N785CA

Part: BULKHEAD — CRACKED (ZONE 200) · airframe 24,894 hrs · 22,036 cycles

FOUND REAR PRESSURE BULKHEAD CRACKED ABOVE CARGO DOOR TRACK. REPAIRED CRACK ABOVE CARGO DOOR TRACK IAW REO 601R-53-61-1541.

Part: BULKHEAD — CRACKED (ZONE 200) · airframe 24,894 hrs · 22,036 cycles

FOUND REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL ATTACHMENT FITTING. REPAIRED CRACK ON REAR PRESSURE BULKHEAD AT LINTEL FITTING IAW REO 601R-53-61-1230 AND REO 601R-53-61-3460.

Part: FUEL CONTROL — FAILED (NR 2 ENGINE) · airframe 23,168 hrs · 20,627 cycles

ON APPROACH, NR2 ENGINE ROLLED BACK TO SHUTDOWN WHILE BEING VECTORED FOR THE APPROACH. EMERGENCY DECLARED, ACFT LANDED SAFELY. REMOVED AND REPLACED RT ENGINE FUEL CONTROL.

Part: PUMP — FAILED (RT ENGINE) · airframe 23,168 hrs · 20,627 cycles

ON APPROACH, NR 2 ENGINE ROLLED BACK TO SHUTDOWN WHILE BEING VECTORED FOR THE APPROACH. EMERGENCY DECLARED, ACFT LANDED SAFELY. REMOVED AND REPLACED RT ENG FUEL PUMP.

Part: SKIN — DAMAGED (LT WING) · airframe 23,029 hrs · 20,526 cycles

LT WING LOWER DRAIN ATTACHMENT HOLE JUST AFT OF PANEL 510 AB, BETWEEN WS 0.00 AND WS 22.50, AFT SCREW HOLE IS DAMAGED. REPAIRED DAMAGE PER EA 10-57-02437.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 23,029 hrs · 20,526 cycles

ENGINE CENTER SUPPORT BEAM IS CRACKED AT RBL 8.5 AT SENSING LOOP SUPPORT BRACKET. REPAIRED ENGINE SUPPORT BEAM PER CRJ REO 601R-53-61345 REV F.

Part: SKIN — DAMAGED (RT WING) · airframe 23,029 hrs · 20,526 cycles

RT WING LOWER DRAIN ATTACHMENT HOLE JUST FWD OF PANEL 640 DB AT WS 85.50 AFT SCREW HOLE IS DAMAGED. REPAIRED DAMAGE PER EA10-57-02437.

Part: SKIN — DAMAGED (ZONE 500) · airframe 23,029 hrs · 20,526 cycles

LT WING LOWER DRAIN ATTACHMENT HOLE JUST FWD OF PANEL 540 AB, AT WS 67.75 AFT SCREW HOLE IS DAMAGED. REPAIRED DAMAGE PER EA 10-57-02437.

Part: SKIN — DAMAGED (LT WING) · airframe 23,029 hrs · 20,526 cycles

LT WING LOWER DRAIN ATTACHMENT HOLES JUST FWD OF PANEL 540AB AT WS.0.00, FWD AND AFT SCREW HOLES ARE DAMAGED. REPAIRED DAMAGE PER EA10-57-02437.

Part: CHECK VALVE — FAILED (RT AGB) · airframe 22,102 hrs · 19,779 cycles

DURING CLIMBOUT FROM CVG RT ENG HIGH OIL TEMP. EMERGENCY DECLARED, ACFT RETURNED BACK TO CVG AND LANDED SAFELY. FOUND RT ENG AGB OVER SERVICED WITH OIL. REMOVED AND REPLACED RT ENG BYPASS CHECK VALVE. (S)

Part: SECU — FAULTY (E&E BAY) · airframe 189 hrs · 18,821 cycles

FLIGHT 5151 - ON TAKEOFF ROLL RECEIVED CONFIG SPOILERS MESSAGE WITH FLIGHT SPOILER MESSAGE. ABORTED TAKEOFF AND RETURNED TO GATE SAFELY. REMOVED AND REPLACED NR 2 SECU.

