N960CA

Part: CONTROL HANDLE — FAILED (TE FLAPS) · airframe 32,285 hrs · 28,197 cycles

ON FINAL RECEIVED FLAPS FAIL CAUTION MSG. EMERGENCY DECLARED, ACFT LANDED SAFELY. REMOVED AND REPLACED FLAP CONTROL HANDLE.

Part: BLEED VALVE — FAILED (LT ENGINE) · airframe 32,108 hrs · 28,047 cycles

EN ROUTE FROM JFK TO CLE LEFT 10TH STAGE BLEED VALVE FAILED TO OPEN. EMERGENCY DECLARED, A/C LANDED SAFELY AT CLE. REMOVED AND REPLACED LEFT 10TH STAGE BLEED VALVE.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 31,308 hrs · 27,438 cycles

COMPLIED WITH MODIFICATION K601R36009-3 ON LT FS 640.00 FRAME AND DOUBLER PER S/B601R-53-061 KIT DRWG K601R36009 REV B, 601R-53-61-506 REV C AND 601R53-61-569. REMOVED AND REPLACED SKIN PANEL BETWEEN LT AND RT TRU DOORS IAW CRJ SRM 51-42-06. DAMAGED SKIN JUST AFT OF LT TRU DOOR REPAIRED IAW REO 601R-53-1538.

Part: WIRE HARNESS — BROKEN (PAX DOOR) · airframe 31,020 hrs · 27,209 cycles

ON CLIMBOUT FROM CVG RECEIVED PAX DOOR OUTER HANDLE MSG. A/C RETURNED BACK TO CVG AND LANDED SAFELY. R&R PAX DOOR WIRE HARNESS. OPS CHECK GOOD.

Part: FLUX DETECTOR — FAILED (NR 2) · airframe 30,807 hrs · 27,020 cycles

EFIS COMP MON MSG, FIRST OFFICER`S HEADING DIFFICULT TO RIGHT. ACFT RETURNED BACK TO CVG, LANDED SAFELY. REMOVED AND REPLACED NR 2 FLUX DETECTOR. (S)

Part: FLOORBEAM — CRACKED (BS 559) · airframe 30,545 hrs · 26,805 cycles

DURING HMV NR 6 INSPECTION, NDT INSPECTION FOUND A CRACK ON THE FS 559 LBL 18, LOWER CAP ANGLE. CUT OUT DAMAGE SECTION OF CAP ANGLE AND SPLICED IN NEW SECTION WITH DOUBLERS IN ACCORDANCE WITH REO 601R 53-41-260. (S)

Part: BULKHEAD — CRACKED (FS 621 LBL 36) · airframe 30,545 hrs · 26,805 cycles

CRACK ON REAR PRESSURE BULKHEAD AT LBL 36.20 WL 80. REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1285. (S)

Part: STRINGER CLIP — CRACKED (BS 625 S15L) · airframe 30,545 hrs · 26,805 cycles

DURING HMV-6, INSPECTION FOUND FRAME 625 TO STRINGER 15L ATTACH CLIP CRACKED. REMOVED AND REPLACED CLIP IN ACCORDANCE WITH SRM 51-42-20. (S)

Part: POST — CRACKED (FS 409) · airframe 30,545 hrs · 26,805 cycles

DURING HMV-6, EDDY CURRENT INSPECTION FOUND CRACK ON LOWER POST, FS 409+128, LBL 18, OUTBOARD SIDE. CUT OUT DAMAGE AND INSTALLED A DOUBLER IN ACCORDANCE WITH REO 601R-53-41-056 REV E. (S)

Part: BULKHEAD — CRACKED (FS 621) · airframe 30,545 hrs · 26,805 cycles

REAR PRESSURE BULKHEAD CRACKED AT THE TOP OF LINTEL FITTING. REPAIRED REAR PRESSURE BULKHEAD AROUND LINTEL FITTING IAW REO 601R-53-61-1230. (S)

