What was found
CRACK ON FUSELAGE SKIN BETWEEN BS 37 AND 110, RIGHT NOSE LANDING GEAR ABOVE AFT STRUT DOOR HINGE BEYOND STOP DRILL. REPAIRED IAW SRM 53-05-00-001.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON FUSELAGE SKIN BETWEEN BS 37 AND 110, RIGHT NOSE LANDING GEAR ABOVE AFT STRUT DOOR HINGE BEYOND STOP DRILL. REPAIRED IAW SRM 53-05-00-001.