Gerald Blank

Document ID: FAA-2010-0122-0004
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: March 02 2010, at 12:00 AM Eastern Standard Time
Date Posted: March 3 2010, at 12:00 AM Eastern Standard Time
Comment Start Date: February 19 2010, at 12:00 AM Eastern Standard Time
Comment Due Date: April 5 2010, at 11:59 PM Eastern Standard Time
Tracking Number: 80ab267a
View Document:  View as format xml

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This proposed AD is misplaced and poorly thought-out. I have flown with the spot-welded v-band clamps for many years and thousands of hours without any failure or problem. The problem you are trying to solve with the proposed AD is human. The bands are not torqued or placed correctly by some mechanics, and then fail. The same thing will happen with the proposed riveted replacement clamps. If they are not installed correctly they too, will fail. Also, there are two or more clamps per engine on many aircraft. The current list price for one clamp is just shy of $750.00, making your economic impact calculations very incorrect. This proposed AD should not be adopted.

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