N963CA

Part: SLIDE — PUNCTURED (ZONE 200) · airframe 68,473 hrs · 17,292 cycles

DURING ROUTINE MAINTENANCE TO REPLACE DOOR 4 LEFT EVACUATION SLIDE/RAFT, SLIDE/RAFT DEPLOYED INSIDE THE AIRCRAFT. WHEN INSTALLING THE CYLINDER SAFETY PIN PER AIRCRAFT MAINTENANCE MANUAL (AMM) TASK 25-66-01-004-154, SUBTASK 25-66-01-014-006, THE CYLINDER SAFETY PIN WOULD NOT FULLY INSTALL. AN ALLEN WRENCH WAS USED AS INSTRUCTED IN THE AMM SUBTASK, BY TURNING THE MECHANISM IN THE COUNTERCLOCKWISE DIRECTION. THE SLIDE INFLATED IN THE GALLEY AREA, CAUSING MINOR INJURY TO THE TECHNICIAN. DUE TO THE TECHNICIAN BEING TRAPPED, THE INFLATABLE WAS PUNCTURED TO RELEASE THE PRESSURE. SERVICEABLE SLIDE/RAFT WAS INSTALL WITHOUT INCIDENT.

Part: NONE — NONE · airframe 67,912 hrs · 17,100 cycles

GIRT BAR LIGHT INOPERATIVE AT DOORS L1, L2, R1, AND R2 WHEN DOOR IS SELECTED TO ENGAGE. CIRCUIT BREAKER POPPED - DEFERRED PER MINIMUM EQUIPMENT LIST 25-66-05-01.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 67,904 hrs · 17,097 cycles

EMERGENCY LIGHT POWER SUPPLY MODULE INOPERATIVE - REPLACED BATTERY PACK PER AIRCRAFT MAINTENANCE MANUAL 33-51-07, TEST NORMAL.

Part: ACTUATOR — DEFECTIVE (ZONE 100) · airframe 81,050 hrs · 16,470 cycles

DURING SCHEDULED OPERATION TEST OF THE L/H OVER-WING ESCAPE SLIDE DEPLOYMENT SYSTEM, SLIDE FAILED TO DEPLOY. FOUND SLIDE PACK DEPLOYMENT ACTUATOR DEFECTIVE. REMOVED AND REPLACED ACTUATOR PER B757 AMM 25-65-03. OPS CHECK NORMAL.

Part: NONE — NONE · airframe 67,345 hrs · 16,906 cycles

#1 RIGHT ENTRY DOOR DIFFICULT TO ARM - RE-SECURED GIRT BAR PER AIRCRAFT MAINTENANCE MANUAL 25-66-01. DOOR ARM/DISARM NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,263 hrs · 16,561 cycles

LEFT OVERWING EMERGENCY EXIT SIGN LIGHT WILL NOT ILLUMINATE - REMOVED AND REPLACED THE BATTERY PACK PER AIRCRAFT MAINTENANCE MANUAL 33-51-07.

Part: SKIN — DENTED (BS 475-485) · airframe 66,257 hrs · 16,559 cycles

REFERENCE 722R'S NON-ROUTINE TASK #049: EXISTING DENT AT BS 480, STRINGER 17L, EXCEEDS B757 SRM LIMITS AND HAS A CREASE. ACCOMPLISHED A CAT-B EXTERNAL DOUBLER REPAIR WITH FIRST STAGE APPROVAL (PENDING DTA TO DETERMINE ULTIMATE REPAIR CATEGORY) AS PER FVCI EO 21095-1 REV. A, DATED 05/29/2021, AND APPROVED BY 8110-3 DATED 06/30/2021, AND ISSUED BY DERT-710167-SW.

Part: SKIN — DENTED (BS 1595-1605) · airframe 66,257 hrs · 16,559 cycles

REFERENCE 722R'S NON-ROUTINE TASK #049: EXISTING DENT AT BS 1600, BETWEEN STRINGER 17L AND 18L, EXCEEDS B757 SRM LIMITS. ACCOMPLISHED A CAT-B EXTERNAL DOUBLER REPAIR WITH FIRST STAGE APPROVAL (PENDING DTA TO DETERMINE ULTIMATE REPAIR CATEGORY) AS PER FVCI EO 21095-2 REV. A, DATED 05/29/2021, AND APPROVED BY 8110-3 DATED 06/30/2021, AND ISSUED BY DERT-710167-SW.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 36,255 hrs · 32,523 cycles

STRINGER 14L ATTACH CLIP CRACKED AT FS 621 FRAME. REMOVED AND REPLACED STRINGER ATTACH CLIP.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 36,255 hrs · 32,523 cycles

STRINGER 14R ATTACH CLIP CRACKED AT FS 621 FRAME. REMOVED AND REPLACED STRINGER ATTACH CLIP.

