N253PS

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,512 hrs · 36,203 cycles

FRONT TWO EMERGENCY GREEN EXIT SIGNS INOP. R+R WARDROBE EMERGENCY BETA LIGHT IAW CRJ 200 AMM 33-51-10-000/400-801 OPS CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (THRUST REVERSER) · airframe 35,560 hrs · 35,305 cycles

AFTER TAKEOFF THE CREW RECEIVED A REVERSER UNSAFE MESSAGE. RAN QRH AND RETURNED TO CAK. DEFERRED LT THRUST REVERSER. SUPPLEMENTAL INFORMATION: REMOVED AND REPLACED THE FOLLOWING: STOW SWITCH, POWER DRIVE UNIT, ORANGE HARNESS, THROTTLE LOCKOUT SWITCH, EMERGENCY STOW PUSH BUTTON SWITCH. MEL WAS CLEARED ON 28JUL19 BY INSTALLING A WIRE ALONGSIDE EXISTING HARNESS FROM CONNECTOR P125-X TO TB117-2 PER REO 601R-78-30-4283. HOWEVER IT FAILED AGAIN AND THE AIRCRAFT HAS RETURNED TO CAK. C/W BBD ACTION PLAN. REMOVED AND REPLACED TB205-5 AND TB207-7 IN JB4. REMOVED AND REPLACED CONTACT PINS ON TB205-5 PINS K AND E AND TB207-7 PINS K AND E. OPS CHECK GOOD.

Part: SWITCH — FAILED (THRUST REVERSER) · airframe 34,910 hrs · 34,673 cycles

ON APPROACH THE CREW RECEIVED AN R REV UNLOCKED WARNING. DID GO AROUND, RAN QRH. DECLARED EMERGENCY, LANDED, WITHOUT INCIDENT AND TAXIED TO GATE. R&R RH STOW SWITCH. OPS CHECK GOOD.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 34,146 hrs · 33,979 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL27.50 WL90 3 INCHES LONG 60% FSH FAILED NDT INSPECTIONS CA REPAIRED REAR PRESSURE BULKHEAD AT RBL27.50 IAW REO 601R-53-61-1285 REV.E DATED 10/31/16

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 34,146 hrs · 33,979 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL18 WL139 1.0 INCH LONG 90% FSH FAILED NDT INSPECTIONC/A: 1. REPAIRED REAR PRESSURE BULKHEAD AT LBL18 IAW REO 601R-53-61-1285 REV.E DATED 10/31/16.

Part: SUPPORT ANGLE — CRACKED (BS 621-625) · airframe 34,146 hrs · 33,979 cycles

L/H F.S.621.00 TO 625.00 OBLIQUE ANGLE IS CRACKED CA REPLACED ANGLE

Part: ANGLE — CRACKED (BS 280) · airframe 34,146 hrs · 33,979 cycles

F.S.280.00 I/B AND O/B CLIPS ARE CRACKED AT LBL9 AND RBL9. CA REPLACED CLIPS

Part: RIB — CRACKED (LT PYLON) · airframe 34,146 hrs · 33,979 cycles

LEFT PYLON RIB IS CRACKED CA REPAIRED RIB

Part: CONTROL HANDLE — DEFECTIVE (COCKPIT) · airframe 33,975 hrs · 33,821 cycles

AFTER TAKEOFF THE GEAR WOULD NOT RETRACT. THE AIRCRAFT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. THE AIRCRAFT FERRIED TO A MAINTENANCE BASE AND THE LANDING GEAR SELECTION HANDLE WAS REPLACED.

Part: WARNING LIGHT — FALSE ACTIVATION (BLEED AIR SYS) · airframe 32,614 hrs · 32,466 cycles

THE CREW HAD A REPORT OF LEFT 14TH STAGE DUCT WARNING MESSAGE. RAN THE QRH, THE MESSAGE WENT AWAY AND REAPPEARED. CREW DECLARED AN EMERGENCY, DIVERTED, AND LANDED WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH OPS CHECK OF THE BLEED AIR LEAK DETECTION AND WARNING SYSTEM AND THE BLEED AIR LEAK SYSTEM OPERATIONAL CHECKED GOOD.

