N929CA

Part: BATTERY — FAULTY (E&E BAY) · airframe 33,162 hrs · 30,776 cycles

FLIGHT 5300 - RECEIVED INTERMITTENT BATTERY BUSS CAUTION MESSAGE. DIVERTED TO MCO, LANDED WITHOUT INCIDENT. REPLACED MAIN BATTERY. NO FURTHER DEFECTS.

Part: WIRE HARNESS — DAMAGED (LT MLG) · airframe 31,962 hrs · 29,799 cycles

FLIGHT 5300 - ABORTED TAKEOFF APPROX 105 - 110 KTS DUE TO ANTI-SKID CAUTION MESSAGE. REPLACED LEFT OUTBOARD LOWER MLG HARNESS ASSEMBLY. NO FURTHER DEFECTS.

Part: POST — CRACKED (FUSELAGE) · airframe 31,723 hrs · 29,601 cycles

DURING HMV7 INSPECTION FOUND BULKHEAD POST LOWER END CRACKED, FS 559, RBL 9. REMOVED DAMAGE AND INSTALLED DOUBLER PER BOMBARDIER REO 601R-53-41-057.

Part: FLOORBEAM — CRACKED (FS 295) · airframe 31,723 hrs · 29,601 cycles

DURING HMV7 INSPECTION FOUND FLOOR SUPPORT CHANNEL CRACKED AT LEFT CORNER FS 295, LBL 10. INSTALLED NEW P/N 600-34017-351 CHANNEL IAW SRM 51-42-06.

Part: BULKHEAD — CRACKED (BS 640) · airframe 31,723 hrs · 29,601 cycles

DURING HMV7 INSPECTION FOUND REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL FITTING. REMOVE DAMAGE AND INSTALLED DOUBLER PER BOMBARDIER REO 601R-53-61-2168 AND REO 301R-53-61-1230.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 31,723 hrs · 29,601 cycles

FLIGHT 5320 - CRACK ON RBL 9.0 O/B RADIUS OF VERTICAL STIFFENER AT FS 559.00. REPAIRED CRACK ON RBL 9.0 O/B RADIUS OF VERTICAL STIFFENER IAW REO 601R-53-41-057.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,723 hrs · 29,601 cycles

CRACK AT RIGHT SIDE FS 574.00 BETWEEN STRINGERS 6 AND 7. REPLACED SPLICE ANGLE IAW SRM 51-42-06.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,723 hrs · 29,601 cycles

TWO CRACKS VERIFIED WITH EDDY CURRENT ON SEMI-PRESSURE BULKHEAD AT FS 559 BETWEEN RBL 9 AND RBL 18. REPAIRED SEMI-PRESSURE BULKHEAD AT FS 559 AS PER REO 601R-53-41-353.

Part: SELECTOR VALVE — FAULTY (NLG) · airframe 31,716 hrs · 29,595 cycles

FLIGHT 9461- GEAR DISAGREE WARNING AND NOSE DOOR OPEN MESSAGE WHEN GEAR SELECTED DOWN. REMOVED AND REPLACED NLG SELECTOR VALVE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 31,141 hrs · 29,153 cycles

FLIGHT 4973 - DURING PREFLIGHT INSPECTION RECEIVED A FLAP FAIL CAUTION MESSAGE. 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: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 30,352 hrs · 28,538 cycles

FLIGHT 5102 - THE EMERGENCY FLOOR LIGHTS FROM ROW 9 TO THE LAVATORY FAILED TO ILLUMINATE DURING TEST. REPAIRED CONNECTOR P40LY.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 30,320 hrs · 28,512 cycles

FLIGHT 5519 - SECTION OF THE EMERGENCY FLOOR LIGHTING IS INOPERATIVE. DISCONNECTED, CLEANED AND INSPECTED AFFECTED CONNECTOR FOR INOPERATIVE SECTION OF FLOOR LIGHTING.

