Jim Sparks

Document ID: FAA-2008-0732-0002
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: July 11 2008, at 09:59 AM Eastern Daylight Time
Date Posted: July 11 2008, at 12:00 AM Eastern Standard Time
Comment Start Date: July 10 2008, at 12:00 AM Eastern Standard Time
Comment Due Date: August 11 2008, at 11:59 PM Eastern Standard Time
Tracking Number: 806681b4
View Document:  View as format xml

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The Falcon 50 does incorporate two independent wing fuel tank "valve boxes" incorporating over pressure relief valves coupled with a stand alone wing tank pressure reducing / over pressure relief valve. Due to the commonality in this system, in other than a static situation, both overpressure relief valves and the regulating valve would have to fail before any over pressure would occur. The pressure relief valves along with the entire system do have manufacturer's recommended intervals for both operational and function testing. The reliability of the of the "valve boxes" have not been stellar so a change to the interval of inspection may be a more practical solution.

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Jim Sparks
Public Submission    Posted: 07/11/2008     ID: FAA-2008-0732-0002

Aug 11,2008 11:59 PM ET