Will AD-2006-16-26 be changed to add the same ending action allowed in the proposed Docket No. FAA-2010-0522?
section (F)(3) "Installing a crankcase that has a S/N 27812 or subsequent terminates the inspection requirements of paragraph (f)(1) of this AD."
This is an important issue as the 912F, 912S and 914F engines that have the new style crankcase should not be burdened with the repetitive inspections as they are not affected by SB-912-029 & SB-914-018.
Related Comments
Total: 3
Robert Seaton Public SubmissionPosted: 06/04/2010
ID: FAA-2010-0522-0004
Jul 06,2010 11:59 PM ET
Robert Seaton Public SubmissionPosted: 06/04/2010
ID: FAA-2010-0522-0005
Jul 06,2010 11:59 PM ET
Robert Seaton Public SubmissionPosted: 06/04/2010
ID: FAA-2010-0522-0003
Robert Seaton
This is comment on Rule
Airworthiness Directives: Various Aircraft Equipped with Rotax Aircraft Engines 912 A Series Engines
View Comment
Related Comments
Public Submission Posted: 06/04/2010 ID: FAA-2010-0522-0004
Jul 06,2010 11:59 PM ET
Public Submission Posted: 06/04/2010 ID: FAA-2010-0522-0005
Jul 06,2010 11:59 PM ET
Public Submission Posted: 06/04/2010 ID: FAA-2010-0522-0003
Jul 06,2010 11:59 PM ET