N242JS

Part: PROXIMITY SENSOR — OUT OF ADJUST (NLG)

THE AIRCRAFT RETURNED TO FIELD AFTER RECEIVING A GEAR DISAGREE. THE AIRCRAFT LANDED WITHOUT FURTHUR INCIDENT. MAINTENANCE ADJUSTED THE NLG PROX SENSOR PS13GA. OPS CHECK GOOD

Part: FUEL LINE — LEAKING (APU BAY) · airframe 33,094 hrs · 32,892 cycles

DURING FLIGHT, THERE WAS A STRONG FUEL ODOR. MAINTENANCE FOUND A FUEL LINE LEAKING INSIDE OF THE APU ENCLOSURE. MAINTENANCE REPAIRED THE FUEL LINE.

Part: RELAY — MALFUNCTIONED (BUSS SENSE) · airframe 32,881 hrs · 21,689 cycles

AIRCRAFT DIVERTED DUE TO A WINDSHIELD HEAT MESSAGE. RAN QUICK REFERENCE HANDBOOK AND MESSAGE CLEARED. THE AIRCRAFT THEN BEGAN RECEIVING NUMEROUS FAIL MESSAGES THAT ARE ALL ELECTRICAL RELATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE ACFT ESSENTIAL BUSS SENSE RELAY K1XD AND TRU 1. OPS CHECKED GOOD.

Part: SEAT TRACK — CORRODED (BS 364-399) · corrosion level 2 · airframe 31,784 hrs · 31,716 cycles

RBL 9 SEAT TRACK CORRODED AND GOUGED BETWEEN BS 364 AND 399. REMOVED AND REPLACED THE SEAT TRACK.

Part: FLOOR SUPPORT — CORRODED (BS 409) · corrosion level 2 · airframe 31,784 hrs · 31,716 cycles

LEFT FLOOR SUPPORT IS CORRODED FROM BS 409+96 - 409+128. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-00-530.

Part: SEAT TRACK — CORRODED (S 559) · corrosion level 2 · airframe 31,784 hrs · 31,716 cycles

RBL 9 SEAT TRACK IS CORRODED FROM BS 559+4 TO 559+80. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-485.

Part: FLOOR SUPPORT — CORRODED (BS 409) · corrosion level 2 · airframe 31,784 hrs · 31,716 cycles

RIGHT FLOOR SUPPORT IS CORRODED AROUND FASTENER HOLES BETWEEN BS 409+96 AND 409+128. REPAIRED FLOOR SUPPORT IAW REO:601R-53-00-530, REV A.

Part: ANGLE — CRACKED (BS 621-625) · airframe 31,784 hrs · 31,716 cycles

LEFT BS 621 - 625 OBLIQUE ANGLE IS CRACKED. INSTALLED A NEW ANGLE.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · corrosion level 2 · airframe 31,784 hrs · 31,716 cycles

LEFT PRESSURE FLOOR SUPPORT AND ANGLE ARE CORRODED FROM BS 409+128 - 559. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-41-666.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · corrosion level 2 · airframe 31,784 hrs · 31,716 cycles

RIGHT PRESSURE FLOOR SUPPORT AND ANGLE ARE CORRODED FROM BS 409+128 - 559. CORROSION REMOVED IAW SRM 51-42-21. 1. COMPLIED WITH REO 601R-53-41-666.

Part: SEAT TRACK — CORRODED (BS 409) · corrosion level 2 · airframe 31,784 hrs · 31,716 cycles

LEFT SEAT TRACK HAD CORROSION FROM BS 409+18 TO 409+128. REMOVED, FABRICATED, AND INSTALLED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 409-559) · corrosion level 2 · airframe 31,784 hrs · 31,716 cycles

RIGHT SIDE SEAT TRACK HAD CORROSION FROM BS 409+128 TO 559+80 & 409 TO 409 +128. FABRICATED A SEAT TRACK AND INSTALLED.

