What was found
DURING OP 16 MAINTENANCE CHECK, FOUND A .25 INCH CRACK IN OUTER FUSELAGE SURFACE ADJACENT TO NOSE GEAR DOOR, RT SIDE. REPAIRED CRACK PER SRM 53-05, FIG 62 SHEET 1 AND 2. SEALED REPAIR PER SRM 51-20-0. (M)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OP 16 MAINTENANCE CHECK, FOUND A .25 INCH CRACK IN OUTER FUSELAGE SURFACE ADJACENT TO NOSE GEAR DOOR, RT SIDE. REPAIRED CRACK PER SRM 53-05, FIG 62 SHEET 1 AND 2. SEALED REPAIR PER SRM 51-20-0. (M)