N986CA

Part: LIGHT — MALFUNCTIONED (LAVATORY) · airframe 39,133 hrs · 35,375 cycles

BURNING TYPE STRONG PUNGENT SMELL EMANATING FROM LAVATORY AREA. FLT#5295 REPLACED LAVATORY VANITY LIGHT ASSEMBLY.

Part: TAPER PIN — DEFECTIVE (CABIN DOOR) · airframe 38,163 hrs · 34,613 cycles

ACFT WOULD NOT PRESSURIZE ON TAKEOFF. RECEIVED CABIN ALT CAUTION MESSAGE AND COOL CAUTION MSG. FOUND MCD PRESSURIZATION FLAPPER DOOR STUCK OPEN WHEN MCD FULLY CLOSED. REPLACED TAPER PINS IAW AMM AND SRM. PRESSURIZED ACFT ON GROUND, PN'S: 601R38656-1 & MS24692-65AP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,924 hrs · 34,434 cycles

GALLEY FLOOR LEVEL EMERGENCY EXIT FLOODLIGHT IS BURNED OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: BEARING SEAL — DEFECTIVE (NLG) · airframe 37,342 hrs · 33,991 cycles

UPON SELECTING GEAR UP, WE RECEIVED A NOSE GEAR OPEN, WOW OUTPUT CAUTION, GEAR DISAGREE, WOW INPUT FAIL STATUS, STEERING INOPERATIVE MESSAGES. CYCLED NOSE STEERING AFTER CLEARING RUNWAY, STEERING CAME BACK ONLINE. (FLT 6532) REPLACED NLG LOWER BEARING SEALS IAW AMM AND SERVICED NLG SHOCK STRUT.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 37,198 hrs · 33,885 cycles

PASSENGER WINDOW BOLT HOLE UPPER FORWARD CORNER OF PASSENGER WINDOW CUTOUT BETWEEN FS 364 AND FS 379, LT SIDE. (SERVICE) COMPLETED REPAIR IAW REO AND SRM.

Part: UNKNOWN — ODOR (CABIN) · airframe 37,198 hrs · 33,885 cycles

F/A REPORTED BURNING SMELL AT ROW 9 C/D. (FLT 6362) REMOVED PANELS, INSPECTED WIRING AND BALLAST FOR LIGHTS, TURNED ON ALL LIGHT SYSTEMS FOR APPROXIMATELY 15 MINUTES, NO DEFECTS OR SMELL NOTED.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 36,508 hrs · 33,347 cycles

THERE IS DAMAGE ON LEFT STRINGER 4 JUST FORWARD OF FS 654.50 THAT PENETRATED COMPLETELY THROUGH THE STRINGER. (FLT 6195) PERFORMED TEMPORARY REPAIR ON STRINGER 4L AT FS 650.00 IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,090 hrs · 32,217 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5518) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,968 hrs · 32,127 cycles

NR 2 LEFT EXTERIOR EMERGENCY LIGHT BULB IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,952 hrs · 32,115 cycles

LEFT WING AFT EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 6387) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,762 hrs · 31,968 cycles

LEFT FORWARD EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6307) RELAMPED EMERGENCY LIGHT.

Part: INVERTER — FAILED (CABIN) · airframe 34,596 hrs · 31,835 cycles

RIGHT LOWER EMERGENCY EXIT ROW LIGHT IS OUT. (FLT 6195) INSTALLED INVERTER ASSEMBLY FOR RIGHT LOWER EMERGENCY EXIT LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,510 hrs · 31,768 cycles

NR 2 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6383) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,118 hrs · 31,476 cycles

NR 3 CEILING EMERGENCY LIGHT IS OUT. (FLT 6226) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,087 hrs · 31,443 cycles

AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 5629) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,982 hrs · 31,361 cycles

THE 2ND FROM AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5834) RELAMPED EMERGENCY LIGHT.

