N719CA

Part: SENSOR — FAULTY · airframe 20,479 hrs · 18,912 cycles

FLIGHT 5164 - UPON REACHING FLIGHT LEVEL 330 DISPLAY COOL CAUTION MESSAGE APPEARED. AIRCRAFT DIVERTED TO GSO AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED FLOW SENSOR.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 20,360 hrs · 18,815 cycles

FLIGHT 5457 - EN ROUTE JFK TO BUF CAPTAIN`S WINDSHIELD CRACKED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LEFT WINDSHIELD.

Part: AIR FILTER — CLOGGED (COCKPIT) · airframe 19,989 hrs · 18,518 cycles

FLIGHT 9479 - EN ROUTE CVG-MHT RECEIVED A DISPLAY COOL MESSAGE, FLIGHT DIVERTED TO PIT. REPLACED CLOGGED AIR FILTER FOR THE ELECTRONIC FLIGHT INSTRUMENT SYSTEM.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 18,996 hrs · 17,715 cycles

FLIGHT 5745 - DURING BTV APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. 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: BPSU — FAULTY (T/E FLAP) · airframe 18,969 hrs · 17,689 cycles

FLIGHT 5686 - DURING OPERATION OF FLAPS WHILE AT THE GATE RECEIVED A FLAP FAIL CAUTION MESSAGE. REPLACED THE RIGHT BRAKE POSITION SENSING UNIT.

Part: ELEMENT — MALFUNCTIONED (ANTI ICE SYSTEM) · airframe 16,796 hrs · 15,814 cycles

FLIGHT 5673- ANTI ICE DUCT WARNING. REPLACED THE LT FUSELAGE SENSING ELEMENT A47WK.

Part: PUMP — FAILED (NR 2 HYD SYSTEM) · airframe 14,833 hrs · 14,135 cycles

FLIGHT 5450 DURING CRUISE FLIGHT RECEIVED A HYDRAULIC SYSTEM NR 2 LOW PRESSURE WARNING. CREW DECLARED AN EMERGENCY AND DIVERTED TO TYS. REPLACED FAILED NR 2 ENGINE DRIVEN HYDRAULIC PUMP.

Part: PUMP — UNRELIABLE (HYD SYSTEM) · airframe 13,633 hrs · 13,175 cycles

FLIGHT 5921 HYDRAULIC SYSTEM 3 LOW PRESSURE CAUTION AND GEAR DISAGREE WARNING. REPLACED SYSTEM 3A HYDRAULIC PUMP.

Part: CONTROLLER — MALFUNCTIONED (TE FLAPS) · airframe 13,537 hrs · 13,091 cycles

FLIGHT 5158 RECEIVED A FLAP FAIL CAUTION MESSAGE DURING CLIMBOUT OF CVG. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. 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 MESSAGE.

Part: ELEMENT — FAILED (ANTI ICE SYSTEM) · airframe 13,178 hrs · 12,809 cycles

FLIGHT 5803 ANTI ICE DUCT WARNING. REPLACED BLEED LEAK SENSING ELEMENT.

Part: WARNING LIGHT — FALSE INDICATION (ANTI ICE SYSTEM) · airframe 13,087 hrs · 12,733 cycles

FLIGHT 5201 LEFT ANTI ICE DUCT WARNING. COULD NOT DUPLICATE. INSPECTED SYSTEM AND FOUND NO DEFECTS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 11,799 hrs · 11,718 cycles

CRACK NOTED AT FLANGE RADIUS OF LT FRAME AT FS 718. REPARIED IAW SB 601R-53-055 PART B IAW EA NR 10-5320-00242.

Part: OIL SYSTEM — LOW (RT ENGINE) · airframe 10,979 hrs · 11,022 cycles

FLIGHT 5533 RT ENGINE OIL PRESSURE WARNING. SERVICED RT ENGINE WITH 4.75 QTS OF OIL.

Part: APU — FAILED (APU) · airframe 7,874 hrs · 8,115 cycles

FLIGHT 5521 SMOKE IN COCKPIT AND CABIN.REPLACED THE APU.

Part: SERVICE DOOR · airframe 7,852 hrs · 8,090 cycles

FLIGHT 5469 LOUD BUZZING NOISE AND STALL FAIL CAUTION PLUS IAS MESSAGE.FOUND 02 SERVICE DOOR OPEN - CLOSED DOOR.

