N256PS

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 33,791 hrs · 33,891 cycles

FLIGHT CREW HAD A "FLAPS FAIL" CAUTION MESSAGE OCCUR EN ROUTE. DECLARED AND EMERGENCY AND DIVERTED TO THE NEAREST SUITABLE AIRPORT. MAINTENANCE DEFERRED FLAP SYSTEM. COMPLIED WITH T/O AND AD, R&R L BPSU. CHECKS GOOD. CLEARED FLAP MEL.

Part: SEAL — LEAKING (ENGINE) · airframe 31,702 hrs · 31,903 cycles

RIGHT ENGINE SHUTDOWN IN FLIGHT BY CREW DUE TO OIL FLUCTUATIONS. AICRAFT LANDED WITHOUT ISSUE. MX ADDED 6 QRTS OF OIL AND THE RT ENGINE FAILED THE CONSUMPTION CHECK. MX REPLACED THE ATS, IDG, AND EDP CARBON SEALS, RUN AND LEAK CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 364-409) · corrosion level 2 · airframe 30,727 hrs · 30,924 cycles

LEFT SIDE PAX SEAT TRACKS CORRODED AT THE FOLLOWING BS 364 - 409+96. REMOVED DAMAGED SEAT TRACKS AND REPLACED WITH NEW IAW AMM 53-01-11-000-802.

Part: PLATE — CORRODED (BS 349) · corrosion level 2 · airframe 30,727 hrs · 30,924 cycles

PASSENGER DOOR AFT ANCHOR FITTING SERATATED PLATE IS CORRODED. REMOVED AND REPLACED NEW SERVICEABLE AFT ANCHOR FITTING SEPARATED PLATE.

Part: SEAT TRACK — CORRODED (BS 409-461) · corrosion level 2 · airframe 30,727 hrs · 30,924 cycles

RH PAX SEAT TRACKS CORRODED AT BS 409.00+32 TO 409.00+64 AND AT BS 461.00. FABRICATED A NEW SEAT TRACK IAW REO 601R-53-00-485. INSTALLED THE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: BULKHEAD WEB — CRACKED (FS 621) · airframe 30,727 hrs · 30,924 cycles

REAR PRESSURE BULKHEAD HAS MULTIPLE CRACK INDICATIONS. PERFORMED A MAJOR REPAIR TO THE BS 621 PRESSURE BULKHEAD AT RBL 9.5, WL76, LBL 9.5, WL 76, LBL 18, WL 76.

Part: SKIN — CORRODED (BS 559) · corrosion level 2 · airframe 30,727 hrs · 30,924 cycles

FUSELAGE SKIN BETWEEN BS 559.16 AND 559.112, STRINGERS 26L AND 26R, CORRODED. PERFORMED A MAJOR REPAIR TO FUSELAGE SKIN.

Part: STRINGER — CRACKED (BS 378) · airframe 30,727 hrs · 30,924 cycles

STRINGER 3L CRACKED AT BS 378.5 AFT END OF PASSENGER DOOR’S UPPER SILL. PERFORMED A MAJOR REPAIR TO STRINGER 3L BETWEEN BS 379 AND 394.

Part: TRANSDUCER — FAULTY (WHEEL SPEED) · airframe 30,110 hrs · 30,326 cycles

LANDING GEAR FAILED TO RETRACT. REMOVED AND REPLACED THE WHEEL SPEED TRANSDUCER.

Part: HANDLE — INOPERATIVE (LANDING GEAR) · airframe 30,110 hrs · 3,026 cycles

LANDING GEAR FAILED TO RETRACT. REMOVED AND REPLACED THE LANDING GEAR HANDLE ASSEMBLY.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,301 hrs · 29,548 cycles

EMERGENCY LIGHTS NOT WORKING. REMOVED AND REPLACED THE NR 3 BATTERY PACK AND CHECKED IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,301 hrs · 29,548 cycles

EMERGENCY LIGHTS NOT WORKING. MAINTENANCE INSPECTED, R & R NR 2 BATTERY PACK AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 29,301 hrs · 29,548 cycles

EMERGENCY LIGHTS NOT WORKING. MAINTENANCE INSPECTED, REMOVED AND REPLACED NR 4 BATTERY PACK AND PERFORMED CHECK IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: GENERATOR — FAILED (LT ENGINE) · airframe 28,561 hrs · 28,806 cycles