Part: LIGHT — FAILED (CABIN) · airframe 30,230 hrs · 28,440 cycles

FLIGHT 5684 - THE EMERGENCY FLOOR PATH EXIT LIGHTING FAILED TEST BETWEEN ROWS 9-12. DEFERRED INOPERATIVE SECTION OF EMERGENCY FLOOR PATH EXIT LIGHTING PER MEL 33-51-01-5.

Part: CABLE — FAULTY (EMERGENCY LIGHT) · airframe 30,070 hrs · 28,311 cycles

FLIGHT 5532 - MOST REAR CABIN EMERGENCY FLOOR STRIP INOPERATIVE. REPLACED INOPERATIVE CABLE ASSEMBLY.

Part: COMPUTER — MALFUNCTIONED (ANTI SKID SYS) · airframe 29,864 hrs · 28,145 cycles

FLIGHT 5023 - PERFORMED A HIGH SPEED ABORT DUE TO ANTI-SKID CAUTION. PERFORMED A SYSTEM RESET FOR SECU NR 1 AND NR 2.

Part: BPSU — FAULTY (T/E FLAP) · airframe 29,634 hrs · 27,965 cycles

FLIGHT 5181 - AFTER LANDING RECEIVED A FLAP FAIL CAUTION AT 45 DEGREES. REPLACED BPSU.

Part: FLAP — MALFUNCTIONED (WING) · airframe 29,614 hrs · 27,947 cycles

FLIGHT 5568 - DURING LGA APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 8 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: CAUTION MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 29,595 hrs · 27,931 cycles

FLIGHT 5455 - FLAP FAIL CAUTION MESSAGE ON GROUND. 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: ACTUATOR — FAULTY (RT FLAP) · airframe 29,570 hrs · 27,915 cycles

FLIGHT 5137 - DURING LANDING AT YYZ, RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREES. REPLACED THE RIGHT INBOARD FLAP INBOARD ACTUATOR.

Part: BPSU — FAULTY (LEFT WING) · airframe 29,570 hrs · 27,915 cycles

FLIGHT 5137 - DURING LANDING AT YYZ RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREES. REPLACED THE BRAKE POSITION SENSING UNIT.

Part: ACTUATOR — FAULTY (LEFT FLAP) · airframe 29,570 hrs · 27,915 cycles

FLIGHT 5137 - DURING LANDING AT YYZ RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREES. REPLACED THE LEFT INBOARD FLAP INBOARD ACTUATOR.

Part: ACTUATOR — FAULTY (RT FLAP) · airframe 27,570 hrs · 27,915 cycles

FLIGHT 5137 - DURING LANDING AT YYZ, RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREES. REPLACED THE RIGHT INBOARD FLAP OUTBOARD FLAP ACTUATOR.

Part: ACTUATOR — FAULTY (LEFT FLAP) · airframe 29,570 hrs · 27,915 cycles

DURING LANDING AT YYZ, RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREES. REPLACED THE LEFT INBOARD FLAP OUTBOARD FLAP ACTUATOR.

Part: BPSU — FAULTY (RT WING) · airframe 29,553 hrs · 27,903 cycles

FLIGHT 5266- FLAPS FAIL CAUTION MESSAGE. REMOVED AND REPLACED RT BPSU.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 29,506 hrs · 27,864 cycles

FLIGHT 5202 - FLAPS FAILED CAUTION MESSAGE OCCURRED ON FINAL APPROACH AT 45 DEGREES. 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: FLAP SYSTEM — WARNING LIGHT (TE FLAPS) · airframe 29,365 hrs · 27,750 cycles

FLIGHT 5616 - DURING TAXI OUT RECEIVED A FLAP FAIL MESSAGE, FLIGHT RETURNED TO THE GATE. 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: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 29,067 hrs · 27,500 cycles

FLIGHT 5078 - DURING BUF APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE AT 45 DEGREES. 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: ACTUATOR — FROZEN (NLG DOOR) · airframe 28,293 hrs · 26,820 cycles