Part: FLOOR SUPPORT — CORRODED (BS 605-615) · corrosion level 2 · airframe 31,784 hrs · 31,716 cycles

LEFT FLOOR SUPPORT IS CORRODED AROUND FASTENER HOLES FROM BS 605 TO 615. REPAIRED IAW REO 601R-53-00-526.

Part: SEAT TRACK — CORRODED (BS 449-559) · corrosion level 2 · airframe 31,784 hrs · 31,716 cycles

LEFT SEAT TRACK HAD CORROION FROM BS 409+128 TO 559+80. REPLACED THE SEAT TRACK.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 31,784 hrs · 31,716 cycles

CRACK INDICATIONS WERE NOTED ON THE BS 621 REAR PRESSURE BULKHEAD IAW 53-11-153, BL 0 WL 104 TO 113, APPROX 53% FULL SCREEN HEIGHT AND AT WL 126 TO WL 133.5 APPROX 63% FULL SCREEN HEIGHT FAILING ND. REPAIRED IAW REO 601R-53-61-1285, REV E.

Part: FLOOR SUPPORT — CORRODED (BS 559) · corrosion level 2 · airframe 31,784 hrs · 31,716 cycles

FLOOR SUPPORT IS CORRODED AROUND FASTENER HOLES FROM BS 559+16 TO 559+36. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-00-526.

Part: POST — CRACKED (BS 409) · airframe 31,784 hrs · 31,716 cycles

BS 409+128 VERTICAL POST AT LBL 27 INBD BOTTOM CRACKED AT BOTTOM FASTENER. REMOVED & REPLACED THE VERTICAL POST IAW SRM 51-42-06, 51-42-22, AND REO 601R-53-41-2217.

Part: A/C PACK — FAILED (RIGHT) · airframe 5,590 hrs · 5,069 cycles

RIGHT PACK OVERHEAT CAUTION MESSAGE, FOLLOWED BY RIGHT PACK FAILURE, DURING CLIMB. AN EMERGENCY WAS DECLARED.

Part: SEAT TRACK — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 30,966 hrs · 30,899 cycles

LEFT AFT SIDEWALL SEAT TRACK CORRODED. REMOVED AND REPLACED THE SEAT TRACK.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 30,077 hrs · 30,056 cycles

EMERGENCY LIGHT STRIPS INOPERATIVE. MAINTENANCE TROUBLESHOT, AND TIGHTENED THE CONNECTOR ON THE NR 4CHARGER ASSEMBLY, AND PERFORMED CHECKS IAW AMM, OPS CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 27,709 hrs · 27,683 cycles

CREW REPORTED EMERGENCY FLOOR LIGHTING INOPERATIVE FROM ROW 2 TO 6. MAINTENANCE TROUBLESHOT, R & R INVERTER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (ROWS 9-13) · airframe 27,704 hrs · 27,677 cycles

CREW REPORTED FLOOR LEVEL EXIT LIGHTING WOULD NOT ILLUMINATE FROM ROW 9 TO 13. MAINTENANCE CHECKED EMERGENCY LIGHTS ELECTRICAL CONNECTIONS AND PERFORMED OPS CHECK IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WIRE — ARCED (CHART HOLDER) · airframe 27,457 hrs · 27,431 cycles

F/O CHART HOLDER LIGHT WIRING ARCING. MAINTENANCE INSPECTED, TIGHTENED HARDWARE ON F/O CHART HOLDER AND PERFORMED CHECKS. ACFT RELEASED FOR SERVICE.

