Paul F. Jenny

Document ID: FAA-2008-0254-0003
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: May 11 2010, at 12:00 AM Eastern Daylight Time
Date Posted: May 11 2010, at 12:00 AM Eastern Standard Time
Comment Start Date: July 2 2008, at 12:00 AM Eastern Standard Time
Comment Due Date: September 2 2008, at 11:59 PM Eastern Standard Time
Tracking Number: 80aeb1b6
View Document:  View as format xml

View Comment

AD2008-13-28 states " repetitive intervals not to exceed 50 hours TIS or 12 months from the previous ECI, whichever occurs first, perform ECIs of the area around the lubrication holes of the hub blade socket".This AD should be revised to TIS only since an Aircraft not flown for 12mos would not incure any Hub damage.

Related Comments

   
Total: 2
M. Fong
Public Submission    Posted: 07/08/2008     ID: FAA-2008-0254-0002

Sep 02,2008 11:59 PM ET
Paul F. Jenny
Public Submission    Posted: 05/11/2010     ID: FAA-2008-0254-0003

Sep 02,2008 11:59 PM ET