N982CA

Part: VALVE — FAULTY (MLG) · airframe 21,512 hrs · 20,541 cycles

FLIGHT 5082- EN ROUTE AZO-CVG, RECEIVED A MLG DISAGREE CAUTION CAUTION WHEN GEAR WAS SELECTED DOWN, CREW DECLARED AN EMERGENCY AND PERFORMED ACTUATION OF THE MANUAL GEAR RELEASE HANDLE. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE MLG SELECTOR.

Part: CONTROL PANEL — MALFUNCTIONED (ADG) · airframe 21,378 hrs · 20,518 cycles

FLIGHT 5828 - ADG DEPLOYED AFTER T/O. REPLACED THE ADG CONTROL PANEL.

Part: OUTFLOW VALVE — OUT OF POSITION (CABIN PRESSURE) · airframe 21,317 hrs · 20,456 cycles

OVERBOARD COOL SYSTEM WAS ALREADY ON DEFERRED MAINTENANCE LIST. SECURED VALVES IN PROPER POSITION.

Part: ACCESS PANEL — OPEN (GROUND COMM) · airframe 20,210 hrs · 19,478 cycles

LOUD SQUEAL DURING ROTATION AND CLIMB. GROUND COMMUNICATION PANEL LEFT OPEN. INSP FOR DAMAGE AND CLOSED DOOR.

Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 19,974 hrs · 19,285 cycles

FLIGHT 5144 - FLAPS FAIL CAUTION. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: ELEMENT — FAULTY (LT ENGIE) · airframe 19,802 hrs · 19,130 cycles

FLIGHT 5530 DURING CRUISE FLIGHT (ABE-CVG) RECEIVED A LEFT 14 STAGE DUCT MESSAGE, CREW DECLARED AN EMERGENCY, DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. REPLACED THE FORWARD LEFT PYLON 14TH STAGE SENSING ELEMENT.

Part: PUMP — MALFUNCTIONED (LT ENGINE) · airframe 19,355 hrs · 18,728 cycles

FLIGHT 5487 LEFT ENGINE OIL PRESSURE WARNING. REPLACED THE LUBE AND SCAVENGE PUMP.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 19,355 hrs · 18,728 cycles

FLIGHT 5535 FLAPS FAIL CAUTION. REPLACED THE FECU.

Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 19,269 hrs · 18,648 cycles

FLIGHT 5436 LEFT FLAP POSITION INDICATES 20 DEGREES AND RIGHT FLAP INDICATES 0 DEGREES. INSPECTED AND OPERATED FLAP SYSTEM, NO DEFECTS FOUND. COULD NOT DUPLCIATE.

Part: DOOR — OPEN (CARGO BAY) · airframe 16,609 hrs · 16,390 cycles

FLIGHT 5109 CARGO DOOR WARNING DURING T/O. CLOSED CARGO DOOR PROPERLY. NO DEFECTS NOTED.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 16,547 hrs · 16,329 cycles

RIGHT AND LEFT SIDE LOWER FUSELAGE SKINS ARE CRACKED AT NOSE LANDING GEAR CUTOUT AT FS 235 STRINGERS 26R AND 26L. CRACKS ARE 1.0 INCH LONG. PERFORMED A MAJOR REPAIR FUSELAGE SKIN AT FS 235 STRINGER 26R AND 26L BY CUTTING OUT DAMAGED AREAS, FABRICATING REPAIR FILLERS AND DOUBLERS FROM 2024T3.050 (WVAC PO 33196/1) AND 2024T3.063 (WVAC PO 32572/1). PERFORMING LP1 TO ENSURE CUTOUT AREAS ARE CRACK FREE AND INSTALLING REPAIR PARTS IAW BOMBARDIER, INC REO 601R-53-11-010 REV C AND REO 601R-53-11-014 REV NC.

