N249PS

Part: DUCT — LEAKING (LEFT PYLON) · airframe 33,623 hrs · 33,692 cycles

DURING CLIMB, THROUGH FLIGHT LEVEL 270, THE CREW RECEIVED A LEFT WING ANTI-ICE MESSAGE AND COMPLIED WITH THE QUICK REFERENCE HAND BOOK AND LEVELED OFF AT LIGHT LEVEL 290.. THE MESSAGE EXTINGUISHED AND THEN RETURNED A FEW MINUTES LATER AS A RED 14TH DUCT MESSAGE THAT WOULD NOT EXTINGUISH. THE CREW DECLARED AN EMERGENCY AND DIVERTED. THE AIRCRAFT WAS LATER FERRIED AND THE LEFT PYLON DUCT WAS REPLACED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 31,218 hrs · 31,402 cycles

FUSELAGE FRAME SEGMENT FS 333 IS CRACKED BETWEEN STR 1L AND STR 0. REPLACED FRAME.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 31,218 hrs · 31,402 cycles

LEFT FLOOR SUPPORT IS CORRODED BETWEEN BS 574 AND 621. REPLACED THE FLOOR SUPPORT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,218 hrs · 3,142 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 18.00 WL 75 APPROX 1" IN LENGTH 100% FSH. REPAIRED CRACK AT FS 621 LBL 18 IAW REO 601R-53-61-6049.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 31,218 hrs · 31,402 cycles

FS 621 TO FS 625 OBLIQUE ANGLE AT STR 14L IS CRACKED. REPLACE OBLIQUE ANGLE.

Part: FLOOR SUPPORT — CORRODED (BS 423-529) · corrosion level 2 · airframe 31,218 hrs · 31,402 cycles

RIGHT PRESSURE FLOOR SUPPORT HAS CORROSION BETWEEN BS 423 - 529. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-41-666, REV C.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,218 hrs · 31,402 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 9.5 WL 74 APPROX 3" IN LENGTH 100% FSH. REPAIRED CRACK AT LBL 9 FS 621 IAW REO 601R-53-61-6049.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,218 hrs · 31,402 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50 WL 130 APPROX 1 INCH IN LENGTH 100% FSH. REPAIR CRACK AT LBL 27.50 AND WL 130 PER GREO 601R-53-61-1541 REVISION F.

Part: SKIN — CRACKED (FUSELAGE) · airframe 31,218 hrs · 31,402 cycles

NLG WHEEL WELL CUT OUT IS CRACKED AT AFT RT CORNER. REPAIR COMPLIED WITH IAW ATTACHED EA 43-2017-065.

Part: FLOOR SUPPORT — CORRODED (BS 499) · corrosion level 2 · airframe 31,218 hrs · 31,402 cycles

LEFT PRESSURE FLOOR SUPPORT HAS CORROSION AT BS 499. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-41-666.

Part: SEAL — DETACHED (PASSENGER DOOR) · airframe 30,572 hrs · 30,762 cycles

PASSENGER DOOR SQUEELS. REMOVED AND REPLACED THE PASSENGER DOOR SEAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (PAX DOOR) · airframe 29,737 hrs · 29,968 cycles

PASSENGER DOOR WARNING AND OVERBOARD COOL CAUTION AND STATUS. PERFORMED CHECKS IAW AMM, OPS CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — DETACHED (CABIN) · airframe 28,870 hrs · 29,106 cycles

EMERGENCY LIGHTS AT IFD IS COMING UP OR LOOSE, MAINTENANCE INSPECTED, REPLACED EMERGENCY FLOOR TRACK LIGHT TRANSISITON CABLE, RESECURED LIGHT COVER AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: INTERCOSTAL — CORRODED (BS 364) · corrosion level 2 · airframe 27,575 hrs · 27,807 cycles

INTERCOSTAL CORRODE,FILIFORM, AT STR 27 FS 364 FWD OF MAIN AVIONICS DOOR CUTOUT. REPAIRED INTERCOSTAL CORROSION AT STGR 27 FS 364 JUST FWD OF THE MAIN AVIONICS DOOR CUT OUT IAWSRM 53-00-00 AND 53-21-06.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,903 hrs · 27,123 cycles

