What was found
DURING C-CHECK, FOUND CRACK ON UPPER FLANGE ON LONGERON 26 LEFT AT, Y=200. REMOVED DAMAGE, FABRICATED INSERT REPAIR AND INSTALLED IAW TIMCO REO-02740 DTD 2/8/97 AND FAA-DER APPROVED CFG-01239 AND 8110-3 FORM (DER NR SO-135).
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND CRACK ON UPPER FLANGE ON LONGERON 26 LEFT AT, Y=200. REMOVED DAMAGE, FABRICATED INSERT REPAIR AND INSTALLED IAW TIMCO REO-02740 DTD 2/8/97 AND FAA-DER APPROVED CFG-01239 AND 8110-3 FORM (DER NR SO-135).