What was found
DURING C CHECK, FOUND A CRACK ON FUSELAGE SKIN LT SIDE OF THE VERTICAL STAB AT FRAME 75. REPAIRED IAW WITH SRM 53-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C CHECK, FOUND A CRACK ON FUSELAGE SKIN LT SIDE OF THE VERTICAL STAB AT FRAME 75. REPAIRED IAW WITH SRM 53-31-01.