What was found
C-2 DOOR SKIN CRACKED IN 2 PLACES AT UPPER EDGE 15 INCHES FWD OF AFT CORNER. REPAIRED PER SRM 52-00-3, FIG 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
C-2 DOOR SKIN CRACKED IN 2 PLACES AT UPPER EDGE 15 INCHES FWD OF AFT CORNER. REPAIRED PER SRM 52-00-3, FIG 3.