N651BR

Part: AUTOPILOT SYS — MALFUNCTIONED (NR 1) · airframe 15,179 hrs · 13,566 cycles

ASH 7109 BNA - CREW RTG DUE TO YAW CAMP NR 1 WILL NOT STAY ENGAGED. MX RESET YAW DAMP AND AUTOPILOT SYSTEMS.

Part: WARNING SYSTEM — MALFUNCTIONED (SPOILER SYS) · airframe 13,567 hrs · 12,175 cycles

ASH 1038 HNL - SPOILERON AND INBOARD GROUND SPOILER FAULT. MX RESET SYSTEM.

Part: FLAP — MALFUNCTIONED (WING) · airframe 13,537 hrs · 12,111 cycles

ASH 1004 HNL.- PILOT DECLARED EMERGENCY FOR A FLAPS FAIL AT 10 DEGREES IN FLIGHT. MX COMPLIED WITH PART A INSPECTION.

Part: LIFE VEST — MISSING (CABIN) · airframe 13,338 hrs · 11,683 cycles

ASH 1043 HNL - 2 ADULT LIFE VESTS WERE MISSING FROM THE AIRCRAFT. MX INSTALLED 2 NEW LIFE VESTS.

Part: STOP — OUT OF ADJUST (PAX DOOR) · airframe 13,323 hrs · 11,641 cycles

ASH 1010 HNL - PAX DOOR LATCH CAUTION WARNING IN FLIGHT. MX ADJUSTED UPPER STOP.

Part: ECU — MALFUNCTIONED · airframe 13,228 hrs · 14,415 cycles

GLD UNSAFE CAUTION MESSAGE IN FLIGHT. MX RESET THE SECUS. OPS CHECK GOOD.

Part: WARNING LIGHT — ILLUMINATED (STALL WARNING)

EVENT SUMMARY STATED THAT STALL FAIL MSG ON CLIMB-OUT. NO FAULT CODES IN MDC. RESET SPS. INSPECTED BOTH AOA VANES. OPS CHK GOOD.

Part: SMOKE DETECTOR — DEFECTIVE (LAVATORY)

TOILET SMOKE EICAS MESSAGE. INSPECTED LAV LIGHTS, PACK COALESCER BAGS AND PERFORMED RUNS. NO DEFECT NOTED. REMOVED AND REPLACED SMOKE DETECTOR.

Part: WARNING LIGHT — ACTIVATED (MLG)

EVENT SUMMARY STATED GEAR DISAGREE. REMOVED AND REPLACED MLG PRIORITY VALVE IN REF TO CRJ MM 32-32-15, NO FIX. FOUND AIR IN NR 3 HYD SYSTEM, DRAINED AIR AND SERVICED HYD SYSTEM IAW CRJ AMM 12-12-29. CREW WROTE THE FOLLOWING, LEFT GEAR UP DISAGREE ON RETRACTION, CLEARED ITSELF IN 1 MINUTE, HYD PUMP 3 WAS 2300 LBS. D/L CODES FROM PSEU AND A HARD FAIL WAS DISCOVERED ON LT MLG CODES WAS LEFT GEAR UPLOCK FAR. DID NOT HAVE A CHANCE TO DO GEAR SWINGS BUT BELIEVED GEAR WAS SLOW TO COME UP. FOUND NR 3 ACCUMULATOR LOW, SERVICED NR 3 ACCUMULATOR IAW CRJ AMM 12-12-29 D/L LOADED CODES FROM PSEU AND RESET PSEU. GEAR SWINGS OP CHECK GOOD. MLG SELECTOR VALVE, NO LEAK NOTED.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB)

CREW REPORT ON 01/11 STATED THAT IMMEDIATELY AFTER T/O THE STAB TRIM AND MACH TRIM CAUTION MSGS POSTED AT THE SAME TIME. RETRIEVED FAULT CODES FROM MDC. PERFORMED HSTCU OPS TEST PER 27-40-00. OPS CHECK GOOD.

Part: FLAP — MALFUNCTIONED (WING)

FLAPS FAIL AT ZERO. RETRIEVED FAULT CODES 1 JAM 2. PDU DIFF 3 UNSPECIFIED, CLEARED FAULTS OPS CHECKS GOOD AT THIS TIME REF 27-51-00.

Part: A/C PACK — CONTAMINATED

LAV SMOKE INDICATION AT 200FT. NO SMOKE OR FUMES BUT ODOR. SUSPECT GLYCOL IN AIR CONDITIONING. MX PERFORMED HIGH POWER RUNS. NO DEFECT NOTED.

Part: VALVE — FAILED (ANTI ICE SYSTEM)

EVENT SUMMARY STATED REJECTED TAKEOFF AT 40KT DUE TO LT COWL ANTI-ICE CAUTION MSG. TROUBLESHOOTING CONFIRMED THE PROBLEM, AND RTG. REMOVED AND REPLACED LT COWL ANTI ICE VALVE REF AMM 30-22-01. PERFORMED OPS CHECK OF ANTI ICE. OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING INSPECTION THE FOWARD FLOOR EMERGENCY FLOOD LIGHT WAS FOUND INOPERATIVE. THE BULB WAS REPLACED AND A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED.

Part: HANDLE — INOPERATIVE (TE FLAPS) · airframe 9,130 hrs · 7,552 cycles

DURING FLAP EXTENSION, THE FLAPS WOULD NOT EXTEND BEYOND 20 DEGREES. THE MALFUNCTION DID NOT INTERFERE WITH THE SAFE OPERATION OF THE FLIGHT. THE FLIGHT WAS COMPLETED NORMALLY AND PASSENGERS DEPLANED NORMALLY. THE FLAP CONTROL LEVER WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS)

DURING APPROACH OF FLIGHT 7522 CREW REPORTED A FLAP SYSTEM FAILURE WITH FLAPS A 8 DEGREES. FLIGHT LANDED UNEVENTFULLY. A SYSTEM OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 8,992 hrs · 7,437 cycles

DURING INSPECTION THE LEFT FORWARD EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND FAULTY AND REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE.

Part: SWITCH — CONTAMINATED (STAB TRIM) · airframe 8,761 hrs · 7,241 cycles

DURING CLIMB OF FLIGHT 7267 CREW REPORTED STABILIZER TRIM SYSTEM 1 AND 2 FAILURE MESSAGES. CREW DECLARED EMERGENCY AND RETURNED TO ORD. FLIGHT LANDED WITHOUT INCIDENT AND PASSENGERS DEPLANED NORMALLY. THE DISCONNECT SWITCHES WERE FOUND ENGAGED DUE TO FOD AND WERE CLEANED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL HANDLE — FAILED (COCKPIT)

DURING CLIMB OF THE FLIGHT FROM IAD TO GSP, THE CREW REPORTED THAT UPON LANDING GEAR RETRACTION HAD NO INDICATION OF GEAR RETRACTION ON THE FLIGHT DECK. THE THREE GREEN GEAR DOWN/LOCKED INDICATORS REMAINED ILLUMINATED. THE CREW REPORTED, RECEIVED ANTI-SKID OUTBOARD AND PARKING BRAKE SOV FAIL MESSAGES. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LANDING GEAR SELECTOR. LANDING GEAR EXTENSION/RETRACTION OPERATIONAL CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.