What was found
DURING OP 16 MAINT CHECK, FUSELAGE SKIN WAS CRACKED APPROX .5 INCH AT TOP AFT ADJUSTMENT HOLE FOR FWD ENTRY DOOR, STA 200 AND STRINGER 9L. REPAIRED PER MO 72M82, PRINT SRO9530252-2001, AND EMLR 70777.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING OP 16 MAINT CHECK, FUSELAGE SKIN WAS CRACKED APPROX .5 INCH AT TOP AFT ADJUSTMENT HOLE FOR FWD ENTRY DOOR, STA 200 AND STRINGER 9L. REPAIRED PER MO 72M82, PRINT SRO9530252-2001, AND EMLR 70777.