N434YV

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,464 hrs · 36,155 cycles

ROW 3 CEILING EMERGENCY LIGHT INOP, CEILING EMERGENCY LIGHT INOP ROW 7, EXIT SIGN ON EXITS, AND OVERHEAD EXIT BY PAX DOOR INOP. REMOVED AND REPLACED ALL 6 EMERGENCY BATTERY PACKS.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 35,384 hrs · 36,067 cycles

FWD/MID CABIN & LT AFT EGRESS LIGHTS INOP. R2 POWER SUPPLY 3352-RS3.

Part: HANDSET — FAULTY (CABIN) · airframe 35,065 hrs · 35,698 cycles

F/A HANDSET STATIC INTERCOMM AND PA. R2 F/A HANDSET AND PA AMPLIFIER.

Part: BATTERY — DISCHARGED (CABIN) · airframe 35,022 hrs · 35,652 cycles

AFT CEILING E-LIGHT OUT. R2 NR 6 -LIGHT BATTERY.

Part: WINDOW — CRACKED (CABIN) · airframe 34,920 hrs · 35,536 cycles

PAX WINDOW 3F CRACKED. R2 PAX WINDOW LEAK CHECK GOOD.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 34,920 hrs · 35,536 cycles

RIGHT AFT EMERGENCY LIGHT INOP. R2 E-LIGHT POWER SUPPLY.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 34,902 hrs · 35,513 cycles

F/A FLASHLIGHT INOP. R2 FLASHLIGHT.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 34,915 hrs · 35,532 cycles

FD FLASHLIGHT INOP. RELAMPED FLASHLIGHT.

Part: SOCKET — DIRTY (EXTERIOR) · airframe 34,879 hrs · 35,483 cycles

RT AFT EXTERIOR E-LIGHT INOP. CLEANED AND RELAMPED LIGHT SOCKET.

Part: SIGN — BROKEN (CABIN) · airframe 34,844 hrs · 35,446 cycles

PAX DOOR EMERGENCY EXIT SIGN CORNER BROKEN. R2 PAX DOOR EMERGENCY EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,844 hrs · 35,446 cycles

EMERGENCY FLOOR TRACK LIGHT X252.30 BROKEN. R2 EMERGENCY TRACK LIGHT.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 34,737 hrs · 35,326 cycles

NR 1 E-LIGHT BATTERY FAILED FUNCTION TEST. R2 NR 1 E-LIGHT POWER SUPPLY.

Part: STEP — SEPARATED (PAX DOOR) · airframe 34,704 hrs · 35,291 cycles

PAX DOOR STEP SEPARATING FROM DOOR. R2 PAX DOOR STEP ASSY.

Part: REGULATOR VALVE — MALFUNCTIONED (NR 2 ENGINE) · airframe 34,463 hrs · 35,027 cycles

NR 2 ENGINE OIL TEMP 110 FOR WHOLE FLIGHT. R2 TEMP REGULATING VALVE AT THE OIL COOLER.

Part: TRANSDUCER — MALFUNCTIONED (NR 1 LIFT) · airframe 34,337 hrs · 34,881 cycles

LEFT STALL WARNING IN FLIGHT. R & R NR 1 LIFT TRANSDUCER.

Part: WIRE — BROKEN (CABIN) · airframe 34,210 hrs · 34,756 cycles

AIRSTAIR LIGHTS INOP. REPAIRED BROKEN WIRE AT DOOR HINGE.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 34,229 hrs · 34,773 cycles

F/A EMERG LIGHT TEST SWITCH INOP. NO DEFECTS NOTED.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 34,210 hrs · 34,756 cycles

F/A EMERGENCY LIGHT TEST SWITCH INOP. NO DEFECTS NOTED.

Part: BRAKE — LEAKING (MLG) · airframe 34,147 hrs · 34,692 cycles

NR 2 BRAKE LEAKING. R2 NR 3 BRAKE. NUMBER 3 BRAKE WAS LEAKING NOT 2.