Part: ENGINE — DAMAGED (LEFT) · airframe 26,486 hrs · 26,472 cycles

CREW REPORTED LT N2 VIBRATION MESSAGE WHILE ON RUNWAY. WHEN SETTING TAKEOFF POWER, CREW HEARD LOUD POP FOLLOWED BY GRINDING SOUND COMING FROM LT SIDE OF ACFT. CREW REJECTED TAKEOFF, SHUTDOWN LT ENGINE AND RETURNED TO GATE. MAINTENANCE INSPECTED LT ENGINE AND FOUND EXTENSIVE AND OUT-OF-LIMITS DAMAGE TO 14TH STAGE HIGH PRESSURE COMPRESSOR BLADES. MAINTENANCE R & R LT ENGINE AND PERFORMED CHECKS. ALL WORK ACCOMPLISHED BY MAINTENANCE IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 25,040 hrs · 25,067 cycles

CREW REPORTED LT FORWARD BULKHEAD EXIT SIGN INOPERATIVE. MAINTENANCE INSPECTED, R & R LT WINDSCREEN EXIT SIGN AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: STATIC WICK — DAMAGED (HORIZONTAL STAB) · airframe 24,408 hrs · 24,428 cycles

CREW REPORTED A POSSIBLE LIGHTNING STRIKE. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION USING AMM. MAINTENANCE REPLACED, STATIC WICKS ON THE HORIZONTIAL STABILIZER, AND REPLACED RIVET AT FS 310 USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: FLOW SENSOR — FAILED (AVIONICS COOLING) · airframe 24,305 hrs · 24,314 cycles

CREW REPORTED DISPLAY COOL AMBER MESSAGE AFTER TAKEOFF. MESSAGE PERSISTED AFTER FLT ALT AND STBY POSITIONS SELECTED. CREW FOLLOWED QRH, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R DISPLAY COOLING LOW FLOW DETECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (BS 409) · airframe 23,956 hrs · 23,988 cycles

DURING SCHEDULED MAINTENANCE, FOUND AT FS 409+32 STRINGER 14L HAD LIGHTNING STRIKE DAMAGE. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: STRINGER — DAMAGED (BS 280) · airframe 23,956 hrs · 23,988 cycles

DURING SCHEDULED MAINTENANCE AT FS 280.0, STRINGER 3L HAD AN ELONGATED HOLE. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: SILL — CORRODED (BS 310-349) · corrosion level 2 · airframe 23,956 hrs · 23,988 cycles

DURING SCHEDULED MAINTENANCE THE MAIN CABIN DOOR SILL AROUND THE PROXIMITY DOOR CUT OUT AND AROUND SEVERAL FASTENER HOLES CORROSION WAS FOUND. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLOORBEAM — CORRODED (BS 559) · corrosion level 2 · airframe 23,956 hrs · 23,988 cycles

DURING SCHEDULED MAINTENANCE, THE CABIN FLOORBEAM CAP AT FS 559 CORRODED. AREA WAS INSPECTED AND REPAIRED IAW AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 23,956 hrs · 23,988 cycles

DURING SCHEDULED MAINTENANCE THE LT ELEVATOR UPPER OTBD SKIN HAS LIGHTNING STRIKE DAMAGE ON OTBD EDGE. THE LEFT ELEVATOR UPPER OTBD SKIN WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED (BS 559) · airframe 23,956 hrs · 23,988 cycles

DURING SCHEDULED MAINTENANCE THE FS 559+64 STRINGER 13L HAD LIGHTNING STRIKE DAMAGE. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — CRACKED (BS 379) · airframe 23,956 hrs · 23,988 cycles

DURING SCHEDULED MAINTENANCE FS 379.0, STRINGER 3L WAS CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: COALESCER BAG — CONTAMINATED · airframe 23,852 hrs · 23,884 cycles

