N251PS

Part: CONTROL LEVER — FAILED (TE FLAPS) · airframe 33,919 hrs · 33,727 cycles

DURING APPROACH THE CREW RECEIVED A FLAPS FAIL MESSAGE. THE AIRCRAFT LANDED WITHOUT FURTHUR INCIDENT. MAINTENANCE REPLACED THE FLAP CONTROL LEVER AND THE FLAPS OPERATIONAL CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSERS) · airframe 31,711 hrs · 31,587 cycles

DURING CLIMB OUT, CREW RECEIVED A RT REVERSER UNLOCK" MESSAGE AND RETURN TO DEPARTURE.

Part: WARNING MESSAGE — ILLUMINATED (THRUST REVERSER) · airframe 31,571 hrs · 31,454 cycles

MADE AN EMERGENCY LANDING DUE TO THE RT REVERSER UNLOCKED MESSAGE, FOLLOWED BY REPEATING AMBER MESSAGES AND AIRCRAFT BUFFETING. N1 FAN GAUGE WAS FLICKERING AND EVENTUALLY STAYED ON. CREW FOLLOWED QRH AND SHUTDOWN THE RT ENGINE AND LANDED WITHOUT INCIDENT,

Part: DETECTOR — FAULTED (FLOW) · airframe 31,549 hrs · 31,430 cycles

THE CREW RECEIVED A DISPLAY COOL CAUTION MESSAGE IN FLIGHT AT APPROXIMATELY FL220 AT 260 KNOTS. THE CREW RETURNED TO THE FIELD. MAINTENANCE REPLACED THE DISPLAY COOLING LOW FLOW DETECTOR AND EVERTHING OPS CHECKED GOOD.

Part: STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 30,728 hrs · 30,608 cycles

BS 559 LEFT FLOOR STRAP AT LBL 42 CORRODED. REMOVED AND REPLACED THE STRAP IAW SRM.

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 30,728 hrs · 30,608 cycles

FRAME CORRODED AT BS 333 AT STRINGER 27 ON FWD AND AFT SIDES. REMOVED AND REPLACED FRAME SECTOR.

Part: DUCT — DAMAGED (RT A/C PACK) · airframe 30,438 hrs · 30,333 cycles

AIRCRAFT WOULD NOT PRESSURIZE DURING CLIMB. CABIN TEMP CONTROL SYSTEM AUTO MODE INOPERABLE. REMOVED AND REPLACED THE RIGHT PACK DISCHARGE DUCT.

Part: UNKNOWN — ABNORMAL (FLT CONTROLS) · airframe 30,348 hrs · 30,257 cycles

AIRCRAFT ROLLED RIGHT UN-COMMANDED, AFTER AUTOPILOT DISCONNECTED. AILERONS OPS CHECKED NORMAL, FLAPS OPS CHECKED NORMAL, GENERAL VISUAL INSPECTION OF FLAPS LEADING EDGES WITH NO DEFECTS NOTED. PERFORMED DETAILED GENERAL VISUAL INSPECTION OF ALL FLIGHT CONTROLS WITH HYDRAULICS PRESSURIZED. NO DEFECTS NOTED.

Part: FILTER — UNKNOWN (RT A/C PACK) · airframe 29,985 hrs · 29,920 cycles

RIGHT PACK STATUS MESSAGE AT FL240 DURING CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT PRSOV SUPPLY INLET FILTER AND PERFORMED CHECKS IAW AMM. OPS CHECKED GOOD, THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — UNKNOWN (EXTERIOR) · airframe 27,664 hrs · 27,639 cycles

CREW REPORTED RT EMERGENCY EXIT LIGHT AFT OF SERVICE DOOR ON EXTERIOR OF ACFT INOPERATIVE. MAINTENANCE PERFORMED OPS CHECK ON RT EXTERNAL EMERGENCY FORWARD LIGHT IAW AMM. OPS CHECK GOOD. ACFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,632 hrs · 27,608 cycles