Part: TRANSDUCER — FAULTY (NLG) · airframe 20,552 hrs · 18,528 cycles

FLIGHT 5350 - RECEIVED STEERING INOP CAUTION. RAN QRH, DIVERTED TO PHL, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. A/C WAS TUGGED FROM RUNWAY. REPLACED RIGHT NOSE STEERING RVDT.

Part: BPSU — FAULTY (T/E FLAP) · airframe 20,466 hrs · 18,457 cycles

FLIGHT 5699 - RECEIVED FLAP CAUTION MESSAGE. LANDED WITHOUT INCIDENT. REPLACED LEFT BPSU. NO FURTHER DEFECTS.

Part: SERVO — FAULTY (AUTOPILOT SYS) · airframe 19,256 hrs · 17,841 cycles

FLIGHT 5042 - AFTER TAKEOFF ENGAGED AUTO PILOT AT 12000 FT, AT 20000 FT FELT SLIGHT VIBRATION AND YAW MOTION. EICAS SHOWED AILERON FLUTTERING. REPLACED AILERON SERVO, INSPECTED AILERON AND RUDDER CONTROL SYSTEMS AND PERFORMED AUTO PILOT OPERATIONAL CHECKS. NO FURTHER DEFECTS.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 19,065 hrs · 17,337 cycles

FLIGHT 5284 - F/O WINDSHIELD CRACKED. REMOVED AND REPLACED RIGHT WINDSHIELD.

Part: PDU — FAULTY (TE FLAPS) · airframe 18,933 hrs · 17,237 cycles

FLIGHT 5206 - RECEIVED FLAP FAIL MESSAGE AT 8 DEGREES. LANDED WITHOUT INCIDENT. REPLACED PDU.

Part: FLAP — MALFUNCTIONED (WING) · airframe 16,892 hrs · 15,578 cycles

FLIGHT 5011 - DURING YUL APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE. 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: AMPLIFIER — FAULTY (LT ENGINE) · airframe 16,859 hrs · 15,552 cycles

FLIGHT 9495 - AFTER TAKEOFF AND DURING CLIMBOUT OF CVG ENCOUNTERED SURGING OF LEFT ENGINE N1 AND N2, FLIGHT RETURNED TO CVG. REPLACED THE LEFT SPEED CONTROL AMPLIFIER.

Part: CONNECTOR — LOOSE (THRUST REVERSER) · airframe 16,547 hrs · 15,285 cycles

FLIGHT 5852 - RT THRUST REVERSER WARNING. SECURED CANNON PLUGS ON THE STOW, DEPLOY AND PDU SWITCHES. OPERATIONAL CHECKS NORMAL.

Part: VENT — OBSTRUCTED (PAX DOOR) · airframe 15,382 hrs · 14,255 cycles

FLIGHT 5811- CABIN ALTITUDE CAUTION. F/A REPORTS LOUD SQUEAL FROM CABIN DOOR. FOUND DOOR TRIM OBSTRUCTING THE DOOR VENT VALVE, SECURED TRIM. PRESSURE CHECKS SATISFACTORY.

Part: GEARBOX — CRACKED (RT ENG THROTTLE) · airframe 15,197 hrs · 14,089 cycles

WHEN PERFORMING EO 76-011 AD, THE RIGHT ENGINE THROTTLE GEARBOX HOUSING WAS FOUND CRACKED AT THE ATR ATTACH POINT. REMOVED AND INSTALLED A SERVICABLE GEARBOX.

Part: VALVE — FAULTY (ENGINE) · airframe 14,642 hrs · 13,596 cycles

FLT 5372 RECEIVED A LT ENGINE COWL CAUTION DURING CRUISE FLIGHT (IND-JFK), AIRCRAFT DIVERTED TO CVG. REPLACED THE LT ENGINE ANTI-ICE COWL VALVE.

Part: CONTROL HANDLE — MALFUNCTIONED (TE FLAPS) · airframe 14,235 hrs · 13,236 cycles

FLIGHT 4961 FLAPS FAIL CAUTION. REPLACED THE FLAP CONTROL HANDLE.

Part: APU — SMOKE (APU BAY) · airframe 13,971 hrs · 13,014 cycles

FLIGHT 5834 APU SMELLED LIKE FUEL, SMOKE COMING FROM INTAKE. COULD NOT DUPLICATE. INSPECTED APU FOR FUEL LEAKS. NO DEFECTS FOUND.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 13,839 hrs · 12,897 cycles

LOWER NOSE SKIN DAMAGED FORWARD OF FS 280 BETWEEN STRINGERS 25R AND 26R. REPAIRED IAW EA 10-5310-00515.