Part: SENSOR — UNSECURE (MLG) · airframe 31,969 hrs · 31,896 cycles

GEAR DISAGREE MESSAGE AFTER TAKEOFF, CREW DECLARED AN EMERGENCY. SECURED THE LT MLG UPLOCK SENSOR PS11GA TARGET, OPS CHECKED GOOD.

Part: ROLL PIN — MISSING (SERVICE DOOR) · airframe 30,341 hrs · 30,822 cycles

SERVICE DOOR CLOSE LATCH HANDLE FREE SPINNING. INSTALLED LOWER LATCH ROLL PIN.

Part: MOTOR — INOPERATIVE (PASSENGER DOOR) · airframe 30,318 hrs · 30,306 cycles

PASSENGER DOOR ASSIST MOTOR NOT WORKING. REMOVED AND REPLACED PASSENGER DOOR ASSIST MOTOR.

Part: SKIN — DENTED (BS 559) · airframe 30,118 hrs · 30,137 cycles

FUSELAGE SKIN DENTED BETWEEN BS 559.96 - 559.112, STRINGERS 16 - 17R. PERFORMED A MAJOR REPAIR.

Part: STRINGER — DAMAGED (BS 235-250) · airframe 30,118 hrs · 30,137 cycles

STRINGER 26R AT BS 235-250 DAMAGED. PERFORMED A MAJOR REPAIR TO THE STRINGER.

Part: RIB — DAMAGED (RT ELEVATOR) · airframe 30,118 hrs · 30,137 cycles

DAMAGE TO RIGHT ELEVATOR RIB NR 3 ALONG BOTTOM SKIN RIB RADIUS. PERFORMED REPAIR TO THE RIGHT ELEVATOR.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 30,118 hrs · 30,137 cycles

REAR PRESSURE BULKHEAD WEB HAS CRACK INDICATION OF APPROXIMATELY 5 INCHES IN LENGTH AT BS 621 BL 0. MAINTENANCE PERFORMED A MAJOR REPAIR IAW AMM.

Part: POSITION SENSOR — FAILED (TE FLAPS) · airframe 29,061 hrs · 29,094 cycles

FLAPS FAIL CAUTION MESSAGE DURING CLIMB AND HYD PUMP 2B FAIL CAUTION MESSAGE WHILE FOLLOWING THE QRH CHECKLIST FOR FLAPS FAIL. MAINTENANCE DEFERRED FLAP SYS MEL 90-10-02 CAT A., INSPECTED AND RESET SYS CIRCUIT BREAKERS. MAINTENANCE R & R THE BRAKE AND POSITION SENSOR UNIT, AND PERFORMED CHECKS IAW THE AMM, WHICH CLEARED THE MEL. THE ACFT WAS RELEASED FOR SERVICE.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 28,175 hrs · 28,181 cycles

CREW REPORTED GEAR DISAGREE RED MESSAGE IN FLIGHT, 6 SECONDS AFTER GEAR HANDLE DEPLOYED. NLG EXTENDED NORMALLY AND MANUAL EXTENSION USED FOR MLG. EMERGENCY DECLARED AND CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOT, R & R MLG SELECTOR VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WINDSHIELD WIPER — BENT (WINDSHIELD) · airframe 28,005 hrs · 28,011 cycles

CREW REPORTED CAPTAIN’S WINDSHIELD WIPER BLADE COMING LOOSE AND THEN BENDING IN HALF IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R CAPTAIN’S WIPER BLADE, REINSTALLED CAPTAIN’S WIPER DRIVE ARM AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: ACM — OVERHEATED (LEFT) · airframe 27,582 hrs · 27,581 cycles

CREW REPORTED, LT PACK OVERTEMP AND AUTO SHUTDOWN AND SMOKE COMING OUT OF GASPERS. MAINTENANCE INSPECTED, R & R LT ACM AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONTROLLER — ODOR (COCKPIT) · airframe 27,030 hrs · 27,048 cycles

CREW REPORTED A STRONG ODOR OF FUEL AND EXHAUST COMING THROUGH VENTS WHEN SWAPPING BLEEDS TO APU. MAINTENANCE TROUBLESHOT AND R & R FLIGHT COMPARTMENT TEMPERATURE CONTROLLER AND CHECKED IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 26,193 hrs · 26,192 cycles

LEFT CARGO FLOOR SUPPORT FROM BS 574 - 621 HAS CORROSION AT NUTPLATE HOLES. REPLACED THE FLOOR SUPPORT IAW REO 601R-53-61-1574.