Part: SKIN — CRACKED (LT WING) · airframe 35,798 hrs · 32,046 cycles

CRACK FOUND ON LT WING ABOUT 6" FROM JACK PAD. REPAIRED LT LOWER WING PLANK AT WS 148.019 IAW BOMBARDIER GREO 601R-57-21-130 REV. -J REPAIR OPTION II.

Part: UNKNOWN — MALFUNCTIONED (NLG STEERING) · airframe 35,481 hrs · 31,739 cycles

EN ROUTE FROM ATL TO TYS RECEIVED NWS INOP CAUTION MSG, WOULD NOT RESET. EMERGENCY DECLARED, A/C LANDED SAFELY IN TYS. AFTER LANDING RESET NWS OPS CHECK GOOD DURING TAXI IN. PERFORMED OPS TEST OF NWS PER AMM. NO FURTHER DEFECTS.

Part: ECU — MALFUNCTIONED (NLG STEERING) · airframe 35,318 hrs · 31,583 cycles

ON APPORACH INTO DTW RECEIVED NOSE WHEEL STEERING CAUTION MSG WHEN LANDING GEAR WAS SELECTED DOWN. EMERGENCY DECLARED, A/C LANDED SAFELY. PERFORMED OPS CHECK OF NWS ECU. OPS CHECK GOOD.

Part: BPSU — FAILED (TE FLAP) · airframe 34,538 hrs · 30,810 cycles

DECENDING INTO MEM AT 14000FT RECEIVED FLAPS FAIL CAUTION MSG, FLAPS FAILED AT 0 DEG. RAN QRH. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED RIGHT BPSU.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 34,535 hrs · 30,808 cycles

ON APPROACH INTO MCI RECEIVED FLAPS FAIL CAUTION MSG AT 12000FT, RAN QRH. EMERGENCY DECLARED, A/C LANDED SAFELY AT MCI. TRANSFERRED TO DEFERRED LIST PER MEL GMM 8.4 CAT 1.

Part: CONTROL UNIT — FAILED (TE FLAP) · airframe 34,538 hrs · 30,810 cycles

DECENDING INTO MEM AT 14000FT RECEIVED FLAPS FAIL CAUTION MSG, FLAPS FAILED AT 0 DEG. RAN QRH. EMERGENCY DECLARED, A/C LANDED SAFELY. REMOVED AND REPLACED FECU.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 33,717 hrs · 30,047 cycles

ON CLIMBOUT FROM GSO TO ATL RIGHT WINDSHIELD OUTER LAYER SHATTERED. EMERGENCY DECLARED, A/C LANDED SAFELY AT ATL. REMOVED AND REPLACED RIGHT WINDSHIELD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 33,698 hrs · 30,031 cycles

ON CLIMBOUT FROM MDT TO CVG LEFT WINDSHIELD CRACKED. EMERGENCY DECLARED, A/C DIVERTED TO IAD LANDED SAFELY. REMOVED AND REPLACED LEFT WINDSHIELD.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 33,494 hrs · 29,839 cycles

ON APPROACH INTO EWR WHEN SELECTING GEAR DOWN RECEIVED GEAR DISAGREE WARNING MSG. FOLLOWED QRH, EMERGENCY DECLARED A/C LANDED SAFELY. REMOVED AND REPLACED MAIN LANDING GEAR SELECTOR VALVE.

Part: FAN — FAILED (CABIN) · airframe 33,158 hrs · 29,527 cycles

EN ROUTE TO JFK RECEIVED DISPLAY COOL CAUTION MSG. PERFORMED QRH, MSG WOULD NOT CLEAR. EMERGENCY DECLARED, A/C LANDED SAFELY IN JFK. REMOVED AND REPLACED PRIMARY FAN.

Part: SELECTOR VALVE — FAILED (NLG DOOR) · airframe 32,767 hrs · 29,169 cycles

ON CLIMBOUT FROM MSP RECEIVED NOSE GEAR DOOR OPEN WARNING MSG. EMERGENCY DECLARED, A/C RETURNED TO MSP LANDED SAFELY. REMOVED AND REPLACED NOSE LANDING GEAR DOOR SELECTOR VALVE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 32,686 hrs · 29,102 cycles

FOUND CORROSION BETWEEN LBL 9 AND RBL 9 AT FS 280.00 ON FORWARD FLOOR ANGLE. TREATED CORROSION IAW SRM 51-25-01 AND REPAIRED SUPPORT ANGLE IAW REO 601R-53-11-137.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,686 hrs · 29,102 cycles

AT FS 559.00 THE FRAME CAP ANGLE IS CRACKED AT RBL 18.00. REPAIRED RT CAP ANGLE AT RBL 18 IAW REO 601R-53-41-260 RT REP.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 32,686 hrs · 29,102 cycles