Part: FRAME — CRACKED (FS 640) · airframe 30,545 hrs · 26,805 cycles

DURING HMV-6, INSPECTION FOUND FLANGE OF FS 640 FRAME CRACKED BETWEEN STRINGERS 13R AND 14R. DAMAGED PORTION OF FLANGE CUT OUT AND REPAIR DOUBLER INSTALLED PER REO 601R-53-61-691. (S)

Part: FRAME — CRACKED (FS 640) · airframe 30,545 hrs · 26,805 cycles

LT FUSELAGE FRAME CRACKED AT FS 640 BETWEEN STRINGERS 9 & 10. PERFORMED MODIFICATION K601R36009-3 AS PER PART C OF SB 601R-53-061E. (S)

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,545 hrs · 26,805 cycles

CRACK ON REAR PRESSURE BULKHEAD ABOVE CARGO DOOR TRACK. REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1541. (S)

Part: STIFFENER — CRACKED (FS 280) · airframe 30,545 hrs · 26,805 cycles

DURING HMV-6, EDDY CURRENT INSPECTION FOUND VERTICAL WEB STIFFENER CRACKED ON FWD SIDE OF FS 280, RBL 12, AT AND ABOVE CABIN FLOOR LINE. REMOVED AND REPLACED DAMAGED ANGLE IN ACCORDANCE WITH SRM 51-42-06 AND 51-42-13. (S)

Part: DOUBLER — CRACKED (FS 718) · airframe 30,545 hrs · 26,805 cycles

RT FS 718.00 FRAME DOUBLER CRACKED ON THE AFT SIDE AT STRINGERS 10 AND 11. REMOVED AND REPLACED FRAME DOUBLER IAW BOMBARDIER REO 601R-53-61-243. (S)

Part: PAN — CRACKED (FS 193) · airframe 30,545 hrs · 26,805 cycles

FLOOR BELOW TRUSS CRACKED ON LT SIDE BELOW ACCUMULATOR GAUGE AT FS 193.00. REPAIRED FLOOR IAW REO 601R-53-11-081. (S)

Part: FLOORBEAM — CRACKED (BS 280) · airframe 30,545 hrs · 26,805 cycles

FS 280 FLOORBEAM (GALLEY SIDE) CRACKED. REPAIRED FS 280 FLOORBEAM IAW REO 601R-53-11-136. (S)

Part: BULKHEAD — CRACKED (FS 202) · airframe 30,545 hrs · 26,805 cycles

FORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE AT FS 202.75. REPAIRED FORWARD PRESSURE BULKHEAD AT FS 202.75 IAW CRJ REO 601R-53-11-563. (S)

Part: BRACKET — BENT (NLG) · airframe 30,000 hrs · 26,372 cycles

FLIGHT 5458 - RECEIVED GEAR DISAGREE MESSAGE AND NOSE DOOR WARNING. NOSE GEAR DID NOT INDICATE UP. COMPLIED WITH QRH. RETURNED TO ATL, LANDED WITHOUT INCIDENT. FOUND NLG OLEO SENSOR BRACKET BENT, INCREASING SENSOR GAP BEYOND LIMIT. REWORKED BRACKET. NO FURTHER DEFECTS.

Part: ANTI-ICE SYSTEM — MALFUNCTIONED (WINGS) · airframe 29,297 hrs · 25,811 cycles

FLIGHT 5181 - DURING TAKEOFF ROLL RECEIVED A WING OVERHEAT WARNING MESSAGE, ABORTED T/O AND RETURNED TO THE GATE. DEFERRED WING ANTI-ICE SYSTEM PER MEL 30-12-03.

Part: NONE — NONE (RT WING) · airframe 28,211 hrs · 24,958 cycles

TEMPORARY REPAIR INCORPORATED FOR RIGHT LOWER WING PLANK CRACK AT WS 148.019 IAW REO 601R-57-21-138. COMPLIED WITH PERMANENT REPAIR OF THE RIGHT LOWER WING PLANK CRACK IAW REO 601R-57-21-130 REV G AND CRJ REO 601R-57-21-829.