FLIGHT 5227 - NLG DOOR OPEN WARNING. LUBRICATED AND FREED UP FROZEN ROLLER IN NLG DOORS OPERATING MECHANISM.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 30,223 hrs · 28,433 cycles

FLIGHT 5306 - THE AFT CABIN EMERGENCY FLOOR LEVEL LIGHTING FAILED TEST. REPAIRED WIRING ON AFT EMERGENCY FLOOR LEVEL FLEX STRIP CONNECTOR.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 27,706 hrs · 26,313 cycles

FLIGHT 5499- OVERBOARD COOL CAUTION. AIRCRAFT DID NOT PRESSURIZE. FOUND OVERBOARD AND INBOARD EXHAUST VALVES IN WRONG POSITION. PREVIOUS DEFERRAL ITEM.

Part: PUMP — FAULTY (HYD SYSTEM) · airframe 27,423 hrs · 26,054 cycles

FLIGHT 5851 - DURING CLIMBOUT OF DSM RECEIVED A GEAR DISAGREE CAUTION. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD, LANDING WITHOUT INCIDENT.

Part: SKIN — CORRODED (PAX DOOR) · corrosion level 2 · airframe 27,330 hrs · 25,969 cycles

DURING HEAVY MAINTENANCE CHECK, THE PAX DOOR FORWARD AND AFT BOTTOM CORNERS WERE FOUND TO BE CORRODED. BOTH PARTS WERE REPLACED WITH FACTORY NEW PARTS USING THE CL 6002B-19 STRUCTURAL REPAIR MANUAL

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 27,335 hrs · 25,969 cycles

DURING COMPLIANCE OF TASK 002-53-160-610 (COMAIR TASK CRJ-2-162011), 1 CRACK WAS FOUND IN THE PRESSURE FLOOR SKIN AT FS 460.0, BETWEEN BL 0.0 AND RBL 9.0 THE CRACK WAS 2.0 INCH IN LENGTH. REPAIRED IN ACCORDANCE WITH BOMBARDIER REO 601R-53-41-102, REV D, DATED 9-29-2003.

Part: SELECTOR VALVE — UNRELIABLE (NLG) · airframe 26,219 hrs · 24,894 cycles

FLIGHT 4962, LOUD CLUNKING NOISE FROM NLG. REPLACED THE NLG DOORS SELECTOR VALVE.

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 25,900 hrs · 24,590 cycles

FLIGHT 5822 GEAR DISAGREE WARNING. COULD NOT DUPLICATE. FUNCTIONAL CHECKS AND INSPECTION OF LANDING GEAR FOUND NO DEFECTS.

Part: WIRE — FAILED (EMERGENCY LIGHT) · airframe 25,281 hrs · 24,065 cycles

FLIGHT 4988 EMERGENCY FLOOR PATH LIGHTS ARE INOP. REPLACED THE FLOOR LIGHTS CABLE ASSY.

Part: UPLOCK HOOK — OUT OF ADJUST (MLG) · airframe 24,323 hrs · 23,259 cycles

FLIGHT 5659 GEAR DISAGREE WARNING ON APPROACH. COULD NOT DUPLICATE. EXTENSION AND RETRACTION CHECKS WERE NORMAL. ADJUSTED NLG UPLOCK HOOK TO M/M SPECS.

Part: UPLOCK — MALFUNCTIONED (NLG) · airframe 24,322 hrs · 23,258 cycles

FLIGHT 5870 GEAR DISAGREE WARNING ON APPROACH. REPLACED THE NLG UPLOCK.

Part: PRIORITY VALVE — FAULTY (NLG) · airframe 24,294 hrs · 23,238 cycles

FLIGHT 5596 GEAR DISAGREE WARNING, NLG INDICATED INTRANSIT. REPLACED THE NLG PRIORITY VALVE.

Part: ACTUATOR — FAULTY (NLG) · airframe 23,339 hrs · 22,430 cycles

FLIGHT 5745 AFTER TAKEOFF AND GEAR RETRACTION RECEIVED A NLG DISAGREE CAUTION WITH A NOSE GEAR DOOR OPEN MESSAGE. AIRCRAFT RETURNED TO DEPARTING CITY (CVG). REPLACED THE NLG DOOR ACTUATOR.