Part: RELAY — FAILED (EMERGENCY LIGHTS) · airframe 33,816 hrs · 31,218 cycles

EMERGENCY LIGHTS ON WHEN SWITCH IS IN ARMED POSITION. (FLT 6406) REPLACED POWER SOURCE RELAY K1XD IN JB6.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,721 hrs · 31,139 cycles

FS 280 FLOORBEAM CRACKED. (C-CHECK) REPAIR PER REO.

Part: POST — CRACKED (FUSELAGE) · airframe 33,721 hrs · 31,139 cycles

FS 409.00+128 RBL INBOARD AND OUTBOARD VERTICAL POSTS ARE CRACKED AT AFT RADIUS. (C-CHECK) REPAIR PER REO.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 35,459 hrs · 32,503 cycles

C-CHECK, CORROSION ALONG LEFT OUTBOARD FLOOR EDGE MEMBER FS 559+80 TO 621 AROUND NUT PLATE FASTENER ATTACH POINTS. REPAIRED LEFT OUTBOARD FLOOR EDGE MEMBER FS 559+80 TO 621.

Part: FRAME — CORRODED (BS 364) · airframe 35,459 hrs · 32,503 cycles

C-CHECK, HEAVY CORROSION ON BOTTOM FRAME FS 364 LBL 18 TO RBL 18 FORWARD TOP FRAME. REPAIRED BOTTOM FRAME STATION FS 364 LBL 18 TO RBL 18 FORWARD TOP FRAME.

Part: SILL — CORRODED (FUSELAGE) · airframe 35,459 hrs · 32,503 cycles

C-CHECK, SERVICE DOOR LOWER SILL AFT SIDE HAS CORROSION. REPAIRED SERVICE DOOR LOWER SILL AFT SIDE.

Part: SKIN — CORRODED (PAX DOOR) · airframe 35,459 hrs · 32,503 cycles

C-CHECK, PASSENGER DOOR INNER SKIN IS CORRODED. REPAIRED PASSENGER DOOR INNER SKIN PER SRM.

Part: BEAM — CORRODED (BS 280) · airframe 35,459 hrs · 32,503 cycles

C-CHECK, SURFACE CORROSION ON BS 280 BEAM BETWEEN LBL 9 AND RBL9. REPAIRED SURFACE CORROSION ON BS 280 BEAM BETWEEN LBL 9 AND RBL 9 IN REFERENCE TO SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,683 hrs · 31,101 cycles

LEFT MIDDLE EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5334) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,646 hrs · 31,061 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6442) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,593 hrs · 31,023 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5378) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,552 hrs · 30,993 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5820) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,249 hrs · 30,757 cycles

LEFT AFT OVERWING EMERGENCY OVERHEAD LIGHT IS OUT. (FLT 6340) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,143 hrs · 30,677 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6885) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 33,115 hrs · 30,653 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6334) RELAMPED EMERGENCY LIGHT.

Part: ROLLER — LACK OF LUBE (CABIN DOOR) · airframe 33,075 hrs · 30,623 cycles

MAIN CABIN DOOR IS DIFFICULT TO OPEN. (FLT 6476) LUBED MAIN CABIN DOOR LEVER ROLLER.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,918 hrs · 30,490 cycles

LEFT AND RIGHT FORWARD OVERWING EXTERIOR EMERGENCY LIGHTS ARE OUT. (FLT 6911) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,870 hrs · 30,447 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 694) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,708 hrs · 30,303 cycles

RIGHT FORWARD OVERWING EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 6999) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,708 hrs · 30,303 cycles

NR 1 CEILING EMERGENCY LIGHT IS OUT. (FLT 6631) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,534 hrs · 30,173 cycles

RIGHT WING AFT EMERGENCY EXIT LIGHT INOPERATIVE. (FLT 6467) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 32,127 hrs · 29,851 cycles

RIGHT FORWARD EXTERIOR EMERGENCY LIGHT OUT. (FLT 6334) RELAMPED EMERGENCY LIGHT.

Part: UNKNOWN — MALFUNCTIONED (CABIN DOOR) · airframe 31,007 hrs · 28,881 cycles

MAIN CABIN DOOR HARD TO OPEN. (FLT 6614) OPERATIONAL CHECK OF DOOR NORMAL.

