N969CA

Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 34,388 hrs · 29,779 cycles

ON APPROACH INTO ATW RECEIVED FLAPS FAIL CAUTION MSG AT 8 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED FLAP CONTROL HANDLE. NO FURTHER DEFECTS NOTED.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 33,702 hrs · 29,155 cycles

ON STRINGER STR 3, 2.5 INCHES AFT FROM FS 280 BULKHEAD THERE IS A VERTICAL CRACK ON STRINGER DOUBLER. REMOVED AND INSTALLED A SERVICEABLE STRINGER 3 DOUBLER AT FS 280.00 AND FS 295.00 IAW SRM SOLID RIVETS 51-42-06, HI LITES 51-42-20 AND EO DRW 601R31522 AND MOD SUM TC 601R17033.

Part: FLOOR SKIN — CRACKED (FUSELAGE) · airframe 33,702 hrs · 29,155 cycles

PRESSURE FLOOR SKIN CRACKED AT FS 460, BL 0.0-RBL 9 APPROX 2 INCHES LONG. REMOVED DAMAGE FROM PRESSURE FLOOR SKIN AT FS 460 AND REPAIRED IAW BOMBARDIER REO TEMPORARY REPAIR 601R-53-41-103.

Part: STRUCTURE — DAMAGED (LT WING) · airframe 33,702 hrs · 29,155 cycles

LT WING FUEL DRAIN AFT HOLE AT WS 88.50 IS MISDRILLED. COMPLIED WITH REO 601R-57-21-1485 ON WS 88.50 LT BY REAMING AND INSTALLING FREEZE PLUG.

Part: STRUCTURE — DAMAGED (RT WING) · airframe 33,702 hrs · 29,155 cycles

RIGHT WING FUEL DRAIN AFT HOLE AT WS 48.00 IS MISDRILLED. COMPLIED WITH REO R01R-57-21-1485 ON WS 48.00 RT BY REAMING AND INSTALLING A FREEZE PLUG.

Part: SKIN — CRACKED (RT WING) · airframe 33,702 hrs · 29,155 cycles

RIGHT WING LOWER WINGPLANK DRAIN HOLE AT WS 65.75 SHOWS CRACK INDICATION AS MARKED VERFIED BY LEVEL 2 NDT. REPAIRED RT WING PLANK AT W/S 65.75 ROUTING OUT DAMAGE IAW REO 601R-57-21-1487.

Part: SKIN — CRACKED (RT WING) · airframe 33,702 hrs · 29,155 cycles

RIGHT WING LOWER WINGPLANK DRAIN HOLE AT WS 85.50 SHOWS CRACK INDICATION AS MARKED. REPAIRED RT WING PLANK AT WS 85.50 BY ROUTING OUT DAMAGE IAW 601R-57-21-1487.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,701 hrs · 29,155 cycles

FUSELAGE SKIN DAMAGE CAUSED BY PAX DOOR AFT-LOWER LATCH PIN AT FS 349 STR 15-16. REPAIRED BY REMOVING DAMAGE IAW REO 601R-53-21-186.

Part: SKIN — DENTED (FUSELAGE) · airframe 33,701 hrs · 29,155 cycles

FUSELAGE SKIN DAMAGE CAUSED BY PAX DOOR FWD-LOWER LATCH PIN AT FS 310 STR 16-17. REPAIRED BY REMOVING DAMAGE AND INSTALLING DOUBLER/TRIPLER IAW REO 601R-53-21-180 AND 601R-53-21-160.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 33,702 hrs · 29,155 cycles

FLOOR SEAT TRACK AT LBL 18 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW CRJ AMM TASK 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 33,702 hrs · 29,155 cycles

FLOOR SEAT TRACK L2 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW CRJ AMM TASK 53-01-11-400-802.

Part: FRAME — CRACKED (FUSELAGE) · airframe 32,603 hrs · 28,107 cycles

CRACK FOUND ON LEFT FS 640.00 FUSELAGE FRAME AT STRINGER 9L. COMPLIED WITH REO 601R-53-61-557. REMOVED DAMAGED SECTION OF 640 FRAME AND INSTALLED A DOUBLER AND FILLER.

Part: FITTING — CRACKED (FUSELAGE) · airframe 32,344 hrs · 27,884 cycles

REAR PRESSURE BULKHEAD LINTLE FITTING IS CRACKED. REPAIRED IAW REO 601R-53-61-1230.