Part: SELCAL — ODOR (CABIN) · airframe 34,113 hrs · 34,654 cycles

ELECRICAL ODOR FROM WARDROBE CLOSET. MX FOUND THE SALCAL BO SMELLING AND COLLARED CIRUIT BREAKER AS PART OF THE MEL PROCEDURES P/N 2800-0015-105 ON REQ. R&R SELCAL DECODER.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 34,114 hrs · 34,653 cycles

ACRID SMELL IN COCKPIT & FWD CABIN. INSP ACFT, INSIDE CKPIT & FWD CABIN, NO ACRID SMELL NOTED.

Part: BRAKE ASSY — LEAKING (NR 4) · airframe 33,759 hrs · 34,318 cycles

HYD FLUID LEAKING FROM NR 4 BRAKE. MX R2 NR 4 BRAKE ASSY.

Part: BRAKE — LEAKING (MLG) · airframe 33,612 hrs · 34,178 cycles

NR 1 MLG BRAKE LEAKING. MX REMOVED AND REPLACED NR 1 BRAKE OPS & LEAK CHECK GOOD.

Part: BRAKE ASSY — LEAKING (MLG) · airframe 33,562 hrs · 34,126 cycles

RIGHT I/B BRAKE LEAKING. MX R2 BRAKE ASSY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,523 hrs · 34,090 cycles

FLOOR LIGHT AT RT EMERGENCY EXIT INOP. MX RELAMPED EMERGENCY LIGHT.

Part: BRAKE — LEAKING (NR 4) · airframe 33,421 hrs · 33,996 cycles

NR 4 MLG BRAKE LEAKING. MX REMOVED AND REPLACED NR 4 BRAKE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,313 hrs · 33,889 cycles

RT FWD EGRESS LIGHT DIM. MX REMOVED AND REPLACED NR 2 E-LIGHT BATTERY, OPS GOOD.

Part: STRUT — CRACKED (PAX DOOR) · airframe 33,313 hrs · 33,889 cycles

AFT UPPER PAX DOOR STRUT CRACKED. MX REMOVED AND REPLACED SUPPORT ROD UPPER STRUT ASSY.

Part: BRAKE ASSY — LEAKING (RT MLG) · airframe 33,251 hrs · 33,831 cycles

FLUID LEAK RT MLG. MX R2 BRAKE NR 3.

Part: LIGHT — INOPERATIVE (DOOR STEP) · airframe 33,244 hrs · 33,825 cycles

PAX DOOR STEP LIGHT INOP. MX RELAMPED PAX DOOR STEP LIGHT.

Part: FUEL NOZZLE — LEAKING (NR 2 ENGINE) · airframe 33,086 hrs · 33,670 cycles

FUEL LEAKING FWD RIGHT ENGINE. MX REMOVED AND REPLACED E2 FUEL NOZZLES AND FLOW DIVIDER.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 32,874 hrs · 33,464 cycles

PAX DOOR EXIT SIGN FELL OFF. MX SECURED EXIT SIGN.

Part: PCU — FAULTY (NR 2 PROPELLER) · airframe 32,888 hrs · 33,478 cycles

NR 2 PROP GOES TO 1140 RPM ON FINAL. R2 PCU & ECU, OP GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 32,849 hrs · 33,430 cycles

GALLEY EXIT LIGHT AND FORWARD ESCAPE LIGHT INOP. MX CHARGED BATTERY PACK.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY) · airframe 32,841 hrs · 33,426 cycles

LAV SMOKE DETECTOR ON CONTINUOUSLY IN FLT. MX REPLACED SMOKE DETECTOR.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 32,784 hrs · 33,396 cycles

CENTERA ISLE EXIT SIGN WILL NOT ILLUMINATE. MX R2 EMERGENCY LIGHT POWER SUPPLY, OP GOOD.

Part: ACM — FAULTY (AC BAY) · airframe 32,128 hrs · 32,688 cycles

SMOKE IN CABIN AND COCKPIT FROM PACK. MX REMOVED AND REPLACED ACM, OPS CHECK GOOD.

