N825MJ

Part: UNKNOWN — ODOR (CABIN) · airframe 19,735 hrs · 18,068 cycles

FLT 6120. DURING TAKEOFF CLIMB AND WHEN THE BLEED SOURCE WAS SWITCHED FROM THE APU BLEED TO THE ENGINE BLEED A FUEL ODOR CAME OVER THE COCKPIT & CABIN. CHECKED FOR LEAKS WITH NONE NOTED. RAN APU FOR AN HOUR WITH NO DEFECTS. PERFORMED ENGINE RUN WITH APU ON AND CYCLED PACKS AND BLEEDS. NO FAULTS FOUND.

Part: FUEL FILTER — LOOSE (APU) · airframe 18,571 hrs · 16,952 cycles

FLR FLT 6223 JFK-CLT. FUEL SMELL IN COCKPIT DURING TAKEOFF. MX FOUND FUEL FILTER ASSY LOOSE. RE-SECURED AND PERFORMED OPS CHECKS AND CHECKS WERE NORMAL.

Part: HANDLE — OUT OF ADJUST (PAX DOOR) · airframe 18,144 hrs · 16,521 cycles

FRL FLT 6268 IAD. MAIN CABIN DOOR INNER HANDLE CATCHES ON DOOR TRIM. MX ADJUSTED HANDLE, OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (PAX DOOR) · airframe 18,018 hrs · 16,394 cycles

FRL FLT 6243 IAD-JFK. MAIN CABIN DOOR HARD TO OPEN. MX LUBED DOOR, OPS GOOD.

Part: PUMP — FAILED (HYDRAULIC SYS)

DECLARED AN EMERGENCY DUE TO HYDR 2 PRESSURE AND QUANTITY WENT TO ZERO. ALSO, HAD AILERON 2 AND RUDDER 2 FAIL IN FLIGHT. MX REMOVED AND REPLACED EDP 2 AND SERVICED HYD. OPS CHECKED MACH 2. (K)

Part: CONNECTOR — DIRTY (EMERGENCY LIGHTS)

GALLEY EMERGENCY LIGHTS INOPERATIVE. MX CLEANED THE CONNECTOR. OPS CHECKED GOOD. (K)

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

GALLEY EMERGENCY LIGHT INOP. MX REPLACED NR 2 EMERGENCY LIGHT BATTERY PACK ASSY, OPS CHECK GOOD. (K)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,678 hrs · 16,057 cycles

FDM RON MCO - COCKPIT EMERGENCY LIGHT INOP. MX RELAMPED, OPS GOOD.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 17,538 hrs · 15,914 cycles

FDM 6073 JFK-ORF (0855 PHX LCL). SERVICE DOOR EMERGENCY LIGHT OUT. MX RESEATED THE CONNECTOR AND OPS CHECKED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,511 hrs · 15,886 cycles

LEFT OUTBOARD SEAT TRACK AT FRAME 30 TO 36 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK (145-32606-003).

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 17,511 hrs · 15,886 cycles

BUTT STRAP AT Y=479 AND FRAME 61 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED BUTT STRAP.

Part: SKIN — DENTED (ESCAPE HATCH) · airframe 17,511 hrs · 15,886 cycles

PASSENGER CABIN ESCAPE HATCH SKIN DENT. REPAIRED DOOR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 17,511 hrs · 15,886 cycles

LEFT OUTBOARD SEAT TRACK AT FRAME 24 TO 30 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK.

Part: SILL — CORRODED (FUSELAGE) · airframe 17,511 hrs · 15,886 cycles

RIGHT OUTBOARD FLOOR SILL AT FRAME 29 TO 35 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED FLOOR SILL.

Part: RIB — CHAFED (LT COWLING) · airframe 17,511 hrs · 15,886 cycles

THE PREVIOUS REPAIR ON THE L/B UPPER RIB ON THE LT LOWER COWLING IS CHAFED. THE RIB HAS BEEN REMOVED AND REPLACED.

