What was found
CRACK ON THE INBOARD HINGE OF THE FOLDING NOSE ASSEMBLY ON THE NR 2 LEADING EDGE VARIABLE CAMBER FLAP LEFT WING. RECOMMENDATION IS TO ADD IT TO THE AGING FLEET INSPECTIONS.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK ON THE INBOARD HINGE OF THE FOLDING NOSE ASSEMBLY ON THE NR 2 LEADING EDGE VARIABLE CAMBER FLAP LEFT WING. RECOMMENDATION IS TO ADD IT TO THE AGING FLEET INSPECTIONS.