Part: PIVOT — LACK OF LUBE (NLG) · airframe 23,337 hrs · 22,429 cycles

FLIGHT 5689 AFTER TAKEOFF AND GEAR RETRACTION THE NLG INDICATED DOWN AND LOCKED WITH THE HANDLE IN THE UP POSITION. AIRCRAFT RETURNED TO DEPARTING CITY (CVG). CLEANED AND LUBRICATED THE NLG PIVOT POINTS.

Part: HANDLE — UNSECURE (PAX DOOR) · airframe 22,532 hrs · 21,761 cycles

FLIGHT 5221 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. FOUND OUTER HANDLE OPEN - OPERATIONAL CHECK OF DOOR SATISFACTORY. NO DEFECTS NOTED.

Part: TRIM SWITCH — MALFUNCTIONED (INSTRUMENT PANEL) · airframe 21,409 hrs · 20,780 cycles

FLIGHT 5219 RUDDER TRIM STUCK AT 1/4 RIGHT. REPLACED THE RUDDER TRIM PANEL.

Part: CONTROL BOX · airframe 20,746 hrs · 20,216 cycles

FLIGHT 5443 LEFT ANGLE OF ATTACK HEAT CAUTION MESSAGE.RESET SYSTEM - COULD NOT DUPLICATE.

Part: DOOR · airframe 20,308 hrs · 19,810 cycles

FLIGHT 5063 LOUD WHISTLING COMING FROM R/H FORWARD SIDE OF AIRCRAFT.FOUND GROUND INTERPHONE DOOR OPEN - INSPECTED FOR DAMAGE AND CLOSED DOOR.

Part: PSEU — MALFUNCTIONED (AVIONICS) · airframe 19,975 hrs · 19,485 cycles

FLIGHT 5984 GEAR DISAGREE MESSAGE.REPLACED THE PSEU.

Part: TRIM MOTOR — MALFUNCTIONED (VERT STAB) · airframe 19,261 hrs · 18,789 cycles

FLIGHT 5433 TRIM CAUTION MESSAGE - TRIM STUCK AT 2.8REPLACED THE HORZ STAB TRIM ACTUATOR.

Part: AUDIO PANEL — MALFUNCTIONED (COCKPIT) · airframe 18,519 hrs · 18,032 cycles

FLIGHT 5553 - PILOT TO COPILOT INTERCOM INTERMITTENT.REPLACED THE #1 ACP.

Part: DOOR ACTUATOR · airframe 17,977 hrs · 17,444 cycles

FLIGHT #5902. GER DISAGREE WARNING - NLG INDICATED UNSAFE. NLG THEN INDICATED DOWN AND LOCK DURING GO AROUND.ADJUSTED THE NLG DOORS ACTUATOR AND MECHANISM. SYSTEM OPERATED NORMALLY.

Part: CONTROL BOX — MALFUNCTIONED (AVIONICS) · airframe 17,764 hrs · 17,227 cycles

STAB CHANNEL 1 INOP MESSAGE DURING APPROACH.REPLACED THE HSTCU.

Part: TRANSMITTER — FAULTY (WING) · airframe 17,721 hrs · 71,185 cycles

FLIGHT #5697. DURING CLIMB OUT OF CVG RECEIVED A FLAP CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD WITH FLAPS OSCILLATING BETWEEN 2 AND 5 ABOVE SELECTED POSITION.REPLACED THE FLAP POSITION TRANSMITTER.

Part: SPOILER · airframe 17,629 hrs · 17,088 cycles

FLIGHT 6082. FLIGHT SPOILER AND OUTBOARD GROUND SPOILER FAULT MESSAGE DURING T/O. T/O ABORTEDRESET SYSTEM AND C/W OPERATIONAL CHECKS. NO FAULTS FOUND.