Part: NONE — NONE (NONE) · airframe 28,211 hrs · 24,958 cycles

TEMPORARY REPAIR INCORPORATED FOR LEFT LOWER WING PLANK CRACK AT WS 148.019 IAW REO 601R-57-21-138. COMPLIED WITH PERMANENT REPAIR OF THE LEFT LOWER WING PLANK CRACK IAW REO 601R-57-21-130 REV G AND CRJ REO 601R-57-21-829.

Part: PRESSURE SWITCH — FAULTY (RT ENGINE) · airframe 27,975 hrs · 24,780 cycles

FLIGHT 5637 - RIGHT ENGINE OIL PRESSURE WARNING DURING CLIMBOUT, AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED RIGHT ENGINE OIL PRESSURE SWITCH. OPS CHECK GOOD.

Part: TRIM SWITCH — FAULTY (COCKPIT) · airframe 27,367 hrs · 24,308 cycles

FLIGHT 5078 - DURING CLIMBOUT CAPTAIN SIDE STAB TRIM WOULD NOT MOVE IN THE DOWN POSITION. AIRCRAFT RETURNED BACK TO BOS AND LANDED SAFELY. REMOVED AND REPLACED CAPTAIN SIDE PITCH TRIM SWITCH.

Part: WARNING SYSTEM — MALFUNCTIONED (DOOR WARNING) · airframe 26,962 hrs · 23,996 cycles

FLIGHT 5056 - DURING CLIMBOUT OF BNA RECEIVED A CABIN DOOR OUTER HANDLE MESSAGE, FLIGHT RETURNED TO BNA. PERFORMED AN OPERATIONAL CHECK OF THE CABIN DOOR OUTER HANDLE AND INDICATION, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE.

Part: WINDOW — CRACKED (COCKPIT) · airframe 26,496 hrs · 23,613 cycles

FLIGHT 5674 - DURING CRUISE FLIGHT, THE LEFT SIDE COCKPIT WINDOW CRACKED. REPLACED THE LEFT COCKPIT SIDE WINDOW.

Part: CONTROL HANDLE — FAULTY (TE FLAPS) · airframe 26,312 hrs · 23,470 cycles

FLIGHT 9482 - DURING APPROACH, FLAPS FAILED AT 30 DEGREES. CREW LANDED WITHOUT INCIDENT. REPLACED FLAP CONTROL HANDLE.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 25,580 hrs · 22,897 cycles

FLIGHT 5301 - CAPTAIN'S WINDSHIELD SHATTERED. REMOVED AND REPLACED CAPTAIN'S WINDSHIELD.

Part: RESERVOIR — MALFUNCTIONED (NR 3 HYD SYSTEM) · airframe 24,106 hrs · 21,678 cycles

FLIGHT 5064 - GEAR DISAGREE WARNING. REPLACED THE NR 3 HYDRAULIC RESERVOIR.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 23,638 hrs · 21,274 cycles

FLIGHT 5521 - GEAR DISAGREE WARNING. REPLACED THE MLG SELECTOR VALVE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 22,179 hrs · 20,016 cycles

FLIGHT 5164, LEFT AND RIGHT AOA HEAT CAUTION. RESET SYSTEM. COULD NOT DUPLICATE.

Part: BATTERY — MALFUNCTIONED (APU) · airframe 20,629 hrs · 18,690 cycles

FLIGHT 5721 DURING CRUISE FLIGHT APU BATTERY INDICATED 99 AMPS, AIRCRAFT DIVERTED TO CLE. DEFERRED THE APU BATTERY PER MEL 24-32-03.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 20,456 hrs · 18,542 cycles

FLIGHT 5399 LEFT THRUST REVERSER UNLOCKED CAUTION MESSAGE. DEFERRED MAINT ON T/R PER MEL.

Part: OXYGEN MASK — ACTIVATED (ROW 9) · airframe 19,987 hrs · 18,170 cycles

FLIGHT 5118 02 MASK AT ROW 9 DROPPED DURING T/O. RESTOWED 02 MASKS AT ROW 9.