CREW REPORTED FIRST FOOT OF FLOOR EMERGENCY LIGHTING NEEDED INSPECTION. MAINTENANCE INSPECTED, R & R NR 1 SECTION OF FLOOR TRACK EMERGENCY LIGHT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BLADES — DAMAGED (LT ENGINE) · airframe 26,663 hrs · 26,889 cycles

CREW REPORTED LOUD VIBRATION ON TAKEOFF AND LT FAN VIBRATION OF 1.6. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH BIRD STRIKE INSPECTION AND FOUND DAMAGE TO LT ENGINE FAN BLADES FROM BIRD STRIKE. NO OTHER DEFECTS NOTED. MAINTENANCE R & R DAMAGED FAN BLADES ON LT ENGINE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WARNING MESSAGE — ACTIVATED (THRUST REVERSER) · airframe 26,432 hrs · 26,674 cycles

CREW REPORTED RIGHT THRUST REVERSER UNLOCKED MESSAGE APPEARED AND EXTINGUISHED IN FLIGHT. CREW DIVERTED AND LANDED SAFELY.

Part: CIRCUIT CARD — FAILED (FCC) · airframe 25,827 hrs · 26,072 cycles

CREW REPORTED YAW DAMPER-1 FAIL FD & AUTO PILOT FAIL IN FLT. INTERROGATED MDC AND FCC DIAGNOSTIC, FOUND FCC 1 FAILING INTERMITTENTLY, R & R NR 1 FCC CARD IAW AMM 22-12-14-00-400-801, OPS CHECK GOOD. ALSO, R & R YAW DAMPER NR 1 PUSH BUTTON IAW CMM 22-22-04 FOR INTERMITTENTLY BEING STUCK.

Part: HANDLE — POPPED (CARGO DOOR) · airframe 25,718 hrs · 25,961 cycles

CREW REPORTED CARGO DOOR MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. AFTER LANDING, DOOR HANDLE WAS REPORTED AS POPPED OUT. MAINTENANCE CLEANED AND INSPECTED CARGO DOOR LATCH AND PERFORMED CHECKS IAW AMM. NO DEFECTS NOTED. ACFT RELEASED FOR SERVICE.

Part: ACTUATOR — MALFUNCTIONED (YAW DAMPER) · airframe 24,985 hrs · 25,205 cycles

CREW REPORTED A LIGHT TO OCCASIONALLY MODERATE DUTCH ROLL IN CLIMB AND CRUISE WITH AUTOPILOT ENGAGED AND DISENGAGED. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R NR 2 YAW DAMPER LINEAR ACTUATOR, R & R FLIGHT CONTROL PANEL (FCP) AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BLADES — DAMAGED (RT ENGINE) · airframe 24,927 hrs · 25,150 cycles

CREW REPORTED BIRD STRIKE AFTER TAKEOFF AND DAMAGED FAN BLADES ON RT ENGINE. CREW DECLARED EMERGENCY, RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED DEBRIS FROM RT ENGINE INLET, R & R 4 FAN BLADES AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CHANNEL — DAMAGED (BS 522-529) · airframe 24,700 hrs · 24,920 cycles

DURING SCHEDULED MAINTENANCE THE RT MLG SUPPORT CHANNEL BETWEEN BS 522-529 FOUND DAMAGED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: COMPUTER — FAILED (ATT & HDG REF SY) · airframe 24,173 hrs · 24,426 cycles

CREW REPORTED EFIS COMP MON MESSAGE WITH F/O ATTITUDE INDICATION ERRATIC AND NO FLIGHT DIRECTOR OR AUTOPILOT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R ATTITUDE AND HEADING COMPUTER (AHC) NR 2 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: DRIVE UNIT — FAILED (THRUST REVERSER) · airframe 24,136 hrs · 24,389 cycles