Part: VALVE — MALFUNCTIONED (R/H) · airframe 7,536 hrs · 7,780 cycles

FLIGHT 5519 R/H ENG COWL ANTI-ICE CAUTION MESSAGE.REPLACED THE R/H COWL ANTI ICE VALVE.

Part: CIRCUIT BREAKER · airframe 6,910 hrs · 7,120 cycles

FLIGHT #5407. EMERGENCY LIGHTS CIRCUIT BREAKER IS TRIPPED.RESET BREAKER AND FUNCTION CHECKED SYTEM. NO FAULTS FOUND.

Part: SMOKE DETECTOR — FAULTY (CARGO BAY) · airframe 6,647 hrs · 6,862 cycles

FLIGHT 5068. DURING CRUISE FLIGHT RECEIVED A CARGO SMOKE CAUTION MESSAGE, CREW DECLARED AN EMERGENCY, DISCHARGED THE CARGO FIRE EXTINGUISHING BOTTLE AND RETURNED TO THE FIELD SAFELY. REPLACED DEFECTIVE CARGO SMOKE DETECTOR.

Part: BPSU — MALFUNCTIONED · airframe 6,366 hrs · 6,579 cycles

FLAPS FAILED.REPLACED THE LEFT HAND BPSU.

Part: BUSHING — OUT OF POSITION (VERTICAL STAB) · airframe 6,311 hrs · 6,526 cycles

RT VERT STAB BUSHING IS MIGRATED AT HORIZONTAL STAB ATTACH POINT. REMOVED MIGRATED BUSHING. INSTALLED BUSHING P/N 600-21061-7 (THAT WAS MACHINED IAW WVAC EO 601R-55-2291) IAW CRJ AMM 20-26-00-910-803. REAMED BUSHING IAW DWG 600-21029.

Part: SENSOR — OUT OF ADJ (PAX DOOR) · airframe 6,132 hrs · 6,350 cycles

CABIN DOOR OUTER HANDLE CAUTION MESSAGE. ADJUSTED DOOR HANDLE PROXIMITY SENSOR.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 6,016 hrs · 6,244 cycles

STALL FAIL CAUTION DURING T/O.RESET THE STALL COMPUTER.

Part: SILL — TORN (CARGO DOORWAY) · airframe 5,949 hrs · 6,171 cycles

THE FORWARD ATTACH FOR THE CARGO NET WAS TORN FROM THE CARGO DOORSILL. TRIMMED THE TORN SILL TO A SMOOTH RADIUS AND FABRICATED A REPAIR DOUBLER AND INSTALLED DOUBLER IAW WVAC EO 601R-53-2142.

Part: DOOR — UNSECURE (SERVICE DOOR) · airframe 5,587 hrs · 5,815 cycles

LOUD UNUSUAL NOISE FROM OUTSIDE THE AIRCRAFT. NOSE SERVICE DOOR NOT LATCHED. SECURED DOOR AND AIRCRAFT RETURNED TO SERVICE.

Part: COMPUTER — FAILED (STALL WARNING) · airframe 5,031 hrs · 5,241 cycles

STALL FAIL AND STICK SHAKER AFTER TAKEOFF. RESET THE STALL COMPUTER. COULD NOT DUPLICATE.

Part: FLOOR SUPPORT — CRACKED (CARGO BAY) · airframe 4,838 hrs · 5,037 cycles

RIGHT AND LEFT CARGO FLOOR SUPPORT ANGLES ARE CRACKED AT FS 621.0. REPAIRED RT AND LT SIDE CARGO FLOOR SUPPORT ANGLES IAW REO 601R-53-61-117 REV A.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 4,609 hrs · 4,806 cycles

PILOTS WINDSHIELD SHATTERED. REPLACED WINDSHIELD.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 4,403 hrs · 4,403 cycles

CARGO SMOKE MESSAGE. FALSE WARNING. DEFERRED CARGO FIRE EXTINGUISHERS.

Part: SMOKE — DETECTED (COCKPIT) · airframe 4,016 hrs · 4,163 cycles

SMOKE IN COCKPIT. RAN ENGINES TO BURN RESIDUAL OIL FROM AIRCRAFT PACKS. SMOKE AND FUMES CEASED.