FOUND CORROSION BETWEEN LBL 9 AND RBL 9 AT FS 280.00 ON FORWARD FLOOR ANGLE. TREATED CORROSION IAW SRM 51-25-01 AND REPLACED CAM-LOC ANGLE IAW SRM 51-42-06.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,686 hrs · 29,102 cycles

AT FS 621.00 (FWD SIDE OF REAR PRESS BULKHEAD) THERE IS A CRACK ON THE WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING. REPAIRED IAW REO 601R-53-61-1230.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 32,686 hrs · 29,102 cycles

AT FS 280.00, THE RIGHT FLOOR SUPPORT ANGLE IS CRACKED JUST O/B OF RBL 9. REPAIRED DISCREPANT SUPPORT ANGLE IAW REO 601R-53-11-137.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 32,686 hrs · 29,102 cycles

FOUND CRACK JUST O/B OF LBL 9 AT FS 280.00 ON AFT FLOOR ANGLE. REPAIRED DISCREPANT SUPPORT ANGLE IAW REO 601R-53-137.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 32,686 hrs · 29,102 cycles

FOUND CRACKED ANGLE AT FS 280 FLOOR SUPPORT STRUCTURE LBL 9. REMOVED AND REPLACED STIFFENER ANGLE IAW SRM 51-42-06 AND 51-42-13.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 32,686 hrs · 29,102 cycles

FOUND CRACKED ANGLE AT FS 280 FLOOR SUPPORT STRUCTURE RBL 9. REMOVED AND REPLACED STIFFENER ANGLE IAW SRM 51-42-06 AND 51-42-13.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,686 hrs · 29,102 cycles

AT FS 621.00 (FWD SIDE OF REAR PRESSURE BULKHEAD) THERE IS A CRACK AT LBL 27.50 JUST ABOVE THE TOP OF THE CARGO DOOR TRACK. REPAIRED DAMAGE IAW REO 601R-53-61-1541.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 32,686 hrs · 29,102 cycles

CRACK FOUND AT FS 559.00, LEFT SIDE CAP ANGLE CRACKED AT LBL 18.00. REPAIRED IAW REO 601R-53-41-260.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 32,686 hrs · 29,102 cycles

BULKHEAD WEB CRACKED AT FS 621.00, RBL 27.50. REPAIRED DAMAGE AT FS 621.00, RBL 27.50 IAW REO 601R-53-61-1285.

Part: ACTUATOR — FAILED (HORIZ STAB) · airframe 31,046 hrs · 27,722 cycles

ON CLIMBOUT FROM CVG RECEIVED STAB TRIM FAIL MSG. EMERGENCY DECLARED, A/C RETURNED TO CVG LANDED SAFELY. REMOVED AND REPLACED STAB TRIM ACTUATOR.

Part: SENSE LINE — CONTAMINATED (P2 LINE) · airframe 30,264 hrs · 27,107 cycles

EN ROUTE FROM JFK TO ORD RECEIVED EFIS COMP MON CAUTION MSG WITH INDICATED A/S FLAG. A/C DIVERTED TO IND, LANDED SAFELY. FOUND A LITTLE WATER CONTAMINATION IN P2 LINE. PURGED OUT WATER, OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: STIFFENER — CRACKED (FS 559 RBL 9) · airframe 29,063 hrs · 26,128 cycles

DURING 559 INSPECTION FOUND .4 INCH CRACK ON INBOARD SIDE AND .5 INCH CRACK AT OUTBOARD SIDE, LOWER END, OF VERTICAL STIFFENER, RBL 9, FS 559. CUT OUT DAMAGE AND INSTALLED DOUBLERS PER BOMBARDIER REO 601R-53-41-057. (S)

Part: STIFFENER — CRACKED (BS 559 RBL 18) · airframe 29,063 hrs · 26,128 cycles

DURING 559 INSPECTION FOUND OUTBOARD SIDE, LOWER END OF VERTICAL POST AT RBL 18 CRACKED. CUT OUT DAMAGE AND INSTALLED DOUBLER PER BOMBARDIER REO 601R-53-41-067. (S)

Part: BULKHEAD — CRACKED (FS 202) · airframe 29,063 hrs · 26,128 cycles

CRACK ON FS 202 AROUND PARKING BRAKE CABLE. REPAIRED CRACK ON FS 202 AROUND PARKING BRAKE CABLE IAW EA 10-5311-01914. (A)

Part: DOOR SEAL — TORN (SERVICE DOOR) · airframe 28,596 hrs · 25,746 cycles

FLIGHT 5689 - EN ROUTE MHT-CVG THE SERVICE DOOR SEAL FAILED TO HOLD PRESSURIZATION AS INDICATED BY SEAL NOISE, CREW DECLARED AN EMERGENCY AND DIVERTED TO ALB. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE SERVICE DOOR SEAL.