Part: STRUCTURE — CORRODED (MAIN DOOR) · airframe 30,952 hrs · 28,836 cycles

MAIN DOOR LOWER AFT CORNER CORRODED UNDER STEP NR 1. (C CHECK) REPAIRED PER SRM.

Part: CIRCUIT BREAKER — TRIPPED (CABIN) · airframe 29,866 hrs · 27,902 cycles

EMERGENCY LIGHTS REMAIN ON WHEN IN THE ARMED POSITION. (FLT 5908) RESET CIRCUIT BREAKER.

Part: BEAM — CRACKED (FUSELAGE) · airframe 29,590 hrs · 27,646 cycles

FS 409 LBL 27 INBOARD VERTICAL BEAM CRACKED. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,031 hrs · 27,221 cycles

AFT CEILING EMERGENCY LIGHT INOP. (FLT 6565) RELAMPED EMERGENCY LIGHT.

Part: FITTING — GOUGED (FUSELAGE) · airframe 29,031 hrs · 27,221 cycles

THE 9G BULKHEAD FITTINGS GOUGED. (C CHECK) REPAIRED PER REO.

Part: ENGINE — SMOKE (RIGHT) · airframe 28,693 hrs · 26,961 cycles

RIGHT ENGINE PRODUCING SMOKE. (FLT 5863) INSPECTIONS AND ENGINE RUNS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,614 hrs · 26,893 cycles

EMERGENCY LIGHT INOP. (FLT 6656) RELAMPED EMERGENCY LIGHT.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 28,027 hrs · 26,459 cycles

GEAR DISAGREE MESSAGE. (FLT 6632) REPLACED NLG SELECTOR VALVE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,549 hrs · 25,969 cycles

FLT 2772 - REAR CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,866 hrs · 25,215 cycles

NR 1 CEILING EMERGENCY FLOOD LIGHT INOP (FLT 2771). RELAMPED EMERGENCY LIGHT.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 26,579 hrs · 24,860 cycles

MAIN CABIN DOOR WOULD NOT OPEN. FLIGHT 2531. LUBRICATED PAX DOOR IAW AMM 12-20-52. OPS CHECK GOOD.

Part: WIRE — LOOSE (FIRE LOOP) · airframe 26,086 hrs · 24,321 cycles

ON CLIMB OUT, RECEIVED A "LEFT JET OVHT FAIL" MESSAGE. MESSAGE CLEARED ON GROUND. (FLT 2701) INSPECTED LOOP A WIRING ON LEFT ENGINE AND REPLACED LOOSE TERMINAL END PER AMM 26-11-04. OPS CHECK GOOD.

Part: FLAP SYSTEM — UNKNOWN (TE FLAPS) · airframe 23,994 hrs · 22,536 cycles

FLIGHT 5251 - RECEIVED FLAP FAIL MESSAGE. LANDED WITHOUT INCIDENT. 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 MESSAGES.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 23,800 hrs · 22,382 cycles

FLIGHT 5507 - DURING DTW APPROACH RECEIVED A FLAP FAIL CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT INCIDENT. 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: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 23,752 hrs · 22,346 cycles

FLIGHT 5505 - RECEIVED FLAP FAIL CAUTION AT 42 DEGREES. 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 MESSAGES.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 23,430 hrs · 22,090 cycles

FLIGHT 4990 - EMERGENCY LIGHT FORWARD OF MAIN CABIN DOOR INOPERATIVE. FOUND CONNECTION LOOSE, RESECURED CONNECTION ON EMERGENCY LIGHT. OPS CHECK GOOD.

Part: CONTROLLER — MALFUNCTIONED (NLG STEERING) · airframe 22,802 hrs · 21,585 cycles

FLIGHT 5183 - DURING TAKEOFF ROLL AT BOS RECEIVED A STEERING INOPERATIVE CAUTION MESSAGE, CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED STEERING SYSTEM RESET.

Part: WARNING LIGHT — ILLUMINATED (LANDING GEAR) · airframe 20,454 hrs · 19,605 cycles

FLIGHT 5414 - GEAR DISAGREE WARNING. OPERATIONAL CHECK OF LANDING GEAR WAS SATISFACTORY.

