AD for the Attach Angle-
http://rgl.faa.gov/Regulatory_and_Guida ... ction_.pdfFrom the AD text-
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for Rockwell International
(Aircraft Specification No. A-2-575 previously held by North American and recently purchased by
Boeing) Models AT-6 (SNJ-2), AT-6A (SNJ-3), AT-6B, AT-6C (SNJ-4), AT-6D (SNJ-5), AT-6F
(SNJ-6), BC-1A, SNJ-7, and T-6G airplanes; and Autair Ltd. (Aircraft Specification No. AR-11
previously held by Noorduyn Aviation Ltd.) Model Harvard (Army AT-16) airplanes. This AD
contains the same information as emergency AD 2005-12-51 and publishes the action in the Federal
Register. It requires immediate and repetitive inspections of the inboard and outboard, upper and
lower wing attach angles (except for the nose angles) of both wings for fatigue cracks; and, if any
crack is found, replacement of the cracked angle with a new angle. This AD is the result of a report of
a Rockwell International Model SNJ-6 (AT-6F) airplane crash that occurred on May 9, 2005,
resulting in two fatalities. We are issuing this AD to detect and correct any fatigue crack in the
inboard and outboard, upper and lower wing attach angles (except for the nose angles) of either wing,
which could result in failure of the wing. This failure could lead to loss of control of the aircraft.