Part: OIL COOLER — LEAKING (NR 1 ENGINE) · airframe 31,227 hrs · 31,769 cycles

ASH FLT 7107 DEN-CPR - ACFT DIVERTED DUE TO LOSS OF OIL PRESSURE IN NR 1 ENGINE. SHUT ENGINE DOWN AND DECLARED EMERGENCY. MX DETERMINED THAT THE OIL COOLER WAS LEAKING. REMOVED AND REPLACED NR 1 ENG OIL COOLER, OPS/LEAK CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 30,774 hrs · 31,250 cycles

ASH FLT 7299 RAP-DEN. DIVERT, DECLARED EMERGENCY TO BFF DUE TO CAPTAIN WINDSHIELD SHATTERED IN FLIGHT. MX REMOVED AND REPLACED CAPTAIN WINDSHIELD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,341 hrs · 30,738 cycles

ASH 7143 DEN-GJT. CAPTAIN REPORTED THE F/A'S EMERGENCY LIGHT WAS INOP. MX REPLACED THE BULB.

Part: SENSOR — DIRTY (MLG) · airframe 27,692 hrs · 27,755 cycles

ASH FLT 7100 DEN-MTJ - CREW REPORTED A WOW CAUTION LIGHT ILLUMINATED AFTER GEAR EXTENSION AND EXTINGUISHED UPON TOUCHDOWN. CLEANED AND INSPECTED RT WOW OB SENSOR, CHECK GOOD.

Part: LIGHT — NO TEST (CABIN) · airframe 27,228 hrs · 27,221 cycles

ASH FLT 7351 DEN-RAP - EMERGENCY LIGHTS WILL NOT TEST FROM FA PANEL. MX PERFORMED, OPS CHECK OF SYSTEM. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: RELAY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 6,896 hrs · 26,849 cycles

ASH INBD FLT 7374 DEN - PILOT REPORTED THAT IN START FEATHER, EMERGENCY LIGHTS DISARM CAUTION NOT ILLUMATED WHEN EMERGENCY LIGHTS IN OFF POSITION. REMOVED AND REPLACED UNDER VOLTAGE RELAY 2431K20.

Part: BLEED VALVE — MALFUNCTIONED (NR 1 ENGINE) · airframe 26,032 hrs · 25,822 cycles

ASH 7086 DEN. SMOKE IN COCKPIT AFTER NR 1 ENGINE START. MX REMOVED AND REPLACED NR 1 IBV AND P2.5 AND 3 AIR SWITCHING VALVE OPS CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 25,877 hrs · 25,632 cycles

ASH FLT 7064 GJT - EMERGENCY LIGHTS WILL NOT TEST FROM FLIGHT ATTENDANT STATION. MX REPAIRED BROKEN WIRE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,922 hrs · 29,419 cycles

ASH 7034 DEN. CREW RETURNED TO THE GATE DUE TO ONE EMERGENCY EXIT FLOOR PATCH LIGHT INOP. MX PLACED ON MEL.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,676 hrs · 24,203 cycles

ASH DEN. ALL EXTERIOR EMERGENCY LIGHTS INOP. MX REPLACED THE BATTERY AND POWER SUPPLY.

Part: DISPLAY — INOPERATIVE (CENTER CONSOLE) · airframe 23,520 hrs · 22,792 cycles

PILOT ABORTED ENGINE START DUE TO A BLANK OFF PANEL THAT FELL OFF INTO THE CENTER CONSOLE AREA. MX LOCATED THE PANEL AND REINSTALLED.

Part: ACTUATOR — MALFUNCTIONED (AILERONS) · airframe 23,057 hrs · 22,253 cycles

ASH 7072 DRO, CAPTAIN REPORTED AILERON TRIM WILL NOT MOVE. MAINTENANCE REMOVED AND REPLACED AILERON TRIM ACTUATOR.

Part: MOTOR — INTERMITTENT (AILERON TRIM) · airframe 23,036 hrs · 22,232 cycles

ASH 7084 DEN - AILERON TRIM MOTOR WORKS INTERMITTENT. MX PERFORMED OP'S CHECK, OP'S CHECK GOOD.

Part: ACTUATOR — OUT OF ADJUST (AILERONS) · airframe 23,006 hrs · 22,196 cycles

ASH 7056 COD, AILERON TRIM STUCK IN FULL LT POSITION. MAINTENANCE R&R POTENTIOMETER AND ADJUSTED ACTUATOR.

