N965CA

Part: VANE — CHAFED (TE FLAP) · airframe 33,951 hrs · 29,461 cycles

RIGHT I/B FLAP VANE LEADING EDGE FOUND TO HAVE CHAFE DAMAGE. REPLACED THE RIGHT I/B FLAP VANE LEADING EDGE IAW CRJ 200 SRM.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 33,951 hrs · 29,461 cycles

FS 559.0 BULKHEAD WEB FOUND TO BE CRACKED. REPAIRED IAW REO 601R-53-41-260 AND DEVIATION REO 601R-53-41-609.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 33,951 hrs · 29,461 cycles

FS 280 FLOOR SUPPORT CROSSBEAM AT LBL 9 TO RBL 9 IS CORRODED. REPAIRED CROSSBEAM PER SRM 51-42-06.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 33,951 hrs · 29,461 cycles

FS 280 BULKHEAD WEB AT LBL 11 TO LBL 13 IS CORRODED. REPAIRED BULKHEAD WEB AT FS 280 PER SRM 53-11-19.

Part: DOUBLER — CRACKED (BS 640) · airframe 30,164 hrs · 26,320 cycles

RT INTERNAL SKIN DOUBLER AT STA 640 IS CRACKED. FABRICATED PARTS AT STA 640 IAW CRJ REO 601R-53-61-506. (S)

Part: SKIN — DAMAGED (BS 310) · airframe 30,164 hrs · 26,320 cycles

PASSENGER DOOR CUTOUT AIRFRAME SIDE FWD LOWER CORNER EXISTING REPAIR IS DAMAGED. REPAIRED PASSENGER DOOR CUTOUT AIRFRAME SIDE LOWER FWD CORNER PER CRJ REO 601R-53-21-180 REV (A) AND SR99-5140-0001 SECTION 1. (S)

Part: FRAME — CRACKED (BS 640) · airframe 30,164 hrs · 26,320 cycles

LT SIDE FUSELAGE FRAME DOUBLER AT FS 640.00 IS CRACKED. COMPLIED WITH MODIFICATION K601R36009-R AT FS 640 IAW S/B 601R-53-061. (S)

Part: SUPPORT BEAM — CRACKED (RT ENGINE) · airframe 30,164 hrs · 26,320 cycles

RT UPPER WEB-ENG SUPPORT BEAM ASSEMBLY CRACKED. COMPLIED WITH REPAIR TO UPPER WEB-ENG SUPPORT. BEAM ASSEMBLY BETWEEN BL 27.5 AND 36.2 PER REO601R-53-61-569. (S)

Part: DOUBLER — CRACKED (BS 640) · airframe 30,164 hrs · 26,320 cycles

LT INTERNAL SKIN DOUBLER AT STA 640 IS CRACKED. FABRICATED PARTS AT STA 640 IAW CRJ REO 601R-53-61-506. (S)

Part: DOUBLER — CRACKED (BS 640) · airframe 30,164 hrs · 26,320 cycles

RT SIDE FUSELAGE FRAME DOUBLER AT FS 640.00 IS CRACKED. COMPLIED WITH MODIFICATION K601R360094 AT FS 640 IAW S/B 601R-53-061. (S)

Part: FLOOR SKIN — CRACKED (BS 460) · airframe 30,164 hrs · 26,320 cycles

PRESSURE FLOOR SKIN AT STA 460 BETWEEN LBL 9 AND RBL 9 IS CRACKED. REPAIRED PRESSURE FLOOR SKIN WEB AT FS 460.00 WITH TEMPORARY REPAIR PER REO 601R-53-41-103 REV D. (S)

Part: SUPPORT BEAM — CRACKED (LT ENGINE) · airframe 30,164 hrs · 26,320 cycles

LT UPPER WEB-ENG SUPPORT BEAM ASSEMBLY CRACKED. COMPLIED WITH REPAIR TO UPPER WEB-ENG SUPPORT. BEAM ASSEMBLY BETWEEN BL27.5 AND 36.2 PER REO601R-53-51-569. (S)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,126 hrs · 26,276 cycles

FLIGHT 9422. DURING LINE CHECK FOUND ROW 2-5 EMERGENCY FLOOR LIGHTS INOP. REMOVED AND REPLACED FLOOR EMERGENCY LIGHT STRIP. (A)

Part: INVERTER — INOPERATIVE (CABIN) · airframe 29,682 hrs · 25,923 cycles

FLIGHT 5326 - EMERGENCY LIGHTS NOT WORKING FROM ROW 9 AFT. REPLACED NR 4 INVERTER. NO FURTHER DEFECTS.