Part: PSEU — MALFUNCTIONED (NLG) · airframe 19,794 hrs · 18,998 cycles

FLIGHT 5371 - GEAR DISAGREE WARNING, NLG FAILED TO RETRACT. REPLACED THE PSEU.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 18,131 hrs · 17,508 cycles

FLIGHT 5092 HYDRAULIC SYSTEM 1 LOW PRESSURE WARNING. REPLACED LEAKING LINE ASSY IN ROA.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 16,602 hrs · 16,255 cycles

FLIGHT 5584 NLG DOOR OPEN CAUTION AFTER GEAR RETRACTION. REPLACED THE NLG SELECTOR VALVE.

Part: WARNING LIGHT — ILLUMINATED (LANDING GEAR) · airframe 16,405 hrs · 16,086 cycles

FLIGHT 5499, GEAR DISAGREE WARNING. CLEANED ICE FROM LANDING GEAR. OPERATIONAL CHECK SATISFACTORY.

Part: SERVICE DOOR — OPEN (FUSELAGE) · airframe 15,683 hrs · 15,488 cycles

AIR SPEED AND MACH TRIM CAUTION, STALL FAIL CAUTION. THE 02 SERVICE DOOR FOUND OPEN. CLOSED SERVICE DOOR.

Part: WARNING SYSTEM — ACTIVATED (PAX DOOR) · airframe 15,255 hrs · 15,147 cycles

FLIGHT 5765 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. DEFERRED DOOR WARNING SYSTEM IAW MEL.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 15,249 hrs · 15,140 cycles

FLT 5077 CABIN DOOR OUTER HANDLE CAUTION MESSAGE. COULD NOT DUPLICATE, LUBED DOOR HANDLE.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 15,013 hrs · 14,944 cycles

FLT 5804 FLAPS FAIL MESSAGE DURING FLIGHT. REPLACED THE FECU.

Part: BPSU — DEFECTIVE (TE FLAPS) · airframe 14,522 hrs · 14,570 cycles

FLIGHT 5584 DURING DESCENT RECEIVED A FLAP FAIL CAUTION, CREW DECLARED AN EMERGENCY. REPLACED RIGHT BRAKE POSITION SENSING UNIT.

Part: BPSU — DEFECTIVE (LT TE FLAPS) · airframe 14,522 hrs · 14,570 cycles

FLIGHT 5584 DURING DESCENT RECEIVED A FLAP FAIL CAUTION, CREW DECLARED AN EMERGENCY. REPLACED THE LEFT BRAKE POSITION SENSING UNIT.

Part: COMPUTER — MALFUNCTIONED (TE FLAPS) · airframe 14,150 hrs · 14,563 cycles

FLIGHT 5422 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU.

Part: RADAR — INOPERATIVE (E/E BAY) · airframe 14,451 hrs · 14,503 cycles

FLIGHT 5359 WEATHER RADAR IS INOPERABLE IN-FLIGHT. REPLACED THE WEATHER RADAR.

Part: CONTROLLER — MALFUNCTIONED (AVIONICS) · airframe 13,728 hrs · 13,881 cycles

FLIGHT 5113 R/H WINDSHEILD HEAT CAUTION MESSAGE.REPLACED THE WINDSHIELD HEAT CONTROLLER.

Part: TRIM SWITCH · airframe 13,512 hrs · 13,697 cycles

FLIGHT 9458 AILERON MASTER CAUTION, T/O ABORTED.FOUND AILERON TRIM OUT OF THE TAKE OFF RANGE.

Part: PSEU — MALFUNCTIONED (AVIONICS) · airframe 13,432 hrs · 13,635 cycles

FLIGHT 5109 GEAR DISAGREE WARNING DURING RETRACTION.REPLACED THE PSEU

Part: PSEU — MALFUNCTIONED (AVIONICS) · airframe 13,432 hrs · 13,635 cycles

FLIGHT 5109 GEAR DISAGREE WARNING DURING RETRACTION.REPLACED THE PSEU

Part: WINDOW · airframe 13,374 hrs · 13,584 cycles

FLIGHT 5608 LEFT WINDOW HEAT CAUTION MESSAGE.SWITCHED TEMP SENSOR LEADS TO BACK UP SENSORS.