CREW REPORTED A LOUD NOISE FROM LT ENGINE FOLLOWED BY PFC, MFD, ACARS, AND LT, RT WINDSHIELD HEAT TEMPORARY FAILURE. THEY DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT ENGINE IDG, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: CARBON SEAL — DAMAGED (LT IDG) · airframe 28,561 hrs · 28,806 cycles

CREW REPORTED A LOUD NOISE FROM LT ENGINE FOLLOWED BY PFC, MFD, ACARS, AND LT/RT WINDSHIELD HEAT TEMPORARY FAILURE. THEY DECLARED AN EMERGENCY, DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE IDG ACCESSORY GEAR BOX CARBON SEAL AND MATING RING. MAINTENANCE PERFORMED CHECKS IAW THE AMM AND THE ACFT WAS RELEASED FOR SERVICE.

Part: SEAL — OBSTRUCTED (PAX DOOR) · airframe 27,729 hrs · 27,948 cycles

CREW REPORTED LOUD SQUEAL FROM MAIN CABIN DOOR IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED DEBRIS FROM PASSENGER DOOR SEAL AREA AND PRESSURIZED ACFT IAW AMM. NO DEFECTS NOTED. ACFT RELEASED FOR SERVICE.

Part: POST — CRACKED (BS 409) · airframe 27,272 hrs · 27,488 cycles

CRACK NOTED AT BS 409 AND VERTICAL POST AT LBL 18, INBD CHANNEL WL 60 APPROXIMATELY .100 INCHES IN LENGTH VERTICALLY AND 53 PERCENT FULL SCREEN HEIGHT.

Part: BATTERY PACK — CREW ERROR (EMERGENCY LIGHTS) · airframe 27,135 hrs · 27,353 cycles

CREW REPORTED EMERGENCY LIGHTS WOULD NOT ILLUMINATE. SWITCH WAS LEFT IN THE ARM POSITION. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHT BATTERY PACK NR 3 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — CREW ERROR (EMERGENCY LIGHTS) · airframe 27,135 hrs · 27,353 cycles

CREW REPORTED EMERGENCY LIGHTS WOULD NOT ILLUMINATE. SWITCH WAS LEFT IN THE ARM POSITION. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHT BATTERY PACK NR 4 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — CREW ERROR (EMERGENCY LIGHTS) · airframe 27,135 hrs · 27,353 cycles

CREW REPORTED EMERGENCY LIGHTS WOULD NOT ILLUMINATE. SWITCH WAS LEFT IN THE ARM POSITION. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHT BATTERY PACK NR 1 AND PERFORMED CHECKS IAW AMM ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — CREW ERROR (EMERGENCY LIGHTS) · airframe 27,135 hrs · 27,353 cycles

CREW REPORTED EMERGENCY LIGHTS WOULD NOT ILLUMINATE. SWITCH WAS LEFT IN THE ARM POSITION. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHT BATTERY PACK NR 2 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,638 hrs · 26,868 cycles

CREW REPORTED FORWARD EMERGENCY LIGHT, NR 1 IN FORWARD CABIN ABOVE ROW 2, INOPERATIVE. MAINTENANCE INSPECTED, R & R FORWARD OVERHEAD CEILING EMERGENCY FLOODLIGHT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,466 hrs · 26,696 cycles

CREW REPORTED FORWARD EMERGENCY FLOOD LIGHT IN CEILING INOPERATIVE. MAINTENANCE INSPECTED, R & R FORWARD CEILING EMERGENCY FLOOD LIGHT BULB AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,115 hrs · 24,328 cycles

CREW REPORTED FORWARD ORANGE SECTION OF FLOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE INSPECTED, R & R NR 1 FLOOR LIGHT ASSY AND ORANGE OVERLAY AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,845 hrs · 24,071 cycles

CREW REPORTED EMERGENCY FLOOR LIGHTS AT ROW 1 AND ROW 2 WOULD NOT LIGHT UP AND WERE TORN OUT OF TRACK. MAINTENANCE INSPECTED, R & R EMERGENCY FLOOR LIGHTS AT ROW 1 AND ROW 2 AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: STATIC WICK — DAMAGED (RT WING) · airframe 23,632 hrs · 23,877 cycles

