N847MJ

Part: CONTROL PANEL — MALFUNCTIONED (SMOKE WARNING) · airframe 14,272 hrs · 13,304 cycles

FDM 6022 JFK (0620 PHX LCL) - LAV SMOKE WARNING IN FLIGHT. MX REMOVED AND REPLACED SMOKE DETECTOR PANEL.

Part: DCU — MALFUNCTIONED (SMOKE DETECTOR) · airframe 14,247 hrs · 13,278 cycles

FDM 6015 JFK-ORF (2100 PHX LCL) - LAV SMOKE INDICATION IN FLIGHT. MX REMOVED AND REPLACED DCU, OPS GOOD.

Part: MANIFOLD — MALFUNCTIONED (AILERONS) · airframe 14,068 hrs · 13,116 cycles

FDM RON MCO (1903 PHX LCL) - AILERON SYSTEM 2 WON'T DEACTIVATE. MX REMOVED AND REPLACED AILERON MANIFOLD ASSY.

Part: FCU — MALFUNCTIONED (FLAPS) · airframe 13,739 hrs · 12,814 cycles

FDM RON RDU (0034 PHX LCL) - LOW FLAP SPEED MESSAGE ON EICAS. MX REMOVED AND REPLACED FECU.

Part: SEAL — UNSECURE (PAX DOOR) · airframe 13,718 hrs · 12,798 cycles

FDM RON RDU - LOUD SQUEAL IN FLIGHT FROM PAX DOOR. MX RESECURED THE DOOR SEAL, PRESSURIZED THE CABIN AND FOUND NO FURTHER LEAK.

Part: SWITCH — LACK OF LUBE (PITCH TRIM) · airframe 13,622 hrs · 12,703 cycles

BACK UP PITCH TRIM DOWN NOT WORKING. LUBED SWITCH, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 13,519 hrs · 12,604 cycles

FDM 6125 MCO (0515 PHX LCL) - ALL EMERGENCY LIGHTS INOP. MX REMOVED AND REPLACED ALL EMERGENCY BATTERY PACKS OPS CK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 14,824 hrs · 14,009 cycles

FDM 6146 GPT (0710 PHX LCL). EMERGENCY LIGHT INOP. MX PERFORMED OPS CHECKS, OPS GOOD.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 13,221 hrs · 12,331 cycles

FDM 6128 FLL (1735 PHX LCL) - CREW RETURNED TO THE FIELD DUE TO LAV SMOKE WARNING. MX PERFORMED DETAILED GVI OF LAV, CABIN, CARGO BAY AND AFT EQUIPMENT BAY NO EVIDENCE OF SMOKE OR FIRE. PERFORMED ENGINE RUN WITH BOTH PACKS ON NO EVIDENCE OF SMOKE NOTED. PERFORMED OPS CHECK OF LAV SMOKE DETECTOR, OPS CHECK GOOD.

Part: SIGN — MALFUNCTIONED (CABIN) · airframe 13,149 hrs · 12,269 cycles

FDM 6003 RIC (0400 PHX LCL). RIGHT OVERWING EMERGENCY SIGN INOP. RESET AIRCRAFT POWER, OPS CHECK GOOD.

Part: TRIM SWITCH — INOPERATIVE (COCKPIT) · airframe 13,111 hrs · 12,231 cycles

FDM 6038 CVG-CLT (1500 PHX LCL). CAPTAIN'S PITCH TRIM SWITCH INOPERATIVE. MX REMOVED AND REPLACED TRIM SWITCH.

Part: TRIM SWITCH — DIRTY (COCKPIT) · airframe 13,110 hrs · 12,230 cycles

FDM 6035 DAY-CVG (1033 PHX LCL). CAPTAINS TRIM SWITCH IN DOWN POSITION INOP. MX CLEANED THE TRIM SWITCH, OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (CABIN) · airframe 13,050 hrs · 12,172 cycles

FDM 6210 JFK-PWM (0529 PHX LCL) - 12BC EMERGENCY DOOR LOCATOR SIGN INOP. MX RESET SYSTEM OPS CK GOOD.

Part: UNKNOWN — UNKNOWN · airframe 12,899 hrs · 12,039 cycles

RUDDER HARD OVER PROTECTION FAIL. RESET NO FURTHER ACTION REQUIRED.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,883 hrs · 12,014 cycles

FDM 6012 ATL-BGM (0917 PHX LCL) - RT ROW 12 EMERGENCY LOCATOR SIGN INOP. MX RESET OPS CK GOOD.