Part: LANDING GEAR · airframe 12,413 hrs · 12,705 cycles

FLIGHT 5460 LANDING GEAR DISAGREE WARNING.COULD NOT DUPLICATE. LANDING GEAR EXTENSION AND RETRACTION CHECKS NORMAL.

Part: WARNING SYSTEM · airframe 12,311 hrs · 12,603 cycles

FLIGHT 5295 CARGO DOOR CAUTION MESSAGE.DEFERRED MAINT PER MEL.

Part: PRIORITY VALVE — MALFUNCTIONED (NLG) · airframe 11,956 hrs · 12,254 cycles

FLIGHT 5234 GEAR DISAGREE MESSAGE ON APPROACH.REPLACED THE NLG PRIORITY VALVE.

Part: TRIM MOTOR — MALFUNCTIONED (HORZ STAB) · airframe 11,905 hrs · 12,207 cycles

FLIGHT 5297 STAB AND MACH TRIM FAIL MESSAGE.REPLACED THE HSTA

Part: ANGLE — CORRODED (FS280) · corrosion level 2 · airframe 11,526 hrs · 11,833 cycles

FWD J ANGLE AT F.S. 280.00 BETWEEN LBL9 AND RBL 9 IS CORRODED.REMOVED AND REPLACED FWD J-ANGLE AT FS 280.00 BETWEEN LBL9 AND RBL 9 I/A/W WVAC EO 601R-53-3229.

Part: SKIN — CRACKED (FS235) · airframe 11,526 hrs · 11,833 cycles

NLG WHEEL WELL SKIN CUT OUT HAS A CRACK IN THE R/H CORNER APPROXIMATELY 3/8 IN. LONG.REMOVED THE CRACKED PORTION OF SKIN CUT OUT, PERFORMED LPI INSPECTION, FABED REPAIR PARTS AND INSTALLED I/A/W CANADAIR R.E.O 601R-53-11-048 REV A AND W.V.A.C.E.O. 601R-53-3253.

Part: FRAME — CRACKED (FS718.0) · airframe 11,526 hrs · 11,833 cycles

THE R/H SIDE FRAME AT FS 718 WAS CRACKED BETWEEN STR'S 10 AND 11.REMOVED THE CRACKED PORTION OF FRAME AND INSTALLED A NEW SECTION OF FRAME I/A/W REO 601R-53-61-193 REV A.

Part: APU — FAILED (AFT EQUIP) · airframe 11,369 hrs · 11,692 cycles

FLIGHT 5432 SMOKE IN COCKPIT DURING BOARDING, APU AUTO-SHUTDOWN.DETERMINED APU TO BE SOURCE OF SMOKE - SECURED APU AND DEFERRED MAINT PER MEL.

Part: RECORDER · airframe 10,073 hrs · 10,406 cycles

FLIGHT #5352. FLIGHT DATA RECORDER MESSAGE ON EICAS.C/W TEST OF DFDR SYSTEM, NO DEFECTS.

Part: LIGHT · airframe 9,707 hrs · 10,030 cycles

DURING PRE-FLIGHT INSPECTION CREW FOUND THE EMERGENCY FLOOR LIGHTING ON THE RIGHT SIDE OF THE CABIN INOPERATIVE.RE-SECURED LOOSE CONNECTOR FOR THE RIGHT SIDE FLOOR EMERGENCY TRACK LIGHTS.

Part: SENSING ELEMENT — FAULTY (RIGHT GEARWELL) · airframe 9,700 hrs · 10,019 cycles

FLIGHT #5432. DURING TAXI OUT WHEN THRUST LEVERS WERE ADVANCED, RIGHT ANTI-ICE DUCT MESSAGE DISPLAYED, AIRCRAFT RETURNED TO THE GATE.REPLACED THE RIGHT GEARWELL SENSING ELEMENT.

