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 SubmissionPosted: 07/08/2008
ID: FAA-2008-0254-0002
Sep 02,2008 11:59 PM ET
Paul F. Jenny Public SubmissionPosted: 05/11/2010
ID: FAA-2008-0254-0003
Paul F. Jenny
This is comment on Rule
Airworthiness Directives; Hartzell Propeller Inc. ( )HC-( )(2,3)Y(K,R)-2 Two- and Three-Bladed Compact Series Propellers
View Comment
Related Comments
Public Submission Posted: 07/08/2008 ID: FAA-2008-0254-0002
Sep 02,2008 11:59 PM ET
Public Submission Posted: 05/11/2010 ID: FAA-2008-0254-0003
Sep 02,2008 11:59 PM ET