Part: UNKNOWN — UNKNOWN (RUDDER) · airframe 12,867 hrs · 12,002 cycles

RUDDER HARD OVER PROTECTION FAIL. MX RESET SYSTEM, OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 12,706 hrs · 11,854 cycles

FDM 6017 (1919 PHX LCL). RT OVERWING EXIT LIGHT INOP. MX RESET SYSTEM OPS GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (FUEL SYSTEM) · airframe 12,579 hrs · 11,741 cycles

FDM 6000 FLL-MCO (0616 PHX LCL). ABORTED T/O AND RTG DUE TO FUEL 1 AND 2 LOW PSI WARNING MESSAGE. CREW PERFORMED ENGINE RUNS WITH NO DEFECTS NOTED, OPS CHECK NORMAL.

Part: CONNECTOR — LOOSE (CABIN) · airframe 12,564 hrs · 11,726 cycles

FDM 6173 FLL-TLH (0645 PHX LCL). BOTH EMERGENCY DOOR LIGHTS INOP. MX RE-SECURED CONNECTOR ON NR 3 POWER SUPPLY.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 12,544 hrs · 11,709 cycles

CARGO DOOR THRESHOLD IS CORRODED OUT OF LIMITS. THE DAMAGED THRESHOLD HAS BEEN REMOVED AND REPLACED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,544 hrs · 11,709 cycles

FLOORBEAM TEE AT FRAME 65 LT SIDE IS CRACKED. THE DAMAGED CROSS FRAME HAS BEEN REMOVED AND REPLACED.

Part: PANEL — CRACKED (OVERWING) · airframe 12,544 hrs · 11,709 cycles

UPPER FLANGE FOR FUSELAGE OVERWING PANEL NR 194 IS CRACKED. THE DAMAGE HAS BEEN REPAIRED.

Part: SWITCH — LACK OF LUBE (CARGO DOOR) · airframe 12,578 hrs · 11,937 cycles

FDM 6026 BNA-MCO (1611 PHX LCL). AIRCRAFT RETURNED TO THE FIELD FOR A CARGO DOOR OPEN EICAS INDICATION IN FLIGHT. MX LUBRICATED MICRO SWITCH AND OPS CHECKED.

Part: FLOOR SUPPORT — CORRODED (LAVATORY AREA) · airframe 12,544 hrs · 11,709 cycles

DIGITAL FLOOR SUPPORT IS CORRODED OUT OF LIMITS UNDER THE COMPOSITE SUPPORT MEMBER, LOCATED LAV AREA ON THE RT SIDE OF THE FUSELAGE. THE DIGITAL HAS BEEN REMOVED AND REPLACED.

Part: SWITCH — FAULTY (THRUST TREVERSER) · airframe 12,208 hrs · 11,418 cycles

FDM 6085 MCO-NAS (0918 PHX LCL). CREW ABORTED T/O DUE TO E1 TR REV DISAGREE MESSAGE. MX REMOVED AND REPLACED LOWER TRANSIT SWITCH.

Part: SWITCH — MALFUNCTIONED (THRUST REVERSER) · airframe 11,924 hrs · 11,176 cycles

FDM 6084 MCO-CMH (0804 PHX LCL). ABORTED T/O DUE TO E1 TR DISAGREE MESSAGE. MX REMOVED AND REPLACED UPPER OUTBOARD STOW SWITCH.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 11,756 hrs · 11,030 cycles

FDM 6097 ATL-CLT (1920 PHX LCL). RT SIDEWALL EMERGENCY LIGHT INOP ROW 12. MX CYCLED THE LIGHT SWITCH AND THE LIGHTS OPERATED NORMALLY.

Part: SWITCH — MALFUNCTIONED (THRUST REVERSER) · airframe 11,707 hrs · 10,980 cycles

FDM 9962 CLT-ATL (0904 PHX LCL). ABORTED T/O DUE TO E2 TR DISAGREE MESSAGE ON T/O. MX REMOVED AND REPLACED STOW TRANSIT SWITCH.