Part: CONTROLLER — FAULTY (WINDSHIELD HEAT) · airframe 28,570 hrs · 25,725 cycles

FLIGHT 5620 - EN ROUTE CVG-YUL RECEIVED A LEFT WINDSHIELD CAUTION MESSAGE, FLIGHT RETURNED TO CVG. REPLACED THE LEFT WINDSHIELD HEAT CONTROLLER.

Part: SEAL — TORN (SERVICE DOOR) · airframe 27,638 hrs · 25,003 cycles

FLIGHT 5326 - LOUD NOISE AT ALTITUDE FROM BOTTOM OF SERVICE DOOR EN ROUTE FROM OKC TO CVG. AIRCRAFT DIVERTED TO STL AND LANDED SAFELY. FOUND PAX DOOR SEAL TORN. REMOVED AND REPLACED PAX DOOR SEAL.

Part: REDUCER — CLOGGED (GALLEY DOOR) · airframe 27,638 hrs · 25,003 cycles

FLIGHT 5326 - LOUD NOISE AT ALTITUDE FROM BOTTOM OF SERVICE DOOR EN ROUTE FROM OKC TO CVG. AIRCRAFT DIVERTED TO STL AND LANDED SAFELY. FOUND GALLEY DRAIN NOISE REDUCER CLOGGED. REMOVED AND REPLACED NOISE REDUCER.

Part: RELAY — FAULTY (FIRE PROTECTION) · airframe 27,227 hrs · 24,666 cycles

FLIGHT 5180 - RECEIVED CARGO BOTTLE LOW MESSAGE. PERFORMED QRH, SQUIBS DID NOT TEST. DIVERTED TO CRW, LANDED WITHOUT INCIDENT. REPLACED RELAY K7HL. NO FURTHER DEFECTS.

Part: RELAY — FAULTY (FIRE PROTECTION) · airframe 27,227 hrs · 24,666 cycles

FLIGHT 5180 - RECEIVED CARGO BOTTLE LOW MESSAGE. PERFORMED QRH, SQUIBS DID NOT TEST. DIVERTED TO CRW, LANDED WITHOUT INCIDENT. REPLACED RELAY K8HL. NO FURTHER DEFECTS.

Part: RELAY — FAULTY (FIRE PROTECTION) · airframe 27,227 hrs · 24,666 cycles

FLIGHT 5180 - RECEIVED CARGO BOTTLE LOW MESSAGE. PERFORMED QRH, SQUIBS DID NOT TEST. DIVERTED TO CRW, LANDED WITHOUT INCIDENT. REPLACED RELAY K6HL. NO FURTHER DEFECTS.

Part: FIRE BOTTLE — LOW (CARGO BAY) · airframe 27,204 hrs · 24,645 cycles

FLIGHT 5570 - CARGO BOTTLE LOW MESSAGE ILLUMINATED IN FLIGHT TO GSO. AIRCRAFT DIVERTED TO IAD AND LANDED SAFELY. REMOVED AND REPLACED CARGO FIRE BOTTLE.

Part: CONNECTOR — LOOSE (FIRE BOTTLE) · airframe 27,200 hrs · 24,640 cycles

FLIGHT 5005 - CARGO BOTTLE LOW MESSAGE. QRH FOLLOWED AND A/C DIVERTED TO BWI AND LANDED SAFELY. FOUND CONNECTOR LOOSE ON CARGO BOTTLE, RESECURED CONNECTOR, OPS CHECK GOOD.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 26,555 hrs · 24,123 cycles

FLIGHT 5048 - DURING CLIMBOUT, CABIN RATE FLUX +-2400 FT. SWITCH PRESS CONT WITH NO CHANGE, AIRCRAFT RETURNED BACK TO SGF AND LANDED SAFELY. REMOVED AND REPLACED CONTROLLER, CABIN PRESSURE.

Part: WIRE — DAMAGED (SENSOR) · airframe 24,465 hrs · 22,507 cycles

FLIGHT 9496 - EN ROUTE SAV-CVG RECEIVED A LEFT 14TH STAGE DUCT WARNING, FLIGHT DIVERTED TO GSP. REPLACED 14TH STAGE PYLON SENSOR WIRING.

Part: PUMP — FAULTY (RT ENGINE) · airframe 23,743 hrs · 21,918 cycles

FLIGHT 5193 - DURING CLIMBOUT OF CVG RECEIVED A HYDRAULIC NR 2 CAUTION MESSAGE, CREW DECLARED AN EMERGENCY. FLIGHT RETURNED TO THE FIELD WITHOUT INCIDENT. REPLACED THE ENGINE DRIVEN HYDRAULIC PUMP.

Part: WINDSHIELD WIPER — BROKEN (RIGHT) · airframe 22,881 hrs · 21,183 cycles

FLIGHT 5314 - RIGHT WINDSHIELD WIPER BROKE IN HALF. REPLACED WIPER BLADE ASSEMBLY.

