What was found
DURING NDT INSPECTION FOUND CRACK ON LOWER SPAR CAP HOLE. PERMANENT REPAIR ACCOMPLISHED IAW FEDEX EO 8-5710-7-3318 P2 CONDITION 3 STEP 5 AND DWG SR10570048 CONFIGURATION -7015.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING NDT INSPECTION FOUND CRACK ON LOWER SPAR CAP HOLE. PERMANENT REPAIR ACCOMPLISHED IAW FEDEX EO 8-5710-7-3318 P2 CONDITION 3 STEP 5 AND DWG SR10570048 CONFIGURATION -7015.