Part: PROXIMITY SENSOR — OUT OF ADJUST (E&E BAY DOOR) · airframe 17,017 hrs · 15,746 cycles

FLIGHT 9492 AVIONICS DOOR CAUTION MESSAGE AT 8000 FT. ADJUSTED THE AVIONICS DOOR PROXIMITY SENSOR.

Part: PUMP — MALFUNCTIONED (3A) · airframe 17,009 hrs · 15,740 cycles

FLIGHT 5510 GEAR DISAGREE WHEN GEAR SELECTED DOWN.REPLACED THE #3A ACMP

Part: COWLING — CRACKED (RT ENGINE) · airframe 15,000 hrs · 14,109 cycles

RIGHT ENGINE FIXED CORE COWL IS CRACKED IN AFT CHANNEL APPROX 1/5 INCH. REPAIRED CRACK BY STOP DRILLING AND INSTALLING A DOUBLER IAW SHORTS CMM 71-13-01 REPAIR SRS 065 AND REO 601R-71-13-1989.

Part: BUSHING — DAMAGED (HORIZ STAB) · airframe 15,001 hrs · 14,109 cycles

THE RIGHT VERTICAL STABILIZER HINGE BUSHING WAS DAMAGED AND REQUIRES REPLACEMENT. REMOVED AND REPLACED BUSHING IAW WVAC EO 601R-55-3359 CRJ AMM 20-26-00-910-803.

Part: FLAP · airframe 14,972 hrs · 14,080 cycles

FLAPS FAILED MESSAGE AFTER LANDING.RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.

Part: COMPUTER — MALFUNCTIONED (AVIONICS) · airframe 14,113 hrs · 13,356 cycles

FLIGHT 5860 MACH TRIM/STAB TRIM CAUTION MESSAGE.REPLACED THE HSTCU.

Part: SPRING — STUCK (AVIONICS) · airframe 13,700 hrs · 12,990 cycles

FLIGHT 5602 AVIONICS BAY DOOR WARNING DURING T/O.FOUND AVIONICS DOOR SWITCH JAMMED. REPLACED SWITCH SPRING.

Part: FLAP · airframe 13,618 hrs · 12,914 cycles

FLIGHT 5553 FLAPS FAILED AT 30 DEGREES DURING APPROACH.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.

Part: COMPUTER · airframe 13,604 hrs · 12,900 cycles

FLIGHT 5285 CONFIG AILERONS AND CONFIG TRIM AURAL WARNING DURING T/O.COULD NOT DUPLICATE. TEST OF AILERON TRIM SYSTEM WAS NORMAL.

Part: PLANK — CRACKED (WING) · airframe 13,495 hrs · 12,800 cycles

EDDY CURRENT INDICATES CRACKS.BLENDED OUT DAMAGE AND ROTO-PEENED I/A/W REO 601R-57-21-030.

Part: BEAM — CRACKED (AFT EQUIP BAY) · airframe 13,495 hrs · 12,800 cycles

ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W REO601R-53-61-345.

Part: BEAM — CRACKED (AFT EQUIP BAY) · airframe 13,495 hrs · 12,800 cycles

ENGINE SUPPORT BEAM CRACKED.REPAIRED DAMAGE I/A/W REO 601R-53-61-366.

Part: SWITCH — FAULTY (COCKPIT) · airframe 13,049 hrs · 12,420 cycles

FLIGHT #5570. DURING TEST OF THE YAW DAMPER SYSTEM THE #2 WOULD NOT ENGAGE.REPLACED THE YAW DAMPER SWITCH.

Part: CONTROLLER — FAULTY (WINDOW HEAT) · airframe 12,704 hrs · 12,091 cycles

FLIGHT 5697. DURING CLIMBOUT OF CVG RECEIVED A RIGHT WINDOW HEAT CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD. REPLACED THE WINDSHIELD HEAT CONTROLLER.

