Inspection of control system cables and pulleys is already part of the annual inspection. This AD is redundant, but then goes on to require disassembly of turnbuckles, which will cause more harm than good. Invasive disassembly of mechanical systems increases the risk of damage and re-assembly issues, ultimately leading to more failures than this AD was meant to address. There have certainly been few control system failures in Cherokee aircraft, and to propose a blanket AD for all models when there were one or two instances of failure in aircraft with significant corrosion history is unnecessary. This proposed AD should be canceled since it is redundant.
Related Comments
Total: 5
Carl Poplawsky Public SubmissionPosted: 09/07/2012
ID: FAA-2012-0731-0004
Sep 17,2012 11:59 PM ET
Eric Stendahl Public SubmissionPosted: 09/07/2012
ID: FAA-2012-0731-0005
Carl Poplawsky
This is comment on Proposed Rule
Airworthiness Directives: Piper Aircraft, Inc. Airplanes
View Comment
Related Comments
Public Submission Posted: 09/07/2012 ID: FAA-2012-0731-0004
Sep 17,2012 11:59 PM ET
Public Submission Posted: 09/07/2012 ID: FAA-2012-0731-0005
Sep 17,2012 11:59 PM ET
Public Submission Posted: 09/18/2012 ID: FAA-2012-0731-0006
Sep 17,2012 11:59 PM ET
Public Submission Posted: 08/15/2012 ID: FAA-2012-0731-0003
Sep 17,2012 11:59 PM ET
Public Submission Posted: 01/17/2013 ID: FAA-2012-0731-0007
Sep 17,2012 11:59 PM ET