CREW SUSPECTED A LIGHTNING STRIKE AND REPORTED 2 STATIC WICKS MISSING, 1 ON TAIL AND 1 ON RT WING. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND R & R RT HORIZONTAL STABILIZER TIP, REPAIRED RT HORIZONTAL STABILIZER TIP RIB SCREW HOLES AND R & R STATIC DISCHARGER BASE AND DISCHARGER ON RT AILERON DUE TO LIGHTNING STRIKE DAMAGE. ALL WORK ACCOMPLISHED BY MAINTENANCE IAW AMM AND REO. ACFT RELEASED FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT) · airframe 23,176 hrs · 23,440 cycles

CREW REPORTED CAPTAIN SIDE WINDOW, BOTTOM RT CORNER LOOKED CRACKED. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED CAPTAIN SIDE WINDOW IAW COMPONENT MM, FOUND NO DAMAGE OR CRACKS, BUT FOUND SPEED TAPE PEELING ON WINDOW SIDE STRAP. MAINTENANCE APPLIED SPEED TAPE AS REQUIRED. ACFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (BS 202) · airframe 22,879 hrs · 23,163 cycles

DURING SCHEDULED MX FOUND FS 202 PRESSURE BULKHEAD CRACKED AROUND THE PARKING BRAKE CUTOUT. FS 202 PRESSURE BULKHEAD AT THE PARKING BRAKE CUTOUT WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (BS 202) · airframe 22,879 hrs · 23,163 cycles

DURING SCHEDULED MX FOUND FS 202 PRESSURE BULKHEAD CRACKED AROUND THE PARKING BRAKE CUTOUT. FS 202 PRESSURE BULKHEAD AT THE PARKING BRAKE CUTOUT WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE. DUP OF 20131103, ADDED END NR TO CONTROL NR,

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 22,361 hrs · 22,674 cycles

CREW REPORTED ALL PRESSURIZATION SHUT OFF AT FL 240. FOLLOWED EMERGENCY DESCENT PROCEDURE AND QRH. LT PACK HIGH TEMP MESSAGE ALSO RECEIVED IN THE DESCENT. DIVERTED, DROPPED MASKS AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED MAINFEED MANIFOLD FOR CRACKS AND SECURITY OF DUCTS. NO DEFECTS NOTED. ACFT PRESSURE CHECK AND LT PACK OPS CHECKED GOOD.

Part: A/C PACK — MALFUNCTIONED (RIGHT) · airframe 22,287 hrs · 22,603 cycles

CREW REPORTED RT PACK HIGH PRESSURE MESSAGE ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. MX COMPLIED WITH OPS CHECK OF RT PACK IAW ACFT MM. ACFT RELEASED FOR SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 20,440 hrs · 20,970 cycles

CREW REPORTED FLOOR EMERGENCY LIGHTS FROM ROW NINE (9) AFT INOPERATIVE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NUMBER FOUR (4) INVERTER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BPSU — FAILED (TE FLAP) · airframe 19,355 hrs · 19,987 cycles

CREW REPORTED FLAPS FAIL CAUTION MESSAGE WHILE CLIMBING THROUGH 11,000 FEET. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING FIM. AIRCRAFT RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 19,350 hrs · 19,982 cycles

CREW RECEIVED FLAPS FAIL AMBER MESSAGE IN FLIGHT. CREW LANDED WITHOUT INCIDENT. SYSTEM RESET AND AIRCRAFT RELEASED FOR SERVICE USING AD PROCEDURE.

Part: BPSU — FAILED (TE FLAP) · airframe 19,350 hrs · 19,982 cycles

CREW RECEIVED FLAPS FAIL AMBER MESSAGE IN FLIGHT. CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING FIM. AIRCRAFT RELEASED FOR SERVICE.