Part: ENGINE — SURGES (LEFT) · airframe 31,225 hrs · 26,889 cycles

ON T/O FROM DTW LEFT ENGINE SURGE, NORMAL THRUST T/O PERFORMED. EMERGENCY DECLARED, A/C RETURNED TO DTW LANDED SAFELY. TRANSFERRED TO DEFERRED LIST PER MEL 76-11-01.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 30,329 hrs · 26,125 cycles

RIGHT CAP ANGLE CRACKED IN RADIUS AT FS 559, AT BL 18. CUT OUT DAMAGED CAP ANGLE AND INSTALLED NEW CAP ANGLE SECTION PER REO 601R- 53-41-260.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,329 hrs · 26,125 cycles

RIGHT FRAME CAP ANGLE BEND RADIUS AT FS 559.00 CRACKED AT BL 18.00. REPAIRED CRACK AT RIGHT FS 559.00 IAW REO 601R-53-41-260.

Part: FRAME — CRACKED (FUSELAGE) · airframe 30,329 hrs · 26,125 cycles

LEFT FRAME CAP ANGLE BEND RADIUS AT FS 559.00 CRACKED AT BL 18.00. REPAIRED CRACK AT LEFT FS 559.00 IAW REO 601R-53-41-260.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,329 hrs · 26,125 cycles

FWD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE CUTOUT. CUT OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW REO 601R-53-11-593 AND EA 10-5311-02720.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 29,067 hrs · 25,077 cycles

FLT 4993 - ON APPROACH INTO JFK A/C BECAME UPRESSURIZED AT 4,000 FT. A/C LANDED SAFELY. REMOVED AND REPLACED CABIN PRESSURE SELECTOR PANEL.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (RT WING) · airframe 28,955 hrs · 25,003 cycles

FLIGHT 5652 - RECEIVED RIGHT WING ANTI-ICE CAUTION MESSAGE ON TAKEOFF. REJECTED TAKEOFF. RETURNED TO GATE WITHOUT INCIDENT. PERFORMED HIGH POWER RUNS. COULD NOT DUPLICATE PROBLEM. COMPLIED WITH RTO INSPECTION. NO FURTHER DEFECTS.

Part: PRESSURE SWITCH — FAILED (ANTI-ICE SYSTEM) · airframe 28,885 hrs · 24,947 cycles

FLIGHT 5516 - RIGHT WING A/I CAUTION MESSAGE ON T/O ROLL, JUST BEFORE 100 KTS. ABORTED TAKEOFF SAFELY. REMOVED AND REPLACED RIGHT PRESSURE SWITCH.

Part: FLAP — MALFUNCTIONED (WING) · airframe 28,881 hrs · 24,943 cycles

FLIGHT 4963 - RECEIVED FLAP FAIL CAUTION MESSAGE. ABORTED APPROACH, DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. COMPLIED WITH SI-2-27I0001 FLAP CAUTION MESSAGE "FIRST EVENT" MAINTENANCE ACTION, FLAP SYSTEM WAS RESET WITH NO FURTHER MESSAGES.

Part: PRIORITY VALVE — FAULTY (NLG) · airframe 28,642 hrs · 24,758 cycles

FLIGHT 5097 - RECEIVED GEAR DISAGREE WARNING MESSAGE. RETURNED TO GRR, LANDED WITHOUT INCIDENT. REPLACED NLG PRIORITY VALVE. NO FURTHER DEFECTS.

Part: SELECTOR VALVE — FAULTY (NLG) · airframe 28,635 hrs · 24,750 cycles

FLIGHT 5313 - RECEIVED GEAR DISAGREE MESSAGE. NOSE GEAR DID NOT RETRACT. PERFORMED QRH, DECLARED EMERGENCY, RETURNED TO IAD. REPLACED NLG SELECTOR VALVE. NO FURTHER DEFECTS.

Part: PRIORITY VALVE — FAULTY (MLG) · airframe 28,430 hrs · 24,591 cycles

RECEIVED NOSE GEAR DISAGREE MESSAGE DURING RETRACTION. DECLARED EMERGENCY, RETURNED TO FSD, LANDED WITHOUT INCIDENT. REPLACED MAIN GEAR PRIORITY VALVE. NO FURTHER DEFECTS.

Part: PRIORITY VALVE — FAULTY (NLG) · airframe 28,430 hrs · 24,591 cycles

FLIGHT 5690 - RECEIVED NOSE GEAR DISAGREE MESSAGE DURING RETRACTION. DECLARED EMERGENCY, RETURNED TO FSD, LANDED WITHOUT INCIDENT. REPLACED NOSE GEAR PRIORITY VALVE. NO FURTHER DEFECTS.

