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Kenichiro Ikeuchi

Document ID: FAA-2008-0412-0002
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: April 24 2008, at 10:07 PM Eastern Daylight Time
Date Posted: April 25 2008, at 12:00 AM Eastern Standard Time
Comment Start Date: April 24 2008, at 12:00 AM Eastern Standard Time
Comment Due Date: June 9 2008, at 11:59 PM Eastern Standard Time
Tracking Number: 8052c23c
View Document:  View as format xml

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AD 2004-22-05 requires repetitive detailed inspection for discrepancies (wear or cracking) of the fuselage skin under the dorsal fin assembly and new AD would retain this requirement. JTA (Japan Transocean Air) plans to install wear strips per Boeing SB 737-53A1266. In order to avoid the removal of wear strip, JTA would like new AD to accept the repetitive inspection for either" fuselage skin" or "wear strip".

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