N112PS

Part: BATTERY — MALFUNCTIONED (SMOKE DETECTOR)

ATC WAS NOTIFIED OF A FIRE WARNING LIGHT ACTIVATION. FLIGHT DIVERTED TO NEAREST SUITABLE AIRPORT. CARGO SMOKE DETECTION LIGHT IN THE FORWARD BAGGAGE COMPARTMENT ILLUMINATED WHILE ENROUTE. THE ONLY ITEMS IN THE COMPARTMENT WAS A FLY AWAY KIT. THE FLIGHT MANUAL WAS CONSULTED AND EMERGENCY PROCEDURES FOLLOWED. FLIGHT WAS MET BY THE FIRE DEPARTMENT UPON LANDING. ALL CARGO COMPARTMENTS WERE CHECKED BY THE CREW AND THE FIRE DEPARTMENT AND NO SIGNS OF FIRE OR SMOKE WERE DETECTED. ALL ITEMS WERE REMOVED FROM BOTH CARGO BAYS. (SO15200324766)

Part: CONTROL VALVE — INOPERATIVE (RT MLG BRAKE)

FLT 319 - FWA-CHYM - ON TAXI TO TAKEOFF, THE FLIGHT CREW DISCOVERED THAT THE RIGHT BRAKE WOULD NOT APPLY. THE AIRCRAFT TAXIED TO PARKING WITHOUT INCIDENT. THE RIGHT BRAKE CONTROL VALVE WAS REPLACED. OPS CHECK ON GROUND SATISFACTORY. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLOORBOARD — DAMAGED (CABIN)

DURING POST FLIGHT INSPECTION, FOUND HOLES PUNCHED IN THE FLOORBOARDS AT THE FOLLOWING STATIONS 480 X=12L, 427 X=38L AND 605 X=12R. THE FLOORBOARDS WERE REPAIRED IAW THE DC-9 SRM, THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — DAMAGED (BS 200)

DURING C-CHECK INSPECTION, FOUND SKIN DAMAGE BY THE MAIN ENTRANCE DOOR AIRSTAIR CUTOUT AT L22L AND STATION 200. THE SKIN WAS REPAIRED IAW KITTY HAWK EA D9-53-069 THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — DELAMINATED (LT TE FLAP)

DURING C-CHECK INSPECTION, FOUND DELAMINATION ON THE LEFT FLAP REMOVABLE PANEL TRAILING EDGE SKIN AT XFLS187. THE SKIN WAS REPLACED IAW KITTY HAWK EA D9-53-073. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SUPPORT — DAMAGED (HORIZ STABILIZER)

DURING C-CHECK INSPECTION, FOUND THE LEFT HORIZONTAL STABILIZER FORWARD LOWER FAIRING SUPPORT DAMAGED. THE SUPPORT WAS REPAIRED IAW KITTY HAWK EA D9-53-070 THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — CRACKED (TE FLAP)

DURING C-CHECK INSPECTION, FOUND A CRACK ON THE LT FLAP LEADING EDGE SKIN AT XW250. THE SKIN WAS REPAIRED IAW KITTY HAWK EA D9-53-072. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — CORRODED (BS 484-544)

DURING C-CHECK INSPECTION, FOUND CORROSION BETWEEN THE LEFT WINDOW BELT AND THE FUSELAGE SKIN FROM STATION 544 TO 484. THE SKIN WAS REPAIRED IAW KITTY HAWK EA D9-53-071 THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: WIRE — BROKEN (RT MLG WW)

KHA - FLT 322 - YIP - ELP - ON CLIMB-OUT FROM YIP, AFTER RETRACTING THE LANDING GEAR, THE UPLATCH CHECK WAS UNSATISFACTORY. THE CREW DECIDED TO RETURN TO YIP. ON GEAR EXTENSION, THREE GREEN LIGHTS CAME ON AND THE RIGHT MAIN RED LIGHT CAME ON. AN UNEVENTFUL LANDING WAS MADE. INSPECTION FOUND, THE RIGHT MLG DOWNLOCK SWITCH CONDUIT PINCHED AND THE WIRES PULLED FROM THE CONNECTOR. THE CONNECTOR WAS REPLACED AND THE WIRES WERE SPLICED. THE SYSTEM WAS OPS CHECKED PER DC9 MM. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FIRE WARNING — ILLUMINATED (NR 2 ENGINE)

KHA - FLT 112 - YIP TO YIP. WHILE IN CRUISE, THE NR 2 ENGINE A-LOOP LIGHT ILLUMINATED. THE FLIGHT CREW PERFORMED FIRE CHECK, ALL NORMAL. DURING TAXI, BOTH LOOPS TESTED NORMAL. INSPECTION PERFORMED FIRE WARNING TEST PER DC-9 MM. ALL TESTS OK. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)

Part: SKIN — DENTED (BS 365-413)

DURING C-CHECK INSPECTION, FOUND SEVERAL GOUGES AND A DENT ON THE FUSELAGE SKIN JUST BELOW THE MAIN CARGO DOOR. THE DAMAGE WAS REPAIRED IAW KITTY HAWK EA D9-53-045. (M)

Part: SKIN — DENTED (BS 180-229)

DURING C-CHECK INSPECTION, FOUND A TEMPORARY REPAIR AND DENT ON THE FUSELAGE SKIN JUST BELOW THE FORWARD SERVICE DOOR BETWEEN LONGERON 21R AND THE CUSP. THE DAMAGE WAS REPAIRED IAW KITTY HAWK EA D9-53-044. (M)

Part: FLOORBEAM — CRACKED (BS 566)

DURING INSPECTION OF PSE 53-09-015 WHILE AIRCRAFT WAS IN C-CHECK, A CRACK WAS FOUND ON THE FLOORBEAM AT STATION Y=566 AT X=54.50. REPLACED FLOORBEAM. (M)

Part: FLOORBEAM — CRACKED (BS 566)

DURING INSPECTION OF PSE 53.09.015 WHILE AIRCRAFT WAS IN C-CHECK, A CRACK WAS FOUND ON THE FLOORBEAM AT STATION Y=566 AT X=54.50. THE FLOORBEAM WAS REMOVED AND REPLACED IAW THE DC-9 SRM. (M)

Part: FRAME — CRACKED (BS 544)

DURING 'B' CHECK INSPECTION FOR AD 73-09-02 A CRACK WAS DISCOVERED ON THE RIGHT FUSELAGE FRAME AT STATION 544 JUST BELOW THE FLOOR LINE. THE AIRCRAFT WAS FERRIED TO DFW FOR REPAIR. (M)

Part: FRAME — CRACKED (BS 544)

DURING B-CHECK INSPECTION FOR AD 73-09-02, A CRACK WAS DISCOVERED ON THE RIGHT FUSELAGE FRAME AT STA 544 JUST BELOW THE FLOOR LINE. THE AIRCRAFT WAS FERRIED TO DFW FOR REPAIR. THE FRAME WAS REPAIRED PER DC-9 SB 53-117. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)