What was found
INSPECTION C, FUSELAGE BS 400, LT SIDE NOSE WHEEL WELL AFT CORNER FOUND CRACKED IN FIRST LAYER FROM SURFACE. FILLER REPLACED IAW SRM 51-10-02, REV 27 AND INSTALLED IAW RI-53-11-10442, REV A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION C, FUSELAGE BS 400, LT SIDE NOSE WHEEL WELL AFT CORNER FOUND CRACKED IN FIRST LAYER FROM SURFACE. FILLER REPLACED IAW SRM 51-10-02, REV 27 AND INSTALLED IAW RI-53-11-10442, REV A.