Part: SELECTOR VALVE — FAULTY (NLG) · airframe 28,333 hrs · 24,519 cycles

FLIGHT 9484 - GEAR DISAGREE ON FINAL APPROACH NOSE GEAR WOULD NOT COME DOWN. FOLLOWED QRH, LOWERED GEAR MANUALLY AND LANDED SAFELY. REMOVED AND REPLACED NLG SELECTOR VALVE.

Part: ANTI-ICE SYSTEM — WARNING MESSAGE · airframe 28,310 hrs · 24,503 cycles

FLIGHT 4945 - AFTER SETTING T/O THRUST FOR T/O, WING AND COWL ANTI-ICE SYSTEM ON, RECEIVED RIGHT WING ANTI-ICE CAUTION MESSAGE. ABORTED TAKEOFF BELOW 80 KTS. TRANSFERRED TO DEFERRED LIST PER MEL 30-12-03-1.

Part: ENGINE — LEAKING (RIGHT) · airframe 27,778 hrs · 24,073 cycles

FLIGHT 9432 - RECEIVED RIGHT ENGINE OIL PRESSURE WARNING MESSAGE. DIVERTED TO PIT, LANDED WITHOUT INCIDENT. REPLACED RIGHT ENGINE. NO FURTHER DEFECTS.

Part: SKIN — CRACKED (ENGINE BEAM) · airframe 27,344 hrs · 23,733 cycles

ENGINE BEAM UPPER CENTER SKIN IS CRACKED ON AFT SIDE FS 640 BETWEEN RBL 0 AND RBL 9 AT FIRE LOOP FASTENER HOLE. REPAIRED UPPER AND LOWER ENGINE BEAM CENTER SKINS WITH A PERMANENT REPAIR PER REO 601R-53-61-345 REV D.

Part: WEB — CRACKED (RT MLG WW) · airframe 27,344 hrs · 23,733 cycles

WHEEL WELL AFT WEB IS CRACKED AT FS 559.00 BETWEEN RBL 9 AND 18 AT RIGHT AILERON BELLCRANK ATTACH HOLES. CUT OUT DAMAGE AND INSTALLED A PERMANENT REPAIR DOUBLER PER COMAIR SR10-5341-0001 REV (A) SECTION 1.

Part: COMPUTER — MALFUNCTIONED (FUEL SYSTEM) · airframe 26,975 hrs · 23,440 cycles

ON TAKEOFF RIGHT SIDE FUEL QTY AND TOTAL FUEL QTY IND AMBER, AUTO CROSS FLOW INHIBIT STATUS MSG. FLIGHT RETURNED TO ACY AND LANDED SAFELY. DEFERRED EICAS FUEL QUANTITY READOUTS (LEFT RIGHT AND TOTAL) PER MEL 28-41-01-2.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 26,783 hrs · 23,282 cycles

FLIGHT 5375 - FLAPS FAILED AT ZERO DEGREES PRIOR TO LANDING. A/C 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: ANTI-ICE VALVE — FAULTY (RT ENGINE) · airframe 26,428 hrs · 23,014 cycles

FLIGHT 5111- ON TAKEOFF ROLL, RECEIVED RIGHT ENGINE COWL ANTI-ICE CAUTION MESSAGE. REMOVED AND REPLACED RIGHT COWL ANTI-ICE PRSOV.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 26,427 hrs · 23,011 cycles

FLIGHT 9467 - LEFT WINDSHIELD SHATTERED FOLLOWED BY LEFT WINDSHIELD HEAT MESSAGE. REPLACED LEFT WINDSHIELD.

Part: COMPUTER — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 26,344 hrs · 22,947 cycles

FLIGHT 5358 - DURING TAKEOFF ROLL RECEIVED AN ANTI-ICE CAUTION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED AN OPERATIONAL CHECK OF THE LEFT AND RIGHT ANTI-ICE SYSTEM, NO DISCREPANCIES NOTED.

Part: ANTI-ICE SYSTEM — WARNING MESSAGE (RT WING) · airframe 24,837 hrs · 21,736 cycles

FLIGHT 4969 - DURING TAKEOFF ROLL RECEIVED A RIGHT WING ANTI-ICE CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT RETURNED TO THE GATE. PERFORMED AN OPERATIONAL CHECK OF THE WING ANTI-ICE SYSTEM, DISCREPANCY COULD NOT BE DUPLICATED.

