N860MJ

Part: DOOR — OUT OF ADJUST (SERVICE DOOR) · airframe 11,818 hrs · 11,800 cycles

FRL FLT 6122 CVG TO CLT. SERVICE DOOR DIFFICULT TO OPEN AND CLOSE. MX ADJUSTED AND LUBED DOOR.

Part: SOLENOID — LEAKING (NLG DOOR) · airframe 11,568 hrs · 11,561 cycles

FRL FLT 6177 CVG-BWI. DECLARED EMERGENCY INTO BWI FOR HYDRAULIC SYSTEM 1 FAIL. MX SERVICED HYDRAULIC FOUND LEAK AT NLG DOOR SOLENOID, ALL OTHER HYDRAULIC SYSTEM CHECKS GOOD WITH NO LEAKS.

Part: SEAL — DIRTY (SERVICE DOOR) · airframe 11,474 hrs · 11,471 cycles

FRL FLT 6120 BNA TO CVG. IN FLIGHT SERVICE DOOR SQUEAL. MX CLEANED AND LUBED SERVICE DOOR SEAL, OPS GOOD.

Part: DOOR — DIRTY (SERVICE DOOR) · airframe 10,929 hrs · 10,945 cycles

FRL FLT 6240 CVG. COMMISSARY OPEN SERVICE DOOR TO STOCK AC IN DOING SO THE DOOR BECAME JAMMED AND WOULD NOT CLOSE. MX CLEANED AND LUBED DOOR.

Part: DOOR — LACK OF LUBE (GALLEY DOOR) · airframe 10,243 hrs · 10,270 cycles

FRL FLT 6283 CVG-DAY - GALLEY DOOR DIFFICULT TO CLOSE. MX CLEANED AND LUBED DOOR, OPS CHECKED GOOD.

Part: FUEL FILTER — DEFECTIVE (APU) · airframe 9,741 hrs · 9,753 cycles

FDM 6028 HSV-MCO (1757 PHX LCL). FUEL ODOR IN CABIN ON APU START. MX REMOVED AND REPLACED FUEL FILTER.

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 9,716 hrs · 9,733 cycles

FDM 6159 CVG-GSO (0503 PHX LCL). BAG DOOR WARNING LIGHT STAYS ILLUMINATED WITH DOOR VERIFIED CLOSED. MX ADJUSTED MICRO-SWITCH OPS CHECKED GOOD.

Part: UNKNOWN — ODOR · airframe 9,697 hrs · 9,716 cycles

FDM 6061 CVG-CHS (1348 PHX LCL). FUEL SMELL DURING BLEED TRANSFER TO APU. MX INSPECTED FOR FUEL LEAKS ON APU AND PERFORMED BLEED OPERATIONAL CHECK, NO LEAKS OR EVIDENCE OF FUEL SMELL FOUND.

Part: DUCT — DEFECTIVE (NR 2 PACK) · airframe 9,476 hrs · 9,511 cycles

FDM 6210 ATL. SMOKE IN CABIN AND COCKPIT. MX REMOVED AND REPLACED NR 2 PACK DUCT, OPS CHECKED GOOD.

Part: ENGINE — SMOKE (NR 1) · airframe 9,174 hrs · 9,218 cycles

FDM FLT 6025 TLH-ATL (1727 PHX LCL) - GROUND CREW REPORTED SMOKE AND FIRE FROM NR 1 ENGINE ON SHUTDOWN. MX PERFORMED ENGINE RUNS SHUTDOWN WAS NORMAL NO EVIDENCE OF FIRE.

Part: RELAY — MALFUNCTIONED (ANTI ICE SYS) · airframe 9,071 hrs · 9,119 cycles

FDM 6199 PWM (0959 PHX LCL) - DECLARED EMERGENCY, ICE CONDITION/ANTI-ICE FAIL, WING ANTI-ICE FAIL, AND BLEED 2 LOW TEM/OVER TEMP. MX REMOVED AND REPLACED K0435, K0531 RELAYS AND WING A/F VALVE.

Part: DOOR — LACK OF LUBE (GALLEY) · airframe 9,717 hrs · 9,074 cycles

FDM 6200 GALLEY DOOR WILL NOT CLOSE. MX PERFORMED ADJUSTMENT CHECK AND LUBED DOOR.