DURING FINAL APPROACH, CREW REPORTED MOMENTARY TOILET SMOKE INDICATION, OIL ODOR AND SOME SMOKE IN CABIN. DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. SMOKE DISIPATED BEFORE LANDING. MAINTENANCE INSPECTED BOTH ENGINES AND APU FOR OIL LEAKS. NO LEAKS FOUND. MAINTENANCE R & R LT AND RT WATER SEPARATOR COALESCERS. LEAK CHECKED GOOD. RAN BOTH LT AND RT PACKS RUN OFF OF BOTH ENGINES AND APU. NO OIL OR SMOKE ODOR DETECTED. MAINTENANCE COMPLIED WITH OPS CHECK OF LAVATORY SMOKE DETECTOR. OPS TEST GOOD. ALL WORK ACCOMPLISHED BY MAINTENANCE IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: FITTING — LOOSE (FUEL SYSTEM) · airframe 21,943 hrs · 22,136 cycles

CREW REPORTED FUEL SMELL IN FLIGHT. CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, TIGHTENED ONE FITTING ON MOTIVE FLOW LINE IN WHEEL WELL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL WHEEL — FAILED (NLG STEERING) · airframe 21,854 hrs · 22,049 cycles

CREW REPORTED AIRCRAFT PULLING TO THE RIGHT WITH FULL LEFT RUDDER DURING TAKEOFF. TILLER WAS CENTERED AND BOTH ENGINES WERE SPOOLED UP IN SYNC. CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT STEERING SYSTEM, REMOVED AND REPLACED PILOT’S HAND WHEEL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (ANTI-ICE SYS) · airframe 21,425 hrs · 21,658 cycles

CREW REJECTED TAKEOFF DUE TO AMBER WING ANTI-ICE CAUTION MESSAGE WITH ANTI-ICE SELECTED ON. CREW RETURNED TO GATE. MAINTENANCE GROUND RAN AIRCRAFT WITH CREW AND PERFORMED CHECKS ON WING ANTI-ICE CONTROL AND INDICATION SYSTEM USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: LENS — DAMAGED (TAIL) · airframe 21,423 hrs · 21,656 cycles

LIGHTNING STRIKE INSPECTION PERFORMED BY MAINTENANCE DUE TO SUSPECTED LIGHTNING STRIKE. MAINTENANCE REMOVED AND REPLACED LOWER TAIL NAV LIGHT LENS AND REMOVED AND REPLACED BOLT AND WASHER TO FDR BRACKET BONDING WIRE DUE TO LIGHTNING DAMAGE. REPAIRS MADE FOR LIGHTNING DAMAGE TO LEFT ELEVATOR OUTBOARD TRAILING EDGE AND TO THREE (3) RIVETS ON LEFT FUSELAGE. MAINTENANCE PERFORMED CHECKS AND AIRCRAFT RELEASED FOR SERVICE. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS.

Part: COMPRESSOR BLADE — DAMAGED (LT ENGINE) · airframe 21,234 hrs · 21,487 cycles

CREW REPORTED LEFT ENGINE WOULD NOT ATTAIN CLIMB POWER WITHOUT EXCEEDING ITT LIMIT. MULTIPLE AIRFRAME VIBRATION / SHUDDERS WERE ALSO REPORTED, WITH ONE SEVERE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LEFT ENGINE AND FOUND COMPRESSOR BLADE DAMAGE TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CARBON SEAL — DEFECTIVE (LT ENGINE) · airframe 20,858 hrs · 21,167 cycles

CREW REPORTED SMOKE IN CABIN. AIRCRAFT RETURNED TO AIRPORT LANDING WITHOUT ISSUE. MAINTENANCE TROUBLESHOT, REMOVED, AND REPLACED THE CARBON SEAL ON THE LEFT ENGINE. OPERATIONAL CHECKS WERE PERFORMED USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 20,846 hrs · 21,154 cycles

CREW REPORTED SMOKE TOILET AMBER MESSAGE ALONG WITH SMOKE IN COCKPIT AND CABIN. AIRCRAFT RETURNED TO AIRPORT LANDING WITHOUT ISSUE. MAINTENANCE TROUBLESHOT, REMOVED,AND REPLACED THE LEFT AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE PERFORMED USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — ODOR · airframe 20,717 hrs · 21,040 cycles

AT FL 290, CREW NOTICED STRONG SCENT OF OIL / FUEL WITH PACK TEMPERATURE SET TO 42 DEGREES CENTIGRADE AND THAT SCENT GOES AWAY WHEN PACKS SET TO COLD. CREW LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE INSPECTED AND DEFERRED LEFT PACK PER MEL. AIRCRAFT RELEASED FOR SERVICE. SUPPLEMENTAL INFORMATION WILL BE PROVIDED WHEN DEFERRAL IS CLEARED.