Part: STATIC WICK — DAMAGED (LT WING) · airframe 24,785 hrs · 24,790 cycles

CREW REPORTED LIGHTNING STRIKE. MAINTENANCE TROUBLESHOT, R & R STATIC WICKS, AND REPAIRED LT OTBD CANOE FAIRING USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — VIBRATION (RT ENGINE) · airframe 24,231 hrs · 24,251 cycles

CREW REPORTED RT ENGINE FAN VIBRATION DURING CLIMB. CREW FOLLOWED QRH, DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED RT FAN BLADES AND PERFORMED CHECKS IAW AMM. NO DEFECTS NOTED. ACFT RELEASED FOR SERVICE.

Part: UNION — LEAKING (HYD PUMP) · airframe 24,022 hrs · 24,038 cycles

CREW REPORTED HYDRAULIC 1 LOW PRESSURE MESSAGE AT 600 FEET AGL. QUANTITY WAS ZERO. CREW RAN QRH, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND UNION LEAKING ON ENGINE DRIVEN PUMP. MAINTENANCE R & R NR 1 ENGINE EDP AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (LEFT) · airframe 22,994 hrs · 23,107 cycles

CREW REPORTED LT WINDSHIELD CRACKED IN FLIGHT. ACFT RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MX TROUBLESHOT, REMOVED, REPLACED, AND OPS CHECKED THE LT WINDSHIELD USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: ENGINE — FAILED (LEFT) · airframe 21,879 hrs · 22,108 cycles

CREW REPORTED AIRCRAFT HAD SMOKE IN THE CABIN. AIRCRAFT RETURNED TO AIRPORT LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE LEFT ENGINE AND OXYGEN EQUIPMENT PER AIRCRAFT MANUALS. CHECKS WERE PERFORMED PER THE AIRCRAFT MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (NLG STEERING) · airframe 21,791 hrs · 22,034 cycles

CREW REPORTED AIRCRAFT PULLED TO THE LEFT AND FAILED TO RESPOND TO RUDDER INPUTS ON TAKEOFF ROLL. CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED HANDWHEEL CONTROL UNIT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,531 hrs · 20,928 cycles

CREW REPORTED THE CEILING EXIT CALL LIGHT WAS NOT LIGHTING. MAINTENANCE TROUBLESHOT AND REPLACED THE LIGHT USING THE AIRCRAFT MANUALS. OPERATIONAL CHECKS WERE DONE USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SHUTOFF VALVE — FAULTY (AC BAY) · airframe 20,416 hrs · 20,830 cycles

WHILE CLIMBING OUT, CREW REPORTED LEFT ENGINE PACK VALVE CLOSED. CREW COULD NOT GET VALVE TO OPEN. RIGHT PACK WAS ALREADY ON DEFERRAL PER MEL. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT PRSOV (PRESSURE REGULATING / SHUTOFF VALVE) FILTER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: TIRE — FLAT (RT MLG) · airframe 20,224 hrs · 20,651 cycles

CREW REPORTED AFTER LANDING RIGHT INBOARD AND RIGHT OUTBOARD MAIN TIRES FLAT. USING AIRCRAFT MANUALS MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD, OUTBOARD MAIN TIRES, AND LEFT OUTBOARD ANTI SKID WIRE HARNESS. OPERATIONAL CHECKS WERE PERFORMED USING AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SWITCH — DEFECTIVE (SERVICE DOOR) · airframe 19,975 hrs · 20,433 cycles

CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURISE. AIRCRAFT RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE SERVICE DOOR OUTER HANDLE SWITCH USING THE AIRCRAFT MANUALS. OPERATIONAL CHECKS WERE PERFORMED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 19,467 hrs · 19,960 cycles

CREW REPORTED FLAPS FAIL CAS MESSAGE WHILE CLIMBING THROUGH FL220. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED RIGHT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: PDU — FAILED (TE FLAP) · airframe 18,426 hrs · 18,960 cycles

CREW REPORTED FLAPS FAILED AT 14 DEGREES ON APPROACH. CREW FOLLOWED QRH (QUICK REFERENCE HANDBOOK) AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FLAP PDU (POWER DRIVE UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: TRANSFER PUMP — CLOGGED (FUEL SYSTEM) · airframe 18,385 hrs · 18,921 cycles