CREW REPORTED RT OVERWING FWD EMERGENCY LIGHT INOPERATIVE. R & R EXTERIOR EMERGENCY LIGHT, PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 27,356 hrs · 27,336 cycles

CREW REPORTED EMERGENCY LIGHT STRIP NOT WORKING. MAINTENANCE INSPECTED, RECONNECTED WIRE TO CONNECTOR FOR AFT EMERGENCY FLOOR LEVEL LIGHTING AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: LINE — CHAFED (HYDRAULIC SYSTEM) · airframe 27,171 hrs · 27,155 cycles

CREW REPORTED THE NR 1 HYDRAULIC SYS HAD A LOW PRESSURE MESSAGE IN FLIGHT. DIVERTED AND LANDED WITHOUT INCIDENT. TROUBLESHOT THE NR 1 HYD SYS, INSPECTED AND FOUND HYDRAULIC PRESSURE LINE IN AFT EQUIPMENT BAY TO BE CHAFED. R & R THE HYDRAULIC LINE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: DUCT — LOOSE (LT PACK) · airframe 26,855 hrs · 26,856 cycles

INSPECTED APU, NO DEFECTS NOTED. NO EVIDENCE OF FIRE. FOUND LT PACK SUPPLY CONNECTOR LOOSE AND DUCT TEMP SENSOR CONNECTOR BONDING WIRE BROKEN. R & R 10TH STG BLEED AIR DUCT, OPS AND LEAK CHECKS GOOD.

Part: CUP — CORRODED (BS 349) · corrosion level 2 · airframe 26,802 hrs · 26,802 cycles

AFT PAX DOOR HANDRAIL CUP ON PAX DOOR SILL HAS FILIFORM CORROSION. R & R AFT PAX DOOR HANDRAIL CUP IAW SRM 51-42-06 AND 51-40-11, PN 601R31527-137.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 26,802 hrs · 26,802 cycles

FS 280 FLOORBEAM IS CRACKED JUST OTBD OF RBL 9.00. CRACK IS APPROXIMATELY 2.00" LONG. REPAIRED IAW REO 601R-53-11-926 AND STANDARD REPAIR 601R-53-0110.

Part: CONNECTOR — FAILED (EMERGENCY LIGHTS) · airframe 25,847 hrs · 25,846 cycles

CREW REPORTED EMERGENCY LIGHTS INOPERATIVE FROM EXIT ROW BACK. MAINTENANCE TROUBLESHOT, R & R THE LIGHT CONNECTOR AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,847 hrs · 25,846 cycles

CREW REPORTED EMERGENCY LIGHTS INOPERATIVE FROM EXIT ROW BACK. MAINTENANCE TROUBLESHOT, R & R EMERGENCY LIGHT BATTERY AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BPSU — FAILED (ZONE 500) · airframe 25,013 hrs · 24,998 cycles

CREW REPORTED FLAPS FAILED ON TAKEOFF. ACFT RETURNED TO AIRPORT LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LT BRAKE POSITION SENSOR UNIT (BPSU). OPS CHECKS WERE ACCOMPLISHED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: BPSU — FAILED (LT BRAKE) · airframe 25,009 hrs · 24,993 cycles

CREW REPORTED FLAPS FAILED ON EXTENSION. MAINTENANCE TROUBLESHOT, R & R LT BRAKE POSITION SENSOR UNIT (BPSU). OPS CHECKS WERE ACCOMPLISHED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (RT WING) · airframe 24,079 hrs · 24,107 cycles

CREW REPORTED POSSIBLE LIGHTNING STRIKE TO RT WING L/E AND T/E. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION, R & R STABILIZER TOP CAP T/E PANEL AND STABILIZER LT LOWER VISOR PANEL DUE TO DAMAGE AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,174 hrs · 22,393 cycles

DURING SCHEDULED MAINTENANCE THE FS 621.0 PRESURE BULKHEAD WAS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 22,174 hrs · 22,393 cycles