Part: WINDSHIELD — FAULTY (NOSE) · airframe 12,704 hrs · 12,091 cycles

FLIGHT #5697. DURING CLIMB OUT OF CVG RECEIVED A RIGHT WINDOW HEAT CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD.REPLACED THE RIGHT WINDSHIELD.

Part: BOLT — MISLOCATED (EMPENNAGE) · airframe 12,613 hrs · 12,006 cycles

FLIGHT #5424. DURING CRUISE FLIGHT DESTINATION YYZ WITH THE AUTOPILOT ENGAGED, RT RUDDER TRIM OF 1.5 UNITS AND LT. DOWN AILERON TRIM OF .5 UNITS HAD TO BE SET TO KEEP STRAIGHT AND LEVEL FLIGHT.UPON INVESTIGATION FOUND THE LOWER MOUNTING BOLT FOR THE #1 YAW DAMPER LINEAR ACTUATOR NOT INSTALLED CORRECTLY, REMOVED AND CORRECTLY-REINSTALLED LOWER MOUNTING BOLT.

Part: DAMPENER — FAULTY (EMPENNAGE) · airframe 12,612 hrs · 12,005 cycles

FLIGHT #5960. AT THE GATE READY FOR PUSH-BACK RECEIVED YAW DAMPER #1 INOPERATIVE MESSAGE.REPLACED THE #1 YAW DAMPER.

Part: STRUT · airframe 12,549 hrs · 11,943 cycles

NOSE LANDING GEAR DISAGREEMENT AFTER TAKE OFF FROM TYS, AIRCRAFT RETURNED TO THE FIELD.PERFORMED FULL SERVICE OF THE NLG SHOCK STRUT TO ALLOW FULL EXTENSION OF STRUT UNDER A NO-LOAD CONDITION.

Part: SPOILER · airframe 2,457 hrs · 11,849 cycles

CONFIG AILERON AND CONFIG SPOILER WARNINGS DURING T/O.COULD NOT DUPLICATE. FOUND CONFIG WARNING SYSTEM FUNCTIONED PROPERLY.

Part: DOOR — OPEN (SERVICE) · airframe 12,001 hrs · 11,390 cycles

EXIT/SERVICE DOOR POPPED OPEN INFLIGHT. INSPECTED FOR DAMAGE, AND CLOSED DOOR.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 11,958 hrs · 11,346 cycles

STALL WARNING DURING T/O. RESET THE STALL COMPUTER.

Part: STRUT — MALFUNCTIONED (NLG) · airframe 11,883 hrs · 11,277 cycles

NLG DID NOT RETRACT, THUMPING NOISE FROM NLG AREA. SERVICED NLG SHOCK STRUT.

Part: WARNING LIGHT — ILLUMINATED (MLG) · airframe 11,870 hrs · 11,263 cycles

NLG DISAGREE MESSAGE,NLG DID NOT INDICATE UP. COULD NOT DUPLICATE. LANDING GEAR RETRACT CHECKS WERE NORMAL.

Part: WARNING LIGHT — ILLUMINATED (PAX DOOR) · airframe 11,788 hrs · 11,187 cycles

CABIN DOOR OUTER HANDLE CAUTION MESSAGE AND DOOR WARNING MESSAGE.ADJUSTED DOOR INNER HANDLE MECHANISM.

Part: WARNING LIGHT — ILLUMINATED (PAX DOOR) · airframe 18,050 hrs · 17,360 cycles

CABIN DOOR LATCH WARNING DURING CLIMB OUT OF ATW, RETURNED TO THE FIELD.DEFERRED PER MEL 52-70-1.

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 11,786 hrs · 17,350 cycles

SPOILER FAULT CAUTION DURING CRUISE FLIGHT. RESET THE SPOILER ELECTRONIC CONTROL UNITS.