CREW REPORTED FUEL IMBALANCE IN FLIGHT, LEFT WING LOW, EN ROUTE FROM DCA TO BNA. CROSSFLOW WAS WORKING, BUT COULD NOT KEEP UP WITH BALANCING FUEL AT HIGH POWER SETTINGS. CREW DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FUEL TRANSFER SYSTEM, REMOVED AND REPLACED LEFT CENTER TANK TRANSFER EJECTOR PUMP AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,370 hrs · 18,905 cycles

AT CLT, CREW REPORTED EMERGENCY LIGHT ON SERVICE DOOR INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED LIGHT BULB AT FORWARD EXTERNAL SERVICE DOOR EMERGENCY LIGHT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,879 hrs · 18,424 cycles

DURING SCHEDULED MAINTENANCE THE FS 621 PRESSURE BULKHEAD WAS FOUND CRACKED. THE FS 621 PRESSURE BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 17,813 hrs · 18,357 cycles

CREW REPORTED GEAR DISAGREE MESSAGE ON GEAR EXTENSION ON FINAL APPROACH TO CLT. PER QRH, CREW PULLED EMERGENCY GEAR EXTENSION. AIRCRAFT LANDED IN CLT WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED MAIN LANDING GEAR SELECTOR VALVE, BLED NUMBER 3 HYDRAULIC SYSTEM AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: POST — CRACKED (FUSELAGE) · airframe 17,543 hrs · 18,117 cycles

DURING SCHEDULED MAINTENANCE THE FS FS409+128 VERTICLE POST WAS FOUND CRACKED. THE FS 409+128 VERTICLE POST WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PUMP — FLUCTUATES (LT ENGINE) · airframe 17,437 hrs · 17,997 cycles

CREW REPORTED LEFT ENGINE OIL PRESSURE MESSAGE IN FLIGHT EN ROUTE FROM CAK TO PHL. CREW FOLLOWED QRH AND SHUT DOWN LEFT ENGINE. AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AIRCRAFT, REMOVED AND REPLACED LEFT ENGINE LUBE AND SCAVENGE PUMP AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: PSEU — MALFUNCTIONED (LANDING GEAR) · airframe 16,771 hrs · 17,358 cycles

CREW REPORTED GEAR DISAGREE WITH GEAR LEVER DOWN WHILE ON FINAL APPROACH TO CLT. CREW COMPLIED WITH QRH AND LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT LANDING GEAR SYSTEM, REMOVED AND REPLACED PSEU (PROXIMITY SENSOR ELECTRONIC UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WIRE HARNESS — PINCHED (VIBRATION SYS) · airframe 15,929 hrs · 16,502 cycles

ON DEPARTURE AND INITIAL CLIMBOUT FROM DAY, CREW REPORTED THE ENGINE NR 2 VIBRATION GAUGE SHOWED AMBER DASHES WITH VIB INDICATION ON THE N2 GAUGE. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE HARNESS FOR THE RIGHT ENGINE VIBRATION SYSTEM AND PERFORMED CHECKS USING THE AIRCRAFT AND ENGINE MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG WW) · airframe 15,874 hrs · 16,450 cycles

CREW REPORTED A GEAR DISAGREE WARNING WHEN SELECTING THE LANDING GEAR DOWN WHILE ON APPROACH TO PHL. NOSE GEAR WENT DOWN, BUT MAIN GEAR REMAINED UP. CREW MANUALLY RELEASED AND PUT DOWN THE GEAR AND LANDED IN PHL WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE MAIN LANDING GEAR SELECTOR VALVE AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ANTI-ICE VALVE — MALFUNCTIONED (LT COWLING) · airframe 15,816 hrs · 16,394 cycles

CREW REPORTED A LEFT COWL ANTI-ICE AMBER MESSAGE UPON TAKEOFF FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE LEFT COWL ANTI-ICE VALVE AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 15,691 hrs · 16,274 cycles

CREW REPORTED A RED GEAR DISAGREE MASTER WARNING IN FLIGHT ON APPROACH TO CLT. CREW COMPLIED WITH QRH, USED MANUAL GEAR EXTENSION AND LANDED IN CLT WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE MAIN LANDING GEAR SELECTOR VALVE AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SWITCH — BROKEN (AC BAY) · airframe 14,999 hrs · 15,583 cycles

