N995CA

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 2,068 hrs · 2,228 cycles

PILOT REPORTED COMBUSTION HEATER FIRE CAS MESSAGE ON IN FLIGHT. MAINTENANCE INSPECTED AND FOUND SHORTED WIRE FWD ON INSTRUMENT PANEL FROM PIN K AT AML CONNECTOR. REPAIRED WIRE WITH NO FURTHER DEFECTS NOTED.

Part: FIRE DETECTOR — FAILED (UNKNOWN) · airframe 2,031 hrs · 2,170 cycles

PILOT REPORTED LEFT ENGINE FIRE CAS MESSAGE IN FLIGHT, WITH NO VISIBLE FIRE. MAINTENANCE REPLACED THE FIRE DETECTOR IN THE LEFT ENGINE COMPARTMENT WITH NO FURTHER DEFECTS NOTED.

Part: FAN — FAILED (UNKNOWN) · airframe 1,890 hrs · 2,019 cycles

PILOT REPORTED COMBUSTION HEATER FIRE CAS MESSAGE CAME ON IN FLIGHT, THEN WENT OFF. MAINTENANCE INSPECTED AND FOUND THE CABIN HEATER VENTILATING AIR FAN AT FAULT. HEATER VENTILATING AIR FAN WAS REPLACED WITH NO FURTHER DEFECT NOTED.

Part: SENSOR — FAILED · airframe 1,655 hrs · 1,748 cycles

PILOT REPORTED LEFT ENGINE LOST FUEL PRESSURE WHEN CLIMBING THROUGH 7000 FEET. CREW NOTICED IT WAS WHEN THE LEFT FUEL PUMP WOULD CYCLE ON AUTOMATICALLY AND THE FUEL PRESSURE WENT INTO RED ARC ACCOMPANIED BY A 'LOW FUEL PRESSURE CAS MESSAGE'. MAINTENANCE INSPECTED AND DETERMINED THE MANIFOLD AIR TEMP SENSORS TO BE AT FAULT. BOTH MAT SENSORS WERE REPLACED WITH NO FURTHER DEFECTS NOTED.

Part: WHEEL — BROKEN (MLG) · airframe 453 hrs · 460 cycles

DURING MAINTENANCE INSPECTION SPOKE ON THE MAIN GEAR WHEEL ASSEMBLY WAS FOUND TO BE BROKEN. THE WHEEL ASSEMBLY WAS REPLACED WITH NO ADDITIONAL DEFECTS NOTED

Part: BPSU — FAILED (T/E FLAP) · airframe 23,611 hrs · 21,825 cycles

FLIGHT 5178 - RECEIVED FLAPS FAIL CAUTION MESSAGE AT 16,000 FT. FLAPS INDICATED FAILING AT 0 DEGREES. AIRCRAFT LANDED SAFELY IN JFK. REMOVED AND REPLACED RIGHT BPSU.

Part: FLAP — MALFUNCTIONED (WING) · airframe 23,610 hrs · 21,824 cycles

FLIGHT 5178 - RECEIVED FLAPS FAIL CAUTION MESSAGE AT 18,000 FT. FLAPS FAILED AT 0 DEGREES. AIRCRAFT LANDED SAFELY. COMPLIED WITH AD 2006-12-21 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (G) 1, 2, 3, (A, B, C). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: WARNING SYSTEM — MALFUNCTIONED (NLG STEERING) · airframe 23,599 hrs · 21,816 cycles

FLIGHT 5181 - NWS INOP CAUTION MESSAGE 3 TIMES IN ROUTE. PERSISTED AFTER QRH PROCEDURE. AIRCRAFT LANDED SAFELY IN MEM. RESET NWS WITH NO FAULTS FOUND IN NWS ECU. TAXI CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 23,156 hrs · 21,480 cycles

FLIGHT 5383 - F/O SIDE WINDOW CRACKED. FOLLOWED QRH, DESCENDED, REDUCED DIFFERENTIAL PRESSURE TO 6.0. REPLACED F/O SIDE WINDOW. NO FURTHER DEFECTS.

Part: LIGHT — LOW (CABIN) · airframe 22,960 hrs · 21,327 cycles

FLIGHT 5047 - CREW REPORTS FIRST EMERGENCY FLOOR LIGHT DIM. REMOVED AND REPLACED LAMP-FLEX SOLID FOR FORWARD MOST EMERGENCY FLOOR TRACK LIGHTING.

Part: ENGINE — VIBRATION (NR 1) · airframe 22,328 hrs · 20,820 cycles

FLIGHT 5350 - NR 1 ENGINE VIB GAUGE PEGGED OFF CHART, REDUCED THRUST TO IDLE AND VIBS STOP. A/C DIVERTED TO LGA AND LANDED SAFELY. PERFORMED ENGINE RUNS WITH CREW WITH NO DEFECTS NOTED. SUSPECT SEVERE ICING.