Part: MOTOR — FAULTY (EMPENNAGE) · airframe 17,607 hrs · 17,066 cycles

FLIGHT #5531. WHILE PARKED AT THE GATE PRIOR TO DEPARTURE RECEIVED A STAB CH #2 TRIM INOPERATIVE MESSAGE.REPLACED THE HORIZONTAL STABILIZER TRIM MOTOR CONTROL UNIT.

Part: ACTUATOR — FAULTY (EMPENNAGE) · airframe 17,607 hrs · 17,066 cycles

FLIGHT #5531. WHILE PARKED AT THE GATE PRIOR TO DEPARTURE RECEIVED A STAB. CH #2 TRIM INOPERATIVE MESSAGE.REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 17,494 hrs · 16,954 cycles

FLIGHT #5322. WHILE PARKED AT THE GATE AT EVV STABILIZER TRIM CHANNEL #2 WOULD NOT ENGAGE.REPLACED STAB/MACH TRIM PANEL ASSEMBLY.

Part: LIGHT · airframe 17,360 hrs · 16,816 cycles

EMERGENCY LIGHT ROW 11 IS INOPERABLE.DEFERRED MAINTENANCE PER M.E.L.

Part: BUSHING — SCORED (VERTICAL STAB) · airframe 17,304 hrs · 16,756 cycles

LEFT AND RIGHT VERTICAL STABILIZER BUSHINGS ARE MIGRATED. REMOVED AND REPLACED LT AND RT VERTICAL STABILIZER BUSHINGS IAW WVAC EO 601R-55-2429.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,304 hrs · 16,756 cycles

THE FRAME AT FS 640 HAS A CRACKED ANGLE ON THE RIGHT SIDE AT THE ENGINE SUPPORT AREA. REMOVED CRACKED ANGLE (P/N 601-36001-30) AND INSTALLED A NEW ANGLE (P/N 601-36001-30) IAW WVAC EO 601R-53-2390.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,304 hrs · 16,756 cycles

THE FRAME AT FS 640 HAS A CRACKED ANGLE ON THE RIGHT SIDE AT THE ENGINE SUPPORT AREA. REMOVED CRACKED ANGLE P/N 601-36001-30 AND INSTALLED A NEW ANGLE P/N 601-36001-30 IAW WVAC EO 601R-53-2390.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 16,593 hrs · 16,063 cycles

FLAPS FAIL MESSAGE. REPLACED THE FECU.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,564 hrs · 16,028 cycles

EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERIES.

Part: POWER UNIT — MALFUNCTIONED (WING) · airframe 16,274 hrs · 15,750 cycles

FLAPS FAIL MESSAGE. REPLACED THE RDU.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 16,167 hrs · 15,636 cycles

FLAPS FAIL MESSAGE. REPLACED THE RT BPSU.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 15,412 hrs · 14,835 cycles

OVERBOARD COOL CAUTION MESSAGE. COULD NOT DUPLICATE. OPERATIONAL CHECK OF PASSENGER DOOR AND WARNING SYSTEM WAS NORMAL.

Part: SPRING — BROKEN (PAX DOOR) · airframe 15,293 hrs · 14,708 cycles

CABIN DOOR OUTER HANDLE CAUTION MESSAGE. REPLACED OUTER HANDLE LATCH SPRING.

Part: DOOR — LACK OF LUBE (PAX DOOR) · airframe 15,152 hrs · 14,565 cycles

PAX DOOR OUTER HANDLE WARNING IN FLIGHT, COULD NOT OPEN DOOR UPON LANDING. INSPECTED AND LUBED DOOR, NO FAULT MESSAGE.

Part: LATCH — OVERSERVICED (FUSELAGE) · airframe 15,138 hrs · 14,560 cycles

PAX DOOR HANDLE CAUTION LIGHTS CAME ON AFTER DEPARTURE. REMOVED EXCESS GREASE FROM HANDLE.