Part: SEAL — LEAKING (COCKPIT WINDOW) · airframe 17,498 hrs · 15,871 cycles

FDM 6031 - JFK- IAD (1638 PHX LCL) - LOUD NOISE FROM F/O'S SIDE WINDOW DURING DESCEND. MX RESECURED THE WINDOW SEAL AND LEAK CHECKED.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 17,405 hrs · 15,775 cycles

FDM 6185 MCO-PNS (1545 PHX LCL) EN ROUTE TO PNS AIRCRAFT DIVERTED TO TLH DUE TO BAG SMOKE WARNING IN EICAS IN FLIGHT. MX REMOVED AND REPLACED SMOKE DETECTOR, SMOKE DETECTOR RELAY, AND FAN RELAY.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 17,400 hrs · 15,771 cycles

FDM 6152 MCO-GSO (1558 PHX LCL) EN ROUTE TO GSO AIRCRAFT DIVERTED TO SAV DUE TO BAG SMOKE WARNING ON EICAS IN FLIGHT. NO EVIDENCE OF FIRE WAS FOUND AND MX REMOVED AND REPLACED SMOKE DETECTOR AND BOTTLES.

Part: CONNECTOR — LOOSE (CABIN) · airframe 17,379 hrs · 15,752 cycles

FDM 6198 JFK. GALLEY/SERVICE DOOR EMERGENCY EXIT LIGHT OUT. MX RESECURED LOOSE CONNECTOR, OPS GOOD.

Part: SWITCH — DIRTY (SPOILERS) · airframe 16,565 hrs · 15,761 cycles

FDM FLT 6042 JFK-ROC (0839 PHX LCL) - SPOILER FAIL CAUTION. MX CLEANED SWITCHES, OPS GOOD.

Part: CONNECTOR — CORRODED (EMERGENCY LIGHTS) · airframe 16,680 hrs · 15,099 cycles

FDM 6101 TLH (1240 PHX LCL) - EMERGENCY FLOOR PATH LIGHTING AT ROW 12 INOP. MX FOUND CORROSION AT CONNECTOR. CLEANED AND RE-SOLDERED.

Part: CONNECTOR — LOOSE (PROX SWITCH) · airframe 16,673 hrs · 15,291 cycles

FDM 9963 MCO - SPOILER FAIL EICAS MESSAGE. MX RESECURED SPOILER PROX SWITCH CONNECTOR AND APPLIED HEAT SHRINK.

Part: PROXIMITY SWITCH — UNKNOWN (SPOILERS) · airframe 1,664 hrs · 15,094 cycles

FDM RON MCO - SPOILER FAIL DURING TEST FLIGHT. MX RIGGED LT GROUND SPOILER AND INSTALLED PROX SWITCH AND RT OB SPEED BRAKE HANDLE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (SPOILERS) · airframe 16,672 hrs · 15,090 cycles

FDM RON MCO (1613 PHX LCL) - SPOILER FAIL MESSAGE IN FLIGHT. MX ADJUSTED INDICATION PROX SENSORS.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 16,664 hrs · 15,086 cycles

FRL RON TPA - SPOILER FAULT, SPOILER OPEN MESSAGE. REMOVED AND REPLACED SPOILER CONTROL UNIT.

Part: PROXIMITY SWITCH — DIRTY (SPOILERS) · airframe 16,675 hrs · 15,305 cycles

FDM 6018 PNS-TPA (1355 PHX LCL) - SPOILER FAIL CAUTION MESSAGE IN FLIGHT. MX CLEANED C/P ON PROX SW, PERFORMED OPS CHECK, OPS GOOD.

Part: CONTROL UNIT — FAULTED (SPOILERS) · airframe 16,675 hrs · 15,305 cycles

FDM 6171 TPA-PNS (1732 PHX LCL) - SPOILER FAIL CAUTION MESSAGE IN FLIGHT. MX REMOVED AND REPLACED THE SPOILER CONTROL UNIT.