DURING SCHEDULED MAINTENANCE THE FS 202.0 CRACKS WERE FOUND. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 21,968 hrs · 22,204 cycles

CREW REPORTED A KEROSENE SMELL WHEN PACKS ON. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED BOTH COALESCER BAGS PER AIRCRAFT MANUALS. OPERATION CHECKS WERE ACCOMPLISHED USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: FIRE LOOP — FAILED (RT PYLON) · airframe 21,968 hrs · 22,204 cycles

CREW REPORTED A RIGHT 14TH STAGE DUCT WARNING. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE RIGHT PYLON LOOP PER AIRCRAFT MANUALS. OPERATION CHECKS WERE ACCOMPLISHED USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: SWITCH — OUT OF POSITION (NLG) · airframe 21,628 hrs · 21,899 cycles

CREW REPORTED GEAR DISAGREE RED CAS MESSAGE AFTER TAKEOFF. MAIN GEAR INDICATION WAS WHITE BOX AND NOSE GEAR STAYED GREEN. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NOSE GEAR DOORS OPEN WITH SWITCH BETWEEN OPEN AND CLOSE POSITION. MAINTENANCE RETURNED SWITCH TO NORM / FLT POSITION AND PERFORMED GEAR SWING USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL LEVER — MALFUNCTIONED (COCKPIT) · airframe 21,292 hrs · 21,608 cycles

CREW REPORTED FLAPS FAIL AMBER CAS MESSAGE OCCURRED FROM SELECTION OF FLAPS 20 DEGREES TO 30 DEGREES ON APPROACH. CREW COMPLETED QRH (QUICK REFERENCE HANDBOOK) AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM PER FIM (FAULT ISOLATION MANUAL), REMOVED AND REPLACED FLAP CONTROL LEVER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG) · airframe 20,168 hrs · 20,598 cycles

CREW REPORTED GEAR DISAGREE MESSAGE (RIGHT MAIN) UPON GEAR RETRACTION. CREW RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, ADJUSTED UPLOCK PROXIMITY SENSOR AND PERFORMED CHECKS OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BPSU — FAILED (TE FLAP) · airframe 20,069 hrs · 20,514 cycles

CREW REPORTED THE FLAPS FAILED WHEN 8 DEGREES SELECTED. AIRCRAFT RETURNED TO AIRPORT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND PERFORMED AD 2009-06-12. THE LEFT BPSU WAS REMOVED AND REPLACED AND OPERATION CHECKS WERE PERFORMED USING AIRCAFT MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ECU — FAILED (TE FLAP) · airframe 20,067 hrs · 20,512 cycles

CREW REPORTED THE FLAPS FAILED AT 8 DEGREES. AIRCRAFT RETURNED TO AIRPORT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND PERFORMED AD 2009-06-12. THE FECU WAS REMOVED AND REPLACED AND OPERATION CHECKS WERE PERFORMED USING AIRCRAFT MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (FLAP SYSTEM) · airframe 18,818 hrs · 19,347 cycles

CREW REPORTED FLAPS FAIL CAUTION MESSAGE ON APPROACH. CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FECU (FLAP ELECTRONIC CONTROL UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CONNECTOR — DIRTY (APU) · airframe 18,277 hrs · 18,808 cycles

CREW REPORTED APU OIL PRESSURE CAUTION MESSAGE IN FLIGHT EN ROUTE FROM TYS TO PHL. CREW FOLLOWED QRH, DIVERTED TO TRI AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED APU, CLEANED APU OIL PRESSURE SWITCH CONNECTOR AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SWITCH — DEFECTIVE (APU) · airframe 18,277 hrs · 18,808 cycles

CREW REPORTED APU OIL PRESSURE CAUTION MESSAGE IN CRUISE FLIGHT AFTER DEPARTURE FROM PHL. CREW FOLLOWED QRH, RETURNED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED APU LOP (LOW OIL PRESSURE) SWITCH AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: RIB — CRACKED (LT WING) · airframe 17,543 hrs · 18,117 cycles