Part: LIGHT — NO TEST (CABIN) · airframe 29,525 hrs · 25,801 cycles

FLIGHT 5027 - THE AFT EMERGENCY EXIT FLOOR LIGHTS FAILED TO TEST. DEFERRED PER MEL 33-51-01-6.

Part: RELIEF VALVE — FAULTY (ANTI-ICE SYSTEM) · airframe 29,154 hrs · 25,612 cycles

FLIGHT 5103- RECEIVED RIGHT COWL ANTI-ICE MESSAGE WHEN ANTI-ICE SELECTED ON. RETURNED TO JFK, LANDED WITHOUT INCIDENT. REPLACED PRESSURE RELIEF VALVE. NO FURTHER DEFECTS.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,320 hrs · 25,636 cycles

FLIGHT 5479 - FLOOR MOUNTED EMERGENCY STRIP BEHIND ROW 8A IS INOP. REPLACED BATTERY PACK NR 4. NO FURTHER DEFECTS.

Part: BULKHEAD — CRACKED (FS 621.00) · airframe 27,846 hrs · 24,453 cycles

REAR PRESSURE BULKHEAD CRACKED AROUND LINTEL FITTING. PERFORMED PERMANENT REPAIR TO AFT PRESSURE BULKHEAD IAW REO 601R-53-11-563.

Part: BULKHEAD — CRACKED (FS 202.75) · airframe 27,846 hrs · 24,453 cycles

FORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE. REPAIRED IAW REO 601R-53-11-563.

Part: ENGINE — OVERTEMP (RIGHT) · airframe 25,517 hrs · 24,184 cycles

FLIGHT 4988 - DURING TAKEOFF ROLL THE RIGHT ENGINE ITT INDICATED 905C, ABORTED TAKEOFF AND RETURNED TO THE GATE. REPLACED THE RIGHT ENGINE ASSEMBLY.

Part: PUMP — MALFUNCTIONED (HYD SYSTEM) · airframe 27,511 hrs · 24,181 cycles

FLIGHT 5389 - HYD PUMP 1B CIRCUIT BREAKER POPPED WHILE STARTING NR 1 ENGINE. RETURNED TO GATE. RESET BREAKER, PERFORMED OPS CHECK, NO FURTHER DEFECTS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,398 hrs · 24,094 cycles

DURING FS 559 INSPECTION FOUND SEMI-BULKHEAD CRACKED AT RBL 18. STOP DRILLED CRACK AND INSTALLED DOUBLER IAW REO 601R-53-41-353.

Part: WIRE — FAULTY (THERMIAL SWITCH) · airframe 26,738 hrs · 23,586 cycles

FLIGHT 5342 - RECEIVED ANTI-ICE DUCT WARNING MESSAGE IN FLIGHT. FOLLOWED QRH AND DIVERTED TO GSO. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THERMAL SWITCH WIRE AT LEFT WING STATION 250. NO FURTHER DEFECTS.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 26,645 hrs · 22,510 cycles

FLIGHT 5206 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING BGR APPROACH AT 30 DEGREE FLAP SETTING. REPLACED THE LEFT OUTBOARD FLAP INBOARD ACTUATOR.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 26,645 hrs · 22,510 cycles

FLIGHT 5206 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING BGR APPROACH AT 30 DEGREE FLAP SETTING. REPLACED THE LEFT INBOARD FLAP INBOARD ACTUATOR.

