What was found
DURING C-CHECK, FOUND 5 INCH CRACK IN FLOORBEAM UPPER FLANGE AT, Y=1580 AND X PLUS 45. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW TIMCO REO-02712 DTD 2/4/97 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 5 INCH CRACK IN FLOORBEAM UPPER FLANGE AT, Y=1580 AND X PLUS 45. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW TIMCO REO-02712 DTD 2/4/97 AND FAA-DER APPROVED CFG-01239 AND 8110-3 FORM (DER NR SO-135).