CREW REPORTED RT THRUST REVERSER MESSAGE IN FLIGHT. CREW RAN QRH, DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT THRUST REVERSER POWER DRIVE UNIT (PDU), AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: O-RING — LEAKING (APU FUEL) · airframe 23,672 hrs · 23,941 cycles

CREW REPORTED A FUEL ODOR WHEN PACKS WERE ON. MAINTENANCE TROUBLESHOT, R & R APU FUEL LINE O-RING AND LEAK CHECKED AREA USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 23,301 hrs · 23,601 cycles

CAPTAIN’S WINDSHIELD CRACKED AT 30,000 FT. LT WINDSHIELD HEAT CAS MESSAGE ALSO REPORTED. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MX INSPECTED, R & R CAPTAIN’S WINDSHIELD AND LT WINDSHIELD TEMP CONTROLLER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SKIN — BURNED (TAILCONE) · airframe 23,036 hrs · 23,349 cycles

CREW REPORTED LIGHTNING STRIKE ON LT NOSE OF ACFT. MX PERFORMED LIGHTNING STRIKE INSPECTION AND FOUND DAMAGE TO T/E OF VHF 2 ANTENNA, BURN MARKS ON TAIL CONE AND BURN MARK ON HORIZ STABILIZER TIP LOWER SIDE. MX R & R VHF NR 2 ANTENNA, R & R RT HORIZ STABILIZER TIP, BLENDED BURN MARKS ON TAIL CONE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: DETECTOR — FAILED (TE FLAPS) · airframe 22,859 hrs · 23,198 cycles

CREW REPORTED FLAP FAILED AT 8 DEGREES IN FLIGHT. DIVERTED AND LANDED WITHOUT INCIDENT. MX TROUBLESHOT FLAP SYS, R & R SKEW DETECTION UNIT (SDU) AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: MODULATING VALVE — DIRTY (ANTI-ICE SYS) · airframe 21,891 hrs · 22,314 cycles

CREW REPORTED LEFT WING ANTI-ICE CAUTION MESSAGE AFTER TAKEOFF POWER ADDED. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED AND DEFERRED WING ANTI-ICE NORMAL MODE PER MEL. ON NEXT FLIGHT, LEFT WING ANTI-ICE AMBER CAUTION MESSAGE WOULD NOT EXTINGUISH IN STANDBY MODE BEFORE TAKEOFF. CREW RETURNED TO GATE. MAINTENANCE REMOVED AND INSPECTED LEFT WING ANTI-ICE SHUTOFF / MODULATING VALVE, CLEANED VALVE AND PRSOV (PRESSURE REGULATING / SHUTOFF VALVE) FILTER, RE-INSTALLED VALVE, PERFORMED CHECKS AND CLEARED DEFERRAL USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: LOOP — DEFECTIVE (RT PYLON) · airframe 21,459 hrs · 21,939 cycles

CREW REPORTED RIGHT 14TH STAGE DUCT WARNING MESSAGE WHILE ON APPROACH. CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT ENGINE PYLON LOOP AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 21,089 hrs · 21,608 cycles

CREW REPORTED CRACK FORMED ON RIGHT WINDSHIELD WHILE CLIMBING THROUGH FL200. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED RIGHT WINDSHIELD AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 20,532 hrs · 21,133 cycles

CREW REPORTED LANDING GEAR DISAGREE CAS MESSAGE DURING GEAR EXTENSION WHILE ON APPROACH. CREW LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE RESET MANUAL LANDING GEAR RELEASE HANDLE, INSPECTED PROXIMITY SENSORS FOR SECURITY, INTERROGATED PSEU (PROXIMITY SENSOR ELECTRONIC UNIT) AND PERFORMED EXTENSION / RETRACTION OF LANDING GEAR USING AIRCRAFT MAINTENANCE MANUALS. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE.