Part: SKIN — CRACKED (LT WING) · airframe 13,839 hrs · 12,897 cycles

LOWER LEFT HAND WING PLANK CRACK INBOARD OF WS 149.85. REPAIRED IAW REO 601R-57-21-539.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 13,839 hrs · 12,897 cycles

FS 280 IS CORRODED ON FORWARD AFT ANGLES AFT OF CREW ENTRY WAY. REPAIRED IAW REO 601R-53-11-584.

Part: FRAME — CRACKED (FUSELAGE) · airframe 13,839 hrs · 12,897 cycles

RIGHT HAND 718 FRAME CRACKED. REPAIRED IAW EO 53-027.

Part: FRAME — CRACKED (FUSELAGE) · airframe 13,839 hrs · 12,897 cycles

LEFT HAND FUSELAGE 718 CRACKED BETWEEN STRINGER 10 AND 12. REPAIRED IAW EO 53-027.

Part: FRAME — CRACKED (FUSELAGE) · airframe 13,839 hrs · 12,897 cycles

LEFT HAND FS FRAME 621.00 CRACKED. REPAIRED IAW REO 601R-53-61-117.

Part: DETECTOR — MALFUNCTIONED (CARGO SMOKE) · airframe 13,007 hrs · 12,195 cycles

FLIGHT 5731, CARGO SMOKE WARNING. COULD NOT DUPLICATE. FOUND NO DEFECTS, REPLACED DISCHARGED FIRE BOTTLES

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM) · airframe 11,911 hrs · 11,320 cycles

FLIGHT 5291 NR 1 HYDRAULIC SYSTEM LOW PRESSURE WARNING, RESERVOIR INDICATED EMPTY. REPLACED HYDRAULIC SUCTION LINE IN AFT EQUIP BAY.

Part: ELEMENT — CHAFED (LT PYLON) · airframe 10,476 hrs · 10,176 cycles

FLIGHT 5808 LEFT 14TH STAGE BLEED LEAK WARNING. REPLACED BLEED LEAK SENSING ELEMENT IN PYLON.

Part: CONTROLLER — MALFUNCTIONED (ANTI ICE) · airframe 9,578 hrs · 9,450 cycles

FLIGHT 5129 WING OVERHEAT WARNING DURING T/O. REPLACED THE ANTI-ICE CONTROLLER.

Part: WARNING LIGHT — ILLUMINATED (ANTI ICE SYSTEM) · airframe 9,572 hrs · 9,442 cycles

FLIGHT 5298 WING OVERHEAT MESSAGE DURING T/O. DEFERRED MAINT PER MEL.

Part: COMPUTER · airframe 8,192 hrs · 8,240 cycles

FLIGHT 5295 NWS CAUTION MESSAGE AFTER T/O.COULD NOT DUPLICATE. SYSTEM TEST NORMAL.

Part: COMPUTER — MALFUNCTIONED (#2) · airframe 7,523 hrs · 7,619 cycles

FLIGHT 5708 WHEN FLIGHT SPOILERS DEPLOYED, AIRCRAFT ROLLED TO LEFT.REPLACED THE #2 SECU.

Part: CONTROL BOX — MALFUNCTIONED (AVIONICS) · airframe 5,478 hrs · 5,584 cycles

FLIGHT 5648 L/H PITOT HEAT CAUTION MESSAGE.REPLACED THE #1 ADSHC.

Part: ACTUATOR — FAILED (R/H OUTBD) · airframe 4,877 hrs · 4,992 cycles

FLIGHT 5420. FLAPS FAILED AT 23 DEGREES DURING LANDING APPROACH. POST FLIGHT INSP. FOUND R/H OUTBD FLAP TWISTED.REPLACED THE R/H OUTBD FLAP, BOTH FLAP ACTUATORS AND THE FLEX DRIVE SHAFT.

