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).
Related Comments
Total: 4
The Boeing Company Public SubmissionPosted: 08/19/2011
ID: FAA-2011-0733-0003
Aug 29,2011 11:59 PM ET
FedEx Express Public SubmissionPosted: 08/26/2011
ID: FAA-2011-0733-0006
Aug 29,2011 11:59 PM ET
David Chrisdebald Public SubmissionPosted: 08/26/2011
ID: FAA-2011-0733-0005
David Chrisdebald
This is comment on Proposed Rule
Airworthiness Directives: Pratt and Whitney Division PW4000 Series Turbofan Engines
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Related Comments
Public Submission Posted: 08/19/2011 ID: FAA-2011-0733-0003
Aug 29,2011 11:59 PM ET
Public Submission Posted: 08/26/2011 ID: FAA-2011-0733-0006
Aug 29,2011 11:59 PM ET
Public Submission Posted: 08/26/2011 ID: FAA-2011-0733-0005
Aug 29,2011 11:59 PM ET
Public Submission Posted: 08/24/2011 ID: FAA-2011-0733-0004
Aug 29,2011 11:59 PM ET