DURING SCHEDULED MAINTENANCE THE LEFT BATT RIB AT WS 53.60 WAS FOUND CRACKED. THE LEFT BAT RIB AT WS 53.60 WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 17,543 hrs · 18,117 cycles

DURING SCHEDULED MAINTENANCE A DENT BELOW THE CARGO DOOR WAS FOUND JUST AFT OF FS 605.0. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — BLOWN (LT MLG) · airframe 17,318 hrs · 17,892 cycles

CREW REPORTED UPON LANDING IN CLT THE LT INBOARD MAIN LANDING GEAR TIRE BLEW CAUSING DAMAGE TO THE UNDERSIDE OF THE LEFT FLAP AND HYDRAULIC LINES. AIRCRAFT WAS TOWED TO GATE. MAINTENANCE TROUBLESHOT, REPAIRED HYDRAULIC LINES, REPLACED LEFT MAIN TIRES, AND LEFT FLAP. WORK WAS DONE PER THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 16,749 hrs · 17,344 cycles

CREW REPORTED RIGHT PACK SHUT DOWN DURING CRUISE FLIGHT EN ROUTE FROM AVL TO CLT. LEFT PACK WAS ALREADY DEFERRED PER MEL. CREW LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AIRCRAFT, REMOVED AND REPLACED RIGHT TENTH STAGE BLEED AIR SHUTOFF VALVE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 16,291 hrs · 16,882 cycles

CREW REPORTED THE FIRST OFFICER’S FRONT WINDSHIELD CRACKED DURING DESCENT TO CLT. CREW LANDED IN CLT WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE FIRST OFFICER’S WINDSHIELD AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WHEEL — VIBRATION (NLG) · airframe 16,042 hrs · 16,641 cycles

ON DEPARTURE FROM CRW, CREW REPORTED A LOUD BANG AND BAD VIBRATION OF THE NOSE WHEEL ON TAKEOFF AND GEAR RETRACTION. CREW CONTINUED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE LEFT AND RIGHT WHEEL / TIRE ASSEMBLIES AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE. LT NLG WHEEL ASSY S/N: JUN04-5558 / RH NLG WHEEL ASSY S/N: NOV03-5246.

Part: CARBON SEAL — DEFECTIVE (RT ENGINE) · airframe 15,950 hrs · 16,544 cycles

CREW REPORTED MULTIPLE RIGHT ENGINE OIL PRESSURE MESSAGES ON DEPARTURE FROM MOB. CREW RETURNED TO MOB AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE AXIS-D CARBON SEAL (AT AIR TURBINE STARTER PAD) FOR THE RIGHT ENGINE ACCESSORY GEARBOX (AGB) AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (WINDOW) · airframe 15,850 hrs · 16,454 cycles

CREW REPORTED THE CAPTAIN’S WINDSHIELD CRACKED IN FLIGHT EN ROUTE FROM MOB TO CLT. CREW DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE LEFT WINDSHIELD AND THE LEFT WINDSHIELD TEMPERATURE CONTROLLER AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT) · airframe 14,726 hrs · 15,350 cycles

CREW REPORTED MULTIPLE SMALL CRACKS ON THE LOWER FORWARD CORNER OF THE LEFT WINDOW AFTER TAKEOFF FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE LEFT SIDE WINDOW AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,406 hrs · 15,033 cycles

AT CLT, CREW REPORTED EMERGENCY PATH ROW LIGHTING BY SEAT 1D NOT ILLUMINATING. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE FLOOR TRACK EMERGENCY LIGHT AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: COMPUTER — FAILED (NR 2) · airframe 12,220 hrs · 12,689 cycles

CREW REPORTED A FD 2 STATUS MSG AND RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INTERROGATED MDC AND FOUND FCC NR 22 DASHED OUT. MAINTENANCE REMOVED AND REPLACED FCC NR 2, PERFORMED OPS CHECK PER AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 11,466 hrs · 11,906 cycles