Part: PROXIMITY SWITCH — DIRTY (SPOILERS) · airframe 16,671 hrs · 15,205 cycles

FDM RON JFK (1714 PHX LCL) - SPOILER FAIL CAUTION MESSAGE IN FLIGHT. MX CLEANED PROX SWITCHES, OPS CHECKED GOOD.

Part: PROXIMITY SWITCH — DIRTY (SPOILERS) · airframe 16,644 hrs · 15,064 cycles

FDM 6089 JFK (0620 PHX LCL) - SPOILER FAIL CAUTION MESSAGE IN FLIGHT. MX CLEANED PROX SWITCHES. OPS GOOD.

Part: PROXIMITY SWITCH — MALFUNCTIONED (SPOILERS) · airframe 16,631 hrs · 15,049 cycles

FDM 6041 JFK (1554 PHX LCL) - SPOILER FAIL CAUTION MESSAGE IN FLIGHT. MX REMOVED AND REPLACED LT O/B SPOILER PROX SWITCH.

Part: CONTROL UNIT — INOPERATIVE (PITCH TRIM) · airframe 16,509 hrs · 14,923 cycles

FDM FLT RON MCO - PITCH TRIM MAIN AND STANDBY SYSTEM INOPERATIVE. MX REPLACED THE HSCU AND OPS CHECKED.

Part: TRIM SYSTEM — INOPERATIVE (PITCH) · airframe 15,460 hrs · 14,639 cycles

FFDM FLT 6174 SYR - PITCH TRIM INOP. MX RESET SYSTEM WITH CREW. NO FURTHER ACTION REQUIRED. OPS GOOD.

Part: FRAME — CHAFED (RT NACELLE) · airframe 16,496 hrs · 14,906 cycles

RT LOWER ENGINE COWLING, THIRD FRAME FROM THE AFT END, IS CHAFED OUT OF LIMITS. REPAIRED THE DAMAGE.

Part: STRUCTURE — BENT (RT ELEVATOR) · airframe 16,496 hrs · 14,906 cycles

THE RT ELEVATOR HAD DAMAGE FROM CONTACT WITH THE HANGAR DOOR. REMOVED AND REPLACED ELEVATOR.

Part: PANEL — DAMAGED (NACELLE) · airframe 16,496 hrs · 14,906 cycles

PANEL 412CL HAS AN ELONGATED HOLE THAT IS BEYOND LIMITS. INSTALLED A DIMPLED WASHER OVER THE DAMAGE.

Part: FRAME — CHAFED (NACELLE) · airframe 16,496 hrs · 14,906 cycles

THE AFT FRAME ON THE LOWER ENGINE COWLING IS CHAFED OUT OF LIMITS. REMOVED AND REPLACED DAMAGED FRAME.

Part: CONTROLLER — ODOR (WINDSHIELD HEAT) · airframe 16,515 hrs · 14,861 cycles

FDM 6201 FLL-TLH (0528 PHX LCL) - DIVERT TO MCO DUE TO A STRONG ELECTRICAL BURNING ODOR WITH NO VISUAL SMOKE WHEN WINDSHIELD HEAT ON. MX INSPECTED WIRING FOR BURNED WIRES, NO DEFECTS FOUND. MX REMOVED AND REPLACED WINDSHIELD 2 HEAT CONTROLLER AND CONTACTOR, NO FURTHER ELECTRICAL ODOR.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 16,145 hrs · 14,581 cycles

FDM 6079 FLL-MCO (1658 PHX LCL). PITCH TRIM BACK UP SYSTEM INOPERATIVE. MX REMOVED AND REPLACED HSCU.

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 16,146 hrs · 14,582 cycles

FDM 9964 MCO-FLL (1005 PHX LCL). PITCH TRIM MAIN INOP MESSAGE. MX REMOVED AND REPLACED HSA.

Part: CONTROL UNIT — FAILED (HORIZ STAB) · airframe 16,138 hrs · 14,574 cycles

FDM 5984 FLL-MCO (0510 PHX LCL). PITCH TRIM FAIL IN FLIGHT. MX REMOVED AND REPLACED HSCU, OPS CHECK GOOD.