Part: ANTI-ICE SYSTEM — WARNING LIGHT · airframe 24,594 hrs · 21,529 cycles

FLIGHT 5333 - DURING TAKEOFF ROLL RECEIVED AN ANTI-ICE CAUTION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. DEFERRED WING ANTI-ICE SYSTEM NORMAL CONTROL.

Part: FLAP — MALFUNCTIONED (WING) · airframe 24,500 hrs · 21,449 cycles

FLIGHT 5108 - DURING YYZ APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES, CREW DECLARED AN EMERGENCY, ABORTED FIRST APPROACH AND 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: IDG — MALFUNCTIONED (LEFT) · airframe 24,014 hrs · 21,055 cycles

FLIGHT 5817- LEFT IDG CAUTION. REPLACED THE IDG.

Part: ACTUATOR — FAULTY (RT TE FLAP) · airframe 23,045 hrs · 21,037 cycles

FLIGHT 5675 - DURING CLIMB-OUT OF CVG RECEIVED A FLAP FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT INBOARD FLAP INBOARD ACTUATOR.

Part: ACTUATOR — FAULTY (RT TE FLAP) · airframe 23,045 hrs · 21,037 cycles

FLIGHT 5675 - DURING CLIMB-OUT OF CVG RECEIVED A FLAP FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE RIGHT INBD FLAP OUTBD ACTUATOR.

Part: PDU — FAULTY (TE FLAPS) · airframe 23,045 hrs · 21,037 cycles

FLIGHT 5675 - DURING CLIMB-OUT OF CVG RECEIVED A FLAP FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE POWER DRIVE UNIT.

Part: TRANSMITTER — FAULTY (RT TE FLAP) · airframe 23,045 hrs · 21,037 cycles

FLIGHT 5675 - DURING CLIMB-OUT OF CVG RECEIVED A FLAP FAIL CAUTION MESSAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE FLAP POSITION TRANSMITTER.

Part: FLAP SYSTEM — WARNING LIGHT · airframe 23,981 hrs · 21,027 cycles

FLIGHT 5709 - FLAPS FAIL CAUTION. CHECKED RIGGING OF LT AND RT BPSU.

Part: FLAP SYSTEM — WARNING LIGHT · airframe 23,981 hrs · 21,027 cycles

FLIGHT 5005- FLAPS FAIL CAUTION. INSPECTED FLAPS IAW AD 98-20-01. NO DEFECTS NOTED.

Part: DRIVE SHAFT — DIRTY (T/E FLAP) · airframe 23,935 hrs · 20,991 cycles

FLIGHT 5343 - FLAPS FAIL CAUTION. CLEANED AND LUBRICATED FLAP FLEX DRIVE SHAFTS.

Part: FLEX COUPLING — LACK OF LUBE (TE FLAPS) · airframe 23,935 hrs · 20,991 cycles

FLIGHT 5888 - FLAPS FAIL CAUTION. CLEANED AND LUBRICATED THE FLAP FLEX DRIVE SHAFTS.

Part: ACTUATOR — UNRELIABLE (RT TE FLAPS) · airframe 23,869 hrs · 20,934 cycles

FLIGHT 5698 - FLAPS FAIL CAUTION. REPLACED THE RT INBD FLAP ACTUATOR.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 23,845 hrs · 20,916 cycles

FLIGHT 5883 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 23,594 hrs · 20,689 cycles

FLIGHT 5605 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.

Part: CONTROL UNIT — ACTIVE (TE FLAPS) · airframe 22,359 hrs · 19,613 cycles

FLIGHT 5142 FLAPS FAIL CAUTION. REPLACED THE FECU.

Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 22,334 hrs · 19,589 cycles

FLIGHT 5727 FLAPS FAIL CAUTION. RESET FLAP SYSTEM, FOUND NO DEFECTS, DEFERRED MAINT PER AD 98-20-01.

Part: LANDING GEAR — LACK OF LUBE · airframe 21,878 hrs · 19,196 cycles

FLIGHT 4987 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. EXTENSION AND RETRACTION CHECKS WERE SATISFACTORY. CLEAN AND LUBED LANDING GEAR.