Part: CIRCUIT BOARD — BURNED (COCKPIT) · airframe 11,772 hrs · 11,168 cycles

LEFT WINDSHIELD HEAT CAUTION MESSAGE. REPLACED BURNED CIRCUIT BOARD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 11,639 hrs · 11,041 cycles

STALL FAIL CAUTION DURING TAKE OFF. RESET STALL COMPUTER.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 11,604 hrs · 11,015 cycles

STALL FAIL WARNING DURING T/O. RESET STALL COMPUTER.

Part: CONTROLLER — MALFUNCTIONED (COCKPIT) · airframe 11,516 hrs · 10,934 cycles

LEFT WINDOW HEAT CAUTION MESSAGE. REPLACED WINDOW HEAT CONTROLLER.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 11,433 hrs · 10,868 cycles

EFIS COMP MON CAUTION DURING T/O. COULD NOT DUPLICATE. MDC HAD NO FAULT CODES.

Part: SPLICE — MISMANUFACTURED (FUSELAGE) · airframe 11,425 hrs · 10,861 cycles

SPLICE PLATE 601R31030-77 WAS FABRICATED INCORRECTLY BY MANUFACTURER. REPAIRED SPLICE PLATE 601R31030-77 AND FABRICATED DOUBLER PLATE IAW WVAC EO 601R-53-1804.

Part: BUSHING — DISLODGED (VERTICAL STAB) · airframe 11,425 hrs · 10,861 cycles

LEFT HAND AND RIGHT HAND VERTICAL STABILIZER BUSHINGS ARE MIGRATED AT HORIZONTAL STABILIZER PIVOT POINT. REMOVED MIGRATED BUSHINGS. INSTALLED NEW BUSHINGS P/N 600-21061-7 (THAT WERE MACHINED IAW WVAC EO 601R-55-1834) IAW CRJ AMM 20-26-00-910-803. REAMED TO FINAL TOLERANCE 1.5001'''' AND 1.5002 IAW DWG 600-21029.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 11,425 hrs · 10,861 cycles

VERTICAL J STIFFENER AT FS 280 INSIDE CBP1 OUTBOARD LBL 9 IS CRACKED. FABBED AND INSTALLED A NEW VERTICAL J STIFFENER AT FS 280 IAW WVAC EO 601R-53-1805A.

Part: FRAME — CRACKED (FUSELAGE) · airframe 11,044 hrs · 10,508 cycles

FRAME FLANGE CRACKED AND AFT DOUBLER CRACKED AT FS 718.0 STR 11 - 12 LT AND RT. PERFORMED A MAJOR REPAIR TO CRACKED FRAME FLANGES AND AFT DOUBLERS AT FS 718.0 STR 11 - 12 LT AND RT IAW CRJ REO 601R-53-61-192 REV A.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 10,591 hrs · 10,115 cycles

FLAPS FAIL CAUTION MESSAGE. REPLACED THE LEFT HAND BPSU.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,485 hrs · 10,032 cycles

EMERGENCY LIGHT AT CABIN DOOR IS INOPERABLE. RECONNECTED WIRES AT LIGHT. OPERATION OF LIGHT SATISFACTORY.

Part: CONNECTOR — INOPERATIVE (CABIN) · airframe 10,433 hrs · 9,985 cycles

FORWARD SECTION OF EMERGENCY FLOOR LIGHTING IS INOPERABLE. REPLACED CABLE CONNECTOR.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 10,354 hrs · 9,928 cycles

FLOOR SUPPORT ANGLES CRACKED AT FS 484.00 RIGHT HAND SIDE AND LEFT HAND SIDE. REPAIRED FLOOR SUPPORT ANGLES AT FS 484.00 RIGHT HAND AND LEFT HAND SIDES IAW WVAC EO 601R-53-1341A.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 10,035 hrs · 9,642 cycles

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

Part: SKIN — CRACKED (WS 76 - 163)

LEFT LOWER WING ACCESS HOLES 540 CB - WS 76.161 AND 550 AB - WS 163.000 CRACKED. REPAIRED DAMAGED IAW REO 601R-57-21-030.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

STABILIZER AND MACH TRIM CAUTION MESSAGE. COULD NOT DUPLICATE. NO FAULT CODES IN COMPUTER. SYSTEM CHECKS NORMAL.

