What was found
AFTER HARD LANDING INSPECTION:-AFT FUSELAGE, Sta Y1345, LOWER SECTION AT -Z37, BETWEEN -X14 TO +X13, ANGLE BENDED & CRACKED.-REPAIRED APU ENCLOSURE ANGLE IN Sta Y1345 BETWEEN +X9 & +X17 AND BETWEEN -X8 & -X16, -Z33 & -Z37 DUE TO CRACK, IAW COOPESA E.O. No.COO-9-53-408-02, DATED JULY 22,2002. DOCUMENTED IN FAA 8110-3 FORM.Note: SEE COOPESA´S WORK ORDER No.PI0701,1-30, VAM100No.036 & 140SDA008.