Part: PITOT LINE — CONTAMINATED · airframe 20,716 hrs · 18,191 cycles

FLIGHT 4990 EFIS COMP MON MESSAGE DURING T/O. REMOVED WATER FROM PITOT STATIC SYSTEM.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 20,248 hrs · 17,795 cycles

FLIGHT 5495 FLAPS FAIL CAUTION MESSAGE. COULD NOT DUPLICATE. C/W EO 27-046 OPERATION NORMAL.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,616 hrs · 17,312 cycles

CORROSION ON CARGO FLOOR CAP AT LBL 9. REMOVED AND REPLACED FLOORBEAM CAP AT LBL 9, IAW CRJ SRM 51-42-06, 51-42-13, 51-42-21, 51-42-34.

Part: PUMP — DEFECTIVE (HYD SYSTEM) · airframe 19,561 hrs · 17,268 cycles

FLIGHT 5187 GEAR DISAGREE WARNING. REPLACED THE 3A HYDRAULIC PUMP.

Part: CONTROL UNIT — UNRELIABLE (AVIONICS) · airframe 17,826 hrs · 15,910 cycles

FLAPS FAIL MESSAGE WHEN TRANSFERRING POWER TO NR 2 GENERATOR. REPLACED THE FECU.

Part: RESERVOIR — MALFUNCTIONED (HYD SYSTEM) · airframe 17,103 hrs · 15,316 cycles

FLIGHT 5647 GEAR DISAGREE WARNING AFTER T/O. REPLACED HYDRAULIC RESERVOIR NR 3.

Part: DUCT — LOOSE (ACM) · airframe 16,373 hrs · 14,730 cycles

FLIGHT 5090 A (POP) SOUND WAS HEARD AND AIRCRAFT LOST PRESSURIZATION. REINSTALLED LOOSE ACM DUCT ON LEFT WATER SEPERATOR.

Part: TERMINAL · airframe 16,097 hrs · 14,521 cycles

FLIGHT 5438 ANTI-ICE DUCT WARNING, R/H WING INDICTED.RECONNECTED LOOSE WIRE TERMINAL AT PB8WK.

Part: ROD — BROKEN (CABIN DOOR) · airframe 14,163 hrs · 12,938 cycles

FLIGHT 5037 AIRCRAFT WOULD NOT PRESSURIZE AFTER T/O.REPLACED BROKEN ROD ASSY AT DOOR VENT VALVE.

Part: VALVE — MALFUNCTIONED (NLG) · airframe 13,519 hrs · 12,405 cycles

FLIGHT 5354 NOSE L/G DOOR DISAGREE MESSAGE DURING APPROACH.REPLACED THE NLG PRIORITY VALVE.

Part: LAMP — BURNED OUT (R/H EXT) · airframe 12,372 hrs · 11,434 cycles

R/H EXTERIOR EMERGENCY LIGHT INOP.REPLACED LIGHT BULB.

Part: LAMP — BURNED OUT (LAMP) · airframe 12,294 hrs · 11,353 cycles

FLIGHT #5497. ONE CABIN EMERGENCY LIGHT IS INOPERABLE.REPLACED LIGHT BULB.

Part: ACTUATOR — FAULTY (EMPENAGE) · airframe 12,047 hrs · 11,148 cycles

FLIGHT #5871. DURING TAXI OUT RECEIVED A STABILIZER CHANNEL #1 INOPERATIVE MESSAGE, AIRCRAFT RETURNED TO THE GATE.REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR.

Part: MOTOR — FAULTY (EMPENAGE) · airframe 12,047 hrs · 11,148 cycles

FLIGHT #5871. DURING TAXI OUT RECEIVED A STABILIZER CHANNEL #1 INOPERATIVE MESSAGE, AIRCRAFT RETURNED TO THE GATE.REPLACED THE HORIZONTAL STABILIZER MOTOR CONTROL UNIT.

Part: VANE — CHAFED (R/H INBOARD FLAP) · airframe 11,965 hrs · 11,073 cycles

R/H INBOARD FLAP INBOARD VANE CAP IS CHAFED BEYOND LIMITS PER S/B 601R-57-022.REMOVED R/H INBOARD FLAP VANE CAP AND INSTALLED NEW SERVICEABLE CAP P/N 601R4303S-54S I/A/W AERODESIGN ENGINEERING REPORT NUMBER 1286-1 REV A.

Part: THRESHOLD — CORRODED (310.00) · airframe 11,964 hrs · 11,073 cycles

THE THRESHOLD/SILL PANEL FORWARD OF THE SERVICE DOOR IS CORRODED.REMOVED CORRODED THRESHOLD AND REPLACED WITH FABED THRESHOLD I/A/W WVAC EO 601R-53-2716.