Part: COMPUTER — FAILED (STALL WARNING) · airframe 8,893 hrs · 8,958 cycles

FDM 6016 JFK (1000 PHX LCL) - SPS INOP/SP FAIL/CDU DATA BUSS FAIL. MX REMOVED AND REPLACED FMS COMPUTER AND UPLOADED DATA.

Part: INSULATION — BURNED (CABIN) · airframe 8,478 hrs · 8,568 cycles

FDM 6003 JFK (0920 PHX LCL). CREW RETURNED TO THE FIELD DUE TO A STRONG SMOKE ODOR COMING FROM ROOF OF GALLEY. MX FOUND INSULATION AGAINST LIGHT ASSY IN GALLEY, REPOSITIONED INSULATION. NO FURTHER SMOKE SMELL FOUND.

Part: BATTERY — DISCHARGED (CABIN) · airframe 8,452 hrs · 8,539 cycles

ASH 7407 IAD - CABIN EMERGENCY LIGHTS INOP. MX REMOVED AND REPLACED CABIN EMERGENCY BATTERIES. OPS GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 8,441 hrs · 8,229 cycles

ASH 7447 CLT - MAIN CABIN DOOR DIFFICULT TO CLOSE. MX CLEANED AND LUBED PAX DOOR.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 8,434 hrs · 8,524 cycles

CARGO DOOR CUT OUT FUSELAGE SKIN DAMAGE. REPAIRED FUSELAGE SKIN.

Part: CAP — CORRODED (MLG BEARING) · airframe 8,435 hrs · 8,524 cycles

RT AND LT MLG FWD BEARING CAP IS CORRODED OUT OF LIMITS. REPLACED CAP.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 8,434 hrs · 8,524 cycles

LT INBD FLOOR FLANGE FOUND CORRODED. REMOVED AND REPLACED FLANGE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 6,675 hrs · 6,735 cycles

ASH 7119 IAD - 4 EMERGENCY LIGHTS INOP. MX REMOVED AND REPLACED BATTERY PACK. OP'S CHECK GOOD.

Part: WARNING MESSAGE — ACTIVATED · airframe 6,543 hrs · 6,703 cycles

ASH 7262 IAD. CREW REPORTED A HARD OVER PROTECTION FAIL MESSAGE. MX RESET THE SYSTEM.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 6,063 hrs · 6,173 cycles

ASH 7189 CLT. ENGINE REV DISAGREE, RUDDER HARD OVER PROTECT MESSAGE. MX RESET SYSTEMS, OPS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (RUDDER) · airframe 5,311 hrs · 5,887 cycles

ASH 7149 IAD - RUDDER HAD OVER PROTECTION FAIL. MX RESET THE SYSTEM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,791 hrs · 5,865 cycles

ASH 7255 IAD - EMERGENCY LIGHT OVER LEFT WING WAS INOP. MX REPLACED THE LIGHT BULB. OP'S CHECK GOOD.

Part: COMPUTER — MALFUNCTIONED (RUDDER) · airframe 5,726 hrs · 5,816 cycles

ASH 7141 IAD - RUDDER HAD OVER PROTECTION FAIL MESSAGE. MX RESET THE FADEC.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 6,677 hrs · 5,738 cycles

ASH 7277 BOS - RUDDER HARDOVER PROTECT FAIL. MX RESET SYSTEM. OP'S CHECK GOOD.

Part: CONTROLLER — MALFUNCTIONED (RUDDER) · airframe 5,662 hrs · 5,720 cycles

ASH 7141 IAD - RUDDER HARD OVER PROTECTION FAIL MESSAGE. MX RESET THE FADEC.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 5,239 hrs · 5,277 cycles

ASH 7390 CLT - BULKHEAD AND GALLEY EMERGENCY LIGHTS INOP. MX REPLACED EMERGENCY LIGHT BATTERY PACK. OP'S CHECK GOOD.

Part: DUCT — ODOR (NR 2 PACK) · airframe 3,358 hrs · 3,256 cycles

ASH 2667 PHF TO CLT, THE CREW HAD THE NR 2 PACK PRODUCING A BURNING SMELL WHILE THE APU WAS SUPPLYING BLEED AIR ON THE GROUND. MAINTENANCE REMOVED AND REPLACED THE HIGH PRESSURE DUCTS AND OVERTEMP SWITCH. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 3,151 hrs · 3,017 cycles

LEFT HAND OVERWING EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT.