Part: CONNECTOR — LOOSE (CONTROLLER) · airframe 16,138 hrs · 14,573 cycles

FDM 5982 MCO-FLL (0510 PHX LCL). PITCH TRIM FAIL IN FLIGHT. MX RESET THE CONNECTOR ON HORIZONTAL CONTROL UNIT, OPS CHECK GOOD.

Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 15,494 hrs · 13,990 cycles

FDM 5969 AVL-ATL (0329 PHX LCL). AUTO PILOT AND YAW DAMP FAIL MESSAGES AT POWER UP. CYCLED AIRCRAFT POWER AND FAULT CLEARED.

Part: LIGHT — UNSECURE (CABIN) · airframe 14,951 hrs · 13,502 cycles

FDM 5975 TYS-MCO (0432 PHX LCL). CREW REPORTED THE EMERGENCY EXIT LIGHT INOP. MAINTENANCE SECURED THE LIGHT, OP'S GOOD.

Part: A/C PACK — ODOR (NR 1) · airframe 14,312 hrs · 12,947 cycles

FDM 6169 FLL. CREW DIVERTED TO TLH DUE TO HAVING A SMOKE ODOR IN THE COCKPIT. MX TROUBLESHOOT AND FOUND THE ODOR COMING FROM THE NR 1 PACK. MX REMOVED AND REPLACED DUCT NR 1 HEAT EXCHANGER.

Part: DAU — MALFUNCTIONED (NR 1) · airframe 14,199 hrs · 12,840 cycles

FDM 6076 ATL. CREW REPORTED SPOILER FAIL MESSAGE AFTER LANDING. MX REMOVED AND REPLACED DAU NR 1

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 14,197 hrs · 12,838 cycles

FDM 6068 ATL. CREW REPORTED SPOILER FAIL MESSAGE AFTER LANDING. MX RESET THE SYSTEM AND OPS CHECK NORMAL ON THE GROUND.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 14,198 hrs · 12,839 cycles

FDM 6081 HSV. CREW REPORTED SPOILER FAIL MESSAGE AFTER LANDING. MX RESET THE SYSTEM AND OPS CHECK NORMAL ON THE GROUND.

Part: WARNING MESSAGE — FALSE ACTIVATION (SPOILERS) · airframe 14,185 hrs · 12,832 cycles

FDM 6125 ATL. CREW REPORTED SPOILER FAIL MESSAGE. MAINTENANCE RESET THE SYSTEM AND OPS CHECK NORMAL.

Part: CONNECTOR — DIRTY (SPOILERS) · airframe 14,164 hrs · 12,809 cycles

FDM 6083 TRI. CREW REPORTED A SPOILER FAIL ON GROUND. MAINTENANCE SECURED AND CLEANED THE CONNECTOR.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 14,158 hrs · 12,803 cycles

FDM 6135 RDU. EMERGENCY EXIT LIGHT UNDER COCKPIT DOOR INOP. MX SECURED LIGHT.

Part: WARNING LIGHT — FALSE ACTIVATION (DAU 1) · airframe 14,151 hrs · 12,798 cycles

FDM 6058 CAE. THE CREW REPORTED A SPOILER FAIL ON EICAS. MAINTENANCE RE-RACKED THE DAU1.

Part: KNOB — LOOSE (AUTOPILOT PANEL) · airframe 13,821 hrs · 12,521 cycles

ASH 6078 MCO - THE CREW NOTED THE ALTITUDE SELECT KNOB LOOSE. MAINTENANCE REMOVED AND REPLACED AUTOPILOT PANEL.

Part: MODULE — MALFUNCTIONED (AILERON SYSTEM) · airframe 13,732 hrs · 12,452 cycles

FDM RDU, THE CREW REPORTED THAT THE AILERON 2 SYSTEM WILL NOT SHUT OFF. MAINTENANCE REPLACED THE MODULE PANEL AND OPS CHECKED.

