David Chrisdebald

Document ID: FAA-2011-0733-0005
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: August 25 2011, at 12:00 AM Eastern Daylight Time
Date Posted: August 26 2011, at 12:00 AM Eastern Standard Time
Comment Start Date: July 14 2011, at 12:00 AM Eastern Standard Time
Comment Due Date: August 29 2011, at 11:59 PM Eastern Standard Time
Tracking Number: 80ef0687
View Document:  View as format xml

View Comment

Please define within the AD how to perform the pro-rata calculation of the parts life limit after the effective date of the AD, concerning parts that have been installed on Engines with different thrust loads (back to birth).

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