Part: CONTROL UNIT — FAILED (T/E FLAP) · airframe 3,107 hrs · 2,974 cycles

A FLAP HALF SPEED ON TAKEOFF. FLIGHT CREW CONTINUED TO CLT. CHANNEL 1 C/B POPPED AND WOULD NOT RESET CAUSING AN SPS ADVANCE CAUTION MESSAGE WHICH DEFERRAL OF THE FLAP SYSTEM. MAINTENANCE REPLACED THE FLAP ELECTRONIC CONTROL UNIT. NO FURTHER DEFECTS NOTED.

Part: DUCT — UNKNOWN (NR 2 PACK) · airframe 2,821 hrs · 2,649 cycles

CLT TO BNA HAD THE NR 2 PACK PRODUCE A BURNING SMELL WHILE IN USE. MAINTENANCE PLACED THE PACK ON MEL. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED 3 DUCTS, OPS CHECKED GOOD. P/N 145-22273-401, 145-22277-403 AND 145-22285-401, ALL NON SEARILIZED.

Part: WARNING LIGHT — ILLUMINATED (FUEL SYSTEM) · airframe 2,478 hrs · 2,287 cycles

ASH 2827 FROM ROC TO CLT ABORTED TAKEOFF DUE TO A FUEL IMBALANCE CAUTION MESSAGE. CONTRACT MAINTENANCE TRANSFERRED FUEL AND OPS CHECKED THE FUEL TRANSFER SYSTEM OPS GOOD. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT.

Part: FAN — ODOR (NR 2 PACK) · airframe 1,957 hrs · 1,753 cycles

MGM PACK NR 2 FAN (RECIRC FAN) PRODUCES ELECTRICAL SMELL. PLACED ON MEL AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT 10/2/04. MAINTENANCE REMOVED AND REPLACED THE RECIRCULATION FAN. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 1,565 hrs · 1,374 cycles

THE AIRCRAFT WAS ON RON AND SCHEDULED FOR A 2 DAY EN ROUTE INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THE GALLEY EMERGENCY LIGHT INOP. MAINTENANCE REPLACED THE LIGHT BULB. OPERATIONAL CHECK GOOD.

Part: CHARGER — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 836 hrs · 702 cycles

AFTER POWERING THE AIRCRAFT UP, THE FORWARD EMERGENCY LIGHT WOULD NOT EXTINGUISH. MX DISCONNECTED THE BATTERY CHARGER FROM THE NUMBER ONE EMERGENCY LIGHT BATTERY PACK. THE CONNECTIONS WERE INSPECTED, CLEANED AND RECONNECTED. THE LIGHTS WORKED NORMALLY UPON RE-POWERING. NO PARTS USED.

Part: ACTUATOR — LEAKING (GUST LOCK) · airframe 696 hrs · 579 cycles

RETURNED TO GATE. RUDDER ELECTRO MECHANICAL GUST LOCK WOULD NOT DISENGAGE. MX CURRENTLY TROUBLESHOOTING 4/1/2004. MX REPLACED THE GUST LOCK ACTUATOR. OP CHECKS GOOD.

Part: ENGINE — FLAMED OUT (NR 2) · airframe 454 hrs · 369 cycles

CREW REPORTED NR 2 ENGINE FLAMED OUT DURING LANDING ROLL-OUT. MX PERFORMED ENGINE RUNS. MX FOUND NO DEFECTS. NO PARTS USED.

Part: ENGINE — SHUTDOWN (NR 1) · airframe 110 hrs · 93 cycles

ASH 2607 ROC-DCA. NR 1 ENGINE SHUTDOWN AFTER PERFORMING FADEC RESET AS A PART OF DE-ICE PROCEDURES. RETURNED TO GATE, MX WAS CALLED. MX COULD NOT DUPLICATE. NO PARTS USED.

Part: UNKNOWN — UNKNOWN · airframe 40 hrs · 32 cycles

ASH 2609 - PITCH OSCILLATIONS IN YOKE AT 200KIAS DURING DESCENT WITH AP ENGAGED. FLAPS UP, GEARUP. PERFORMED GVI OF FLIGHT CONTROL SYSTEMS AND CHECKED CABLE TENSION. ALL CHECKED GOOD. MX COULD NOT DUPLICATE. NO PARTS USED.