What was found
INSPECTION FOUND A 2 CRACK ON INBOARD SIDE OF LT UPPER SPAR WHERE CENTER HINGE OF LT REV COWL ATTACHES, NR 1 PYLON. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-33-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 CRACK ON INBOARD SIDE OF LT UPPER SPAR WHERE CENTER HINGE OF LT REV COWL ATTACHES, NR 1 PYLON. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-33-01.