Robert J. Golo

Document ID: FAA-2008-1232-0006
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: December 01 2008, at 02:57 PM Eastern Standard Time
Date Posted: December 2 2008, at 12:00 AM Eastern Standard Time
Comment Start Date: November 24 2008, at 12:00 AM Eastern Standard Time
Comment Due Date: January 23 2009, at 11:59 PM Eastern Standard Time
Tracking Number: 807c7d57
View Document:  View as format xml

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The proposed AD regarding the PW610F-A engines would be just as effective, with less restrictions for operators, if operations above 37,000 feet were to include a restriction to keep the cabin and cockpit air temperatures set at 68 degrees or below - the bleed air would stay on LOW and no carbon buildup on the static vanes would occur. This has worked well since the problem was discovered months ago. Thanks. BOB GOLO

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Total: 9
Kenneth Meyer
Public Submission    Posted: 11/26/2008     ID: FAA-2008-1232-0002

Jan 23,2009 11:59 PM ET
Robert J. Golo
Public Submission    Posted: 12/02/2008     ID: FAA-2008-1232-0006

Jan 23,2009 11:59 PM ET
Marc Arnolds
Public Submission    Posted: 12/05/2008     ID: FAA-2008-1232-0007

Jan 23,2009 11:59 PM ET
TGV Rockets, Inc.
Public Submission    Posted: 12/09/2008     ID: FAA-2008-1232-0008

Jan 23,2009 11:59 PM ET
Robert Brodersen
Public Submission    Posted: 12/12/2008     ID: FAA-2008-1232-0009

Jan 23,2009 11:59 PM ET