Part: MANIFOLD — DEFECTIVE (AILERON) · airframe 13,676 hrs · 12,607 cycles

THE CREW REPORTED THE AILERON SYSTEM 2 DOES NOT SHUT OFF WITH HYDRAULICS ON DURING THE TEST. MAINTENANCE REPLACED NR 2 MANIFOLD ASSEMBLY AND OPS CHECKED.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 13,677 hrs · 12,605 cycles

THE CREW REPORTED A SPOILER FAIL MESSAGE ON LANDING. OPS CHECKED GOOD.

Part: CONTROL HANDLE — MALFUNCTIONED (SPEED BRAKE) · airframe 13,552 hrs · 12,302 cycles

SPOILER FAULT MESSAGE ON LANDING AND DURING DESCENT. MX REPLACED SPEED BRAKE CONTROL HANDLE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 13,538 hrs · 12,294 cycles

THE CREW NOTED A SPOILER FAIL IN FLIGHT MESSAGE. MAINTENANCE COULD NOT DUPLICATE. OP'S CHECK GOOD.

Part: CONTROL UNIT — FAULTY (SPOILER) · airframe 13,528 hrs · 12,287 cycles

THE CREW REPORTED A SPOILER FAIL MESSAGE WHEN AIRBORNE AND ON GROUND. MAINTENANCE REMOVED AND REPLACED THE SPOILER CONTROL UNIT.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 13,428 hrs · 12,218 cycles

CREW ABORTED TAKEOFF AND REPORTED AN SPS ADVANCE MESSAGE. MAINTENANCE RERACKED THE SPS COMPUTER AND RAN A GOOD SYSTEM CHECK.

Part: GROUNDING STRAP — BROKEN (PAX DOOR) · airframe 13,302 hrs · 12,127 cycles

THE CREW NOTED THAT THE MAIN CABIN DOOR GROUNDING STRAP IS BROKEN. MAINTENANCE SECURED THE STRAP.

Part: SEAL — MISSING (FIRE BOTTLE) · airframe 12,055 hrs · 11,273 cycles

THE CREW REPORTED FWD CABIN FIRE EXTINGUISHER SEAL MISSING. MAINTENANCE REPLACED THE FIRE EXTINGUISHER.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 12,047 hrs · 11,265 cycles

FRL 9430 CAE-MCO. THE CREW REPORTED A FWD EMERGENCY EXIT LIGHT INOP. OPS CHECKED GOOD.

Part: ESCAPE ROPE — UNSECURE (COCKPIT)

(REF NR F05004) THE CREW HAD A F/O EMERGENCY ESCAPE ROPE THAT WAS NOT SECURE IN ITS CONTAINER. MAINTENANCE SECURED ESCAPE ROPE. (K)

Part: PUMP — LEAKING (APU) · airframe 12,047 hrs · 11,265 cycles

THE CREW NOTED A STRONG ODOR OF FUEL IN THE CABIN. MAINTENANCE HAS TROUBLESHOT FAULT TO LEAKING PACKINGS AT THE APU ACCELERATION UNIT. MAINTENANCE REMOVED AND REPLACED APU FUEL PUMP.

Part: PUMP — LEAKING (APU FUEL)

(REF NR F05005)THE CREW NOTED A STRONG ODOR OF FUEL IN THE CABIN (ACTUAL). MAINTENANCE HAS TROUBLESHOT FAULT TO LEAKING PACKINGS AT THE APR ACCELLERATION UNIT. MAINTENANCE REMOVED AND REPLACED APU FUEL PUMP. (K)

Part: ODOR — DETECTED (GALLEY)

(REF NR F05002) THE CREW REPORTED A SMOKE LIKE SMELL IN GALLEY DURING FLIGHT. MAINTENANCE PERFORMED A GVI TO GALLEY AREA AND WIRING. MAINTENANCE CHANGED TRASH OUT AND CLEANED COFFEE POTS. NO SMOKE SMELL DETECTED. (K)

Part: ESCAPE ROPE — UNSECURE (COCKPIT) · airframe 12,047 hrs · 11,265 cycles

THE CREW HAD A F/O EMERGENCY ESCAPE ROPE THAT WAS NOT SECURE IN ITS CONTAINER. MAINTENANCE SECURED ESCAPE ROPE.