Part: CONTROL PANEL — MALFUNCTIONED (AILERON TRIM) · airframe 22,992 hrs · 22,179 cycles

ASH 7073 DEN, AILERON TRIM INOP. MX R2 CONTROL PANEL.

Part: TRIM SYSTEM — STUCK (AILERONS) · airframe 22,976 hrs · 22,158 cycles

ASH 7050 EGE - AILERON TRIM STUCK IN FULL LT POSITION. MAINTENANCE COULD NOT DUPLICATE. OPS CHECKED GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY EXIT) · airframe 21,094 hrs · 18,946 cycles

ASH 6211 PHX-FLG, THE EMERGENCY EXIT SIGN ABOVE THE MAIN CABIN DOOR WILL NOT ILLUMINATE. MX REPOSITIONED LIGHT ASSEMBLY SOCKET AND SYSTEM CHECKED NORMALLY.

Part: DISPLAY — CONTAMINATED (WX RADAR)

FLT 6207 - RETURNED TO FIELD BECAUSE WEATHER RADAR DISPLAY WENT BLANK AND WOULD NOT RESET. MAINTENANCE FOUND WATER IN SEPARATOR. CLEANED AND REPLACED DESICANTOR. OP CHECKS GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (EXTERIOR)

FLT 6200 - FLG-PHX - THE CREW FOUND A LEFT EXTERIOR FUSELAGE AFT EMERGENCY EGRESS LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT AND OPS CHECKED GOOD. (M)

Part: SWITCH — INOPERATIVE

FLT 6327 - GJT-PHX - THE EMERGENCY EXIT LIGHTS WOULD NOT TURN OFF. MAINTENANCE TROUBLESHOT AND REPLACED THE F/A'S SWITCH. OPS CHECK GOOD. THE AIRPLANE WAS RETURNED TO SERVICE. (M)

Part: GUST LOCK — LOOSE (ELEVATOR)

DURING ROUTINE MAINTENANCE, THE ELEVATOR GUST LOCK PLATES WERE FOUND TO HAVE LOOSE AND SMOKING JO-BOLTS. A REPAIR WAS COMPLIED WITH IAW RO DHC82-55-0004GJT (DEHAVILLAND RD 8-55-112). OP CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING ROUTINE MAINTENANCE, LT FORWARD FUSELAGE EMERGENCY LIGHT FAILED TO ILLUMINATE. REMOVED AND REPLACED POWER SUPPLY. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — INOPERATIVE (CABIN)

FLT 6321 - GJT-PHX - REPORTED DURING PRE-FLIGHT THAT EMERGENCY POWER LIGHTS WERE INOPERATIVE. THE BATTERIES WERE REPLACED. SYSTEM OP CHECKED GOOD. AIRRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

SBP/PHX - FLT 6550 - THE CAPTAIN FOUND THE EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS FERRIED TO PHX. MAINTENANCE REPLACED ALL BATTERY PACKS FOR THE LIGHTS. OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (X)

Part: BULB — FAILED (CABIN)

WHILE PERFORMING ROUTINE MAINTENANCE INSPECTION, FOUND THE F/A'S EMERGENCY LIGHT SWITCH FAILED TO ILLUMINATE IN THE NORMAL POSITION. REMOVED AND REPLACED THE BULBS, OPS CHECK GOOD. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 6282 - PHX-ASE - PRIOR TO DEPARTURE, THE CAPTAIN REPORTED THE CEILING EMERGENCY LIGHTS NR 2 AND NR 4 WOULD NOT ILLUMINATE. MAINTENANCE RESET THE COCKPIT EMERGENCY LIGHT SWITCH. NO FURTHER DISCREPANCIES WERE NOTED. SYSTEM OPERATED NORMAL. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

FLT 7565 - GCC-DEN - CREW REPORTED TWO RED AND THREE WHITE EMERGENCY FLOOR TRACK LIGHTS INOP. MAINTENANCE RESECURED THE LIGHT STRIP, OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVIEC. (M)

Part: BULB — FAILED (CABIN)