Part: ACTUATOR — FAULTY (RT FLAP OB) · airframe 21,314 hrs · 20,026 cycles

FLIGHT 5304 - FLAPS FAIL MESSAGE ON APPROACH, FLAPS AT 0, 210 KTS. CREW DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. REPLACED RT OUTBOARD FLAP, O/B ACTUATOR.

Part: ACTUATOR — FAULTY (RT FLAP OB) · airframe 21,314 hrs · 20,026 cycles

FLIGHT 5304 - FLAPS FAIL MESSAGE ON APPROACH, FLAPS AT 0, 210 KTS. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED RT OUTBOARD FLAP, I B ACTUATOR.

Part: ROD — BROKEN (PAX DOOR) · airframe 20,314 hrs · 22,375 cycles

FLIGHT 5297 - DURING CLIMBOUT OF MCO THE CABIN FAILED TO PRESSURIZE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE SPRING ROD ASSEMBLY FOR THE CABIN DOOR PRESSURE FLAP SEAL.

Part: DRIVE SHAFT — WORN (TE FLAPS) · airframe 20,295 hrs · 19,219 cycles

FLIGHT 5870 - DURING BOS APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT WING NR 2 FLEX DRIVE SHAFTS.

Part: DRIVE SHAFT — WORN (TE FLAPS) · airframe 20,295 hrs · 19,219 cycles

FLIGHT 5870 - DURING BOS APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT AND RIGHT WING NR 5 FLEX DRIVE SHAFTS.

Part: DRIVE SHAFT — WORN (TE FLAPS) · airframe 20,295 hrs · 19,219 cycles

FLIGHT 5870 - DURING BOS APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT AND RIGHT WING NR 3 FLEX DRIVE SHAFTS.

Part: DRIVE SHAFT — WORN (TE FLAPS) · airframe 20,295 hrs · 19,219 cycles

FLIGHT 5870 - DURING BOS APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT AND RIGHT WING NR 4 FLEX DRIVE SHAFTS.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 20,296 hrs · 19,218 cycles

FLIGHT 5870 - DURING YHZ APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND ABORTED FIRST APPROACH, THEN LANDED WITHOUT INCIDENT ON SECOND ATTEMPT. COMPLIED WITH AD 98-20-01 FLAP CAUTION MESSAGE -FIRST EVENT- MAINTENANCE ACTION, PARAGRAPH (B) 1, 2, 3 (A, B, C AND E). FLAP SYSTEM WAS RESET WITH NO FURTHER FLAP CAUTION MESSAGES.

Part: DRIVE SHAFT — WORN (TE FLAPS) · airframe 20,295 hrs · 19,219 cycles

FLIGHT 5870 - DURING BOS APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE LEFT WING NR 1 FLEX DRIVE SHAFTS.

Part: ACTUATOR — UNRELIABLE (TE FLAPS) · airframe 19,827 hrs · 18,844 cycles

FLIGHT 5399 - FLAPS FAIL CAUTION. REPLACED THE LT NR 4 FLAP ACTUATOR.

Part: PDU — MALFUNCTIONED (TE FLAPS) · airframe 19,768 hrs · 18,795 cycles

FLIGHT 5541 - FLAPS FAIL CAUTION. REPLACED THE PDU.

Part: COALESCER BAG — DIRTY (ACM) · airframe 19,450 hrs · 18,529 cycles

STRONG OILY SMELL FUMES IN COCKPIT AND CABIN. REPLACED THE COALESCER SOCKS. NO FURTHER SMELL.

Part: POWER CABLE — BROKEN (CABIN) · airframe 18,867 hrs · 17,999 cycles

FLIGHT 5610 - CABIN EMERGENCY LIGHTS FLICKER. REPLACED POWER CABLE.

Part: LIGHT — MALFUNCTIONED (ROW 8) · airframe 18,746 hrs · 17,890 cycles

FLIGHT 4954 - CABIN EMERGENCY LIGHTS FLICKER OFF AND ON. REPLACED LIGHT ASSEMBLY AT ROW 8.

Part: DOOR — CRACKED · airframe 17,626 hrs · 16,901 cycles

THREE CRACKS FOUND PAX FS 320.00, 329.00 AND 338.00. REPAIRED IAW REO 601R-52-11-684.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 17,626 hrs · 16,901 cycles

LEFT AFT ANGLE ON FS 280.00. REPAIRED IAW REO 601R-53-11-136 AND EO 10-5310-00587.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 17,626 hrs · 16,901 cycles

INTERCOSTAL AT FS 484.00 IS CRACKED. REPAIRED IAW REO 601R-53-41-059.