EMERGENCY FLOOR LIGHTS AT ROW 2 TO ROW 5 DID NOT WORK IN AGS. MAINTENANCE REMOVED AND REPLACED THE CABLE ASSEMBLY (102.0 IN. LONG) IAW THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE PERFORMED AND NO FURTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — FUMES (COCKPIT & CABIN) · airframe 11,300 hrs · 11,743 cycles

CREW REPORTED STRONG JET FUEL FUMES IN PHL ON FLT DECK/CABIN. INSPECTED RT ENGINE & APU COMPARTMENT / AVIONIC COMPARTMENT, NO LEAKS NOTED GROUND RAN RT ENGINE, NO FUEL FUMES NOTED. AIRCRAFT RELEASED FOR SERVICE.

Part: BLEED VALVE — MALFUNCTIONED (ENGINE) · airframe 11,032 hrs · 11,458 cycles

ON CLIMB THE CREW REPORTED THE 10TH STAGE BLEED AIR ISOLATION VALVE WOULD NOT CLOSE, DURING AFTER T/O CHECKS. THE CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE 10TH STAGE BLEED VALVE. NO OTHER DEFECTS WERE NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — OPEN (GROUND POWER) · airframe 10,590 hrs · 10,955 cycles

CREW ELECTED TO RETURN TO DEPARTURE WITH A SUSPTECTED GROUND POWER DOOR OPEN. ACFT LANDED WITHOUT INCIDENT. MAINT REMOVED AND REPLACED THE AFT LATCH SPRING ON THE GROUND POWER DOOR. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE. (K)

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS)

CREW REPORTED THE EMERGENCY LIGHTS FROM ROW 2 TO ROW 5 DID NOT WORK. MAINT REMOVED AND REPLACED CABLE AT ROW 6. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE. (K)

Part: WINDOW — FAILED (COCKPIT) · airframe 10,305 hrs · 10,642 cycles

CREW REPORTED A WINDOW HEAT CAS MESSAGE AND ELECTED TO DIVERT TO CLT. ACFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT AND CHANGED RT WINDSHIELD. NO DEFECTS WERE NOTED AND ACFT RETURNED TO SERVICE. (S)

Part: ELBOW — FAILED (HYD SYSTEM) · airframe 9,659 hrs · 9,951 cycles

CREW REPORTED A NR 3 HYDRAULIC LOW PRESSURE IN FLIGHT. CREW ELECTED TO DIVERT TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BULKHEAD ELBOW IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE ALSO PROPERLY SERVICED THE NR 3 HYDRAULIC SYSTEM. NO FURTHER LEAKS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TRIM SWITCH — STICKING (COCKPIT) · airframe 8,057 hrs · 8,244 cycles

CREW REPORTED THE CAPTAINS TRIM SWITCH STICKING AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLEANED THE TRIM SWITCH. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OIL SYSTEM — LOW (NR 2 IDG) · airframe 6,831 hrs · 6,933 cycles

CREW REPORTED A NR 2 IDG CAS MESSAGE ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE IDG NR 2 OIL LEVEL LOW. MAINTENANCE PROPERLY SERVICED THE OIL LEVEL IAW MM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ANTENNA — FAILED (RADAR) · airframe 5,819 hrs · 5,845 cycles

CREW REPORTED A LIGHTNING STRIKE ON DESCENT. MAINTENANCE INSPECTED AIRCRAFT. RADAR ANTENNA WAS REPLACED. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 5,161 hrs · 5,144 cycles

CREW REPORTED INTERMITTENT PASSENGER DOOR WARNING AND SERVICE DOOR CAUTION MESSAGE DURING DESCENT. INSPECTIONS OF THE PASSENGER AND SERVICE DOOR WIRING HARNESSES FROM FUSELAGE TO DOORS WERE PERFORMED. NO DEFECTS NOTED. OPERATIONAL CHECKS OF THE INDICATION SYSTEMS WERE PERFORMED. OPERATIONAL CHECKS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (PAX DOOR) · airframe 3,578 hrs · 3,516 cycles