DURING ROUTINE MAINTENANCE, FOUND ONE RED EMERGENCY ESCAPE PATH LIGHT INOP. REPLACED LAMP, OPS CHECK GOOD. (M)

Part: BULB — FAILED (CABIN)

DURING ROUTINE LINE CHECK INSPECTION, THE F/A EMERGENCY LIGHT SWITCH WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE SWITCH BULB. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

DURING ROUTINE LINE INSPECTION, THE NR 2 OVERHEAD EMERGENCY LIGHT WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE BULB, AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LAMP — FAILED (CABIN)

ON INTERIOR LIGHT OPS CHECK, FOUND THE FARTHEST AFT CEILING EMERGENCY EXIT LIGHT WOULD NOT ILLUMINATED. MAINTENANCE FOUND A BLOWN LIGHT BULB. REMOVED AND REPLACED BULB AND OPS CHECK GOOD. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

FLT 7722 - DEN-HDN - PILOT WAS DOING TEST ON EMERGENCY LIGHTS WHEN HE FOUND THREE EXTERNAL LIGHTS THAT WERE INOP. MAINTENANCE CHANGED TWO EMERGENCY BATTERY PACKS. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: AIR DISTRIBUTION — SMOKE (CABIN)

FLT 7537 - DRO-DEN - CRWE REPORTED, THAT IN FLIGHT WITH LEFT BLEED AIR ON HAD SMOKE IN COCKPIT. AIRCRAFT WAS INSPECTED AND RUNUP WAS PERFORMED IN DEN. NO DISCREPANCIES WERE NOTED AND THE PROBLEM COULD NOT BE DUPLICATED. DE-ICE FLUID WAS SUSPECTED TO HAVE CAUSED THE PROBLEM. AIRCRAFT WAS RETURNED TO SERVICE (M)

Part: CONNECTOR — LOOSE (CABIN)

DURING ROUTINE LINE CHECK INSPECTION, THE FORWARD 6 INCH EXIT LIGHT STRIP DID NOT ILLUMINATE DURING OPS CHECK OF THE EMERGENCY LIGHT SYSTEM. MAINTENANCE FOUND THE 6 INCH SECTION TO HAVE A BAD CONNECTION AT THE PLUG. THE PLUG WAS REPAIRED WITH NO OTHER FAULTS FOUND. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY — DISCHARGED (E/E COMPT)

DEN/COD - FLT 7708 - DURING CLIMB-OUT, MAIN BATTERY TEMPERATURE INCREASED RAPIDLY. THE CREW TURNED THE BATTERY OFF PER THE QRH. TEMPERATURE CONTINUED TO INCREASE ABOVE RED LINE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO LAR. MAINTENANCE REMOVED AND REPLACED THE MAIN BATTERY, OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (X)

Part: BULB — FAILED (CABIN)

DURING NIGHT MAINTENANCE, TEN BULBS IN THE EMERGENCY EXIT LIGHT ASSY ABOVE THE CABIN ENTRY DOOR WOULD NOT ILLUMINATE DURING TEST. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE BULBS, OPS CHECK GOOD AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — DENTED (BS 580-618)

DEN/FJT - FLT 7568 - AFTER ARRIVING IN GJT, THE AIRCRAFT WAS STRUCK BY A BAGGAGE CART. AIRCRAFT RECEIVED DAMAGE BETWEEN STA X580.5 AND STA 618.0 ALONG STR 29P AND STR 30P. THE AIRCRAFT WAS REPAIRED IAW FAA 337 AND DEHAVILLAND RD 8-53-2949 DATED 7-26-97. AIRCRAFT WAS THEN RETURNED TO SERVICE. (X)

Part: PITCH LEVER — LOOSE BOLTS (LT/RT ELEVATOR)

DURING NIGHT MAINTENANCE, UPON COMPLETION OF FOD 97-14, INSPECTED THE LEFT AND RIGHT ELEVATOR OUTPUT LEVER BOLT TORQUE. FOUND 3 LOOSE BOLTS ON THE CAPTAINS SIDE AND 2 LOOSE BOLTS WERE FOUND ON CO-PILOTS SIDE. ALL BOLTS WERE TORQUED IAW DASH 8 200 MM 27-32-41. (M)