Airbus

Document ID: FAA-2012-1038-0004
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: November 16 2012, at 12:00 AM Eastern Standard Time
Date Posted: November 20 2012, at 12:00 AM Eastern Standard Time
Comment Start Date: October 4 2012, at 12:00 AM Eastern Standard Time
Comment Due Date: November 19 2012, at 11:59 PM Eastern Standard Time
Tracking Number: 1jw-820h-pbrz
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This is comment on Proposed Rule

Airworthiness Directives: Airbus Airplanes

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Dear, Please find below AIRBUS comments: NPRM Docket No. FAA-2012-1038; Directorate Identifier 2011-NM-166-AD 1. Paragraph (g): Please correct typo error, it should read: “(g) Repetitive Eddy Current Inspection At the applicable compliance time in paragraph (g)(1) or (g)(2) of this AD:..” instead of (k)(1) and (k)(2) mentioned. 2. Paragraph (k)(2): Please update the contact details (singlum) of AIRBUS Office of Airworthiness. Please replace EAS by EIAS. 3. AIRBUS requests FAA to consider each AIRBUS Repair Approval Sheet (RAS) approved under AIRBUS DOA EASA.21J.031 - provided after cracking is reported - as an approved method for repair as required by par (h)(2). Thank you. Best Regards, Konstantinos SIDERIS Single Aisle Aircraft Continued Airworthiness Engineer Product Integrity Division - EIAS AIRBUS Phone: +33 (0) 5 61 93 11 24 Fax: +33 (0) 5 61 93 44 51 Mailto: konstantinos.sideris@airbus.com

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Total: 3

Airbus
Public Submission Posted: 11/20/2012 ID: FAA-2012-1038-0004

Comment Period Closed
Nov 19,2012 11:59 PM ET

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Public Submission Posted: 11/20/2012 ID: FAA-2012-1038-0003

Comment Period Closed
Nov 19,2012 11:59 PM ET

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Public Submission Posted: 02/06/2013 ID: FAA-2012-1038-0005

Comment Period Closed
Nov 19,2012 11:59 PM ET