Part: SENSOR — FAULTY (LEFT WIGN) · airframe 4,674 hrs · 4,792 cycles

FLIGHT #5725. DURING CRUISE FLIGHT RECEIVED A FLAP SYSTEM FAIL CAUTION WITH FLAP AT ZERO DEGREE POSITION, CREW DECLARED AN EMERGENCY AND LANDED AT DESTINATION CITY ATW SAFELY.REPLACED THE LEFT BRAKE AND POSITION SENSING UNIT.

Part: LIGHT · airframe 4,597 hrs · 4,709 cycles

FLIGHT #N/A. EMERGENCY CEILING LIGHT AT ROW 13 IS INOPERATIVE.REPLACED THE EMERGENCY FLOOD LIGHT BULB AT ROW 13.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,471 hrs · 4,558 cycles

LEFT HAND EMERGENCY LIGHT IS INOPERABLE. REPLACED THE LIGHT BULB.

Part: POWER UNIT — MALFUNCTIONED (WING) · airframe 4,273 hrs · 4,345 cycles

FLAPS FAIL CAUTION MESSAGE. REPLACED THE PDU.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT) · airframe 4,242 hrs · 4,307 cycles

LEFT WINDOW HEAT CAUTION MESSAGE. REPLACED THE LT WINDOW HEAT CONTROLLER.

Part: SPOILER — BROKEN (RIGHT) · airframe 3,987 hrs · 4,069 cycles

WHEN FLAP SELECTED TO 45 DEGGREES, THE AIRCRAFT ROLLED RIGHT. POST FLIGHT INSP FOUND RT FLIGHT SPOILER BROKEN. REPLACED FLIGHT SPOILER.

Part: ACTUATOR — MALFUNCTIONED (VERTICAL STAB) · airframe 3,983 hrs · 4,065 cycles

CONFIG STAB AND CONFIG TRIM WARNING. REPLACED THE HSTA.

Part: SWITCH — MALFUNCTIONED (APU) · airframe 3,859 hrs · 3,941 cycles

APU OIL PRESSURE MESSAGE. REPLACED APU LOW OIL PRESSURE SWITCH.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,849 hrs · 3,930 cycles

EMERGENCY LIGHTS AFT OF ROW 9 ARE INOPERABLE. AFTER AIRCRAFT WARMED, COULD NOT DUPLICATE, EMERGENCY LIGHTS OPERATE NORMAL.

Part: WARNING LIGHT — ILLUMINATED (AOA HEAT) · airframe 3,558 hrs · 3,633 cycles

LEFT AOA HEAT CAUTION MESSAGE. RESET CIRCUIT BREAKERS, SYSTEM FUNCITONS NORMAL.

Part: LEVER — FAILED (INSTRUMENT PANEL) · airframe 3,290 hrs · 3,382 cycles

FLAPS FAILED MESSAGE. REPLACED THE FLAP SELECTOR LEVER.

Part: WARNING LIGHT — ILLUMINATED (TE FLAP) · airframe 2,211 hrs · 2,267 cycles

FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.

Part: CIRCUIT BREAKER — TRIPPED (RT AOA)

DURING CLIMBOUT FROM CVG, THE RIGHT AOA CAUTION MESSAGE ACTIVAGED. AIRCRAFT RETURNED TO THE FIELD. CYCLED THE CIRCUIT BREAKER FOR THE RIGHT AIR DATA SENSING HEATER CONTROLLER.

Part: WARNING — ACTIVATED (ANTI ICE SYS)

DURING CLIMB-OUT FROM CVG, THE ANIT-ICE WARNING ACTIVATED, CREW FOLLOWED QRH PROCEDURE, MESSAGE CLEARED AFTER CLOSING 14TH STAGE BLEED AIR. PERFORMED AN ELECTRICAL CHECK OF LEFT AND RIGHT 14TH STAGE LOOPS AND PERFORMED AN OPERATIONAL CHECK, NO DEFECTS NOTED.

Part: WARNING — ACTIVATED (ANTI ICE DUCT)

ANTI ICE DUCT WARNING. COULD NOT DUPLICATE. AIRCRAFT RETURNED TO SERVICE.

Part: OVERHEAT WARNING — ACTIVATED (CARGO FAN)

CARGO OVERHEAT WARNING. DEFERRED CARGO FAN.

Part: FECU — MALFUNCTIONED (T/E FLAPS)

FLAPS FAIL MESSAGE. REPLACED FECU.