What was found
TWO CRACKS FOUND ON THE FUSELAGE SKIN FWD UPPER DOOR FRAME CORNER BS 375 BETWEEN LONGERONS 20 - 21R. THE AREA WAS REPAIRED IAW SRM 53-05, FIG 105, 51-30-5 AND 51-10-3 PAR 14,21. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
TWO CRACKS FOUND ON THE FUSELAGE SKIN FWD UPPER DOOR FRAME CORNER BS 375 BETWEEN LONGERONS 20 - 21R. THE AREA WAS REPAIRED IAW SRM 53-05, FIG 105, 51-30-5 AND 51-10-3 PAR 14,21. MAJOR REPAIR.