Flint Aero, Inc.

Document ID: FAA-2011-0450-0003
Document Type: Public Submission
Agency: Federal Aviation Administration
Received Date: May 05 2011, at 12:00 AM Eastern Daylight Time
Date Posted: May 9 2011, at 12:00 AM Eastern Standard Time
Comment Start Date: May 4 2011, at 12:00 AM Eastern Standard Time
Comment Due Date: June 20 2011, at 11:59 PM Eastern Standard Time
Tracking Number: 80c40309
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Appendix 1, Section 11 As part of the installation of the Flint tip tanks it is necessary to modify the rib at WS222. These modifications include cutting out the rib to accommodate the fuel and vent lines for the aux tanks. We also give the installer the option of removing the rib completely aft of the aileron. This portion of the rib is used to close out and add integrity to the Cessna rib. The Cessna rib is removed and replaced by the Flint tips. Our recommendation is for the aft potion of the rib to be removed since it is no longer performing any function and could become dislodged at some point and interfere with aileron function. The Flint tip has its own closeout rib which maintains the structural integrity of the wing at WS222. Appendix 1, Section 13 Per Flint Aero Drawing FA337-IN, Rev F Dated 8/24/96 there should be no unreinforced cutouts in the wing skin. Flint Aero provides doublers for all added inspection openings. Appendix 1, Section 14 Per Flint Aero Drawing FA337-IN, Rev F Dated 8/24/96 there should be no penetrations of the spar cap except as necessary for the mounting of the tip tanks.

Related Comments

   
Total: 3
Dennis Hamblin
Public Submission    Posted: 05/11/2011     ID: FAA-2011-0450-0004

Jun 20,2011 11:59 PM ET
Natonal Transportation Safety Board
Public Submission    Posted: 06/24/2011     ID: FAA-2011-0450-0005

Jun 20,2011 11:59 PM ET
Flint Aero, Inc.
Public Submission    Posted: 05/09/2011     ID: FAA-2011-0450-0003

Jun 20,2011 11:59 PM ET