Part: STATIC WICK — DAMAGED · airframe 20,373 hrs · 20,999 cycles

CREW REPORTED LIGHTNING STRIKE IN NOSE AREA. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND REMOVED AND REPLACED THREE (3) BURNED STATIC WICKS, ONE EACH ON RIGHT OUTBOARD HORIZONTAL, RIGHT LOWER WINGLET AND LOWER TAIL CONE. A BURNED SCREW ON TOP OF HORIZONTAL STAB TIP ON RIGHT SIDE WAS REMOVED AND REPLACED. OTHER MINOR ALLOWABLE RIVET AND BURN DAMAGE PER SRM WAS TREATED. MAINTENANCE PERFORMED CHECKS. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: HYDRAULIC LINE — SHEARED (HYDRAULIC SYS) · airframe 20,364 hrs · 20,989 cycles

CREW REPORTED HYD 1 LOW PRESS AMBER CAUTION MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND HYDRAULIC LINE SHEARED. MAINTENANCE REMOVED AND REPLACED HYDRAULIC LINE AND LEFT EDP (ENGINE DRIVEN PUMP) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,309 hrs · 18,999 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: NUT PLATE — BROKEN (FUSELAGE) · airframe 18,309 hrs · 18,999 cycles

DURING SCHEDULED MAINTENANCE FOUND PANEL 195BB NUT PLATE BROKEN. PANEL 195BB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 18,309 hrs · 18,999 cycles

DURING SCHEDULED MAINTENANCE A DENT WAS FOUND ON FUSELAGE SKIN AT FS 654.30. THE SKIN AT FS 654.30 WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROBE — OBSTRUCTED (PITOT/STATIC SYS) · airframe 18,026 hrs · 18,735 cycles

CREW REPORTED REJECTED TAKEOFF AT PHL DUE TO CAPTAIN’S AIRSPEED INDICATOR BEING STAGNANT. MAINTENANCE INSPECTED AIRCRAFT, FOUND PITOT PROBE PARTIALLY OBSTRUCTED WITH BIRD REMAINS, PERFORMED BIRD STRIKE INSPECTION, REMOVED AND REPLACED LEFT PITOT PROBE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SKIN — DENTED (RT WING) · airframe 17,518 hrs · 18,239 cycles

AT ROA, CREW REPORTED BIRD STRIKE ON LEADING EDGE OF RIGHT WING. MAINTENANCE INSPECTED, REMOVED AND REPLACED RIGHT OUTBOARD LEADING EDGE ASSEMBLY AND PICCOLO DUCT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CIRCUIT CARD — FAILED (COCKPIT) · airframe 17,148 hrs · 17,880 cycles

CREW REPORTED LOST FMS, THEN LOST NAV 1 IN FLIGHT EN ROUTE FROM DCA TO TYS. CREW DIVERTED TO IAD AND LANDED WITHOUT INCIDENT. USING AIRCRAFT MAINTENANCE MANUALS, MAINTENANCE PERFORMED CHECKS OF NR 1 NAV SYSTEM. NO DEFECTS NOTED. MAINTENANCE DEFERRED FMS PER MEL. SDR WILL BE REVISED WHEN DEFERRAL IS CLEARED. MAINTENANCE SUBSEQUENTLY CLEARED DEFERRAL BY REMOVAL AND REPLACEMENT OF FMC (FLIGHT MANAGEMENT COMPUTER) NR 1 AND PERFORMANCE OF CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,578 hrs · 15,374 cycles

DURING MAINTENANCE A CRACK WAS FOUND ON THE PRESSURE BULKHEAD FS 559. MAINTENANCE REPAIRED AIRCRAFT USING AIRCRAFT MANUALS AND RELEASED AIRCRAFT FOR SERVICE.