Part: ELEMENT — MALFUNCTIONED (LT PYLON) · airframe 22,613 hrs · 20,953 cycles

FLIGHT 5414 - LEFT 14TH DUCT WARNING MESSAGE. REPLACED THE BLEED LEAK SENSE ELEMENT.

Part: WARNING SYSTEM — ACTIVATED (THRUST REVERSER) · airframe 24,513 hrs · 19,975 cycles

FLIGHT 5134 DURING TAKEOFF DID NOT RECEIVE A T/O CONFIGURATION OK MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. CYCLED THE RIGHT THRUST REVERSER.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 21,253 hrs · 19,747 cycles

FLIGHT 5210 LEFT THRUST REVERSER UNLOCKED MESSAGE. DEFERRED MAINT ON T/R PER MEL.

Part: IDG — FAILED · airframe 21,133 hrs · 19,638 cycles

FLIGHT 5082 - DURING TAKEOFF ROLL AT 60 KNOTS RECEIVED AN IDG CAUTION MESSAGE, ABORTED TAKEOFF AND RETURNED TO THE GATE. DEFERRED FAILED IDG PER MEL 24-11-01-1.

Part: ANTI-ICE SYSTEM — FAULTY (LT WING) · airframe 21,023 hrs · 19,543 cycles

FLIGHT 5574 RECEIVED A LEFT WING ANTI-ICE WARNING DURING CRUISE FLIGHT, RETURNED TO CVG. REPLACED THE LEFT WING LEADING EDGE INBOARD AND MIDDLE ANTI ICE SENSORS.

Part: TRANSDUCER — MALFUNCTIONED (LT ENG OIL) · airframe 19,579 hrs · 18,320 cycles

FLIGHT 5806, LT ENGINE OIL PRESSURE WARNING. REPLACED THE OIL PRESSURE TRANSDUCER.

Part: DOUBLER — CRACKED (FRAME) · airframe 17,437 hrs · 16,460 cycles

718 FRAME DOUBLER CRACKED, COMPLIED WITH EO 53-077, IAW MAJOR WORK ORDER NR 71396.

Part: DOUBLER — CRACKED (FRAME) · airframe 17,437 hrs · 16,460 cycles

FRAME 718 DOUBLER CRACKED. COMPLIED WITH EO 53-027, PER MAJOR WORK ORDER 71396.

Part: DOUBLER — CRACKED (FRAME) · airframe 17,437 hrs · 16,460 cycles

640 FRAM DOUBLER CRACKED, REMOVED AND REPLACED LT 640 FRAME DOUBLER IAW CRJ SRM 51-21-06, 51-42-20 AND 51-42-21.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 17,022 hrs · 16,070 cycles

FLIGHT 5488 FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: BPSU — MALFUNCTIONED (T/E FLAP) · airframe 17,023 hrs · 16,072 cycles

FLIGHT 5667 FLAPS FAIL MESSAGE. REPLACED THE LT BPSU.

Part: DOOR — OPEN (EXTERNAL POWER) · airframe 16,613 hrs · 15,699 cycles

FLIGHT 5843 UNUSUAL NOISE FROM RT SIDE OF AIRCRAFT. FOUND THE EXTERNAL POWER SERVICE DOOR OPEN. INSPECTED FOR DAMAGE AND SECURED DOOR CLOSED.

Part: MECHANISM — CORRODED (CABIN DOOR) · airframe 16,186 hrs · 15,317 cycles

FLIGHT 5865 CABIN DOOR OUTER HANDLE WILL NOT STOW. REPLACED THE CABIN DOOR BELL CRANK MECHANISM.

Part: SEAT BELT — BROKEN (COPILOT SEAT) · airframe 15,530 hrs · 14,732 cycles

FLIGHT 5485 COPILOTS SEAT BELT BROKEN.REASSEMBLED CABLE FOR BELT LOCK.

Part: PRESSURE PANEL · airframe 15,401 hrs · 14,620 cycles

CABIN ALTITUDE CAUTION MESSAGE.COULD NOT DUPLICATE, CABIN PRESSURE CONTROL SYSTEM OPERATIONAL TEST NORMAL.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 15,401 hrs · 14,620 cycles

CABIN ALTITUDE CAUTION MESSAGE. COULD NOT DUPLICATE, CABIN PRESSURE CONTROL SYSTEM OPERATIONAL TEST NORMAL.

Part: CARBON SEAL — WORN (LT ENG) · airframe 14,405 hrs · 13,686 cycles

FLIGHT 5542 LEFT ENGINE LOW OIL PRESSURE WARNING.REPLACED THE #6 BEARING CARBON SEAL.

Part: TARGET — LOOSE (R/H MLG) · airframe 14,226 hrs · 13,518 cycles

FLIGHT 5566 R/H MLG INDICATES INTRANSIT AFTER GEAR RETRACTION.TIGHTENED LOOSE PROX SENSOR TARGET ON UPLOCK.