DURING CRUISE THE PASSENGER DOOR WARNING MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING AT DESTINATION. MAINTENANCE INSPECTED THE PASSENGER DOOR LATCHING AND WARNING SYSTEMS. NO DISCREPANCIES WERE FOUND AND THE PROBLEM COULD NOT BE DUPLICATED. THE SYSTEMS OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — UNDAMAGED (LT AILERON) · airframe 3,346 hrs · 3,304 cycles

DURING AN FAA RAMP CHECK, THE INSPECTOR DISCOVERED EVIDENCE OF LIGHTNING STRIKE DAMAGE ON TOP OF THE LT AILERON. THE AIRCRAFT WAS FERRIED TO CAK. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION AND FOUND NO LIGHTNING DAMAGE TO THE AIRCRAFT. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRIKER — DAMAGED (PAX DOOR SEAL) · airframe 3,346 hrs · 3,304 cycles

DURING AN FAA RAMP CHECK, THE INSPECTOR DISCOVERED DAMAGE TO THE PASSENGER DOOR SEAL STRIKER. THE AIRCRAFT WAS FERRIED TO CAK. MAINTENANCE PERFORMED A TYPE II REPAIR IAW REO 601R-53-22-033. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — UNKNOWN · airframe 2,296 hrs · 2,248 cycles

THE CREW ABORTED THE TAKEOFF AFTER RECEIVING A CONFIG TRIM VOICE WARNING AT 80 KTS. AFTER CONFERRING WITH MAINTENANCE CONTROL, THE CREW PUT THE AIRCRAFT INTO PROPER TAKEOFF CONFIGURATION. THE CONFIGURATION WARNING SYSTEM OPS CHECKED GOOD. THE AIRCRAFT THEN DEPARTED WITH NO INCIDENT.

Part: TIRE — DAMAGED (RT MLG) · airframe 2,247 hrs · 2,200 cycles

EN ROUTE TO DAY THE CREW WAS NOTIFIED OF POSSIBLE NOSE WHEEL DAMAGE DUE TO A MISSING TOW BAR SHEAR PIN IN PHL. THE CREW CONTINUED TO DAY AND MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE RT NLG TIRE CHINE DAMAGED. THE WHEEL & TIRE ASSEMBLY WAS REMOVED & REPLACED IAW CRJ 200 AMM 32-42-01-000-801 AND 32-42-01-400-801. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 1,401 hrs · 1,367 cycles

DURING APPROACH TO PIT, WHEN THE FLIGHT SPOILER HANDLE WAS MOVED TO DEPLOY, A FLIGHT SPOILER FAULT WHITE STATUS MESSAGE WAS DISPLAYED. THE PILOT RETURNED THE FLIGHT SPOILER HANDLE TO THE NORMAL POSITION AND MADE AN UNEVENTFUL LANDING. NO INCORRECT FLIGHT SPOILER POSITION OR HANDLING ABNORMALITIES WERE REPORTED BY THE CREW. AFTER TROUBLESHOOTING THE SYSTEM PSA MAINTENANCE REMOVED & REPLACE THE LT INBOARD & OUTBOARD FLIGHT SPOILER POWER CONTROL UNITS IAW CRJ 200 AMM 27-62-01-000-801/400-801. RIGGING AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: ADC — FAILED (LEFT) · airframe 63 hrs · 62 cycles

DURING TAKEOFF, THE CREW RECEIVED A CONFIG FLAP RED WARNING MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE AIR DATA COMPUTER IN ACCORDANCE WITH 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 63 hrs · 62 cycles

DURING TAKEOFF, THE CREW RECEIVED A CONFIG FLAP RED WARNING MESSAGE AND ABORTED TAKEOFF. THE CREW RESET THE CONFIG AND THE MESSAGE CLEARED. FLIGHT 2377 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT.