What was found
DURING HEAVY MAINTENANCE VISIT, A CRACK WAS FOUND EXTENDING FROM A FLANGE RADIUS AT THE BOTTOM OUTBD CORNER OF THE REAR SPAR WING TO BODY FITTING. FABRICATED AND INSTALLED REPAIRS IN ACCORDANCE WITH B727 SRM 51-20-1 AND 51-30-2.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING HEAVY MAINTENANCE VISIT, A CRACK WAS FOUND EXTENDING FROM A FLANGE RADIUS AT THE BOTTOM OUTBD CORNER OF THE REAR SPAR WING TO BODY FITTING. FABRICATED AND INSTALLED REPAIRS IN ACCORDANCE WITH B727 SRM 51-20-1 AND 51-30-2.