N14570

Part: CONTROL UNIT — INTERMITTENT (SPOILERS) · airframe 36,995 hrs · 30,126 cycles

PILOT REPORTED SPEED BRAKES DEPLOYED IN FLIGHT, NEG/DOWN TRIM EXPERIENCED WITH AUTO PILOT DISCONNECTED-TRIM UNCOMMANDED. MX AS PER ENGINEERING REMOVED AND REPLACED SPOILER CONTROL UNIT WITH OPERATIONAL CHECK GOOD. FAULT NO DUPLICATED. A/C WAS APPROVED FOR RETURN TO SERVICE.

Part: TUBE — BROKEN (NR 2 ENGINE OIL) · airframe 41,662 hrs · 25,400 cycles

ENGINE 2 SHUTDOWN IN FLIGHT, STARTING DECENT DUE TO E2 LOW OIL PRESSURE EICAS MSG. R&R #2 ENGINE AFT TUBE OIL LINE FROM OIL FILTER TO OUTER BYPASS. OPS & LEAK CHECK GOOD.

Part: REINFORCEMENT — LEAKING (RT WING) · airframe 35,196 hrs · 28,660 cycles

IAH - MAINTENANCE REMOVED AND REPLACED A REINFORCEMENT PLATE ON THE RIGHT WING SKIN PANEL 5 DUE TO A FUEL LEAK. LEAK CHECKS WERE PERFORMED SATISFACTORILY AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: TORQUE BOX — GOUGED (RT WING) · airframe 27,451 hrs · 33,668 cycles

RIGHT HAND WING TORQUE BOX BOLT HOLE INBOARD LOWER (1 POSITION) GOUGED.

Part: COFFEEMAKER — DEFECTIVE (GALLEY) · airframe 31,244 hrs · 25,508 cycles

THE CREW REPORTED AN ELECTRICAL BURNING ODOR FROM THE LT COFFEE POT. THE ACFT LANDED WITHOUT INCIDENT WHERE MAINTENANCE R & R THE LT COFFEE BREWER, OPS TESTED WITH NO DEFECTS NOTED, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,097 hrs · 24,596 cycles

DURING ROUTINE MAINTENANCE THE NR 3 EMERGENCY FLOOR PROXIMITY LIGHT STRIP WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 3 EMERGENCY FLOOR LIGHT STRIP. OPS CHECKS WERE GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,195 hrs · 19,111 cycles

DURING SCHEDULED MX INSPECTION THE RT AFT EXTERIOR OVERWING EMERGENCY LIGHT WAS FOUND INOPERATIVE. MX RELAMPED THE RT AFT EMERGENCY LIGHT WITH OPS CHECK SUCCESSFUL. ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FLOOR SUPPORT — CORRODED (CABIN) · corrosion level 2 · airframe 18,510 hrs · 15,391 cycles

SHV - DURING C-CHECK THE CENTER OMEGA BEAM AT FRAME 59 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW EC5310-01473.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,510 hrs · 15,391 cycles

SHV - SHEAR CLIP AT FRAME 68 AND STRINGERS 16L TO 17L CORRODED AT CARGO DOOR CUTOUT LOWER AFT CORNER. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW EC5320-01494. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,510 hrs · 15,391 cycles

SHV - DURING C-CHECK THE SHEAR CLIP AT THE CARGO DOOR CUTOUT FORWARD LOWER CORNER WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A SPLICE REPAIR IAW EC5320-01494. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: PITOT SYSTEM — CONTAMINATED (PITOT/STATIC SYS) · airframe 18,278 hrs · 15,172 cycles

FLIGHT 6040 - BUF - FLIGHT CREW REPORTED IAS MISCOMPARE ON EICAS. CREW DIVERTED FLIGHT AND LANDED UNEVENTFULLY. MX DRAINED BOTH PITOT SYSTEMS AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 17,726 hrs · 14,688 cycles

ORD FLT 6008 THE CREW REPORTED A LOUD "CLUNK" NOISE WHEN RETRACTING AND EXTENDING THE GEAR. MAINTENANCE INSPECTED AND REPLACED THE EXTEND/RETRACT SOLENOID. THE NOISE CAME BACK ON FLT 5809. MAINTENANCE INSPECTED AND REPLACED THE NOSE LANDING GEAR DOWNLOCK HARNESS (A) W017. OPERATIONAL CHECKS WERE GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,544 hrs · 14,535 cycles

DURING ROUTINE MAINTENANCE THE AISLE PATH EMERGENCY LIGHT STRIP WAS FOUND INOPERATIVE.2ND STRIP FROM THE BACK. MAINTENANCE REPLACED THE FLOOR LIGHT STRIP AND OPERATIONAL CHECKS WERE GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 17,319 hrs · 14,362 cycles

DEN - FLIGHT 6014, THE CREW REPORTED A BURNT ELECTRICAL SMELL IN THE COCKPIT WHEN STARTING THE APU WITH GROUND POWER ASSIST. MAINTENANCE INSPECTED THE GPU & APU CONTACTOR, WITH NO DEFECTS NOTED, STARTED THE APU AND WAS UNABLE TO DUPLICATE THE DISCREPANCY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BATTERY — OVERTEMP (MASTER) · airframe 15,740 hrs · 12,890 cycles

BATTERY NR 1 OVERTEMP. REMOVED AND REPLACED NR 1 MAIN BATTERY IAW EMB 145 AMM 24-36-01, OPS CHECK GOOD.

