Lloyd Fries

Document ID: FAA-2007-0286-0009
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: January 07 2008, at 10:09 AM Eastern Standard Time
Date Posted: January 7 2008, at 12:00 AM Eastern Standard Time
Comment Start Date: December 10 2007, at 12:00 AM Eastern Standard Time
Comment Due Date: January 9 2008, at 11:59 PM Eastern Standard Time
Tracking Number: 8038a1c8
View Document:  View as format xml

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The AD continues be based more on the Factory desire to make money rather than a demonstrated need for the AD. Yes struts have failed the test but too date NO strut has failed in flight. There must be a reason other than luck. While no one wants to see anyone die before there is an AD the evidence clearly indicates the "emergency" nature was blown out of proportion. A more reasonable compliance time would be at the next annual or 100 hour inspection (if required). The new AD is a relief in terms of periods between inspections which I am grateful but which I don't intend to need.It fails to take into account that currently there is only one manuf. of the struts.One may be on line in 30 days and another may never be on line even after taking peoples money. There should be at least a 90 day extention for compliance after the initial visual inspection if the next annual is considered too extreme. Furthur, the Factory SB on the attach fittings complicates compliance. What if there is an AD issued and a method other than the SB is required. Don't hold us hostage to issues that have more to do with a greedy factory rather than safety of flight.

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Total: 20
David E Whitaker
Public Submission    Posted: 01/07/2008     ID: FAA-2007-0286-0006

Jan 09,2008 11:59 PM ET
Roland C Robinson
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Shawn Coleman
Public Submission    Posted: 01/07/2008     ID: FAA-2007-0286-0008

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Lloyd Fries
Public Submission    Posted: 01/07/2008     ID: FAA-2007-0286-0009

Jan 09,2008 11:59 PM ET
James K Stallings
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Jan 09,2008 11:59 PM ET