CREW REPORTED A LEFT PACK OVERHEAT CAUTION MESSAGE ON THE GROUND AT CLT. UPON SELECTING THE LEFT PACK ON, A STRONG SMOKE ODOR FILLED THE COCKPIT. CREW TURNED OFF THE LEFT PACK. MAINTENANCE INSPECTED AND TROUBLESHOT THE AIRCRAFT AND FOUND BROKEN PINS ON THE COMPRESSOR OUTLET TEMPERATURE SWITCH. MAINTENANCE REMOVED AND REPLACED THE TEMPERATURE SWITCH AND CONNECTOR AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — GOUGED (FUSELAGE) · airframe 14,865 hrs · 15,444 cycles

DURING SCHEDULED MAINTENANCE, RIGHT FUSELAGE APPROX 12 INCHES AFT AND 6 INCHES O/B OF DRAIN MAST (AFT) HAS 2 GOUGES APPROX .008 DEEP. REPAIRS WERE MADE USING AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,865 hrs · 15,444 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND AT RIGHT FS 559 BULKHEAD WEB. REPAIRS WERE MADE USING AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — BLOWN (RT MLG) · airframe 13,680 hrs · 14,215 cycles

CREW FOUND THE RT INBOARD MLG TIRE SHREDDED AND THE RT INBOARD FLAP ASSEMBLY DAMAGED. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE RT INBOARD MLG WHEEL / TIRE ASSEMBLY, THE RT INBOARD FLAP ASSEMBLY, A PROXIMITY SENSOR AND A CONDUIT ASSEMBLY. MAINTENANCE REPAIRED A DENT ON THE RT FUSELAGE AND DAMAGE TO THE FLAP STUB FAIRING. CHECKS WERE PERFORMED BY MAINTENANCE. ALL WORK WAS ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS AND REO’S. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PANEL — DAMAGED (WING) · airframe 13,277 hrs · 13,772 cycles

PITTING WAS FOUND ON THE RADIUS OF FUEL PANEL 510AB. REPAIRS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: NOSE COWL — DENTED (RT ENGINE) · airframe 12,799 hrs · 13,276 cycles

AFTER ARRIVAL IN GNV, THE CREW REPORTED A DENT ON THE RT ENGINE COWL LIP AT APPROXIMATELY THE 11:30 POSITION DUE TO A POSSIBLE BIRD STRIKE. MAINTENANCE INSPECTED THE DENT AND REMOVED AND REPLACED THE RT ENGINE NOSE COWL ASSEMBLY USING THE AIRCRAFT MAINTENANCE MANUAL. NO OTHER DAMAGE WAS NOTED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: IDG — MALFUNCTIONED (NR 2) · airframe 10,671 hrs · 11,061 cycles

CREW REPORTED AN ABORTED TAKEOFF IN MGM FOR NR 2 IDG CAS MESSAGE. THE AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED AND DEFERRED THE NR 2 IDG. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. AT ANOTHER STATION, THE IDG WAS SERVICED AND THE DEFERRAL WAS CLEARED.

Part: A/C PACK — MALFUNCTIONED (LEFT) · airframe 9,337 hrs · 9,646 cycles

CREW REPORTED A LT PACK FELL OFF LINE FOLLOWED BY A HIGH PRESSURE CAS MESSAGE. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED AN OPERATIONAL TEST OF THE ACS SYSTEM IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — SEPARATED (RT MLG) · airframe 8,820 hrs · 9,081 cycles

CREW REPORTED THE RIGHT INBOARD TIRE SEPARATED. MAINTENANCE INSPECTED AND FOUND THE TREAD SEPARATION AND DAMAGE TO THE RIGHT INBOARD FLAP. MAINTENANCE REMOVED AND REPLACED THE NR 3 AND NR 4 MAIN TIRES. MAINTENANCE REPAIRED FLAP DAMAGE PER REO 601R57-52-716 AND TEMP REPAIR 11000. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ADG — DAMAGED (RIGHT) · airframe 7,471 hrs · 7,594 cycles

CREW REPORTED THE ADG DEPLOYED IN FLIGHT WITH NO CAUSE. MAINTENANCE REMOVED AND REPLACED THE ADG IAW THE AIRCRAFT MM. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 7,228 hrs · 7,335 cycles