Part: SENSOR — MALFUNCTIONED (RT WING) · airframe 15,085 hrs · 14,492 cycles

WING OVERHEAT WARNING. REPLACED THE RIGHT HAND WING CONTROL SENSOR.

Part: SPRING — BROKEN (DOOR HANDLE) · airframe 15,000 hrs · 14,400 cycles

CABIN DOOR WARING. REPLACED OUTER HANDLE LATCH SPRING.

Part: BALLAST — FAILED (ROW 5)

SMOKE IN CABIN DURING TAXI OPS. REPLACED DEFECTIVE LIGHT BALLAST AT ROW 5.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

DISPLAY COOL CAUTION MESSAGE. CLEANED DUST FROM THE CRT DISPLAY SCREENS.

Part: ANGLE — CORRODED (BS 280)

FS 280.00 AFT J ANGLE (P/N 600-34017-595) WAS CORRODED. TRIMMED OUT DAMAGED AREA OF J ANGLE AND FABED NEW SECTION, INSTALLED IAW WVAC EO 601R-53-0774.

Part: ANGLE — CORRODED (BS 280)

FS 280.00 FWD J ANGLE (P/N 600-34017-351) IS CORRODED. REMOVED DAMAGED J ANGLE AND REPLACED IAW WVAC EO 601R-53-0758.

Part: WEB — CORRODED (BS 280)

FS 280.00 WEB (P/N 600-34017-587) CORRODED. REMOVED FORWARD J ANGLE TO ACCESS WEB, TRIMMED OUT DAMAGED AREA FAB FILLER AND REPAIR DOUBLER, INSTALLED, REINSTALLED FWD J ANGLE IAW WVAC EO 601R-53-0773.

Part: CLIP — CRACKED (BS 280)

FS 280.00 LBL 9 HAD CRACKED FLOOR SUPPORT ANGLE. REMOVED DAMAGED ANGLE AND FABED NEW ANGLE, INSTALLED IAW WVAC EO 601R-53-0760.

Part: STIFFENER — CRACKED (BS 280)

VERTICAL STIFFENESS CRACKED AT FS 28 DEGREES BELOW CBP-1 AND CBP-2 AT LBL 12 AND RBL 12. INSTALLED NEW STIFFENERS IAW WVAC EO 601R-53-0759.

Part: DOUBLER — CORRODED (BS 310 - 319)

DOUBLER PLATE AT RBL 42 FS 310 - FS 319 (P/N 601R38669-49) WAS CORRODED. INSTALLED NEW DOUBLER PLATE AT RBL 42 FS 310 - 319 IAW WVAC EO 601R-53-0778.

Part: WEB — DAMAGED (BS 307)

OUTBOARD WEB AT LBL 27 FS 307 HAD ELONGATED HOLE .27 DEGREES DIAMETER (P/N 601R31113-17). INSTALLED NEW WEB IAW WVAC EO 6501R-53-0772.

Part: THRESHOLD — CORRODED (BS 317 - 342)

SERVICE DOOR THRESHOLD TOP ANGLE (P/N 601R38303 105) WAS CORRODED FS 317 - FS 342. INSTALLED NEW THRESHOLD TOP ANGLE IAW WVAC EO 601R-53-0757.

Part: THRESHOLD — CORRODED (BS 310)

PAX DOOR THRESHOLD TOP ANGLE (P/N 601R31527-46) WAS CORRODED. INSTALLED NEW PAX DOOR THRESHOLD ANGLE IAW WVAC EO 601R-53-0757.

Part: ANGLE — CRACKED (BS 480)

THE ATTACH ANGLES AT FS 484 AT RBL 27 AND LBL 36 WERE CRACKED. INSTALLED NEW BRACKETS IAW WVAC EO 601R-53-07628.

Part: SCUPPER — DAMAGED (RT WING)

CENTER TANK GRAVITY FILL SCUPPER ASSY HAS SEVERAL DAMAGED HI-LOC PIN HOLES. REPAIRED IN ACCORDANCE WITH REO 601R-57-21-077.

