N655BR

Part: TRIM SYSTEM — INOPERATIVE (AILERON) · airframe 12,591 hrs · 12,411 cycles

ASH 1026 HNL. AILERON TRIM SYSTEM INOP. MX DEFERRED THE AILERON TRIM SYSTEM.

Part: SPOILER — MALFUNCTIONED (WING) · airframe 12,394 hrs · 11,957 cycles

ASH 1010 HNL. ABORTRED T/O DUE TO A CONFIG SPOILER FAULT. MX RESET SPOILERS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,973 hrs · 10,973 cycles

ASH RON HNL - CEILING EMERGENCY LIGHT INOP. MX RELAMPED.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 11,949 hrs · 10,908 cycles

ASH RON HNL. LT EMERGENCY LIGHT OVER WING LOWER INTERIOR LIGHT INOP. MX RE-SECURED THE CONNECTOR.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 11,376 hrs · 9,860 cycles

LEFT BATTERY RIB SUPPORT ANGLE LWS 48.3 IS CRACKED .25 INCH.

Part: ANGLE — CRACKED (BS 280) · airframe 11,376 hrs · 9,860 cycles

LEFT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS.

Part: ANGLE — CRACKED (BS 280) · airframe 11,376 hrs · 9,860 cycles

RIGHT 280 VERTICAL ANGLE IS CRACKED AT .5 INCH BETWEEN FASTENERS.

Part: DOUBLER — CRACKED (FRAME) · airframe 11,376 hrs · 9,860 cycles

RIGHT FRAME DOUBLER CRACKED IN RADIUS AT 1 INCH IN LENGTH.

Part: SUPPORT ANGLE — CRACKED (RT WING) · airframe 11,376 hrs · 9,860 cycles

RIGHT BATTERY RIB SUPPORT ANGLE RWS 48.3 IS CRACKED .25 INCH.

Part: SUPPORT BEAM — CRACKED (RT ENGINE) · airframe 11,376 hrs · 9,860 cycles

RIGHT ENGINE SUPPORT BEAM IS CRACKED IN LOWER WEB AT .75 INCH.

Part: LINE — LEAKING (SCAVANGE PUMP)

LT ENG OIL PRESSURE WARNING, PRESS FLUXUATION IN FLIGHT DOWN TO 19-22 PSI IN-FLIGHT ENGINE SHUTDOWN. C SUMP SCAVENGE LINES LEAKING - REPLACED LINES,OIL FILTER, INSPECTED CHIP DETECTOR.

Part: HANDLE — LACK OF LUBE (PARKING BRAKE)

TWO ABORTED TAKEOFFS FOR RED EICAS 1 BRAKE MSG FOLLOWED BY CONFIG BRAKE WARNING. MX FOUND PARKING BRAKE HANDLE STICKING IN THE UP POSITION INTERMITTENTLY. LUBED PARK BRAKE HANDLE.

Part: DUCT — FAILED (ANTI ICE SYSTEM)

EVENT SUMMARY STATED THAT HIGH SPEED ABORT DUE TO MX. REMOVED AND REPLACED BLEED AIR CONTROL UNIT PER OPS CHECK OF ANTI ICE SYSTEM WITH NO DEFECTS NOTED.

Part: BRAKE ASSY — STICKING (NR 4)

EVENT SUMMARY STATES THAT AIRCRAFT PULLS HARD TO RIGHT. PERFORMED INSP OF WHEELS AND BRAKES. FOUND NR 4 BRAKE STICKING. CLEANED AND TESTED IAW MM 32-43-00. CHECKS GOOD ON TAXI CHECK BY CREW.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING INSPECTION THE PASSENGER DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — INOPERATIVE (AUTOPILOT)

DURING CRUISE OF FLIGHT 7387 CREW REPORTED A STAB/MACH TRIM FAILURE. THE CREW DIVERTED TO NEAREST SUITABLE FIELD AND FLIGHT LANDED UNEVENTFULLY. THE HORIZONTAL STABILIZER TRIM CONTROL UNIT WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK PERFORMED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: BPSU — FAULTY (T/E FLAP)

DURING APPROACH OF FLIGHT TO BDL CREW REPORTED A FLAP FAIL WITH FLAPS AT 20 DEGREES ON APPROACH. FLIGHT LANDED UNEVENTFULLY AND PASSENGERS DEPLANED NORMALLY. THE BPSU WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: CIRCUIT BOARD — FAULTY (AUTOPILOT SYS) · airframe 7,385 hrs · 6,200 cycles

DURING FINAL APPROACH THE CREW REPORTED RECEIVING AUTOPILOT PITCH TRIM MESSAGES. FLIGHT LANDED UNEVENTFULLY. FAULT WAS TROUBLESHOT TO THE NR 2 FCC CARD AND UNIT WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: AXLE — CORRODED (NLG) · airframe 7,180 hrs · 6,023 cycles

DURING HEAVY CHECK CORROSION WAS IDENTIFIED AT THE NOSE LANDING GEAR AXLE ASSEMBLY. THE AXLE ASSEMBLY WAS REMOVED AND REPLACED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING MAINTENANCE INSPECTION, THE AFT CEILING EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LAMP

During maintenance inspection the L/H aft exterior emergency exit light was found to be inoperative. Maintenance personnel removed and replaced the lamp in the emergency exit light. An operational check was satisfactory and the aircraft was returned to service.

Part: LAMP — BURNED OUT (AFT EMER LIGHT)

AFT EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERSONNEL RELAMPED EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICE.

Part: LIGHT — INOPERATIVE (CABIN)

RIGHT SIDE OVER WING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED OVER WING EMERGENCY LIGHT. OPERATIONAL CHECK GOOD. AIRCRAFT RELEASED FOR CONTINUED SERVICE

Part: LIGHT — INOPERATIVE (CABIN)

DURING TAXI OF THE FLIGHT FROM ORD TO MSN, CREW REPORTED CABIN OVERHEAD EMERGENCY LIGHT BURNED OUT. MAINTENANCE PERSONNEL RELAMPED OVERHEAD CABIN EMERGENCY LIGHTING. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.