Lawrence La Beau

Document ID: FAA-2011-0639-0004
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: June 25 2011, at 12:00 AM Eastern Daylight Time
Date Posted: June 27 2011, at 12:00 AM Eastern Standard Time
Comment Start Date: June 22 2011, at 12:00 AM Eastern Standard Time
Comment Due Date: August 8 2011, at 11:59 PM Eastern Standard Time
Tracking Number: 80eb38e7
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From the Federal Register: With FAA assistance, the National Institute for Aviation Research (NIAR) investigated and concluded the root cause of the stabilator horn cracking was stress corrosion. (also)There is no service history of this unsafe condition on the Models PA-24-400, PA-30, and PA-39 airplanes, including inspections from the ICS operator survey. Also, these models have a thicker torque tube, which reduces clamp-up forces; clamp-up forces are a key factor of the stress corrosion cracking. Therefore, we are not including the..... From the above comments it would seem the torque values of the stabilator horn need to be reviewed and reduced. Also the torque tube needs to be replaced with a thicker tube reducing clamp-up forces reducing cracking of the horn.

Related Comments

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Total: 40
Kristin Amelia Winter
Public Submission    Posted: 06/24/2011     ID: FAA-2011-0639-0002

Aug 08,2011 11:59 PM ET
Lawrence La Beau
Public Submission    Posted: 06/27/2011     ID: FAA-2011-0639-0004

Aug 08,2011 11:59 PM ET
Charles Parker
Public Submission    Posted: 06/27/2011     ID: FAA-2011-0639-0005

Aug 08,2011 11:59 PM ET
David Charles Meigs
Public Submission    Posted: 06/29/2011     ID: FAA-2011-0639-0007

Aug 08,2011 11:59 PM ET
David Ray Fitzgerald
Public Submission    Posted: 07/05/2011     ID: FAA-2011-0639-0008

Aug 08,2011 11:59 PM ET