Part: HANDLE — OUT OF ADJUST (PASSENGER DOOR)

DOOR OUTER HANDLE WARNING AFTER TAKEOFF. ADJUSTED DOOR HANDLE SPRING TENSION.

Part: HANDLE — NOT LATCHED (PASSENGER DOOR)

DOOR UNLOCKED WARNING AFTER TAKEOFF. FOUND DOOR HANDLE UNLATCHED. INSPECTED LATCH MECHANISM AND FOUND NO DEFECTS.

Part: WARNING — ACTIVATED (CABIN DOOR)

CABIN DOOR OUTER HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE. NO DEFECTS FOUND WITH CABIN DOOR.

Part: SENSOR — OUT OF ADJUST (PASSENGER DOOR)

AFTER TAKEOFF, PASSENGER OUTER DOOR HANDLE STOW AND OVERBOARD COOL CAUTION MESSAGE CAME ON. ADJUSTED PROX SENSOR.

Part: HANDLE — NOT LATCHED (PAX DOOR)

OUTER DOOR HANDLE MESSAGE AFTER TAKEOFF. COULD NOT DUPLICATE DISCREPANCY. NO DEFECTS FOUND.

Part: FAIL MESSAGE — ACTIVATED (TE FLAPS)

FLAPS FAIL CAUTION MESSAGE. INSPECTED FLAPS PER EO 27-045 AND AD 98-20-01. NO DEFECTS FOUND.

Part: WARNING — ACTIVATED (PAX DOOR)

CABIN DOOR OUTER HANDLE CAUTION MESSAGE. INSPECTED AND FOUND NO DEFECTS WITH DOOR HANDLE.

Part: DUCT — CRACKED (RT WING)

WING ANTI-ICE DUCT WARNING MESSAGE ON EICAS. REPLACED THE RIGHT WING BLEED AIR PICCOLO TUBE.

Part: OVERHEAT ELEMENT — FAILED (LT PYLON)

LEFT 14TH STAGE DUCT LEAK MESSAGE. REPLACED THE LEFT HAND ENGINE PYLON BLEED LEAK SENSING ELEMENT.

Part: ELEMENT — FALSE WARN (LT PYLON)

ANTI-ICE DUCT LEAK WARNING MESSAGE. REPLACED THE LEFT ENGINE PYLON SENSING ELEMENT.

Part: CONTROL UNIT — MALFUNCTIONED (BLEED AIR DUCT)

BLEED AIR DUCT LEAK WARNING DURING TAKEOFF. REPLACED THE BLEED LEAK CONTROL UNIT.

Part: CONTROLLER — MALFUNCTION (ANTI ICE DUCT)

ANTI-ICE DUCT LEAK WARNING DURING TAKEOFF. REPLACED THE BLEED AIR LEAK CONTROLLER.

Part: BATTERIES — DISCHARGED (CABIN)

EMERGENCY LIGHTS ARE INOP. REPLACED THE EMERGENCY LIGHTS BATTERIES.

Part: CONTACTOR — MALFUNCTION (E/E COMPT)

A/C UTILITY BUS NR 2 SHED IMMEDIATLEY AFTER FLAPS ARE SELECTED OUT OF 0 DEGREES. REMOVED THE A/C UTILITY BUS CONTACTOR NR 1K4XD IAW CRJ CONCESSION LETTER CO95-651.

Part: CONRTOLLER — MALFUNCTION (PITOT HEAT)

LEFT PITOT HEAT CAUTION MESSAGE ON EICAS. REPLACED THE HEAT CONTROLLER.

Part: CONTROL CABLE — SEIZED (RT TE FLAP)

DURING CLIMBOUT, FLAPS STUCK AT 12 DEGREES. AIRCRAFT RETURNED TO THE FIELD. REPLACED RIGHT OUTBOARD FLAP DRIVE CABLE ASSEMBLY, CABLE WAS FOUND SEIZED.

Part: DRIVE CABLE — WORN (RT TE FLAP)

FLAPS FAIL MESSAGE ON EICAS. REPLACED THE RT OUTBOARD FLAP DRIVE CABLE.