Part: CONTROL UNIT — MALFUNCTIONED (THRUST REVERSER) · airframe 11,602 hrs · 11,060 cycles

FDM 5964 HSV-ATL (0523 PHX LCL). ABORTED TAKEOFF AND RETURNED TO GATE DUE TO AN E1 REVERSER DISAGREE MESSAGE. MX REMOVED AND REPLACED NR 1 ICU.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 11,471 hrs · 10,789 cycles

FDM 6085 PFN-MCO (0602 PHX LCL). CREW ABORTED TAKEOFF DUE TO AN E2 T/R MESSAGE. OPS CHECKED GOOD BY MAINTENANCE.

Part: CONTROL SYSTEM — MALFUNCTIONED (AILERONS) · airframe 11,307 hrs · 10,653 cycles

FDM 6113 PNS. AILERON SYSTEM 2 INOPERATIVE EICAS MESSAGE. MX RESET WITH THE CREW AND MESSAGE CLEARED.

Part: WARNING LIGHT — FALSE ACTIVATION (COCKPIT) · airframe 11,190 hrs · 10,563 cycles

FDM 6091 PHF. THE CREW REPORTED A RUDDER HARD OVER PROTECTION FAIL AT POWER UP. MAINTENANCE RESET SYSTEM.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSER) · airframe 11,156 hrs · 10,533 cycles

FDM 6195 MCO - CREW RECEIVED E1 REV MESSAGE DURING TAKEOFF ROLL. MAINTENANCE OPS CHECKED THE E1 REV GOOD.

Part: STALL WARNING — MALFUNCTIONED (NR 2) · airframe 11,131 hrs · 10,517 cycles

FDM 6201 ATL - CREW REPORTED THE STALL PROTECTION SYSTEM NR 2 INOP. MAINTENANCE RESET THE SYSTEM AND OP CHECK NORMAL.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 11,135 hrs · 10,521 cycles

CREW NOTED EMERGENCY FLOOR STRIPS AT ROW 3 THROUGH 7 INOP. MAINTENANCE CYCLED THE SWITCH AND THE LIGHTS FUNCTIONED NORMALLY.

Part: WARNING SYSTEM — MALFUNCTIONED (RUDDER) · airframe 11,130 hrs · 10,516 cycles

FDM 9961 BNA - CREW REPORTED A RUDDER HARD OVER PROTECTION FAIL MESSAGE. MAINTENANCE RESET THE SYSTEM AND OPS CHECK NORMAL.

Part: LIGHT — UNKNOWN (CABIN) · airframe 10,933 hrs · 10,340 cycles

FDM 6134 MCO. THE CREW REPORTED THE FIRST ROW EMERGENCY LIGHT INOP. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,933 hrs · 10,340 cycles

FDM 6156 MCO. THE CREW REPORTED THE 1ST ROW EMERGENCY LIGHTS INOP. MAINTENANCE REPLACED THE LIGHTS. OPS GOOD.

Part: WARNING SYSTEM — MALFUNCTIONED (RUDDER) · airframe 10,907 hrs · 10,316 cycles

FDM 6118 MCO - THE CREW REPORTED A RUDDER HARDOVER PROTECTION FAIL EICAS CAUTION MESSAGE. MAINTENANCE RESET THE FADEC.

Part: WARNING MESSAGE — FALSE ACTIVATION (RUDDER) · airframe 10,816 hrs · 10,245 cycles

FDM 6083 AUS - THE CREW REPORTED A RUDDER HARDOVER PROTECTION MESSAGE. RESET FADEC WITH THE CREW MESSAGE CLEARED.

Part: RELAY — FAILED · airframe 10,648 hrs · 10,115 cycles

THE CREW DECLARED AN EMERGENCY AND DIVERTED TO ATL DUE TO VISUAL SMOKE IN THE CABIN AND STRONG ELECTRICAL SMOKE SMELL. MAINTENANCE REPLACED THE RELAY AND THE RELAY BASE.

Part: BONDING STRAP — BROKEN (PAX DOOR) · airframe 10,635 hrs · 10,104 cycles

THE CREW NOTED THE BONDING STRAP BROKEN ON MAIN CABIN DOOR. MAINTENANCE RECONNECTED BONDING STRAP ON MAIN CABIN DOOR.

Part: CONNECTOR — LOOSE (CABIN) · airframe 10,632 hrs · 10,102 cycles

RTL 6061 MCO. FWD EMERGENCY FLOOR LIGHT STRIP WAS INOP. MX RESECURED CONNECTOR. OP'S CHECK GOOD.