Part: SPRING — BROKEN (DOOR) · airframe 14,166 hrs · 13,463 cycles

FLIGHT 5693 CABIN DOOR OUTER HANDLE MESSAGE.REPLACED SPRING ON OUTER DOOR HANDLE.

Part: PLANK — CRACKED (WING) · airframe 13,459 hrs · 12,803 cycles

CRACK FOUND ON LT LOWER WING PLANK AT PANEL 540EB.REPAIRED I/A/W 601R-57-21-030.

Part: ACTUATOR — MALFUNCTIONED (VERT STAB) · airframe 12,752 hrs · 12,120 cycles

FLIGHT #5797 STAB CHANNEL 1 INOP MESSAGE.REPLACED THE HSTA.

Part: ACTUATOR — MALFUNCTIONED (VERT STAB) · airframe 12,725 hrs · 12,088 cycles

FLIGHT #5011. STABILIZER TRIM INOP.REPLACED THE HORZ. STAB. TRIM ACTUATOR.

Part: BEAM — MISDRILLED · airframe 11,979 hrs · 11,369 cycles

TRANSVERSE BEAM AT FS 333, RBL9 HAS TWO EXISTING MISDRILLED FASTENER HOLES IN LOWER FLANGE.REPAIRED I/A/W WVAC EO 601R-53-2577.

Part: BEAM — CRACKED (FUSELAGE) · airframe 11,979 hrs · 11,369 cycles

FOUND CRACK ON LEFT AND RIGHT SIDE LOWER WEB OF ENGINE SUPPORT BEAM - FORWARD, INBOARD OF ACCESS PANEL. REPAIRED THE ENGINE SUPPORT BEAM LOWER RIGHT AND LEFT WEB IAW CANADAIR REO 601R-53-61-366.

Part: CHANNEL — CORRODED · airframe 11,979 hrs · 11,369 cycles

FORWARD AND AFT PAX DOOR U-CHANNELS CORRODED.REMOVED AND REPLACED U-CHANNELS I/A/W WVAC EO 601R-53-2584.

Part: ANGLE — CORRODED · airframe 11,979 hrs · 11,369 cycles

THRESHOLD SUPPORT ANGLES AT PAX DOOR CORRODED.REMOVED AND REPLACED I/A/W WVAC EO 601R-53-2575.

Part: ANGLE — CORRODED · airframe 11,979 hrs · 11,369 cycles

FORWARD J-ANGLE AT FS 280 BETWEEN LBL9 AND RBL9 CORRODED.REMOVED AND REPLACED I/A/W WVAC EO 601R-53-2576.

Part: ANGLE — MISDRILLED · airframe 11,979 hrs · 11,369 cycles

THE CLEAT FOR LBL27 AT F.S. 364.0 WAS MISDRILLED WHILE INCORPORATING SB601R-53-037 (TITANIUM FLOOR BEAM MOD).FABRICATED AND INSTALLED A NEW CLEAT I/A/W WVAC EO 601R-53-2583.

Part: COMPUTER — MALFUNCTIONED (E&E BAY) · airframe 11,924 hrs · 11,321 cycles

ENGINE OUTLINE ON EICAS HYDRAULIC PAGE, ALTERNATES FROM CYAN TO WHITE THEN BACK TO CYAN. REPLACED THE NR 2 DCU.

Part: BATTERY — DISCHARGED (CABIN) · airframe 11,886 hrs · 11,285 cycles

EMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY LIGHTS BATTERY.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 11,582 hrs · 11,015 cycles

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

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 11,540 hrs · 10,970 cycles

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

Part: LAMP — BURNED OUT (CABIN) · airframe 11,483 hrs · 10,915 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB.

Part: FIRE LOOP — OUT OF POSITION (LT ENGINE) · airframe 11,291 hrs · 10,727 cycles

DURING CLIMB OUT OF CVG, RECEIVED LEFT JET PIPE OVERHEAT FAIL CAUTION MESSAGE, AIRCRAFT RETURNED TO THE FIELD. READJUSTED HARDWARE ON JET PIPE SENSING ELEMENTS LOOP "A" AND LOOP "B".

Part: CONTROLLER — MALFUNCTIONED (E/E BAY) · airframe 11,271 hrs · 10,707 cycles

RIGHT HAND WING ANTI-ICE CAUTION MESSAGE.COULD NOT DUPLICATE. REPLACED THE ANTI-ICE TEMP CONTROLLER FOR TROUBLESHOOTING.

Part: ENGINE — FAILED (LEFT) · airframe 11,001 hrs · 10,465 cycles

LEFT ENGINE LOW OIL PRESSURE WARNING, AND THEN LEFT ENGINE FAILED. REPLACED ENGINE.