Part: ODOR — DETECTED (GALLEY) · airframe 12,047 hrs · 11,265 cycles

THE CREW REPORTED A SMOKE LIKE SMELL IN GALLEY DURING FLIGHT. MAINTENANCE PERFORMED A GVI TO GALLEY AREA AND WIRING. MAINTENANCE CHANGED TRASH OUT AND CLEANED COFFEE POTS. NO SMOKE SMELL DETECTED.

Part: LAMP — INOPERATIVE (RT EXT OVERWING) · airframe 111,778 hrs · 10,973 cycles

THE AIRCRAFT WAS ON R.O.N. LAST NIGHT AND SCHEDULED FOR A ROUTINE CHECK INSPECTION. DURING THE WALK AROUND IT WAS DISCOVERED THE RT EXTERNAL OVERWING EMERGENCY LIGHT NOT ILLUMINATING. REPLACED THE LIGHT BULB. OPERATIONAL CHECK GOOD.

Part: LIGHT — MALFUNCTIONED (ROW 12) · airframe 11,424 hrs · 10,571 cycles

ROW 12 EMERGENCY EXIT LIGHT INOPERATIVE. MX REPLACED LIGHT ASSEMBLY.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 11,111 hrs · 10,220 cycles

IN CHECK, FLOOR RISER AT RT CORRODED FR 23. REMOVED RT OUTBOARD CLIP ON RISER OUT OF LIMIT. FAB NEW PER SAMPLE AND INSTALLED.

Part: SEAT TRACK — CORRODED (FUSLEAGE) · airframe 11,111 hrs · 10,220 cycles

IN C-CHECK, SEAT TRACK AT LT Y479 CORRODED FROM FR 18 TO FR 24, OUT OF LIMITS REF SRM 53-00-11. REPLACED TRACK.

Part: BUTTSTRAP — CORRODED (FLOOR SUPPORT) · airframe 11,111 hrs · 10,220 cycles

IN C-CHECK, BUTT STRAP CORRODED AT LT Y4790 FROM FR 18 TO FR 24 OUT OF LIMITS REF SRM 53-21-10. REPLACED BUTT STRAP.

Part: SKIN — DENTED (FUSELAGE) · airframe 11,111 hrs · 10,220 cycles

IN C-CHECK, PERFORM PERMANENT REPAIR ON SKIN FORWARD OF APU DOOR DUE 1034 FC SHARP DENT REPAIRED, EXTERNAL REPAIR DOUBLER REF SRM 53-32-01.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 10,811 hrs · 9,894 cycles

AN AFT EMERGENCY CEILING LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LAMP, OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 10,096 hrs · 9,114 cycles

ASH 2646 DCA-CAE, 3RD CEILING EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED THE LIGHT, OPS CHECKED GOOD. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 9,955 hrs · 8,982 cycles

DURING PREFLIGHT NOTICED EMERGENCY LIGHTING AT THE OVERWING EXITS WERE INOP. MAINTENANCE WAS NOTIFIED AND RELAMPED THE LIGHTS AS NEEDED. AIRCRAFT CONTINUED OPERATIONS.

Part: LIGHT — BURNED OUT (ROW 8 & 9) · airframe 9,228 hrs · 8,320 cycles

AIRCRAFT WAS ON RON AND SCHEDULED FOR A 2 DAY EN ROUTE INSPECTION. DURING THE WALK-AROUND DISCOVERED THAT ROW 8 & 9 EMERGENCY LIGHT STRIP INOP. MAINTENANCE REPLACED THE LIGHT STRIP AND OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT) · airframe 9,210 hrs · 8,299 cycles

LEFT OVERWING EMERGENCY EXIT INDENTIFER SIGN INOP. RESET LIGHTING SYSTEM AND OPS CHECKED GOOD. NO PARTS USED.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 9,142 hrs · 8,233 cycles

THE LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. MX COULD NOT DUPLICATE THE DISCREPANCY. A/C DEPARTED WITHOUT FURTHER DISCREPANCY. NO PARTS USED.