Part: BATTERIES — DISCHARGED (CABIN)

EMERGENCY LIGHTS ARE INOP. REPLACED THE EMERGENCY BATTERIES.

Part: ACTUATOR — FAILED (TE FLAP)

FLAP FAIL CAUTION WARNING ACTIVATED DURING APPROACH INTO CVG. REPLACED THE INBOARD FLAP ACTUATORS.

Part: CHECK VALVE — FAILED (RT ENGINE)

INFLIGHT SHUT DOWN NR 2 ENGINE DUE TO LOW OIL PRESSURE. REPLACED THE OIL REPLENISH SYSTEM CHECK VALVE.

Part: FAN — FAILED (CABIN)

SMOKE IN CABIN. REPLACED BROKEN FAN BY PASS CHECK VALVE.

Part: FLEXSHAFT — SEPERATED (RT ENG TR UNIT)

RIGHT THRUST REVERSER NR 2 FLEXSHAFT HAS STRAND SEPARATION. REPLACED FLEXSHAFT.

Part: DAMPENER — LEAKING (LT AILERON)

DURING C-CHECK, FOUND LEFT AILERON FLUTTER DAMPENER LEAKING AROUND PISTON SIGHT GLASS. REPLACED FLUTTER DAMPENER.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO)

CARGO SMOKE WARNING. REPLACED CARGO SMOKE DETECTORS.

Part: RIVET — BURNED (BS 333)

DURING LIGHTNING STRIKE INSPECTION, FOUND A DEEP BURN ON AIRCRAFT BELLY AT FUSELAGE STATION 333.00. UPON FURTHER INVESTIGATION, FOUND BURN TO BE IN A RIVET HEAD. REMOVED THE RIVET AND INSTALLED A NEW ONE IN ACCORDANCE WITH CANADAIR STRUCTURAL REPAIR MANUAL CHAPTER 51-42-06.

Part: ADC — MALFUNCTION (NR 2)

COPILOTS AIRSPEED INDICATION IS ERRATIC. REPLACED THE NR 2 ADC.

Part: WARNING — ACTIVATED (CABIN DOOR)

CABIN DOOR OUTER HANDLE CAUTION MESSAGE ON EICAS. COULD NOT DUPLCIATE DISCREPANCY. DOOR AND HANDLE OPERATION AND INDICATION NORMAL.

Part: RELAY — FAILED (AC BUS)

AC ESS BUS FAILED AFTER NR 1 ENGINE START. REPLACED RELAY K3XD.

Part: DETECTOR — MALFUNCTIONED (LT ENGINE)

14TH STAGE DUCT LEAK WARNING DURING FLIGHT. ENGINE WAS SHUT DOWN, BUT WARNING REMAINED. REPLACED DEFECTIVE 14TH STAGE BLEED LEAK DETECTOR.

Part: ACTUATOR — LEAKING (NLG STEERING)

NOSE WHEEL STEERING ACTUATORS LEAKING. REPLACED THE STEERING ACTUATORS.

Part: SECU — INOPERATIVE (NR 2)

SPOILER FAULT MESSAGE ON EICAS. REPLACED NR 2 SECU, OPERATIONAL CHECK GOOD.

Part: DOOR — FOD (CABIN)

CABIN DOOR WARNING ON DURING FLIGHT. REMOVED 5 CENT FOD 1 US NICKEL FROM DOOR FRAME. DOOR WARNING CHECK SATISFACTORY.

Part: SENSOR — FAILED (PAX DOOR)

PAX DOOR LATCH CAUTION MESSAGE CAME ON IN FLIGHT. REPLACED PROX SENSOR ON NR 1 LATCH PIN, OPS CHECK GOOD.

Part: SECU — FAILED (NR 1 SPOILER)

SPOILERONS FAULT MESSAGE ON EICAS. REPLACED THE NR 1 SPOILER ELECTRONIC CONTROL UNIT.