Part: FLAP — MALFUNCTIONED (WING) · airframe 26,630 hrs · 22,499 cycles

FLIGHT 5206 - RECEIVED A FLAP FAIL CAUTION MESSAGE DURING BGR APPROACH AT 30 DEGREE FLAP SETTING. 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: WIRE HARNESS — CHAFED (ANTI-ICE SYS) · airframe 26,610 hrs · 22,480 cycles

FLIGHT 5323 - DURING CLIMBOUT RECEIVED AN ANTI-ICE DUCT CAUTION MESSAGE, FLIGHT RETURNED TO CVG. REPAIRED CHAFED WIRING ON THE LEFT WING LEADING EDGE AT STA 330.25 AND 377.40.

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 25,860 hrs · 22,899 cycles

DURING INSPECTION OF THE ENGINE SUPPORT BEAM IAW EO 53-021 (AD 2004-10-03) FOUND CRACK AT LOCATION FS 640, LBL 9.0, WL 119.12 (UPPER BOX BEAM SKIN).PERFORMED REPAIR IAW REO 601R-53-61-345.

Part: PRESSURE VALVE — MALFUNCTIONED (CABIN DOOR) · airframe 30,136 hrs · 28,509 cycles

FLIGHT 5063 - DURING CLIMBOUT OF GSO RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, FLIGHT RETURNED TO THE FIELD. RE-RIGGED THE CABIN DOOR PRESSURE VALVE VENT FLAP.

Part: WARNING SYSTEM — MALFUNCTIONED (DOOR WARNING) · airframe 25,466 hrs · 22,600 cycles

FLIGHT 5063 - AFTER TAKEOFF FROM GSO RECEIVED A CABIN DOOR OUTER HANDLE CAUTION MESSAGE, FLIGHT RETURNED TO THE FIELD. DEFERRED THE CABIN DOOR INDICATION PER MEL 52-70-01-1.

Part: ECU — FAULTY (E/E BAY) · airframe 25,533 hrs · 22,498 cycles

FLIGHT 5285 - RECEIVED A FLAP FAIL CAUTION MESSAGE AT ZERO DEGREES DURING TAXI AT DCA. REPLACED THE FLAP ELECTRONIC CONTROL UNIT.

Part: CAUTION MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 25,316 hrs · 22,485 cycles

FLIGHT 5719 - FLAP FAIL MESSAGE AT 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 — OUT OF RIG (TE FLAPS) · airframe 25,241 hrs · 22,423 cycles

FLIGHT 5450 - FLAP FAIL CAUTION MESSAGE. FLAPS WILL NOT COME OUT OF ZERO POSITION. FOUND LEFT SIDE FLAP SYSTEM OUT OF RIG. MECHANICALLY AND ELECTRICALLY RIGGED LEFT SIDE FLAP SYSTEM.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 25,235 hrs · 22,420 cycles

FLIGHT 5049 - FLAP FAIL MESSAGE ON GROUND AT 0 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 — MALFUNCTIONED (TE FLAPS) · airframe 25,208 hrs · 22,395 cycles

FLIGHT 5381 - DURING PUSHBACK RECEIVED A FLAP FAIL CAUTION MESSAGE AT 20 DEGREES, 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: LATCH — DAMAGED (PAX DOOR) · airframe 29,566 hrs · 28,009 cycles

FLIGHT 5701 - EN ROUTE BTV-ATL RECEIVED A CABIN DOOR LATCH CAUTION MESSAGE, FLIGHT DIVERTED TO SYR. ADJUSTED ROD-END OF CABIN DOOR LATCH ROLLER ASSEMBLY.

Part: PRESSURE SWITCH — FAULTY (LT ENGINE) · airframe 24,784 hrs · 22,052 cycles

FLIGHT 5093 - DURING CLIMB-OUT OF EVV RECEIVED A LEFT ENGINE COWL A/ICE CAUTION MESSAGE, FLIGHT RETURNED TO EVV. REPLACED THE LEFT ENGINE COWL ANTI ICE PRESSURE SWITCH.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 24,668 hrs · 21,960 cycles

FLIGHT 5701- PILOT'S WINDSHIELD SHATTERED. REPLACED WINDSHIELD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 24,362 hrs · 21,704 cycles

FLIGHT 5850 - RECEIVED A FLAP FAIL CAUTION MESSAGE AFTER LANDING WHEN FLAPS WERE SELECTED TO 20 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: LIGHT — INOPERATIVE (CABIN) · airframe 23,736 hrs · 21,185 cycles

FLIGHT 5565 - EMERGENCY FLOOR LIGHTING INOPERATIVE FROM ROWS 2 THROUGH 5. CLEANED CONTACTORS ON EMERGENCY FLOOR TRACK LIGHT STRIP.