Part: THRESHOLD — CORRODED (FS 310.00) · corrosion level 2 · airframe 11,964 hrs · 11,073 cycles

THE THRESHOLD/SILL PANEL FORWARD OF THE SERVICE DOOR IS CORRODED.REMOVED CORRODED THRESHOLD AND REPLACED WITH FABED THRESHOLD I/A/W WVAC EO 601R-53-2716.

Part: ANGLE — CORRODED (F.S. 310.00) · airframe 11,964 hrs · 11,073 cycles

THE THRESHOLD SUPPORT ANGLE AT THE PASSENGER DOOR IS CORRODED.REMOVED CORRODED THRESHOLD SUPPORT ANGLE. FABED NEW THRESHOLD SUPPORT ANGLE AND INSTALLED I/A/W WVAC EO 601R-53-2717.

Part: ANGLE — CRACKED (FS 280.00) · airframe 11,964 hrs · 11,073 cycles

THE VERTICAL J ANGLE CLIP LOCATED INSIDE OF CBP1 AT LBL 9 L/H SIDE WAS FOUND CRACKED.REMOVED AND REPLACED VERTICAL J ANGLE CLIP INSIDE OF CBP1 WITH NEW ANGLE P/N 600-34017-723S I/A/W WVAC E.O. 601R-53-2720.

Part: ANGLE — CORRODED (FS 280.00) · corrosion level 2 · airframe 11,964 hrs · 11,073 cycles

THE FORWARD J ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL9 IS CORRODED.REMOVED AND REPLACED FORWARD J ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL9 WITH NEW P/N 6000-34017-351 ANGLE I/A/W WVAC EO 601R-53-2718.

Part: ANGLE — CORRODED (FS 310.00) · corrosion level 2 · airframe 11,964 hrs · 11,073 cycles

THE THRESHOLD SUPPORT ANGLE AT THE PASSENGER DOOR IS CORRODED.REMOVED CORRODED THRESHOLD SUPPORT ANGLE. FABED NEW THRESHOLD SUPPORT ANGLE AND INSTALLED I/A/W WVAC EO 601R-53-2717.

Part: ANGLE — CRACKED (F.S.280.00) · airframe 11,964 hrs · 11,073 cycles

THE VERTICAL J ANGLE CLIP LOCATED INSIDE OF CBP1 AT LBL9 L/II SIDE WAS FOUND CRACKED.REMOVED AND REPLACED VERTICAL J ANGLE CLIP INSIDE OF DBPJ WITH NEW ANGLE P/N 600-34017-723S I/A/W WVAC EO 601R-53-2720.

Part: ANGLE — CORRODED (F.S.280.00) · airframe 11,964 hrs · 11,073 cycles

THE FORWARD J ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL9 IS CORRODED.REMOVED AND REPLACED FORWARD J ANGLE AT F.S.280.00 BETWEEN LBL9 AND RBL9 WITH NEW P/N 6000-34017-351 ANGLE I/A/W WVAC EO 601R-53-2718.

Part: DOUBLER — CORRODED (F.S.310.00) · airframe 11,964 hrs · 11,073 cycles

THE DOUBLER FORWARD OF THE SERVICE DOOR IS CORRODED P/N 601R38669-49.REMOVED AND REPLACED DOUBLER FORWARD OF SERVICE DOOR WITH NEW P/N 601R38669-49 I/A/W WVAC EO 601R-53-2719.

Part: PUMP · airframe 11,838 hrs · 10,959 cycles

FLIGHT #5995. DURING TAXI OUT FROM CVG THE CIRCUIT BREAKER FOR HYDRAULIC PUMP 3A TRIPPED, AIRCRAFT RETURNED TO THE GATE.TRANSFERRED THE ALTERNATING CURRENT MOTOR PUMP 3A TO THE DEFERRED DISCREPANCY LIST PER MEL.

Part: WEB — CRACKED · airframe 11,722 hrs · 10,826 cycles

DURING COMPLIANCE OF EO 53-021 (VISUAL INSPECTION OF THE ENGINE SUPPORT BEAM) FOUND RIGHT LOWER WEB OF ENGINE SUPPORT BEAM CRACKED.REPAIRED THE ENGINE SUPPORT BEAM IN ACCORDANCE WITH CRJ REO 601-53-61-366 REV B.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,703 hrs · 10,809 cycles

EMERGENCY FLOOR LIGHTS, ROW 2 TO 5, ARE INOPERABLE. REPLACED FLOOR LIGHTS CABLE ASSY.