Part: FLAP — CHAFED · airframe 9,475 hrs · 9,757 cycles

LT INBD FORE-FLAP CHAFFED AT IMPACT STRIPS.PERFORMED S.B. 601R-57-022.

Part: FLAP — CHAFED (RT WING) · airframe 9,475 hrs · 9,757 cycles

RT INBD FORE-FLAP CHAFFED AT IMPACT STRIPS.PERFORMED S.B. 601R-57-022

Part: TORQUE BOX — FAILED · airframe 9,475 hrs · 9,757 cycles

LEFT THRUST REVERSER BLOCKER DOOR HAS BROKEN ATTACH BRACKET AT 10 O'CLOCK POSITION.REMOVED AND REPLACED LEFT THRUST REVERSER TORQUE BOX ASSY.

Part: CONTROLLER — MALFUNCTIONED (ANTI-ICE SYS) · airframe 9,226 hrs · 9,490 cycles

ANTI ICE DUCT WARNING. REPLACED THE BLEED LEAK CONTROL UNIT.

Part: VALVE — MALFUNCTIONED (NLG) · airframe 9,205 hrs · 9,496 cycles

LANDING GEAR DISAGREE MESSAGE. NLG DID NOT RETRACT. REPLACED THE NLG PRIORITY VALVE.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 7,602 hrs · 7,874 cycles

FS 718 RIGHT AFT DOUBLER CRACKED BETWEEN STRINGERS 11 AND 12, LEFT HAND FRAME FLANGE AND AFT DOUBLER CRACKED BETWEEN STRINGERS 11 AND 12. REMOVED AND REPLACED RIGHT HAND AFT DOUBLER, REPAIRED LEFT HAND FRAME FLANGE, REMOVED AND REPLACED LEFT HAND AFT DOUBLER I/A/W CANADAIR REO 601R-53-61-193 REV A AND WVAC E.O. 601R-53-1481.

Part: WARNING SYSTEM — FALSE INDICATION (CARGO BAY) · airframe 7,140 hrs · 7,400 cycles

CARGO OVERHEAT MESSAGE. COULD NOT DUPLICATE. NO EVIDENCE OF OVERHEAT.

Part: SKIN — DENTED (FUSELAGE) · airframe 5,535 hrs · 5,637 cycles

LARGE DENT IN FUSELAGE IN FRONT OF GPU DOOR. REPAIRED LARGE DENTED AREA IN FRONT OF GPU DOOR IAW WVAC EO 601R-53-110B.

Part: INDICATION — MALFUNCTIONED (LANDING GEAR)

CREW REPORTED LANDING GEAR INDICATION WAS IN ERROR. LANDING GEAR RETRACTION CHECKS WERE NORMAL.

Part: SMOKE DETECTOR — ACTIVATED (LAVATORY)

THE LAVATORY SMOKE WARNING ACTIVATED DURING DESCENT INTO CVG. AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED SAFELY. INSPECTED THE CARGO AREA AND FOUND NO EVIDENCE OF SMOKE. PERFORMED TEST OF LAVATORY SMOKE DETECTOR, NO DEFECTS NOTED.

Part: HYD LINE — FAILED (LT PYLON)

NR 1 HYDRAULIC SYSTEM LOW PRESSURE WARNING. REPLACED LEAKING HIGH PRESSURE LINE IN LEFT HAND PYLON.

Part: WHEEL — CRACKED (MLG)

WHEEL WAS REMOVED FOR A BRAKE CHANGE. DURING CLEANING OF THE WHEEL SUB-ASSEMBLY A CRACK WAS DETECTED AT THE SPOKE IN THE WHEEL. (TOTAL TIRE CHANGES 14). WHEEL HAS BEEN REMOVED FROM SERVICE AND SENT TO ABS FOR EVALUATION.

Part: CONNECTOR — LOOSE (CABIN)

EMERGENCY FLOOR LIGHTING AFT OF WING IS INOPERABLE. RECONNECTED LOOSE WIRING CONNECTOR.