Part: FRAME — CRACKED (FUSLAGE) · airframe 17,626 hrs · 16,901 cycles

LEFT HAND 640 FRAME CRACKED. REPAIRED IAW REO 601R-53-61-487 AND CRJ SRM 51-23-00, 51-25-06, 51-25-16, 51-42-06, 51-42-21, 51-41-02 AND 51-42-20.

Part: FRAME — CRACKED (FUSELAGE) · airframe 17,626 hrs · 16,901 cycles

RIGHT HAND 640 FRAME CRACKED. REPAIRED IAW CRJ SRM 51-42-06, 51-42-21 AND 51-25-01.

Part: PDU — OUT OF ADJUST (THRUST REVERSER) · airframe 17,634 hrs · 16,907 cycles

FLIGHT 9468 - LT THRUST REVERSER UNLOCKED MESSAGE. ADJUSTED THE PDU, OPERATIONAL CHECK SATISFACTORY.

Part: UPLOCK TARGET — OUT OF ADJUST (MLG) · airframe 17,425 hrs · 16,726 cycles

FLIGHT 5146 DURING APPROACH RECEIVED A GEAR DISAGREE WARNING. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. ADJUSTED THE NLG LANDING GEAR UPLOCK TARGET GAP.

Part: WARNING LIGHT — FALSE INDICATION (MLG) · airframe 17,410 hrs · 16,713 cycles

FLIGHT 5401 RECEIVED A NOSE LANDING GEAR DISAGREE CAUTION DURING APPROACH INTO NAS. INTERROGATED PSEU, CHECKED UPLOCK GAP AND SENSOR FOR SECURITY AND CYCLED GEAR MULTIPLE TIMES. DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE.

Part: CONNECTOR — UNSECURE (RADAR ALTIMETER) · airframe 16,752 hrs · 16,115 cycles

FLIGHT 5532 F/O'S RADAR ALTIMETER IS INTERMITTENT. RESECURED COAX CONNECTOR ON NR 2 RADIO ALTIMETER.

Part: WARNING SYSTEM — ACTIVATED (RUDDER CONFIG) · airframe 14,861 hrs · 14,566 cycles

FLIGHT 5158 RUDDER CONFIG WARNING DURING T/O. COULD NOT DUPLICATE. FOUND NO DEFECTS WITH CONFIG SYSTEM.

Part: LANDING GEAR — SLOW (NOSE) · airframe 14,500 hrs · 14,255 cycles

GEAR DISAGREE WARNING, NLG TOOK SEVERAL MINUTES TO EXTEND. COULD NOT DUPLICATE. FOUND NO DEFECTS, OPERATIONAL CHECK NORMAL.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 14,460 hrs · 14,222 cycles

FLIGHT 5481 NR 3 HYDRUALIC SYSTEM LOW PRESSURE & LOW QUANTITY WARNING. REPLACED THE 3A HYDRAULIC PUMP.

Part: FLAP · airframe 11,477 hrs · 11,709 cycles

FLIGHT 5423 FLAPS FAILED AT 9 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.

Part: FLAP · airframe 11,238 hrs · 11,486 cycles

FLIGHT 5226 FLAPS FAILED WHEN SELECTED TO 8 DEGREES.RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: SEAL — LEAKING (L/H ENGINE) · airframe 10,702 hrs · 10,965 cycles

LEFT ENGINE OIL PRESSURE WARNING.REPLACED THE INTEGRATED DRIVE GENERATOR

Part: IDG · airframe 9,655 hrs · 9,950 cycles

FLIGHT 5268 DURING TAKE OFF ROLL RECEIVED AN IDG AND GENERATOR #1 MESSAGE, TAKE OFF WAS ABORTED AND RETURNED TO THE GATE.SERVICED THE #1 ENGINE IDG WITH OIL AND PERFORMED FUNCTIONAL CHECK, AIRCRAFT RETURNED TO SERVICE.

Part: TANK — SHORTED (AVIONCIS) · airframe 8,172 hrs · 8,479 cycles

FLIGHT #5819 - F/A REPORTED SMOKE SMELL. GALLEY AND LAV WATER SERVICE INOP. GALLEY BREAKERS WERE TRIPPED.REPLACED THE GALLEY WATER TANK.

Part: ROD — MISRIGGED (NLG) · airframe 8,257 hrs · 8,346 cycles

FLIGHT 5521 - NOSE L/G DOORS CYCLE CONSTANTLY AFTER GEAR RETRACTION.ADJUSTED THE L/H NLG DOOR LINKAGE.