Part: SENSOR — MALFUNCTIONED (E&E BAY) · airframe 11,678 hrs · 10,787 cycles

RT STATIC, PITOT, AND AOA HET CAUTION MESSAGE. REPLACED THE RT ADSHC.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 11,320 hrs · 10,467 cycles

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

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 11,292 hrs · 10,442 cycles

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

Part: CONTROL UNIT — MALFUNCTIONED (INTERPHONE) · airframe 11,197 hrs · 10,360 cycles

DURING T/O AT 115 KTS, SINGLE CHIME HEARD AND T/O ABORTED. COULD NOT DUPLICATE. REPLACED THE INTERPHONE CONTROL FOR TROUBLESHOOTING.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 11,142 hrs · 10,305 cycles

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

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 10,803 hrs · 10,007 cycles

CARGO DOOR CAUTION MESSAGE. HANDLE WAS NOT CLOSED PROPERLY. CLOSED DOOR AND AIRCRAFT RETURNED TO SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (HS TRIM) · airframe 10,634 hrs · 9,840 cycles

HORIZONTAL STAB TRIM WENT NOSE DOWN UNCOMMANDED. REPLACED THE HSTCU.

Part: FRAME — CRACKED (FUSELAGE) · airframe 10,478 hrs · 9,692 cycles

FRAME FLANGE AT FS 718.0 RHS CRACKED. PERFORMED A MAJOR REPAIR TO CRACKED FRAME FLANGE AT FS 718.0 RHS IAW CRJ REO 601R-53-61-193 REV A.

Part: ACTUATOR — FAILED (TE FLAPS) · airframe 10,474 hrs · 9,688 cycles

FLAPS FAIL CAUTION MESSAGE. REPLACED THE RIGHT INBOARD FLAP ACTUATOR.

Part: BPSU — MALFUNCTIONED (LEFT) · airframe 10,452 hrs · 9,672 cycles

FLAPS FAILED AT 39 DEGREES. REPLACED THE LEFT HAND BPSU.

Part: BPSU — OUT OF RIG (TE FLAPS) · airframe 10,374 hrs · 9,604 cycles

FLAPS FAILED AT 39 DEGREES. C/W RIGGING OF THE LEFT AND RIGHT BPSU.

Part: WARNING SYSTEM — ACTIVATED (TE FLAPS) · airframe 10,368 hrs · 9,595 cycles

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

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 10,174 hrs · 9,432 cycles

FLAPS FAILED MESSAGE. REPLACED THE RIGHT HAND BPSU.

Part: CONTROLLER — MALFUNCTIONED (TE FLAP) · airframe 10,129 hrs · 9,392 cycles

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

Part: LOOP — FALSE INDICATION (LT ENGINE PYLON) · airframe 9,912 hrs · 9,192 cycles

LEFT HAND 14TH STAGE BLEED DUCT LEAK WARNING. REPLACED THE LEFT HAND ENGINE PYLON DUCT LEAK SENSOR LOOP.

Part: WARNING SYSTEM — ACTIVATED (THRUST REVERSER) · airframe 9,759 hrs · 9,055 cycles

LEFT THRUST REVERSER UNLOCK MESSAGE. DEFERRED MAINTENANCE PER MEL.

Part: PANEL — CRACKED (WING) · airframe 9,740 hrs · 7,884 cycles

CRACKS AT 5 LOCATINS ON LOWER WING ACCESS HOLE 640CB. REPAIRED AFFECTED AREAS IAW REO 601R-57-21-030.

Part: WARNING SYSTEM — ACTIVATED (TE FLAPS) · airframe 9,727 hrs · 9,025 cycles

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

Part: PIN — INSTALLED (NLG) · airframe 9,339 hrs · 8,730 cycles

NLG WILL NOT RETRACT. FOUND DOWN LOCK PIN INSTALLED. REMOVED DOWNLOCK PIN, INSPECTED NLG, AND A/C RETURNED TO SERVICE.

Part: LIGHT — CABIN (INOPERATIVE)

ONE LIGHT OUT ON AIRSTAIRS. DEFERRED PER MEL.

Part: SKIN — DAMAGED (BS 349)

FUSELAGE SKIN AT 349.0, STR 16 LT DAMAGED BY PAX DOOR PIN. REPAIRED FUSELAGE SKIN AT FS 349.0, IAW CANADAIR REO 601R-53-21-186.

Part: DOUBLER — CRACKED (BS 718)

FS 718.00 AT STR 11 LT AND RT SIDES HAVE CRACKED DOUBLERS. REMOVED CRACKED DOUBLERS AT FS 718.00 AT STR 11 BOTH LT AND RT REPLACED DOUBLERS WITH NEW DOUBLERS IAW WVAC EO 601R-53-0422.