Part: SMOKE — DETECTED (COCKPIT) · airframe 4,015 hrs · 4,162 cycles

SMOKE IN COCKPIT AND CABIN WHEN BLEED AIR TRANSFERRED TO APU. DEFERRED THE APU PER MEL.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 3,993 hrs · 4,139 cycles

FS 718.00 LEFT AND RIGHT SIDES, AFT DOUBLERS CRACKED BETWEEN STRINGERS 11 AND 12. FS 718.00 LEFT AND RIGHT SIDES AFT DOUBLERS REPLACED IAW REO 601R-53-61-192 REV A.

Part: PFCS — MALFUNCTIONED (SPOILER)

CONFIG SPOILER WARNING DURING TAKEOFF.. REPLACED THE RIGHT SPOILERON PCU.

Part: VALVE — MALFUNCTIONED (LT ENGINE)

LEFT ENGINE COWL ANTI-ICE MESSAGE. REPLACED COWL ANTI-ICE VALVE.

Part: LIGHT — INOPERATIVE (ROW 8)

FLOOR PATH EMERGENCY LIGHTS ARE INOPERABLE FROM ROW 8 AFT. REPLACED FLOOR LIGHTING.

Part: FLAP — FAILED (RT TE FLAP)

FLAP FAIL ON APPROACH 19 DEGREES. REMOVED AND REPLACED RT OUTBOARD FLAP INBOARD ACTUATOR.

Part: CONTROL HANDLE — FAILED (TE FLAPS)

FLAP FAIL ON APPROACH 19 DEGREES. REMOVED AND REPLACED FLAP CONTROL HANDLE.

Part: ACTUATOR — FAILED (LT TE FLAP)

FLAPS FAILED ON APPROACH AT 19 DEGREES. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATORS.

Part: ACTUATOR — FAILED (LT TE FLAP)

FLAP FAIL ON APPROACH AT 19 DEGREES. REMOVED AND RELACED LT OUTBOARD FLAP INBOARD ACTUATOR.

Part: FECU — FLAP FAIL (TE FLAPS)

FLAP FAIL ON APPROACH 19 DEGREES. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT (FECU).

Part: WIRE HARNESS — DAMAGED (LT TE FLAP)

WHEN FLAPS WERE SELECTED TO 45 DEGREES FLAP FAIL CAUTION MESSAGE ILLUMINATED AT 32 DEGREES. REMOVED AND REPLACED LEFT WING BPSU WIRING HARNESS. CHECKED TORQUE OF FLAP SYSTEM RIGGED FLAP SYSTEM.

Part: ACTUATOR — FAILED (LT TE FLAP)

FLAPS FAILED 42 DEGREES ON APPROACH. REMOVED AND REPLACED BOTH LEFT INBOARD FLAP ACTUATORS (FAILED TORQUE CHECK).

Part: BPSU — FAILED (LT TE FLAP)

FLAPS FAIL MESSAGE. REPLACED THE LT BPSU.

Part: BPSU — MALFUNCTION (TE FLAPS)

FLAPS FAIL MESSAGE. REPLACED THE LEFT AND RIGHT BPSU.

Part: LATCH — OUT OF ADJUST (PAX DOOR)

WHILE CLIMBING THROUGH 23,000, PAX DOOR LATCH CAUTION AND PAX DOOR EMERGENCY WARNING ILLUMINATED. AIRCRAFT WAS DIVERTED TO SDF AND THEN FERRIED TO CVG WHERE THE UPPER CAMS AND CAM PROX SENSOR TARGETS WERE ADJUSTED. ALSO, CHECKED RIIGGING OF ENTIRE PAX DOOR.

Part: ACTUATOR — FAILED (RT TE FLAP)

FLAPS FAILED AT 17 DEGREES. REPLACED RIGHT HAND OUTBOARD FLAP ACTUATOR.

Part: BPSU — FAILED (LT TE FLAP)

FLAPS FAILED IN FLIGHT AT ZERO DEGREES. REPLACED LEFT BPSU.

Part: BPSU — MALFUNCTIONED (LT TE FLAP)

FLAPS FAILED WHEN SELECTED FOR LANDING. COULD NOT DUPLICATE PROBLEM. REPLACED LT BPSU FOR TROUBLESHOOTING.