What was found
LEFT MAIN LANDING GEAR WHEEL WELL MAIN GEAR DOOR FOUND CRACKED AT HOLE PLUG AREA OF STRUT FITTING. CRACK REPAIRED AS PER SRM 52-10-00 FIG 13 VOL I. REPAIR DOUBLER FABRICATED AS PER SRM 52-10-00 FIG 13 VOL I.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT MAIN LANDING GEAR WHEEL WELL MAIN GEAR DOOR FOUND CRACKED AT HOLE PLUG AREA OF STRUT FITTING. CRACK REPAIRED AS PER SRM 52-10-00 FIG 13 VOL I. REPAIR DOUBLER FABRICATED AS PER SRM 52-10-00 FIG 13 VOL I.