Part: WARNING — ACTIVATED (PAX DOOR)

CABIN DOOR OUTER HANDLE CAUTION MESSAGE. INSPECTED DOOR, NO DEFECTS FOUND. AIRCRAFT RETURNED TO SERVICE.

Part: DISPLAY — FAILED (RT COCKPIT)

NR 2 ED WENT BLANK DURING TAKE FF. TAKEOFF CONFIG WARNING. COULD NOT DUPLCIATE SPOILER CONFIG WARNING. REPLACED NR 2 ED.

Part: PSEU — MALFUNCTIONED (AVIONICS)

LANDING GEAR DID NOT EXTEND WHEN SELECTED TO DOWN POSITION. REPLACED THE PSEU.

Part: ENGINE — VIBRATION (NR 1)

NR 1 ENGINE N1 FAN VIB PEAKED AT 4.0 DURING CRUISE IN ICING CONDITIONS. ALL INDICATIONS IS NORMAL RANGE UPON LANDING. INSPECTED FAN INLET AND TURBINE, NO DAMAGE WAS NOTED. OPERATED LEFT ENGINE AT VARIOUS POWER SETTINGS FOR 25 MINUTES. LEFT ENGINE N1 VIBS WERE .6. SUBMITTER STATES: SUSPECT ICE ON SPINNER IN FLIGHT WAS THE CAUSE OF THE PROBLEM.

Part: FECU — FAILED (E/E COMPT)

FLAPS FAILED WHEN SELECTED FOR LANDING. REPLACED THE FECU.

Part: LAMP — FAILED (CABIN)

EMERGENCY LIGHT AT CABIN ENTRANCE IS INOP. REPLACED LAMPS.

Part: SKIN — CHAFED (LT TE FLAP VANE)

C-CHECK TASK 002-27-580-100, LEFT HAND INBOARD FLAP VANE LEADING EDGE HAS CHAFE DAMAGE AT WS 56.3. REPLACED FLAP VANE LEADING EDGE.

Part: SKIN — CHAFED (RT TE FLAP VANE)

C-CHECK TASK 002-27-680-100, RT INBD FLAP VANE LEADING EDGE HAS CHAFE DAMAGE AT WS 56.3. REPLACED FLAP VANE LEADING EDGE SKIN.

Part: WARNING SYST — MALFUNCTIONED (COCKPIT)

LEFT STATIC HEAT AND LEFT AOA HEAT CAUTION MESSAGE. COULD NOT DUPLICATE DISCREPANCY. OPERATIONAL CHECK SATISFACTORY.

Part: CONTROL UNIT — MALFUNCTION (E/E COMPT)

SPOILERONS CAUTION MESSAGE DURING FLIGHT. REPLACED THE NR 1 SECU.

Part: LINE — LEAKING (LT PYLON)

HYDRAULIC SYSTEM NR 1 FAILED. TOTAL LOSS OF SYSTEM PRESSURE AND FLUID. REPLACED LEAKING HYDRAULIC PRESSURE LINE AT LEFT HAND ENGINE PYLON.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

FLAP FAILED AT 20 DEGREES WHEN SELECTED FOR LANDING APPROACH. CYCLED FLAP SYSTEM CIRCUITS BREAKERS. COULD NOT DUPLICATE DISCREPANCY.

Part: FUEL LINE — LOOSE (LT ENGINE)

DURING DESCENT AT 5,000 FEET, THE LT ENGINE FLAMED OUT. FOUND LOOSE FUEL LINE AT NR 13 FUEL NOZZLE. TIGHTENED FUEL LINE AND AIRCRAFT RETURNED TO SERVICE.

Part: BPSU — MALFUNCTION (RT TE FLAP)

FLAPS FAIL MESSAGE ON EICAS DURING CRUISE FLIGHT. REPLACED THE RIGHT FLAP BPSU.

Part: SENSOR — OUT OF ADJUST (TE FLAPS)

FLAPS FAIL MESSAGE ON EICAS. ADJUSTED THE LEFT HAND AND RIGHT HAND FLAP BRAKE AND POSITION SENSORS.

Part: BPSU — MALFUNCTION (LT TE FLAP)

FLAPS FAIL CAUTION MESSAGE WHEN FLAPS SELECTED FOR LANDING. REPLACED THE LEFT FLAP BRAKE AND POSITION SENSOR UNIT.