What was found
INSPECTION FOUND A 1 CRACK IN ANGLE AT LT WHEEL WELL REAR SPAR, WS 118. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-00, 51-33-01, AND 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 CRACK IN ANGLE AT LT WHEEL WELL REAR SPAR, WS 118. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-00, 51-33-01, AND 51-31-01.