Part: STRIKER — DAMAGED (PASSENGER DOOR)

PAX DOOR SEAL STRIKER DAMAGED AT FS 310.00, LOWER PART OF PAX DOOR OPENING. REPAIRED IN ACCORDANCE WITH REO CRJ601R-52-11-008 REPAIR A.

Part: ANGLE — CRACKED (BS 621)

CARGO FLOOR SUPPORT ANGLE AT FS 621.00, WL 73, RIGHT SIDE CRACKED. REPAIRED IN ACCORDANCE WITH CANADAIR REO 601R-53-61-117 REV A.

Part: ANGLE — CRACKED (BS 621)

CARGO FLOOR SUPORT ANGLE AT FS 621.00, WL 73, LEFT SIDE IS CRACKED. REPAIRED IN ACCORDANCE WITH REO 601R-53-61-117 REV A.

Part: SUPPORT — CRACKED (BS 62100)

CARGO FLOOR SUPPORT ANGLES AT FS 62100, WL 73, LEFT AND RIGHT SIDE CRACKED. REMOVED CRACKED PART AND REPLACED WITH NEW ANGLE AND DOUBLER IAW CANADAIR REO 601R5361117, REV A.

Part: DUCT — LOOSE (E & E COMPT)

DISPLAY COOL CAUTION MESSAGE. CONNECTED LOOSE AVIONICS COOLING DUCT.

Part: BPSU — FAILED (LT TE FLAP)

FLAPS FAIL MESSAGE WHILE CLIMBING THROUGH 21,000 FEET. REPLACED LEFT BPSU AND PERFORMED EO 27-046.

Part: WARNING — ACTIVATED (TE FLAPS)

FLAP FAIL MESSAGE ILLUMINATED WHILE CLIMBING THROUGH 24,000 FEET. COMPLIED WITH EO 24-045 AND DEFERRED MAINT ACTION.

Part: CHECK VALVE — FAILED (APU COMPT)

APU AIR SUPPORT CHECK VALVE MISSING SPRING. REPLACED VALVE.

Part: FLEXSHAFT — CORRODED (RT TE FLAP)

RIGHT WING NR 5 FLAP FLEXSHAFT IS HEAVILY CORRODED. REMOVE AND REPLACE FLEXSHAFT.

Part: FLEXSHAFT — CORRODED (LT TE FLAP)

LEFT WING NR 5 FLEXSHAFT IS HEAVILY CORRODED. REPLACED FLEXSHAFT.

Part: PRESSURE SYST — MALFUNCTIONED (CABIN)

CABIN PRESSURE WAS FLUCTUATING AT 8,000 FT. COULD NOT DUPLICATE DISCREPANCY. SYSTEM TEST NORMAL.

Part: ICE DETECTOR — DEFECTIVE (NOSE SECTION)

DURING T/O ROLL AT STL ICE DETECTOR NR 1 WARNING ACTIVATED. REPLACED THE NR 1 ICE DETECTOR.

Part: HYDRAULIC LINE — CRACKED (AFT EQUIP BAY)

NR 1 HYDRAULIC SYSTEM LOW PRESSURE WARNING AND QUANTITY INDICATES 0 PERCENT. REPLACED CRACKED HYDRAULIC PRESSURE LINE ASSY IN AFT EQUIP BAY.

Part: PSEU — MALFUNCTION (E/E COMPT)

PROXIMITY SYSTEM FAULT MESSAGE ON EICAS DURING LANDING. REPLACED THE PROXIMITY SENSOR ELECTRONIC UNIT.

Part: WINDSHIELD — SHATTERED (RT COCKPIT)

COPILOTS WINDSHIELD SHATTERED DURING FLIGHT. REPLACED THE COPILOTS WINDSHIELD.

Part: TURBINE — DAMAGED (LT ENGINE)

LEFT ENGINE WILL NOT START. HUNG START TWO TRIES. FOUND DAMGE TO HPT. REPLACED ENGINE.

Part: LINE — LEAKING (NR 1 HYD SYST)

NR 1 HYDRAULIC SYSTEM FAILED DURING FLIGHT. REPLACED DEFECTIVE PRESSURE LINE AT LEFT PYLON.