What was found
FOUND FUSELAGE INNER CHORD RING CRACKED. CRACK LOCATED AT FASTENER HOLE LBL 33.5 AND WL 153 BS 140 FPB (REAR FACE). FOUND DURING INSPECTION IAW AD/B747/159 AND EI 747-053-0215.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FOUND FUSELAGE INNER CHORD RING CRACKED. CRACK LOCATED AT FASTENER HOLE LBL 33.5 AND WL 153 BS 140 FPB (REAR FACE). FOUND DURING INSPECTION IAW AD/B747/159 AND EI 747-053-0215.