Part: BONDING STRAP — BROKEN (PAX DOOR) · airframe 10,547 hrs · 10,440 cycles

THE CREW FOUND THE BONDING STRAP ON PAX DOOR WAS BROKEN. MAINTENANCE RE-ATTACHED THE STRAP.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 10,532 hrs · 10,032 cycles

THE CREW REPORTED A RUDDER HARD OVER PROTECTION MESSAGE ON EICAS. MAINTENANCE RESET WITH THE CREW.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 10,014 hrs · 9,594 cycles

ASH RON CAE - ROW 12 LOOKING FWD EMERGENCY LIGHT INOP. MX RELAMPED.

Part: SWITCH — MALFUNCTIONED (THRUST REVERSER) · airframe 9,813 hrs · 9,393 cycles

ABORTED TAKEOFF DUE TO A E-2 THRUST REVERSER DISAGREE. MAINTENANCE REPLACED STOW TRIM SWITCHES.

Part: CONTROL UNIT — MALFUNCTIONED (THRUST REVERSERS) · airframe 9,710 hrs · 9,274 cycles

ASH 2901 CLT. E2 REVERSE DISAGREE. MAINTENANCE REMOVED AND REPLACED ICU.

Part: CARBON SEAL — LEAKING (ENGINE) · airframe 9,699 hrs · 9,265 cycles

ASH 2829 MGM. SHUTDOWN THE ENGINE DUE TO THE LOST OF ENGINE OIL PRESSURE AND THE LOST OF ENGINE OIL. MAINTENANCE REPLACED NR 2 GENERATOR AND NR 2 GENERATOR CARBON SEAL.

Part: RELAY — FAILED (THRUST REVERSER) · airframe 9,670 hrs · 9,240 cycles

ASH 2989 CLT, NR 2 THRUST REVERSER DISAGREE. MAINTENANCE REPLACED THE AIR TO GROUND RELAY.

Part: ELT — MALFUNCTIONED (CABIN) · airframe 9,498 hrs · 9,064 cycles

ASH 2994 CLT - AIRCRAFT RETURNED TO FIELD DUE TO ELT CAME ON UNCOMMANDED IN FLIGHT. MX RESET ELT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,098 hrs · 8,644 cycles

LT FWD FLOOR EMERGENCY STRIP INOP. REPLACED STRIP.

Part: SIGN — LOOSE (EMERGENCY EXIT) · airframe 8,253 hrs · 7,699 cycles

ASH 2686 CLT TO GSO - THE CREW NOTED THAT THE OVERWING CEILING EMERGENCY EXIT SIGN WAS INTERMITTENT DURING TEST. MAINTENANCE RE-SECURED THE SIGN ASSEMBLY AND IT OPERATED NORMALLY. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 7,868 hrs · 7,275 cycles

CLT - FOURTH FROM FWD OVERHEAD EMERGENCY CABIN LIGHT INOP. MAINTENANCE REPLACED THE LIGHT.

Part: ROD — OUT OF ADJUST (THRUST REVERSER) · airframe 7,431 hrs · 6,843 cycles

AIRCRAFT ABORTED TAKEOFF DUE TO AN E2 REV DISAGREE MESSAGE DURING TAKEOFF ROLL. CONTRACT MX PLACED THE NR 2 THRUST REVERSER ON MEL. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. OPEN PENDING RESOLUTION OF MEL. 12/29 MAINTENANCE ADJUSTED LOWER ACTUATOR ROD AND RIGGED ALL SWITCHES. OPS CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 7,427 hrs · 6,837 cycles

ABORTED TAKEOFF DUE TO E2 REVERSER DISAGREE ON TAKEOFF. MESSAGE WENT AWAY, AN ON-CALL MAINTENANCE PERFORMED OPERATIONAL CHECK AND RETURNED THE AIRCRAFT TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,436 hrs · 5,859 cycles

ASH 2994 DCA, CREW REPORTED THE EMERGENCY EXIT LIGHT AT GALLEY INOP. MX TROUBLESHOT TO BAD POWER SUPPLY. MX REPLACED THE POWER SUPPLY ASSY.

Part: SWITCH — INOPERATIVE (THRUST REVERSER) · airframe 5,862 hrs · 5,356 cycles

AIRCRAFT ABORTED TAKEOFF AND RETURNED TO GATE WITH NR 2 ENGINE THRUST REVERSER DISAGREE MSG. MX PLACED THRUST REV ON MEL. MX REPLACED THE LOWER DOOR OUTBOARD STOW/TRANSIT SWITCH, OPS CHECKED GOOD.