N841MJ

Part: DOOR — MALFUNCTIONED · airframe 15,306 hrs · 14,155 cycles

FDM FLT 6118 MCO (0616 PHX LCL), MAIN CABIN DOOR WILL NOT SEAL WHEN CLOSED. MX CAN NOT DUPLICATE DISCREPANCY, OPS GOOD.

Part: COMPUTER — FAULTED (STALL WARNING) · airframe 15,159 hrs · 14,019 cycles

FDM 6003 RIC (0502 PHX LCL) - SPS 1/2 INOP MSG AND STICK PUSHER FAIL. MX RE-RACKED SPS COMPUTER, OPS CK GOOD.

Part: NONE — NONE (NONE) · airframe 15,160 hrs · 14,022 cycles

FDM 6118 MCO (1120 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO OPEN FROM INSIDE. MX CANNOT DUPLICATE DISCREPANCY. OPERATED NORMAL.

Part: WARNING LIGHT — ILLUMINATED (STALL WARNING) · airframe 15,161 hrs · 14,022 cycles

FDM 6118 MCO (1218 PHX LCL) - STICK PUSHER FAIL ON EICAS. MX RESET, SYSTEM OPS GOOD.

Part: CONNECTOR — DIRTY (RUDDER SYSTEM) · airframe 15,127 hrs · 13,993 cycles

FDM 6150 TYS. RUDDER SYSTEM NR 1 WILL NOT SHUT OFF. MX CLEANED CONNECTORS ON CONTROL PANEL SWITCH AND NR 1 PRESSURE SWITCH. OPS CK GOOD.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 14,969 hrs · 13,840 cycles

FDM 6005 MCO (1036 PHX LCL) - FLAP FAIL. MX REMOVED AND REPLACED FECU.

Part: HANDLE — DAMAGED (TE FLAPS) · airframe 14,972 hrs · 15,842 cycles

FDM RON DAY - FLAPS FAIL ON LANDING. MX REPLACED FLAP SELECT HANDLE, OPS CHECKED GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 14,944 hrs · 13,817 cycles

FDM 6137 ATL (0857 PHX LCL) - FLAP FAIL STUCK AT 45 DEGREES. MX RESET FLAP SYSTEM. OPS GOOD.

Part: LINE — DAMAGED (BLEED SYSTEM) · airframe 14,528 hrs · 13,417 cycles

FDM 9961 MCO (0807 PHX LCL) - ABORT T/O DUE TO NR 1 ENGINE OVERTEMP EXCEEDING 915 DEGREE C WITH MASTER WARNING. MX REMOVED AND REPLACED BLEED LINE.

Part: SERVO — FAILED (RUDDER) · airframe 14,154 hrs · 13,064 cycles

FDM 9964 JFK (1250 PHX LCL) YAW DAMPER FAIL. MX REMOVED & REPLACED RUDDER SERVO, OPS CHECK GOOD.

Part: PRESSURE SWITCH — FAULTY (RUDDER) · airframe 14,129 hrs · 13,042 cycles

FDM FLT 6134 MCO-PNS (1616 PHX LCL). RUDDER SYSTEM 1 WON'T SHUT OFF. MX REMOVED AND REPLACED RUDDER PRESSURE SWITCH.

Part: SENSOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 13,485 hrs · 12,469 cycles

FDM 6148 MCO-ATL (1020 PHX LCL). AIRCRAFT RETURNED TO THE FIELD FOR FUEL 2 LOW LEVEL MESSAGE IN FLIGHT. MX REMOVED AND REPLACED FUEL FLOW SENSOR.

Part: WARNING SYSTEM — MALFUNCTIONED (RUDDER SYS) · airframe 13,478 hrs · 12,457 cycles

FDM 9961 ATL-MCO (1635 PHX LCL). WHEN RUDDER SYSTEM 1 IS DEACTIVATED THERE IS NO ASSOCIATED EICAS MESSAGE. MX RESET THE SYSTEM AND OPS CHECKED.

Part: DOOR — LEAKING (SERVICE DOOR) · airframe 12,905 hrs · 11,972 cycles

FDM 6072 MCO-FLL (1716 PHX LCL). SERVICE DOOR LEAKING AIR IN FLIGHT. MX LEAK CHECK, OPS CHECKED GOOD.