Part: SHUTOFF VALVE — MALFUNCTIONED (AC BAY) · airframe 14,033 hrs · 14,791 cycles

CREW REPORTED A BURNING SMELL JUST AFTER BLEEDS WERE SWITCHED FROM APU TO ENGINES AFTER TAKEOFF FROM CLT EN ROUTE TO OAJ. THE LEFT AIR CONDITIONING PACK WAS FOUND TO BE CAUSING THE SMELL. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE LEFT PRESSURE REGULATING SHUTOFF VALVE (PRSOV) FILTER AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: COMPUTER — MALFUNCTIONED (NR 1 & NR 2) · airframe 13,593 hrs · 14,294 cycles

CREW REPORTED AN EFIS COMP MON MESSAGE AT ROTATION ON TAKEOFF FROM IND. COMPASSES BECAME ERRATIC. AIRCRAFT RETURNED TO IND AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND REMOVED AND RE-INSTALLED THE NR 1 AND NR 2 ATTITUDE HEADING COMPUTERS (AHC) USING THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. RESULTS OF CHECKS WERE NORMAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 13,357 hrs · 14,027 cycles

DURING INSPECTION TWO DENTS WERE FOUND AT FS 605 BETWEEN STRINGER 24L AND 26L. MAINTENANCE REPAIRED THE DENTS AND RELEASED THE AIRCRAFT FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 13,357 hrs · 14,027 cycles

DURING INSPECTION A CRACK WAS DISCOVERED ON THE REAR PRESSURE BULKHEAD AROUND THE LINTEL ATTACHMENT. MAINTENANCE REPAIRED THE CRACK AND RELEASED THE AIRCRAFT FOR SERVICE.

Part: WIRE — LOOSE (OVERHEAT SYS) · airframe 11,398 hrs · 11,937 cycles

CREW REPORTED A WING OVHT RED CAS MSG IN FLIGHT. CREW CONSULTED QRH, ELECTED TO RETURN TO CLT WITHOUT INCIDENT. MAINTENANCE INSP WING ALL OFF/STBY/NORM SW AND FOUND WIRES LOOSE ON SWITCH. REPAIRED WIRES AND OPERATIONAL CHECKS WERE PERFORMED PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: A/C PACK — SMOKE (LEFT) · airframe 12,287 hrs · 12,728 cycles

CREW REPORTED ODOR OF SMOKE IN COCKPIT & PASSENGER COMPARTMENT AND LT PACK, PACK HIGH TEMP CAS MSG ON GROUND. AIRCRAFT RETURNED TO GATE IN XNA. MAINTENANCE INSPECTED APU & PACKS NO VISUAL DEFECTS OR LEAKS NOTED PER THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE DEFERRED THE LT PACK SYSTEM AND AIRCRAFT RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 11,227 hrs · 11,756 cycles

EMERGENCY LIGHTS AT ROW 2 TO ROW 6 DID NOT WORK AT CLT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY PACK NR 2 PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: MODULE — FAILED (COCKPIT) · airframe 10,311 hrs · 10,769 cycles

CREW REPORTED ON TAKE OFF ACFT PULLED HARD LT NEEDED FULL RT RUDDER AND TILLER TO MAINTAIN RUNWAY HEADING. TAKE OFF ABORTED AT UNKNOWN SPEED. ACFT RETURNED TO GATE WITHOUT INCIDENT. MX INSPECTED ACFT AND R&R THE HAND CONTROL MODULE. NO OTHER DEFECTS WERE NOTED. ACFT RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED (ELEVATOR) · airframe 10,226 hrs · 10,672 cycles

CREW REPORTED A POSSIBLE LIGHTNING STRIKE AFTER LANDING AT XNA. MX INSPECTED AND REPAIRED DAMAGE TO THE ELEVATOR. NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 10,210 hrs · 10,656 cycles

CREW REPORTED A FLAPS FAIL AT 45 DEG. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX INSPECTED ACFT AND R&R LT OUTBOARD ACTUATOR. CHECKS WERE MADE AND NO OTHER DEFECTS WERE NOTED. ACFT WAS RELEASED FOR SERVICE.