Part: LAMP — INOPERATIVE (CABIN) · airframe 23,702 hrs · 21,155 cycles

FLIGHT 5387 - EMERGENCY LIGHTS ROW 1-5 INOPERABLE. RESECURED LIGHT STRIP.

Part: BPSU — OUT OF RIG (TE FLAPS) · airframe 23,575 hrs · 21,038 cycles

FLIGHT 5858 - FLAPS FAIL CAUTION. ADJUSTED THE RIGGING OF THE RT BPSU.

Part: ELEMENT — MALFUNCTIONED (LT PYLON) · airframe 23,474 hrs · 20,959 cycles

FLIGHT 5105 - LT 14TH STAGE DUCT WARNING. REPLACED THE PYLON DUCT LEAK SENSING ELEMENT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 20,896 hrs · 18,683 cycles

FS 574 LEFT HAND SIDE HAS TWO CORRODED FASTENERS AT 8 POSITION ABOVE FLOOR. REPAIRED IAW REO 601R-53-61-1135.

Part: FLOORBEAM — CRACKED (CARGO BAY) · airframe 20,896 hrs · 18,683 cycles

CARGO FLOOR CAP CRACKED. IAW SRM 51-42-06, 51-42-13, 51-42-21 AND 51-42-26.

Part: SKIN — CRACKED (RT WING) · airframe 20,896 hrs · 18,683 cycles

RT WING PLANK AT VS 148 IS CRACKED. IAW EO 57-020.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 20,896 hrs · 18,683 cycles

FS 280 HAS CORROSION ON WEB AT BL AFT SIDE AND CRACKS LOCATED OUTBOARD OF LBL/RBL 9. REPAIRED IAW REO 601R-53-11-136.

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 20,896 hrs · 18,683 cycles

FS 280 HAS CORROSION ON WEB AT CBP WALLS. REPAIRED IAW REO 601R-53-11-584.

Part: WEB — CRACKED (FUSELAGE) · airframe 20,896 hrs · 18,683 cycles

CARGO CAP WEB AT LIGHTING HOLE IB SIDE CRACKED FROM EXCESSIVE STRESS.IAW SRM 51-42-06, 51-42-13.

Part: ACTUATOR — MALFUNCTIONED (YAW DAMPNER) · airframe 20,002 hrs · 17,975 cycles

FLIGHT 5405 RUDDER FLUTTER DURING FLIGHT. REPLACED THE YAW DAMPNER ACTUATOR.

Part: THRUST REVERSER — MALFUNCTIONED (LEFT) · airframe 19,904 hrs · 17,892 cycles

FLIGHT 5005 LEFT THRUST REVERSER UNLOCKED CAUTION. SECURED AND DEFERRED MAINT ON T/R PER MEL.

Part: OIL SYSTEM — OVERSERVICED (RT ENGINE) · airframe 17,965 hrs · 16,327 cycles

FLIGHT 5244 RT ENGINE, HIGH OIL TEMP. FOUND OIL SYSTEM OVERSERVICED - DRAINED OIL TO NORMAL LEVEL.

Part: PUMP — UNRELIABLE (HYD SYSTEM) · airframe 17,294 hrs · 15,788 cycles

FLIGHT 5704 GEAR DISAGREE WARNING WHEN GEAR EXTENDED. REPLACED HYDRAULIC PUMP 3A.

Part: ACTUATOR — MALFUNCTIONED (HORIZONAL STAB) · airframe 17,136 hrs · 15,675 cycles

FLIGHT 5843 STAB TRIM, MACH TRIM AND AUTO PILOT NOSE DOWN CAUTION MESSAGE. REPLACED THE HSTA.

Part: CONTROLLER · airframe 16,155 hrs · 14,874 cycles

FLIGHT 5554 LT AOA, LT STATIC, LT PITOT HEAT CAUTION.RESET C/B, COULD NOT DUPLICATE PROBLEM, SYSTEM TEST NORMAL.

