-AD: - § (j): In case of positive findings and AOG, Airtac can also be contacted: AIRTAC (Airbus Technical AOG Center) Customer Services Phone: +33 (0)5 61 93 34 00 Fax: +33 (0)5 61 93 35 00 Mailto: airtac@airbus.com - § (k): Additional works for rudders previously inspected a per AOT 55A1038 original issue or rev 01 can be of two types and should be further detailed: additional areas to be inspected (this is covered by the current proposed § k) and additional ultrasonic inspection for rudders on which temporary vacuum loss hole restoration with resin or permanent vacuum loss hole restoration has been performed previously in reinforced area (refer to instructions of Airbus AOT A320-55A1038 Revision 02).

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Airbus
Public Submission    Posted: 05/18/2010     ID: FAA-2010-0279-0004

May 17,2010 11:59 PM ET