Part: WARNING SYSTEM — ACTIVATED (TE FLAPS) · airframe 10,484 hrs · 9,992 cycles

FLAPS FAIL MESSAGE. RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 982001.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 10,396 hrs · 9,926 cycles

STALL FAIL WARNING DURING TAKEOFF. REPLACED THE SPC.

Part: SENSOR — MALFUNCTIONED (AOA) · airframe 10,396 hrs · 9,926 cycles

STALL FAIL MESSAGE DURING TAKEOFF. REPLACED THE LEFT AND RIGHT AOA SENSORS.

Part: CIRCUIT BREAKER — TRIPPED (STALL WARNING) · airframe 10,320 hrs · 9,836 cycles

CONFIG AND STALL FAIL WARNING DURING TAKEOFF. RESET THE SPC CIRCUIT BREAKERS, SYSTEM TEST SATISFACTORY. COULD NOT DUPLCIATE.

Part: STALL WARNING — MALFUNCTIONED (E/E BAY) · airframe 10,321 hrs · 9,838 cycles

STALL FAIL DURING TAKEOFF. REPLACED THE SPC.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 10,258 hrs · 9,760 cycles

LEFT INBOARD FLAP VANE CAP AT WS 53.60 CHAFED BEYOND LIMITS. REMOVED DAMAGED VANE CAP AND INSTALLED NEW SERVICEABLE VANE CAP IAW WVAC EO 601R-57-1520.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 10,258 hrs · 9,760 cycles

RIGHT INBOARD FLAP VANE CAP AT WS 53.60 CHAFED BEYOND LIMITS. REMOVED DAMAGED VANE CAP AND INSTALLED NEW SERVICEABLE VANE CAP IAW WVAC EO 601R-57-1522.

Part: FCU — MALFUNCTIONED (E/E BAY) · airframe 9,864 hrs · 9,427 cycles

FLAPS FAIL MESSAGE. REPLACED THE FECU.

Part: WARNING SYSTEM — ACTIVATED (TE FLAP) · airframe 9,864 hrs · 9,427 cycles

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

Part: FLAP — MALFUNCTIONED (WINGS) · airframe 9,818 hrs · 9,822 cycles

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

Part: ACTUATOR — MALFUNCTIONED (VERTICAL STAB) · airframe 9,641 hrs · 9,220 cycles

TAKEOFF CONFIG WARNING WHEN POWER ADVANCED. REPLACED THE STAB TRIM ACTUATOR.

Part: PANEL — CRACKED (WING) · airframe 9,504 hrs · 9,105 cycles

LOWER ACCESS HOLE AT 610 AB CRACKED. REPAIRED DAMAGED IAW REO 601R-57-21-030.

Part: WATER SEPARATOR — CONTAMINATED (AIR DIST)

STRONG FUEL SMELL IN CABIN AND COCKPIT WHEN BLEED AIR SOURCE SWITCHED TO THE APU. CLEANED THE AIRCRAFT WATER SEPERATORS. RAN AIRCRAFT AND NO FUEL SMELL NOTED.

Part: DETECTOR — MALFUNCTIONED (LT ENGINE)

LEFT 14TH STAGE BLEED AIR DUCT LEAK WARNING. REPLACED FAULTY BLEED AIR LEAK DETECTOR.

Part: LAMP — FAILED (RT EMER EXIT)

AFT OVERWING EMERGENCY EXIT LIGHT IS INOPERABLE. REPLACED LIGHT BULB.

Part: CONTROL PANEL — FAILED (STAB TRIM)

STABILIZER CHANNEL NR 1 INOPERATIVE MESSAGE APPEARED SEVERAL TIMES AFTER DEPARTURE FROM CVG. AIRCRAFT RETURNED TO THE FIELD. REPLACED THE STABILIZER TRIM PANEL.

Part: WARNING — ACTIVATED (PAX DOOR)

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

Part: PISTON — LEAKING (NLG)

NLG WILL NOT RETRACT. NLG FOUND LEAKING. REPLACED THE NLG PISTON ASSY.

Part: BUSHING — MIGRATED (LT & RT MLG)

LEFT HAND AND RIGHT HAND MLG AFT TRUNNION BUSHING MIGRATED. PERFORMED SERVICE BULLETIN 601R-32054. REPLACED LEFT HAND AFT AND RIGHT HAND AFT TRUNNION BUSHING.

Part: LEADING EDGE — DENTED (RT WING)

RIGHT WING OUTBOARD LEADING EDGE HAS A DENT. REPAIRED RIGHT WING OUTBOARD LEADING EDGE AT FS 279.699 AND 288.641 IAW WVAC EO NR 601R-57-0211.

Part: FRAME — CRACKED (BS 718)

FRAME AT FS 718 LT DISCOVERED TO BE CRACKED IN THE RADIUS EXTENDING 3 INCHES ABOVE STR 11, IN THE FLANGE BELOW STR 11, AND IN THE DOUBLER ON AFT SIDE OF FRAME AT STR 11. REPAIRED FRAME AT FS 718 IAW WVAC EO 601R-53-0208A AND REPAIRED DOUBLER IAW WVAC EO 601R-53-0210.

