What was found
FLAP COVE IN AREA OF RT WHEEL BENT UP AND HAS A 5 INCH CRACK. REPAIRED DAMAGED TO LOWER RT TRAILING EDGE WING SKIN FROM WS 57.20 TO 73.00 IAW EA SEM 500-0105 REV A DATED JULY 23, 2008. COMPLIED WITH TSR 57071208D REV C DATED 8/4/08. AFTER DAMAGE WAS CUT OUT NDT REPORTED NO INDICATIONS. SEE NDT REPORT FOR DETAILS. WEIGHT AND BALANCE FOR REPAIR NEGLIGIBLE. NOTE: SEE OTHER RELATED DOCUMENTS FAA FORM: 337 & 8110-3. (S)