Part: FIRE CONTROLLER — MALFUNCTION (E/E COMPT)

ALL ENGINE AND APU FIRE WARNINGS AND FAIL LIGHTS CAME ON. REPLACED THE FIRE DETECTION CONTROLLER.

Part: ACTUATOR — FAILED (STICK PUSHER)

STALL FAIL ABNORMAL CAPTION DISPLAYED. REPLACED STICK PUSHER ACTUATOR.

Part: ADC — FAILED (NR 1)

PILOTS ALTIMETER AND VERTICAL SPEED INDICATORS FAILED. REPLACED THE NR 1 AIR DATA COMPUTER.

Part: HANDLE — NOT STOWED (PAX DOOR)

PASSENGER DOOR OUTER HANDLE NOT STOWED MESSAGE ON EICAS. AIRCRAFT WOULD NOT PRESSURIZE. COULD NOT DUPLICATE DISCREPANCY. DOOR OPERATION AND OUTER HANDLE STOW MECHANISM ALL OPERATE NORMAL.

Part: BPSU — DEFECTIVE (LT/RT TE FLAPS)

FLAPS FAILED AT 20 DEGREES DURING RETRACTION. REPLACED THE LT AND RT BRAKE AND POSITON SENSOR UNITS. PART TOTAL CYCLES, 5,181.

Part: HYD HOSE — LEAKING (NR 1 HYD SYST)

NR 1 HYDRAULIC SYSTEM CAUTION MESSAGE RECEIVED AFTER TAKEOFF. NR 1 HYDRAULIC SUPPLY LINE CHAFED AND LEAKING AT SUPPORT CLAMP. REPLACED LEAKING LINE.

Part: FAN BLADES — FOD DAMAGE (LT ENGINE)

LEFT ENGINE FAN SECTION HAS FOD DAMAGE. REPLACED 5 SETS OF FAN BLADES.

Part: DOOR — NOT LATCHED (OXYGEN SERVICE)

OXYGEN SERVICE DOOR OPEN IN FLIGHT. CLOSED AND SECURED DOOR.

Part: DRAG BRACE — DEFECTIVE (NLG)

NOSE LANDING GEAR DID NOT RETRACT. REPLACED THE NLG DRAG BRACE ASSY.

Part: DRAG BRACE — DEFECTIVE (NLG)

UNABLE TO RETRACT NOSE LANDING GEAR. REPLACED NLG DRAG BRACE ASSY.

Part: HSTA — FAILED (VERT STAB)

HORIZONTAL STABILIZER TRIM CHANNEL NR 2 INOP. REPLACED THE HORIZONTAL STABILIZER TRIM ACTUATOR.

Part: EEL LENSE — BROKEN (CABIN)

LOWER EMERGENCY LIGHT ON MAIN PASSENGER DOOR HAS A BROKEN LENSE AND DOES NOT WORK. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY.

Part: CONTROL BOX — DEFECTIVE (ANTISKID SYST)

ANTI-SKID SYSTEM FAIL, CIRCUIT BREAKER TRIPPED. REPLACED ANTI-SKID CONTROL BOX.

Part: PSEU — FALSE WARNING (COCKPIT)

INBD ANTI-SKID MESSAGE AND PROXIMITY SYSTEM FAULT MESSAGE ON EICAS. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT.

Part: SELECTOR VALVE — DEFECTIVE (NLG STEERIUG)

NLG STEERING IS INOP. REPLACED THE NLG SELECTOR VALVE.

Part: VALVE — DEFECTIVE (NLG)

GEAR DISAGREE MESSAGE ON EICAS, NLG DID NOT DOWN LOCK. EMERGENCY PROCEDURE USED TO EXTEND LANDING GEAR. REPLACED NLG SELECTOR VALVE.

Part: SBW HARNESS — DEFECTIVE (NLG STEERING)

NOSE WHEEL STEERING IS INOP. REPLACED THE SBW HARNESS ON NLG.