Part: CLAMP — LOOSE (BLEED SYSTEM) · airframe 8,324 hrs · 7,524 cycles

AIRCRAFT DIVERTED TO PIT FOR AN E-2 BLEED LEAK MSG. MX WAS CALLED AND TIGHTENED A LOOSE CLAMP. OP CHECKS GOOD. NO PARTS USED.

Part: LIGHT — INOPERATIVE (ROW 12) · airframe 8,226 hrs · 7,435 cycles

ASH 2807 CLT-SDF, CEILING EMERGENCY EXIT LIGHT INOP AT ROW 12. WHEN MX ARRIVED THE LIGHT WAS OPERATING NORMALLY. NO PARTS USED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,654 hrs · 6,940 cycles

CLT-HSV AN EMERGENCY EXIT LIGHT AT ROW 12R INOP. MX RELAMPED, OP CHECKS GOOD.

Part: CHARGER — INOPERATIVE (CABIN)

PREFLIGHT, ROW 12 EMERGENCY EXIT LIGHTS INOPERATIVE ON LEFT AND RIGHT OVERHEAD. MAINTENANCE REPLACED THE BATTERY CHARGER ASSEMBLY. (M)

Part: CONNECTOR — LOOSE (STALL WARNING)

FLT 5717 - IN GSP, ABORTED TAKEOFF ROLL DUE TO SPS 1 AND 2 INOPERATIVE AND STICK SHAKER FAIL MESSAGE. MAINTENANCE RESEATED CONNECTOR PLUG TO STICK SHAKER AND REMOVED AND REINSTALLED SPSP COMPUTER. MESSAGE CLEARED. SYSTEM OP CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: GENERATOR — MALFUNCTIONED (NR 1 ENGINE)

FLT 5892 - PRIOR TO TAKEOFF THE CAPTAIN STARTED THE TAKEOFF ROLL WHEN A CHIME WAS HEARD. THE CAPTAIN NOTICED THE NR 3 GENERATOR OFF BUS MSG. CAPTAIN ABORTED TAKEOFF AT 40 KIAS AND EXITED THE RUNWAY ONTO THE TAXIWAY. THE CAPTAIN RESET THE GENERATOR. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LENS — CRACKED (CABIN)

FLT 5873 - THE CREW HAD FOUND THE FORWARD EMERGENCY OVERHEAD LIGHT LENS CRACKED. MAINTENANCE REPLACED THE LENS AND OPS CHECKS GOOD. (M)

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

FLT 5752 - IN FLIGHT, THE CREW RECEIVED A LAVATORY SMOKE DETECTOR MESSAGE ON THE EICAS. THE AIRCRAFT RETURNED TO THE FIELD AND UPON LANDING THE INDICATION CLEARED. THE FIRE DEPARTMENT INSPECTED THE LAVATORY AND FOUND NO PROBLEMS. THE SMOKE DETECTOR WAS RETESTED AND FOUND TO BE IN WORKING ORDER. NO FURTHER ACTION WAS TAKEN. (M)

Part: FABRIC — INOPERATIVE (RT RR EM FLD LT)

DURING A PREFLIGHT INSPECTION, THE CREW FOUND THE RIGHT AFT FUSELAGE EXTERNAL EMERGENCY FLOOD LIGHT INOPERATIVE. THIS ITEM WAS DEFERRED PER MEL. LATER MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOD LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR)

FLT 5875 - DCA-SDF - DURING PREFLIGHT, THE CAPTAIN REPORTED EXIT LIGHT AFT FUSELAGE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BULB. OPS CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (CABIN) · airframe 597 hrs · 457 cycles

DCA/ATL - FLT 5865 - REPORTED THE EMERGENCY LIGHTING SWITCH HAD BEEN LEFT IN THE ARM POSITION OVERNIGHT AND THE BATTERY PACKS DEPLEATED. BATTERIES WERE RECHARGED. OP CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (X)