CREW REPORTED A LIGHTNING STRIKE WHILE IN FLIGHT. CREW LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE PERFORMED AN EN ROUTE LIGHTNING STRIKE INSPECTION. MAINTENANCE REMOVED AND REPLACED THE RADOME IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 53-81-01-400-801. MAINTENANCE REPAIRED ALL DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ENGINE — FAILED (NR 2) · airframe 5,624 hrs · 5,617 cycles

CREW REPORTED SMOKE IN COCKPIT AND CABIN ON TAKEOFF. CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED AND FOUND COKING ON 10TH STAGE DUCTING. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 5,582 hrs · 5,575 cycles

CREW REPORTED SMOKE IN CABIN. AIRCRAFT RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLEANED ACM. MAINTENANCE ALSO SERVICED ACM OIL. OPERATIONAL CHECKS WERE PERFORMED. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 5,545 hrs · 5,536 cycles

CREW REPORTED SMOKE AND TOILET MESSAGE. MAINTENANCE CHECKED AIRCRAFT FOR SOURCE OF SMOKE, NONE FOUND. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 5,313 hrs · 5,280 cycles

CREW REPORTED A BURNING SMELL IN GALLEY AREA AT CRUISE AFTER LEAVING CAE. AIRCRAFT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED A DETAILED VISUAL INSPECTION OF GALLEY AREA ELECTRICAL COMPONENTS, ELECTRICAL CONTACTOR PANEL, AND AVIONICS BAY ELECTRICAL COMPONENTS. COULD NOT DETECT ANY BURNING SMELL AT THIS TIME. NO VISUAL EVIDENCE OF ELECTRIC BURNING OR ARCING. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CAUTION MESSAGE — ILLUMINATED (SPOILERS) · airframe 5,132 hrs · 5,097 cycles

THE CREW REPORTED A FLIGHT SPOILER CAS MESSAGE IN FLIGHT. MAINTENANCE PERFORMED CRJ200 SL-27-001F AND CRJ200 FIM 27-60-00. NO DEFECTS OR FAULTS FOUND. OPERATIONAL CHECKS WERE PERFORMED. OPS CHECKS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS) · airframe 5,125 hrs · 5,088 cycles

THE CREW REPORTED A FLIGHT SPOILER CAS MESSAGE IN FLIGHT. MAINTENANCE PERFORMED CRJ200 SL-27-001F AND CRJ200 FIM 27-60-00. NO DEFECTS OR FAULTS FOUND. OPERATIONAL CHECKS WERE PERFORMED. OPS CHECKS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — OPEN · airframe 4,049 hrs · 3,980 cycles

AFTER TAKEOFF THE CREW DETERMINED THE GROUND COMMUNICATION DOOR WAS OPEN. THE FLIGHT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE CONFIRMED THE OPEN DOOR. INSPECTION REVEALED NO DISCREPANCIES. THE DOOR WAS PROPERLY SECURED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 2,471 hrs · 2,448 cycles

DURING CLIMBOUT THE OVERBOARD COOL CAUTION MESSAGE ILLUMINATED AND THE CABIN DID NOT PRESSURIZE. THE CREW RETURNED TO DAY. MAINTENANCE FOUND THE OVERBOARD EXHAUST SHUTOFF VALVE OPEN. THE SOV WAS SECURED CLOSED IAW CRJ200 AMM 21-24-00-040-806 AND MEL 21-24-06. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: STRUCTURE — VIBRATION (AIRFRAME) · airframe 38 hrs · 37 cycles

AT 28,000, THE CREW FELT A MODERATE VIBRATION AND SLOWED TO 290 AND THE VIBRATION LESSENED. AFTER SELECTING THE FLAPS TO 20, THE VIBRATION INCREASED THEN LESSENED AGAIN. THE MODERATE VIBRATION CONTINUED UNTIL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT IN ACCORDANCE WITH BOMBARDIER AMM 32-20-00-210-801, 32-10-00-210-801, 27-64-00-710-801, 27-40-00-720-801 AND 27-54-00-310-801, NO DEFECTS WERE NOTED. AN OPERATIONAL CHECK FLIGHT WAS PERFORMED AND AGAIN, NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.