What was found
DURING ROUTINE INSP, RT WING UPPER SKIN LEAD EDGE FOUND CRACKED AT WS 46, 8 INCHES FWD OF THE FWD WING SPAR.** S/D ** FAB & REPAIR PER IAW BAC 727 SRM 57-30-4 & SRM 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING ROUTINE INSP, RT WING UPPER SKIN LEAD EDGE FOUND CRACKED AT WS 46, 8 INCHES FWD OF THE FWD WING SPAR.** S/D ** FAB & REPAIR PER IAW BAC 727 SRM 57-30-4 & SRM 51-30-2.