Part: SPLICE — DAMAGED (CABIN) · airframe 15,930 hrs · 14,690 cycles

FLIGHT 5748 ONE SEGMENT OF EMERGENCY FLOOR LIGHTING IS INOP. REPAIRED WIRE SPLICE AT ROW 8.

Part: FLAP · airframe 14,891 hrs · 13,823 cycles

FLIGHT 5789 FLAS FAIL MESSAGE WHEN SELECTED TO 30 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.

Part: FLAP · airframe 14,891 hrs · 13,823 cycles

FLIGHT 5789 FLAPS FAIL MESSAGE WHEN SELECTED 30 DEGREES.RESET FLAP SYSTEM AND DEFERRED MAINT. PER AD 98-20-01.

Part: CHECK VALVE — MALFUNCTIONED (R/H ENG) · airframe 14,654 hrs · 13,608 cycles

FLIGHT 9471 R/H ENGINE HIGH OIL TEMP.REPLACED THE ENGINE LUBE PUMP BYPASS CHECK VALVE.

Part: COMPUTER — MALFUNCTIONED (AVIONICS) · airframe 14,524 hrs · 13,495 cycles

FLAPS FAILED CAUTION AT 30 DEGREES.REPLACED THE FECU.

Part: FLAP · airframe 14,360 hrs · 13,375 cycles

FLIGHT 5160 FLAPS FAILED AT 45 DEGREES DURING LANDING.RESET FLAP SYSTEM AND DEFERRED MAINT PER AD 98-20-01.

Part: ACM · airframe 14,306 hrs · 13,324 cycles

FLIGHT 5124 DURING BLEED AIR TRANSFER, COCKPIT FILLED WITH SMOKE AFTER LANDING WHILE TAXIING TO THE GATE.SECURED R/H COOLING PACK AND DEFERRED MAINT PER MEL.

Part: PLANK — CRACKED (WING) · airframe 13,460 hrs · 12,628 cycles

CRACK FOUND ON R/H LOWER WING PLANK AT PANEL 650BB.REPAIRED I/A/W 601R-57-21-030.

Part: PLANK — CRACKED (WING) · airframe 13,460 hrs · 12,628 cycles

CRACK FOUND ON L/H LOWER WING PLANK AT PANEL 550BB.REPAIRED I/A/W 601R-57-21-030.

Part: PLANK — CRACKED (WING) · airframe 13,460 hrs · 12,628 cycles

CRACK FOUND ON L/H LOWER WING PLANK AT PANEL 550AB.REPAIRED I/A/W 601R-57-21-030.

Part: PLANK — CRACKED (WING) · airframe 13,460 hrs · 12,628 cycles

CRACK FOUND ON R/H LOWER WING PLANK AT PANEL 650DB.REPAIRED I/A/W 601R-57-21-030.

Part: PLANK — CRACKED (WING) · airframe 13,460 hrs · 12,628 cycles

CRACK FOUND ON R/H LOWER WING PLANK AT PANEL 650 AB.REPAIRED I/A/W 601R-57-21-030.

Part: BRACKET · airframe 13,182 hrs · 12,391 cycles

FLIGHT 5773 LOUD SQUEAL FROM SERVICE DOOR AREA. CABIN DOOR WITNESS MARKS NOT ALIGNED.FOUND STAIR HANDRAIL NOT STOWED PROPERLY DUE TO BENT PIN RETAINING BRACKET. REPOSITIONED BRACKET.

Part: SENSOR — MALFUNCTIONED (R/H WING) · airframe 12,847 hrs · 12,071 cycles

FLIGHT - R/H WING OVERHEAT FLOW LINE IS MISSING DURING WING OVERHEAT TEST.REPLACED R/H WING OVERHEAT SENSOR.

Part: BPSU — FAULTY (RIGHT WING) · airframe 12,284 hrs · 11,546 cycles

FLIGHT #5650. DURING DESCENT INTO SRQ RECEIVED A FLAP FAIL CAUTION MESSAGE WITH FLAPS AT 20 DEGREES.REPLACED THE BRAKE AND POSITIONING SENSING UNIT.

