AIRBUS S.A.S.

Document ID: FAA-2007-0345-0003
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: January 14 2008, at 09:21 AM Eastern Standard Time
Date Posted: January 14 2008, at 12:00 AM Eastern Standard Time
Comment Start Date: December 19 2007, at 12:00 AM Eastern Standard Time
Comment Due Date: January 18 2008, at 11:59 PM Eastern Standard Time
Tracking Number: 8039a37f
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This is comment on Rule

Airworthiness Directives; Airbus Model A310-304, -322, -324, and -325 Airplanes; and A300 Model B4-601, B4-603, B4-605R, B4-620, B4-622, B4-622R, F4-605R, F4-622R, and C4-605R Variant F Airplanes (Commonly Called Model A300-600 Series Airplanes)

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Comment to paragraph (e) of FAA NPRM FAA-2007-0345: Airbus kindly requests FAA to review the description of the corrective actions as detailed in paragraph (e) of NPRM to add the following points (block letters): "Related investigative and corrective actions (reinforcement) include: (...) reaming the fastener holes AND INSTALLING NEW OVERSIZED FASTENERS (ALL A/C); INSTALLING REINFORCING BRACE PLATES ON THE DIAGONAL STRUTS BETWEEN FR87 AND FR91 (FOR A/C PRE-MOD 06133); and contacting Airbus (...) Sincerely, Valia Smith A300/A310/A300-600 Continued Airworthiness Engineer AIRBUS Central Entity

Related Comments

Total: 2

AIRBUS S.A.S.
Public Submission Posted: 01/09/2008 ID: FAA-2007-0345-0002

Comment Period Closed
Jan 18,2008 11:59 PM ET

AIRBUS S.A.S.
Public Submission Posted: 01/14/2008 ID: FAA-2007-0345-0003

Comment Period Closed
Jan 18,2008 11:59 PM ET