Part: STATIC WICK — DAMAGED (HORIZ STAB) · airframe 7,897 hrs · 8,156 cycles

CREW REPORTED A LIGHTNING STRIKE ON LEFT SIDE OF NOSE. MAINTENANCE PERFORMED A VISUAL EN ROUTE INSPECTION FOR LIGHTNING STRIKE DAMAGE. MAINTENANCE PERFORMED A DETAILED LIGHTNING STRIKE INSPECTION AND FOUND DAMAGE TO THE LEFT HAND HORIZONTAL STAB TIP AND STATIC WICK AS WELL AS A DAMAGED RIVET ON TOP OF THE LEFT HAND ELEVATOR. MAINTENANCE REPLACED DAMAGED RIVET, STATIC WICK AND TEMP REPAIRED THE HORIZONTAL STAB TIP AS PER THE REO 10855 FROM BOMBARDIER. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ECU — FAILED (T/E FLAP) · airframe 7,537 hrs · 7,751 cycles

CREW REPORTED ON APPROACH A FLAPS FAIL CAS MESSAGE AT 45 DEGREES. MAINTENANCE INSPECTED AND FOUND FECU BITE CHECK NOT WORKING AND RIGHT HAND BPSU RIG INDICATION ERRATIC. MAINTENANCE REMOVED AND REPLACED THE FECU IN ACCORDANCE WITH THE MAINTENANCE MANUAL 27-51-05-000/400-801. OPERATIONAL CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 7,537 hrs · 7,751 cycles

CREW REPORTED ON APPROACH A FLAPS FAIL CAS MESSAGE AT 20 DEGREES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED A RESET OF THE SDU. MAINTENANCE INSPECTED FLAP LEFT HAND AND RIGHT HAND, NO SKEW NOTED IN ACCORDANCE WITH THE MAINTENANCE MANUAL 27-51-15. MAINTENANCE PERFORMED OPS CHECK OF THE FLAPS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 27-54-00-866-801 AND 27-54-00-866-802. OPERATIONAL CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BPSU — FAILED (RT TE FLAP) · airframe 6,867 hrs · 7,004 cycles

CREW REPORTED A FLAPS FAIL CAS MESSAGE ON DESCENT. CREW LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE BRAKE AND POSITION SENSOR UNIT IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: QUICK DISCONNECT — DISCONNECTED (HYD SYSTEM) · airframe 5,322 hrs · 5,240 cycles

CREW REPORTED THAT ON A NORMAL LANDING EXCESSIVE BRAKING WAS REQUIRED AND THE ANTI SKID CYCLED SEVERAL TIMES. MAINTENANCE INSPECTED THE RIGHT I/B BRAKE AND FOUND THE -QUICK DICONNECT- UNATTACHED TO THE BRAKE. THE -QUICK DISCONNECT- WAS REATTACHED. OPERATIONAL CHECKS WERE PERFORMED. OPS CHECKS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 3,312 hrs · 3,333 cycles

THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON APPROACH WITH FLAPS 20 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE INSPECTED THE FLAP SYSTEM AND RESET THE FECU IAW CRJ200 FIM 27-50-00. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — OPEN (O2 SERVICING) · airframe 770 hrs · 765 cycles

ON CLIMBOUT CREW REPORTED A LOUD SQUEAL FROM THE RIGHT FORWARD SECTION OF THE AIRCRAFT. MAINTENANCE INSPECTED AND FOUND THE OXYGEN SERVICING DOOR OPEN. MAINTENANCE CLOSED THE DOOR AND PERFORMED A DETAILED VISUAL INSPECTION PER THE SRM. NO DEFECTS WERE NOTED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACTUATOR — FAILED (LT HYD SYSTEM) · airframe 712 hrs · 707 cycles

THE CREW REPORTED THAT THE HYDRAULIC ACTUATOR WOULD NOT CLOSE WHEN YOU PUSH THE LEFT HAND FIRE BUTTON. MAINTENANCE INSPECTED AND REPLACED THE HYDRAULIC ACTUATOR IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 29-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PUMP — FAILED (APU FUEL) · airframe 53 hrs · 55 cycles

APPROXIMATELY 20 MINUTES FROM PHL, THE CREW RECEIVED A FUEL IMBALANCE INDICATION. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND SHUTDOWN THE LEFT HAND ENGINE AND LANDED AT PHL. MECHANICS WERE SENT FROM DAY. MAINTENANCE THEN INSPECTED AND REPLACED THE APU PUMP IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 28-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.