Part: FCU — FAULTY (AVIONICS BAY) · airframe 12,279 hrs · 11,543 cycles

FLIGHT #5073. DURING APPROACH INTO TLH RECEIVED A FLAP FAIL CAUTION MESSAGE WITH FLAPS AT ZERO DEGREES.REPLACED THE FLAP ELECTRONIC CONTROL UNIT.

Part: PCU — FAULTY (CENTER WING) · airframe 12,279 hrs · 11,543 cycles

FLIGHT #5073. DURING APPROACH INTO TLH RECEIVED A FLAP FAIL CAUTION MESSAGE WITH FLAPS AT ZERO DEGREES.REPLACED THE POWER DRIVE UNIT.

Part: FCU — FAULTY · airframe 11,990 hrs · 11,271 cycles

DURING APPROACH INTO CVG, THE FLAP CAUTION MESSAGE ACTIVATED WHEN FLAPS WERE SELECTED TO 45 DEGREES.REPLACED THE FLAP ELECTRONIC CONROL UNIT.

Part: BEAM — CRACKED · corrosion level 3 · airframe 11,987 hrs · 11,268 cycles

CRACKS FOUND IN ENGINE SUPPORT BEAM LOWER WEB BETWEEN F.S. 640.0 - 625.30 ON LEFT HAND AND RIGHT HAND SIDES.REPAIRED CRACKS I/A/W REO 601R-53-61-366 REV B AND WVAC E.O.'S 601R-53-2560-1A AND 601R-53-2545B.

Part: BUSHING — LOOSE (LT MLG) · airframe 11,184 hrs · 10,541 cycles

LEFT HAND MLB AFT TRUNION BUSHING MIGRATED .030.S/B 601R-32-054 MAIN LANDING GEAR SYSTEM - INSPECTION REPLACEMENT OF THE LEFT HAND AFT TRUNNION BUSHING INSPECTION AND RECERTIFICATION INCORPORATED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 11,184 hrs · 10,541 cycles

RIGHT HAND SIDE FRAME AND DOUBLER AT F.S. 718.0 BETWEEN STR'S 11 AND 12 IS CRACKED.REPAIRED CRACKED 718 FRAME AND DOUBLER IAW REO 601R-53-61-193 REV A.

Part: VANE CAP — CHAFED (RT INBD FLAP) · airframe 11,184 hrs · 10,541 cycles

RIGHT HAND WING INBOARD FLAP INBOARD LEADING EDGE VANE CAP IS CHAFED .020. REMOVED CHAFED VANE CAP AND INSTALLED NEW SERVICEABLE VANE CAP IAW WVAC EO 601R-57-2009.

Part: SKIN — DAMAGED (PAX DOOR) · airframe 11,184 hrs · 10,541 cycles

PAX DOOR SKIN REPAIR AT F.S. 310.00 IS DAMAGED. REPAIRED PAX DOOR SKIN REPAIR AT 310.00 IAW WVAC EO 601R-53-2006.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 11,107 hrs · 10,470 cycles

STALL FAIL CAUTION MESSAGE DURING TAKE OFF. RESET STALL COMPUTER.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 10,692 hrs · 10,077 cycles

STALL FAIL AND CONFIG SPOILER WARNING DURING T/O. RESET STALL COMPUTER.

Part: SENSOR — MALFUNCTIONED (LT AOA) · airframe 10,395 hrs · 9,807 cycles

STALL FAIL AND CONFIG WARNING DURING TAKEOFF. REPLACED THE AOA TRANSDUCER.

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 9,895 hrs · 9,332 cycles

DURING LANDING GEAR EXTENSION, NLG REMAINED UP. COULD NOT DUPLICATE. ALL EXTENSION AND RETRACTION CHECKS NORMAL.

Part: WHEEL — CRACKED (RT MLG) · airframe 9,546 hrs · 9,036 cycles

WHEEL ASSEMBLY WAS REMOVED FROM AIRCRAFT FOR TIRE CHANGE. FOUND WHEEL WAS CRACKED AT SPOKE AREA. MARKED LOT NR 1550.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,482 hrs · 8,976 cycles

EMERGENCY FLOOD LIGHT AT CABIN DOOR IS INOPERABLE. SECURED LOOSE WIRE AT LIGHT.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 9,382 hrs · 8,879 cycles

STALL FAIL MESSAGE. COULD NOT DUPLICATE. SYSTEM CHECK NORMAL.

Part: NUT — LOOSE (CONTROL YOKE) · airframe 9,247 hrs · 8,773 cycles

CO-PILOTS CONTROL YOKE HAS A SLIPPING FEEL WHEN MOVED LEFT OR RIGHT. RETORQUED THE CONTROL YOKE NUT TO M/M SPECIFICATIONS.

Part: ACTUATOR — BINDING (TE FLAP)

FLAPS FAILED MESSAGE. REPLACED THE LEFT WING NR 3 AND NR 4 FLAP ACTUATORS.

Part: BPSU — FAILED (TE FLAP)

FLAPS FAIL CAUTION MESSAGE. REPLACED THE RIGHT BPSU.

Part: TE FLAPS — FAILED (WINGS)

FLAPS FAILED AT 20 DEGREES DURING APPROACH. RESET FLAP SYSTEM PER AD 98-20-01.

Part: THRUST REVERSER — MALFUNCTIONED (RT ENGINE)

RIGHT HAND THRUST REVERSER UNLOCK MESSAGE. DEACTIVATED AND DEFERRED THE RIGHT HAND THRUST REVERSER.

Part: TE FLAP — FAILED (WING)

FLAPS FAILED AT 8 DEGREES DURING APPROACH. RESET FLAP SYSTEM PER AD 98-20-01.

Part: BULB — FAILED (ROW 5)

EMERGENCY LIGHT IN CEILING ABOVE ROW 5 IS INOPERABLE. REMOVED AND REPLACED BULK.

Part: RETRACT MECH — MALFUNCTIONED (TE FLAPS)

FLAPS FAILED AFTER LANDING. RESET FLAP SYSTEM PER AD 98-20-01.

Part: FRAME — CRACKED (BS 718)

FS 718, STR 11 RHS AFT DOUBLER CRACKED. REPAIRED CRACKED DOUBLER AT FS 718.0 STR 11 RHS IAW WVAC EO 601R-53-0099.

Part: FRAME — CRACKED (BS 718)

FS 718.0, STRI 11 LHS FRAME FLANGE CRACKED AND AFT SIDE OF FRAME DOUBLER CRACKED. REPAIRED CRACKED FRAME FLANGE AND CRACKED DOUBLER AT FS 718.0 STRI 11 LHS IAW WVAC EO 601R-53-0098 AND WVAC EO 601R-53-0100A.

Part: FRAME — CRACKED (BS 718)

FS 718 STR 11 RIGHT AND LEFT SIDE DOUBLERS CRACKED. ALSO, FRAME AT FS 718 LT SIDE HAS 2 INCH CRACK. REPAIRED FRAME AT FS 718 LT SIDE AND DOUBLERS ON RT AND LT SIDE IAW WVAC EO 601R-53-0098, 601R-53-0099 AND 601R-53-0100A.

Part: SKIN — NICKED (BS 310)

DURING INCOMING INSPECTION OF AIRCRAFT FOR EXTERNAL DAMAGE NOTICED THAT FUSELAGE SKIN WAS NICKED AT FS 310 STR 16 BY DOOR LATCH PIN. SKIN WAS BLENDED IAW BOMBARDIER REO 601R-53-21-160.

Part: OIL SYSTEM — REQ'D SERVICE (RT ENGINE)

CVG - FLT 9600 - RIGHT ENGINE OIL PRESSURE FLUCTUATING BETWEEN 35 PSI AND 55 PSI. SERVICED OIL TANK TO PROPER LEVEL. (X)

Part: BATTERY PACK — DISCHARGED (CABIN)

FLOOR EMERGENCY EXIT LIGHTS WILL NOT COME ON. REPLACED BATTERY AT NR 3 POSITION.

Part: FECU — MALFUNCTIONED (TE FLAPS)

FLAPS FAILED AFTER LANDING. REPLACED THE FECU.