Part: DOUBLER — BENT · airframe 16,547 hrs · 16,329 cycles

PREVIOUS REPAIR TO LEFT SIDE FUSELAGE SKIN HAS SUBSTAINED FURTHER DAMAGE ON FUSELAGE SKIN EXTERNAL DOUBLER. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN AT FS 310 BETWEEN STRINGER 15R AND 16R BY REMOVING DAMAGED TOP REPAIR DOUBLER. NO DAMAGE FOUND ON BOTTOM DOUBLER AND FILLER. FABRICATING NEW REPAIR DOUBLER FROM 2024T3.063 (WVAC PO 32572/1) AND INSTALLING IAW BOMBARDIER INC REO 601R-53-21-180 REV NC.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 16,547 hrs · 16,329 cycles

RIGHT FS 718 BETWEEN STRINGERS 10R AND 12R P/N 600-36030-32 IS CRACKED. PERFORMED A MAJOR REPAIR TO FS 718 BETWEEN STRINGERS 10R AND 12R BY REMOVING AND REPLACING DOUBLER P/N 600-36030-32 IAW CRJ 200 SRM 51-42-00 AND 51-42-21.

Part: SWITCH — FAULTY (RT WING) · airframe 16,117 hrs · 15,978 cycles

FLIGHT 5491 WING OVERHEAT WARNING. REPLACED THE RT WING OVERHEAT SWITCH.

Part: LINE — BROKEN (NR 2 HYD SYSTEM) · airframe 15,679 hrs · 15,596 cycles

HYDRAULIC SYSTEM 2 LOW PRESSURE WARNING AND LOSS OF ALL FLUID. REPLACED BROKEN RETURN LINE AT NR 2 HYD MANIFOLD.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 15,564 hrs · 15,493 cycles

FLIGHT 5096 HYDRAULIC SYSTEM 2 LOW PRESSURE WARNING.REPLACED LEAKING PRESSURE LINE IN PYLON.

Part: BPSU — MALFUNCTIONED (RIGHT) · airframe 15,251 hrs · 15,232 cycles

FLIGHT 5587 FLAPS FAIL CAUTION MESSAGE. REPLACED THE RT BPSU.

Part: FLEX DRIVE — BROKEN (T/E FLAP) · airframe 15,013 hrs · 15,022 cycles

FLIGHT 5623 FLAPS FAIL CAUTION. REPLACED THE RT NR 4 FLEX DRIVE SHAFT.

Part: CONTROL UNIT — MALFUNCTIONED (E/E BAY) · airframe 14,759 hrs · 14,792 cycles

FLIGHT 5778 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FLAP ELECTRONIC CONTROL UNIT.

Part: CONTROLLER — MALFUNCTIONED (TE FLAPS) · airframe 14,487 hrs · 14,566 cycles

FLIGHT 5240 FLAPS FAILED AFTER LANDING. RESET THE FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: FLASHLIGHT — SHORTED (GALLEY) · airframe 14,322 hrs · 14,408 cycles

FLIGHT 5794 - FLIGHT ATTENDANT REPORTED EMERGENCY FLASHLIGHT DID NOT ILLUMINATE AFTER TAKING IT OUT OF HOLDER. AFTER ABOUT 40 SECONDS IT STARTED SMOKING AND BECAME HOT TO THE TOUCH. CREW DEACTIVATED IT BY REMOVING THE BATTERY. LATER INVESTIGATION SHOWED THAT THE CONTROLLING CIRCUIT BOARD HAD SHORTED OUT.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 14,204 hrs · 14,305 cycles

FLIGHT 5840 TAKEOFF CON FIG SPOILERS, GROUND AND FLIGHT. REPLACED THE NR 1 SECU.

Part: BATTERY — DISCHARGED (CABIN) · airframe 13,788 hrs · 13,947 cycles

FLIGHT 5242 EMERGENCY LIGHTS ARE INOPREPLACED EMERGENCY BATTERIES

Part: RESERVOIR — UNRELIABLE (#3) · airframe 13,566 hrs · 13,741 cycles

FLIGHT 6811 GEAR DISAGREE WARNING - L/H MLG INDICATED INTRANSIT.REPLACED THE #3 HYDRAULIC RESERVOIR

Part: TRIM MOTOR · airframe 12,795 hrs · 13,040 cycles

FLIGHT 5674 STAB TRIM CAUTION MESSAGE DURING T/O.COULD NOT DUPLICATE. FOUND NO DEFECTS WITH SYSTEM.

Part: HYDRAULIC SYSTEM · airframe 11,621 hrs · 11,905 cycles

FLIGHT 5620 GEAR DISAGREE WARNING WHEN SELECTED UP.SERVICED AND BLED AIR FROM #3 HYDRAULIC SYSTEM, RETRACT CHECKS WERE NORMAL.

Part: DOUBLER — CRACKED (FS718.0) · airframe 11,621 hrs · 11,917 cycles

THE L/H SIDE 718.0 FRAME AND DOUBLER WERE CRACKED BETWEEN STINGERS 10 AND 11.REPAIRED THE CRACKED FRAME AND REPLACED THE DOUBLER I/A/W REO 601R-53-61-193 REV A AND WVAC EO 601R-53-3158.

Part: VALVE — MALFUNCTIONED (NLG) · airframe 11,138 hrs · 11,396 cycles

FLIGHT 5922 NLG DID NOT EXTEND WHEN GEAR SELECTED DOWN.REPLACED THE NLG SELECTOR VALVE.

Part: PSEU — MALFUNCTIONED (AVIONICS) · airframe 10,991 hrs · 11,255 cycles

FLIGHT 5032 GEAR DISAGREE WARNING AFTER T/O.REPLACED THE PSEU.

Part: LAMP · airframe 10,829 hrs · 11,105 cycles

FLIGHT 5480 EMERGENCY FLOOR PATH LIGHTING AFT OF ROW 9 IS INOPERATIVE.CLEANED WIRE CONNECTION AT ROW 9, SYSTEM TEST OK.

Part: LIGHT · airframe 9,999 hrs · 10,275 cycles

FLIGHT #5558. DURING PRE-FLIGHT INSPECTION DISCOVERED THE ORANGE EMERGENCY LIGHT AND THE LEFT AND RIGHT FLUSH EXIT LIGHTED SIGNS INOPERATIVE.REPALCED TERMINAL BLOCK FOR AFFECTED EMERGENCY LIGHTING.

Part: VALVE — LEAKING · airframe 9,808 hrs · 10,036 cycles

R/H 14TH STAGE DUCT WARNING MESSAGE AND ANTI-ICE DUCT WARNING.FOUND 14TH STAGE BLEED VALVE LEAKING, REMOVED AND REINISTALLED VALVE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 9,807 hrs · 10,035 cycles

ANGLE P/N 601R-31527-181 CORRODED AT LOWER LONGENON, PASSENGER DOOR ANGLE LOCATED AT STR 17 FS 342.7 - 317.70. FABRICATED ANGLE - 181 AND INSTALLED IAW WVAC EO 601R-53-2366.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 9,807 hrs · 10,035 cycles

ANGLE P/N 601R-31527-181 CORRODED AT LOWER LONGERON, PASSENGER DOOR ANGLE LOCATED AT STR 17 FS 342.7 - 317.70. FABRICATED ANGLE - 181 AND INSTALLED IAW WVAC EO 601R-53-2366.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 9,802 hrs · 10,029 cycles

RIGHT MLG DISAGREE WARNING. COULD NOT DUPLICATE. OPERATIONAL CHECKS WERE SATISFACTORY.

Part: VANE — CHAFED (WING) · airframe 7,735 hrs · 7,897 cycles

LEFT AND RIGHT INBOARD MOVEABLE VANE CAPS CHAFED BEYOND LIMITS. REMOVED CHAFED VANE CAPS AND INSTALLED NEW VANE CAPS (P/N 601R14303-10) IAW WVAC EO 601R-57-1350.

Part: FRAME — CRACKED (FUSELAGE) · airframe 7,735 hrs · 7,897 cycles

RIGHT FS 718.00 FRAME AND AFT DOUBLER CRACKED. REPAIRED RIGHT FS 718.00 FRAME AND AFT DOUBLER IAW CANADAIR REO 601R-53-61-193 REV A.

Part: STRIKER — DENTED (BS 349)

SEAL STRIKER AT FS 349.00 IS DENTED TOP AREA. REPAIRED SEAL STRIKER AT FS 349.00 TOP AREA IAW REO 601R-52-11-008 REV B REPAIR A.

Part: STRINGER — DENTED (FS 310)

FS 310 STRINGER 16-17 LHS PREVIOUS REPAIR DAMAGED BY PAX DOOR PIN. REMOVED AND REPAIRED AND INSTALLED NEW REPAIR IAW REO 601R-53-21-180 REV NC.

Part: DOWNLOCK PIN — INSTALLED (NLG)

NLG DID NOT RETRACT. DOWNLOCK PIN LEFT INSTALLED. REMOVED DOWNLOCK PIN.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

CARGO SMOKE AND OVERHEAT WARNINGS. REPLACED CARGO SMOKE DETECTORS.

Part: PITOT — DIRTY (LEFT)

AIRSPEED COMPARATOR WARNING DURING TAKEOFF. REMOVED FOREIGN MATERIAL FROM LEFT HAND PITOT HEAD.

Part: STRUT — LEAKING (NLG)

NLG DID NOT RETRACT WHEN GEAR SELECTED UP. REPLACED THE NLG PISTON TUBE ASSY.

Part: BULB — FAILED (EXTERIOR)

EXTERIOR EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB.

Part: FAN — OVERHEATED (AVIONICS)

STRONG ELECTRICAL BURNING SMELL IN COCKPIT. REPLACED THE DISPLAY COOLING FANS.

Part: FLEXSHAFT — CORRODED (LT WING)

LEFT SIDE TE FLAP NR 2 FLEXSHAFT FOUND UNSERVICEABLE DUE TO CORROSION. REPLACED FLEXSHAFT.

Part: FLEXSHAFT — DAMAGED (RT TE FLAP)

DURING C-CHECK, FOUND NR 5 TE FLAP FLEXSHAFT BAD (RIGHT WING) THREADS ON ONE OF THE B-NUTS WERE STRIPPED. REPLACED FLEXSHAFT.

Part: SKIN — CRUSHED (FUSELAGE)

MECHANIC NOTICED FORWARD AND AFT FUSELAGE SKIN IN THE AREA OF THE LOWER DOOR LATCH PINS WAS DAMAGED. SKIN WAS REPAIRED IN ACCORDANCE WITH REO NR 601R-53-21-176 AND 601R-53-21-160.

Part: SMOKE DETECTOR — MALFUNCTION (CARGO COMPT)

CARGO SMOKE WARNING DURING FLIGHT. REPLACED CARGO SMOKE DETECTOR.

Part: LIGHT — WATER CONTAM (CABIN)

CABIN EMERGENCY LIGHTS AT ROW 8 ARE INOP. CLEANED WATER FROM FLOOR PATH LIGHTING. LIGHTING SYSTEM FUNCTIONS NORMALLY.

Part: COMPUTER — MALFUNCTION (E/E COMPT)

STALL FAIL MESSAGE DURING FLIGHT. REPLACED THE STALL PROTECTION COMPUTER.

Part: HOSE — FAILED (RT PYLON)

HYDRAULIC LOW PRESSURE MESSAGE FOR SYSTEM NR 2 DURING CRUISE. REPLACED FAILED HYDRAULIC HOSES IN RIGHT ENGINE PYLON P/N AE-709006-1 AND AE-712030-1.