Part: STRUCTURE — DAMAGED (PAX DOOR) · airframe 11,438 hrs · 10,746 cycles

DURING ROUTINE OVERNIGHT MAINTENANCE SCRATCHES/DAMAGE WERE NOTED ON THE MAIN CABIN DOOR. MAINTENANCE COMPLIED WITH RO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,174 hrs · 10,543 cycles

THE CREW REPORTED ONE EMERGENCY EXIT LIGHT INOP. MAINTENANCE RESET THE LIGHT SYSTEM.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 11,182 hrs · 10,547 cycles

THE CREW REPORTED A FALSE CARGO SMOKE WARNING AND FALSE APU WARNING. MAINTENANCE COULD NOT DUPLICATE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,114 hrs · 10,498 cycles

FDM 6115 MIA. THE CREW REPORTED A CABIN EXIT SIGN WOULD NOT ILLUMINATE. MAINTENANCE REPLACED THE EXIT SIGN.

Part: WARNING LIGHT — FALSE ACTIVATION (THRUST REVERSER) · airframe 10,894 hrs · 10,334 cycles

THE CREW ABORTED TAKEOFF ROLL DUE TO A NR 2 ENGINE THRUST REVERSER DISAGREE MESSAGE. CONTRACT MAINTENANCE PERFORMED AND OPERATIONAL CHECK OF THE THRUST REVERSER SYSTEM WITH NO FAULTS NOTED.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 10,824 hrs · 10,289 cycles

THE CREW FOUND THAT THE EMERGENCY LIGHTS WERE LEFT ON. MAINTENANCE REPLACED BOTH BATTERY PACKS.

Part: FLEX DUCT — UNKNOWN (NR 2 PACK)

DURING OVERNIGHT MAINTENANCE, A NR 2 PACK DUCT WAS REPLACED THROUGH A FLEET CAMPAIGN DIRECTIVE (FCD).

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 9,287 hrs · 8,804 cycles

DURING WALK AROUND DISCOVERED LT EXTERNAL OVERWING EMERGENCY LIGHT NOT ILLUMINATING. MX REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 10,055 hrs · 9,187 cycles

EMERGENCY OVERWING EXIT SIGN INOP. MAINTENANCE RESEATED THE CONNECTOR AND THE LIGHT WORKED.

Part: SWITCH — INOPERATIVE (THRUST REVERSER) · airframe 7,958 hrs · 7,084 cycles

ABORTED TAKEOFF DUE TO AN E2 REVERSE DISAGREE MESSAGE. MX PLACED NR 2 THRUST REVERSER ON MEL. A/C DEPARTED WITHOUT FURTHER INCIDENT. 8/30/04 MAINTENANCE REPLACED STOW/TRANSIT SWITCHES. S/N'S OFF 0037, 0040, 0041, 0039.

Part: CONNECTOR — LOOSE (BATTERY PACK) · airframe 7,151 hrs · 6,605 cycles

FLOOR PROX LIGHTS INOP BETWEEN ROWS 8-12. MX RECONNECTED BATTERY PACK CONNECTORS. NO PARTS USED.

Part: FIRE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 7,091 hrs · 6,543 cycles

ASH 2758 CLT. BAG FIRE EXTINGUISHER LIGHT W/N ILLUMINATE DURING FIRE TEST. FOUND BOTH BAG COMPARTMENTS FIRE EXTINGUISHERS EXPENDED. REPLACED BOTH EXTINGUISHERS. 224 CU IN P/N 33700027-1, S/N 39422D1, 360 CU IN P/N 34600073-1, S/N 19779F1.

Part: FIRE DETECTOR — MALFUNCTIONED (NR 2 ENGINE) · airframe 6,618 hrs · 6,138 cycles

CREW RETURNED TO FIELD REPORTING NR 2 ENG SHOWED FIRE INDICATION ON EICAS. MX PERFORMED THE REQUIRED FIRE WARNING INSPECTION AND CHECKS COUPLED WITH THE FIRE SYSTEM TEST AND ENGINE RUNS. NO DEFECTS NOTED. NO PARTS USED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 6,317 hrs · 5,894 cycles

DURING A RON, DISCOVERED THE LEFT OVERWING EMERGENCY LIGHT WAS INOP. MX REPLACED THE LAMP. OP CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,450 hrs · 5,173 cycles

ASH NR 2666. PIT AFT CABIN CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. MECHANIC REPLACED LIGHT. OP CHECKS GOOD.