Part: FAIRING — DAMAGED (TE FLAP) · airframe 18,500 hrs · 19,179 cycles

DURING PREFLIGHT INSPECTION, CREW REPORTED DAMAGE TO RIGHT WING ON INBOARD FAIRING. MAINTENANCE INSPECTED AND FOUND DAMAGE TO RIGHT INBOARD FLAP INBOARD HINGE FAIRING TO BE FROM LIGHTNING STRIKE. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION, REPAIRED RIGHT WING FLAP FAIRING, REMOVED AND REPLACED THREE (3) STATIC WICKS AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SENSING ELEMENT — FAULTY (FUSELAGE) · airframe 18,460 hrs · 19,141 cycles

CREW REPORTED ANTI-ICE DUCT RED WARNING MESSAGE 500 FEET AFTER TAKEOFF. ALL ANTI-ICE WAS OFF AT THE TIME. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED LEFT FUSELAGE SENSING ELEMENT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,147 hrs · 18,846 cycles

DURING SCHEDULED MAINTENANCE THE FS 280.0 BULKHEAD WEB WAS FOUND CRACKED. THE FS 280.0 BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,147 hrs · 18,846 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: BATTERY — DISCHARGED (CABIN) · airframe 18,127 hrs · 18,823 cycles

AT CLT, CREW REPORTED FLOOR EMERGENCY LIGHTS INOPERATIVE FROM ROW EIGHT (8) TO REAR OF CABIN. MAINTENANCE INSPECTED, REMOVED AND REPLACED NUMBER FOUR (4) EMERGENCY BATTERY AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 17,843 hrs · 18,535 cycles

AT CAK, CREW REPORTED BIRD STRIKE TO RIGHT SIDE OF NOSE. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION, REMOVED AND REPLACED RADOME AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 17,494 hrs · 18,200 cycles

CREW REPORTED ELECTRICAL SMOKE ODOR IN CABIN ON DESCENT INTO PHL. AIRCRAFT LANDED IN PHL WITHOUT FURTHER INCIDENT AND PASSENGERS EVACUATED AIRCRAFT. MAINTENANCE INSPECTED AIRCRAFT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. REPORTED DISCREPANCY COULD NOT BE DUPLICATED AND NO DEFECTS FOUND. AIRCRAFT RELEASED FOR SERVICE.

Part: WEB — CRACKED (FUSELAGE) · airframe 15,082 hrs · 15,827 cycles

DURING SCHEDULED MAINTENANCE THE FS 559 WEB WAS FOUND CRACKED. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CABLE — DEFECTIVE (CABIN) · airframe 14,138 hrs · 14,895 cycles

AT CLT, CREW REPORTED FLOOR EMERGENCY LIGHTS FROM ROW 2 TO ROW 5 NOT ILLUMINATING WHEN IN THE ON POSITION. MAINTENANCE INSPECTED, REMOVED AND REPLACED A FLAT CABLE ASSEMBLY AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ANTENNA — DAMAGED (ELT) · airframe 13,488 hrs · 14,185 cycles

CREW REPORTED A LIGHTNING STRIKE ON CLIMBOUT FROM AVL EN ROUTE TO CLT. AIRCRAFT CONTINUED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE EMERGENCY LOCATOR TRANSMITTER (ELT) ANTENNA AND TWO (2) STATIC WICKS AND REPAIRED FUSELAGE DAMAGE. CHECKS WERE PERFORMED. ALL WORK WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: THROTTLE — OUT OF RIG (COCKPIT) · airframe 8,932 hrs · 9,252 cycles

CREW REPORTED THE RIGHT HAND THRUST LEVER AT FULL FORWARD DOES NOT PRODUCE POWER UP TO CLIMB BUGS. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RIGGED THE RIGHT HAND THROTTLE CONTROLS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE GROUND RAN AIRCRAFT, POWER ASSURANCE CHECKS WERE GOOD. AIRCRAFT PRODUCING POWER TO MAX ALLOWABLE LIMITS AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BLADES — DAMAGED (NR 2 ENGINE) · airframe 8,668 hrs · 8,963 cycles

CREW REPORTED A BIRD STRIKE TO THE RIGHT HAND ENGINE ON APPROACH. MAINTENANCE PERFORMED A VISUAL INSPECTION OF THE ENGINE AND FOUND REMAINS AND DAMAGE TO SEVERAL BLADES. MAINTENANCE REMOVED AND REPLACED DAMAGED BLADES IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE ALSO BORESCOPED THE ENGINE, COMPLETED POWER ASSURANCE AND VIBE CHECKS. ALL OPS CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 8,487 hrs · 8,780 cycles

CREW REPORTED WHEN THE APU WAS TURNED ON FOR LANDING, IT CAUSED THE CABIN TO FILL WITH SMOKE. CREW FOLLOWED THE QRH, TURNED OFF THE APU AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE OIL LEVEL TO BE OVERSERVICED. MAINTENANCE PROPERLY SERVICED THE OIL LEVEL IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: VALVE — FAILED (ANTI ICE) · airframe 6,105 hrs · 6,196 cycles

