What was found
CRACK OF MORE THEN 50 PERCENT OF CHORD WIDTH TO NR 1 ENGINE 7 O'CLOCK EXHAUST STRUT. NO CORRECTIVE ACTION, TO BE INSPECTED EVERY 100 HOURS PER BAC MM 72-53-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK OF MORE THEN 50 PERCENT OF CHORD WIDTH TO NR 1 ENGINE 7 O'CLOCK EXHAUST STRUT. NO CORRECTIVE ACTION, TO BE INSPECTED EVERY 100 HOURS PER BAC MM 72-53-02.