Part: FECU — MALFUNCTIONED (TE FLAPS)

FLAPS FAILED AFTER LANDING. REPLACED THE FECU.

Part: WIRE — LOOSE (ROW 9-13)

EMERGENCY FLOOR LIGHTING INOPERABLE FROM ROW 9 TO ROW 13. CONNECTED LOOSE WIRING, SYSTEM OPERATION NORMAL.

Part: LIGHT — INOP (ROW 8)

EMERGENCY FLOOR LIGHTING AFT OF ROW 8 IS INOPERABLE. DISCONNECTED AND RECONNECTED LIGHT STRIP SYSTEM, OPERATION NORMAL.

Part: CONNECTOR — LOOSE (ROW 8)

EMERGENCY FLOOR PATH LIGHTING AFT OF ROW 8 IS INOPERABLE. RECONNECTED STRIP LIGHTING, SYSTEM TEST NORMAL.

Part: BPSU — MALFUNCTION (LT TE FLAP)

FLAPS FAILED AT 24 DEGREES DURING APPROACH. REPLACED THE LEFT HAND BPSU.

Part: WIRE — BROKEN (ROW 5)

SEVERAL EMERGENCY FLOOR LIGHTS ARE INOP. REPAIRED BROKEN WIRE AT ROW 5.

Part: SIGN — BROKEN (CABIN)

EMERGENCY EXIT SIGN AT GALLEY SERVICE DOOR IS BROKEN. REPLACED EXIT SIGN.

Part: FLEX SHAFT — BROKEN (LT TE FLAP)

FLAPS FAILED WHEN SELECTED FOR LANDING APPROACH. REPLACED THE LEFT HAND WING NR 5 FLAP FLEX DRIVE CABLE. CABLE WAS CORRODED AND BROKEN.

Part: WIRE — LOOSE (CABIN)

SOME OF THE EMERGENCY FLOOR LIGHTS ARE INOP. SECURED LOOSE WIRING CONNECTOR AT TRACK LIGHTING.

Part: SECU — FAILED (E/E COMPT)

FLIGHT SPOILERS CAUTION MESSAGE. REPLACED THE NR 2 SECU.

Part: SECU — MALFUNCTION (AVIONICS)

DURING TAKEOFF, CONFIG WARNING, SPOILERONS CAUTION MESSAGE. REPLACED THE NR 1 SECU.

Part: ACTUATOR — FAILED (LT TE FLAP)

AFTER LIFT OFF, 7 UNITS OF ROLL TRIM NEEDED TO REMAIN LEVEL. FLAPS FAILED DURING RETRACTION. THE LEFT OUTBOARD FLAP, INBOARD ACTUATOR FAILED CAUSING STRUCTURAL DAMAGE AND DEFORMATION OF THE FLAP ASSY. REPLACED ACTUATOR AND FLAP ASSY.

Part: LIGHTS — INOPERATIVE (CABIN)

LEFT AND RIGHT EXTERIOR FORWARD EMERGENCY LIGHTS INOPERATIVE. DEFERRED FORWARD EXTERIOR EMERGENCY LIGHTS IN ACCORDANCE WITH MEL 33-51-2.

Part: SENSOR — INOPERATIVE (NLG)

LANDING GEAR DISAGREE WARNING. NLG DID NOT RETRACT. REPLACED THE NLG WEIGHT ON WHEELS PROXIMITY SENSOR.

Part: ENGINE — FOD (RIGHT)

RT ENGINE FOD DURING TAKEOFF. ITT EXCEEDED LIMITS. REPLACED RIGHT HAND ENGINE.

Part: SERVO VALVE — FAILED (NLG STEERING)

NEW INOP MESSAGE DURING FLIGHT. STEERING INOP ON GROUND. REPLACED THE ELECTRO HYDRAULIC SERVO VALVE.

Part: SECU — INOPERATIVE (E/E COMPT)

SPOILERON FAULT MESSAGE. REPLACED NR 1 SECU. PART TOTAL CYCLES, 3,204.

Part: COMPUTER — TRIPPED (STALL WARNING)

STALL FAIL MESSAGE ON EICAS. RESET THE STALL WARNING COMPUTER AND AIRCRAFT RETURNED TO SERVICE.