CREW REPORTED A LEFT HAND COWL ANTI-ICE MESSAGE IN FLIGHT. CREW PERFORMED AN UNSCHEDULED LANDING IN TRI WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE LEFT HAND COWL ANTI ICE VALVE. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — LOOSE (MLG) · airframe 6,077 hrs · 6,169 cycles

CREW REPORTED A GEAR DISAGREE WARNING MESSAGE ON APPROACH. CREW ABORTED THE APPROACH, FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND A LOOSE CONNECTOR TO THE MAIN LANDING GEAR SELECTOR VALVE. MAINTENANCE REINSTALLED THE CONNECTOR. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 5,689 hrs · 5,773 cycles

CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE RIGHT HAND HORIZONTAL STABILIZER TIP. MAINTENANCE REPAIRED ALL DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 5,068 hrs · 5,136 cycles

THE CREW REPORTED WHILE INFLIGHT WHEN SELECTING FLAPS 30 AND FLAPS 45 THE AIRCRAFT ROLLED RIGHT WING DOWN WITH AND WITHOUT THE AUTO PILOT ENGAGED. GEAR WAS UP FOR FLAPS 30 AND DOWN FOR FLAPS 45. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE FLAPS AND AILERONS. OPS CHECKS GOOD. FUNCTIONAL CHECK FLIGHT WAS COMPLETED-4 CYCLES OF FLAPS AND GEAR-NO ROLLING MOVEMENT NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WHEEL — VIBRATION (NLG) · airframe 4,616 hrs · 4,628 cycles

DURING TAKEOFF ROLL NOSE WHEEL VIBRATED SEVERELY ABOVE 90 KNOTS AND UP TO 45 SECONDS AFTER RETRACTION. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES. AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — OPEN (A/C DOOR) · airframe 3,311 hrs · 3,334 cycles

THE GROUND AIR CONNECTION DOOR WAS FOUND OPEN AFTER THE FLIGHT. MAINTENANCE INSPECTED AND FOUND THE DOOR HINGE CRACKED. THE DOOR WAS REMOVED AND REPLACED WITH A SERVICEABLE UNIT. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — NONE (UNKNOWN) · airframe 3,173 hrs · 3,210 cycles

THE CREW REPORTED ENCOUNTERING SEVERE TURBULENCE DURING DESCENT BETWEEN FL230 AND FL210. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE PERFORMED AN EXTREME TURBULENCE / MANEUVER INSPECTION IAW CRJ200 AMM 05-51-03-210-801. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — CRACKED (LT WINGLET) · airframe 2,636 hrs · 2,644 cycles

DURING THE INTERMEDIATE INSPECTION THE CREW DISCOVERED A CRACK AND DELAMINATION DAMAGE ON THE LEFT WINGLET TRAILING EDGE FAIRING. AFTER INSPECTION THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE PERFORMED A TEMPORARY REPAIR IAW BOMBARDIER REO 601R-57-31-668. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 1,712 hrs · 1,723 cycles

AFTER LANDING CREW REPORTED THAT ACRFT HAD TAKEN A LIGHTNING STRIKE. MX PERFORMED AN ENROUTE LIGHTNING STRIKE INSP IAW CRJ 200 AMM. ENTRY POINT FOUND ON LT AOA TRANSDUCER VANE, & EXIT POINT LOCATED AT RT LOWER WING TIP. NO OTHER DAMAGE NOTED. ACRFT RELEASED FOR SERVICE & SCHEDULED FOR A DETAILED LIGHTNING STRIKE INSP AFTER LAST FLT. PSA MX PERFORMED DETAILED LIGHTNING STRIKE INSP IAW CRJ 200 AMM.

Part: WARNING LIGHT — ILLUMINATED (EMERGENCY EXIT) · airframe 53 hrs · 54 cycles

DURING DESCENT, THE CREW RECEIVED A LEFT HAND EMERGENCY EXIT DOOR AMBER CAS MESSAGE WHICH EXTINGUISHED AT 8,000 FEET. MAINTENANCE THEN MEL'D THE EXIT DOOR IN ACCORDANCE WITH 52-70-03 CODE-C.