Part: FRAME — CRACKED (BS 718)

FRAME AT FS 718 RHS DISCOVERED CRACK 4 INCHES ABOVE STR 11 IN THE FLANGE ATTACHING TO THE SKIN AND CRACKED IN 2 PLACES IN THE RADIUS BELOW STR 11 AND CRACKED IN DOUBLER 2 ON AFT SIDE OF FLAME STR 11. REPAIRED FRAME AT FS 718 STR 11 IAW WVAC EO 601R-53-0207A AND REPAIRED DOUBLER IAW WVAC EO 601R-53-0209.

Part: WINDOW — SHATTERED (LT COCKPIT)

LEFT SIDE WINDOW CRACKED AT 33,000 FT. SHATTERED ON FINAL APPROACH. REPLACED WINDOW.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO COMPT)

CARGO SMOKE WARNING DURING TAXI. FALSE WARNING. REPLACED SMOKE DETECTOR.

Part: STRUCTURE — DAMAGED (RT WING)

DURING TAXI, THE RIGHT HAND WING STRUCT A POWER CART. REPAIRED WING.

Part: WIRE — FAILED (CABIN)

CABIN OVERHEAD EMERGENCY EXIT SIGN IS INOPERABLE. REPAIRED WIRING AT EMERGENCY LIGHT.

Part: FILLER — MISSING (PAX DOORWAY)

LOUD WIND NOISE FROM CABIN DOOR. REPLACED MISSING FILLER MATERIAL AT PREVIOUS REPAIR OF DOOR FRAME SEAL AREA.

Part: DETECTOR — MALFUNCTIONED (LT BLEED AIR)

LEFT 14TH STAGE BLEED AIR LEAK WARNING. REPLACED THE PYLON LEAK DETECTOR LOOP.

Part: ACTUATOR — LEAKING (LT MLG)

NR 3 HYDRAULIC SYSTEM QUANTITY IS LOW. REPLACED THE LEFT HAND MLG RETRACT ACTUATOR.

Part: ECU — FAILED (APU)

APU FAILED AFTER TAKEOFF. REPLACED THE APU ECU.

Part: SIGN — MISSING (CABIN)

EMERGENCY EXIT LIGHT OVER SERVICE DOOR MISSING. REPLACED SIGN ASSEMBLY.

Part: ACTUATOR — LEAKING (RT MLG)

HYDRAULIC LEAK RIGHT HAND MLG RETRACT ACTUATOR. REPLACED ACTUATOR.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO)

CARGO SMOKE WARNING DURING FLIGHT. FIRE EXTINQUISHERS WERE DISCHARGED. REPLACED SMOKE DETECTOR AND FIRE BOTTLES. DETERMINED TO BE FALSE WARNING.

Part: PITCH CONTL UNIT — FAILED (RT SPOILER)

RIGHT FLIGHT SPOILER FAULT MESSAGE AND WHITE INDICATION ON FLIGHT CONTROL PAGE. REMOVED RIGHT INBOARD SPOILERON PITCH CONTROL UNIT.

Part: ACTUATOR — FAILED (NR 4 TE FLAP)

FLAPS FAILED AT 25 DEGREES ON APPROACH. REPLACED 4 FLAP ACTUATORS ON LT WING.

Part: BPSU — MALFUNCTION (TE FLAPS)

FLAPS FAIL MESSAGE, FLAPS STUCK AT 33 DEGREES. REPLACED THE BRAKE AND POSITION SENSING UNITS.

Part: CONNECTOR — LOOSE (LT BLEED AIR VLV)

LEFT ENGINE WILL NOT START. SECURED LOOSE WIRING CONNECTOR AT ENGINE BLEED AIR VALVE.

Part: DE-ICE FLUID — SMOKING (WINGS)

PASSENGER REPORTED SMOKE COMING FROM WINGS. SMOKE FOUND TO BE DE-ICING FLUID EVAPORTING.

Part: FAN BLADE — FOD (RT ENGINE)

AT 25,000 FT A BANG SOUND WAS HEARD FOLLOWED BY A 2.2 VIB ON RT ENGINE. MAINTENANCE REPLACED TWO SETS OF DAMAGED FAN BLADES ON RT ENGINE. IT IS PROBABLE THAT THIS FOD WAS CAUSED BY ICE FROM THE GALLEY WATER DRAIN MAST.

Part: PITOT SYST — WATER CONTAM (COCKPIT)

TAKE OFF ABORTED DUE TO 50 KTS DIFFERENCE BETWEEN PILOT AND COPILOTS AIRSPEED INDICATORS. REMOVED WATER FROM PITOT SYSTEM, SYSTEM TEST SATISFACTORY.