Part: WINDSHIELD — DELAMINATED (COCKPIT)

FLIGHT 5703 - IAD - FLIGHT CREW REPORTED NR 2 WINDSHIELD DELAM AND ARCING. EWR MX REMOVED AND REPLACED NR 2 WINDSHIELD AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.

Part: SENSOR — INOPERATIVE (PITOT HEAT) · airframe 14,522 hrs · 11,848 cycles

CLE FLIGHT NR 109 THE CREW REPORTED AN PITOT 1 HEAT FAIL DURING ICING CONDITIONS. THE ACFT RETURNED TO CLE AND LANDED WITHOUT INCIDENT. MX INSPECTED AND REPLACED THE PITOT CURRENT SENSOR KOO53 AND STATIC SENSOR SO335. OPS CHECKS WERE GOOD.

Part: DUCT — BLOWN (BLEED AIR SYS) · airframe 14,487 hrs · 11,821 cycles

SDF - FLIGHT 152, THE CREW REPORTED THAT AFTER TAKE OFF AN ENGINE 2 ANTI-ICE FAIL MSG APPEARED. SHORTLY AFTER THEY RECEIVED AN ENGINE 2 FIRE INDICATION ON EICAS. THE FIRE HANDLE WAS PULLED, ENGINE SHUTDOWN, AND THE FIRE WARNING EXTINGUISHED. THE ACFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MX R&R THE Y-DUCT AT THE CUSTOMER SERVICE MANIFOLD, OPS AND LEAK CHECKED WITH NO DEFECTS, AND THE ACFT WAS APPROVED FOR RETURN TO SERVICE.

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 12,804 hrs · 10,445 cycles

FLT 7823 - GEG TO LAX - FLIGHT CREW REPORTED ATO NR 2 FUEL QTY INDICATION CHANGED VALUE AND GAVE FUEL IMBALANCE MSG WHEN THRUST LEVERS ADVANCED. AFTER RETURNING TO BLOCK FLIGHT CREW PERFORMED A SYSTEM REST AND RAN UP THE ENGINES AND FOUND NO PROBLEMS. NO W/U AND NO MX ACTION. A/C WAS RELEASED TO RETURN FOR SERVICE.

Part: EXTINGUISHER — DISCHARGED (BAGGAGE) · airframe 12,646 hrs · 10,322 cycles

FLT 7756 - LAX TO LAX - DURING GROUND HANDLING BY TOWING CREW BOTH BAGGAGE FIRE BOTTLES WERE DISCHARGED. MX AT LAX REMOVED AND REPLACED BOTH FIRE BOTTLE AND AIRCRAFT WAS RETURN FOR SERVICE IN AIRWORTHY CONDITIONS.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 8,226 hrs · 4,369 cycles

IAH - FLIGHT 2866, DURING CLIMB THE CREW REPORTED A LAV SMOKE INDICATION. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LAV SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: FIREWALL — CHAFED (APU BAY) · airframe 8,693 hrs · 6,921 cycles

SHV - DURING C-CHECK THE APU FIREWALL WAS FOUND TO BE CHAFED AT THE 6 O`CLOCK POSITION. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5310-01359. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: BEAM — CORRODED (FUSELAGE) · airframe 8,693 hrs · 6,921 cycles

SHV - DURING C-CHECK THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE CORROSION AND PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS EC5330-01458. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: ENGINE — LEAKING (NR 2) · airframe 6,891 hrs · 5,486 cycles

CREW REPORTED, LAV SMOKE WARNING. EWR MAINTENANCE INSPECTED THE AIRCRAFT AND MAINTENANCE FERRIED AIRCRAFT TO BTV MAINTENANCE REMOVED AND REPLACED NR 2 ENGINE IAW TASKCARD 6271001, OPS CHECKED AND LEAKS CHECKS GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 6,877 hrs · 5,477 cycles

IAH - FLIGHT 2596, THE CREW REPORTED A LAV SMOKE MASTER WARNING WITH WHITE SMOKE IN THE CABIN AND RETURNED TO IAH WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE LAV SMOKE DETECTOR, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.

Part: SMOKE DETECTOR — INTERMITTENT (LAVATORY) · airframe 6,784 hrs · 5,407 cycles

CLE FLIGHT 2469 THE CREW REPORTED A LAV SMOKE WARNING ON CLIMBOUT AFTER SHUTTING DOWN THE APU. NO SMOKE OR FUMES WERE NOTICED AFTER VISUAL INSPECTION. THE SYSTEM WAS RESET AND NO INDICATION WAS NOTICED. MAINTENANCE INSPECTED AND REPLACED THE FORWARD GALLEY SMOKE DETECTOR PANEL. OPERATIONAL CHECKS WERE GOOD.