Part: STRUCTURE · airframe 7,987 hrs · 8,281 cycles

FLIGHT #5574. DURING CLIMB OUT OF GRB AIRCRAFT ENCOUNTERED MULTIPLE BIRD STRIKES, RETURNED TO THE FIELD.PERFORMED BIRD STRIKE INSPECTION, NO DAMAGE NOTED.

Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 7,780 hrs · 8,050 cycles

FLIGHT 5336. DURING DESCENT INTO CVG, RECEIVED A FLAP FAIL CAUTION AT 25 DEGREE FLAP POSITION, CREW DECIDED TO DECLARE AN EMERGENCY, AIRCRAFT LANDED SAFELY.REPLACED THE FLAP CONTROL HANDLE.

Part: FRAME — CRACKED (FUSELAGE) · airframe 7,624 hrs · 7,871 cycles

LEFT AND RIGHT FS 718 STR 10 AND 11 ARE CRACKED. REPAIRED LEFT AND RIGHT FUSELAGE FRAME STR 10 - 12 AT FS 718.00 IAW CANADAIR REO 601R-53-61-193.

Part: SMOKE — DETECTED (APU) · airframe 7,475 hrs · 7,717 cycles

SMOKE COMING FROM APU INLET WHEN APU WAS SHUT DOWN. INSPECTED APU AND FOUND NO DEFECTS.

Part: LIGHT — CONTAMINATED (CABIN) · airframe 6,668 hrs · 6,303 cycles

FORWARD FLOOR EMERGENCY LIGHTING IS INOPERABLE. DRIED WATER IN FLOOR LIGHTING SYSTEM. SYSTEM TEST SATISFACTORY.

Part: PCU — MALFUNCTIONED (TE FLAPS) · airframe 5,991 hrs · 6,220 cycles

FLAPS HALF SPEED AND FLAPS FAIL MESSAGE. REPLACED THE PCU.

Part: WARNING SYSTEM — FALSE INDICATION (COCKPIT) · airframe 5,021 hrs · 5,217 cycles

RIGHT HAND AOA HEAT CAUTION MESSAGE. RESET CIRCUIT BREAKERS, SYSTEM TEST NORMAL. COULD NOT DUPLICATE.

Part: ANGLE — CRACKED (BS 621)

FS 621 FLOOR SUPPORT STRUCTURE CRACKED BETWEN LBL 42 AND LBL9 AT WL 73. REPAIRED IAW BOMBARDIER REO 601R-53-61-117 REV A.

Part: VALVE — FAILED (MLG)

LANDING GEAR DISAGREE MESSAGE. MLG DID NOT EXTEND. REPLACED THE MLG SELECTOR VALVE.

Part: SENSOR — LOOSE (RT MLG)

GEAR DISAGREE WARNING WHEN GEAR EXTENDED. SECURED LOOSE TARGET ON RIGHT MLG UPLOCK SENSOR.

Part: GENERATOR — FAILED (RT ENGINE)

RIGHT ENGINE GENERATOR FAILED DURING TAKEOFF. TRANSFERRED DISCREPANCY TO DEFERRED LIST PER MEL.

Part: ANGLE — CRACKED (BS 621)

RT SIDE FS 621 FLOOR SUPPORT ANGLE IN BAGGAGE BAY IS CRACKED. REPAIRED RT SIDE FS 621 FLOOR SUPPORT ANGLE IAW CANADAIR REO 601R53-61-117REVA.

Part: DOUBLER — CRACKED (BS 718)

DOUBLERS CRACKED AT FS 718.00 STRG 11 LT AND RT SIDES. REMOVED AND REPLACED CRACKED DOUBLERS IAW WVAC EO 601R-53-0468.

Part: ACM — FAILED (LEFT)

DURING APPROACH INTO CVG, A STRONG SMELL OF ELECTRICAL ODOR WAS NOTED IN THE COCKPIT AND CABIN ASSOCIATED WITH SMOKE. THE CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY. INVESTIGATION REVEALED THE LEFT AIR CONDITIONING UNIT FAILED CAUSING SLIGHT SMOKE AND FOUL ODOR. THE LEFT ACM WAS DEFERRED AND AIRCRAFT RETURNED TO SERVICE.

Part: FECU — MALFUNCTION (TE FLAPS)

FLAPS FAILED MESSAGE. REPLACED THE FECU.

Part: CIRCUIT BREAKER — TRIPPED (ADC SYST)

A 20 KNOT DIFFERENCE BETWEEN PILOT AND CO PILOT AIR SPEED INDICATORS. INSPECTED PITOT SYSTEM, FOUND NO DISCREPANCIES. RESET ADC CIRCUIT BREAKERS AND RETURNED AIRCRAFT TO SERVICE.

Part: VALVE — FAILED (NLG)

NLG DOES NOT RETRACT. REPLACED THE NLG SELECTOR VALVE.