Part: POWER STRIP — INOPERATIVE (CABIN) · airframe 20,308 hrs · 20,679 cycles

CREW REPORTED FLOOR LEVEL EMERGENCY LIGHTS AT ROWS TWO (2) THROUGH FIVE (5) AND EMERGENCY EXIT SIGN AT FLOOR LEVEL ON LEFT OVERWING DOOR TO BE INOPERATIVE. MAINTENANCE INSPECTED AND TROUBLESHOT EMERGENCY LIGHT SYSTEM, REMOVED AND REPLACED FORWARD CABIN FLOOR TRACK LIGHT POWER STRIP AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,797 hrs · 19,449 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE BULKHEAD WEB. THE BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ROD — DISCONNECTED (LT COWLING) · airframe 18,798 hrs · 19,236 cycles

CREW REPORTED LEFT THRUST LEVER WAS JAMMED IN POSITION DURING FLIGHT. CREW FOLLOWED QRH (QUICK REFERENCE HANDBOOK), SHUT DOWN LEFT ENGINE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND LEFT ENGINE AFT CORE UPPER COWL UPPER SUPPORT ROD DISCONNECTED AND JAMMED, BLOCKING FUEL CONTROL ROD. SUPPORT ROD WAS MISSING ITS KEEPER BOLT. MAINTENANCE INSTALLED NEW SECURING PIN ON LEFT ENGINE UPPER CORE COWL USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SKIN — DENTED (TE FLAP) · airframe 18,296 hrs · 18,750 cycles

AT CRW, CREW REPORTED A BIRD STRIKE BELOW CAPTAIN’S WINDSHIELD. MAINTENANCE COMPLIED WITH BIRD STRIKE INSPECTION AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. MAINTENANCE FOUND LEFT OUTBOARD FLAP UNDERSIDE SKIN DENTED AND DETERMINED DENT TO BE WITHIN SRM LIMITS. AIRCRAFT RELEASED FOR SERVICE.

Part: UNKNOWN — ODOR (A/C PACK) · airframe 18,112 hrs · 18,571 cycles

CREW REPORTED A STRONG OIL ODOR FROM RIGHT PACK WHEN BLEEDS SWITCHED FROM APU TO ENGINE ON TAKEOFF FROM DAY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPS CHECKS ON RIGHT PACK, NO OIL ODOR DETECTED. WORK ACCOMPLISHED IAW MM. AIRCRAFT RELEASED FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 17,994 hrs · 18,462 cycles

CREW REPORTED LEFT ENGINE OIL PRESSURE RED WARNING AND THAT OIL PRESSURE WENT TO ZERO PSI IN FLIGHT EN ROUTE FROM PHL TO BNA. CREW PERFORMED IN-FLIGHT SHUTDOWN OF LEFT ENGINE AND DIVERTED TO GSO. AIRCRAFT LANDED IN GSO WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT ENGINE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 17,530 hrs · 17,994 cycles

CREW REPORTED STEERING INOP MESSAGE IN FLIGHT ON APPROACH TO PHL. CREW RAN QRH AND MESSAGE CLEARED. AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. CREW RESET NOSE WHEEL STEERING SYSTEM WITH MAINTENANCE USING MAINTENANCE MANUAL. SYSTEM CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE.

Part: COMPUTER — FAILED (IAPS) · airframe 17,456 hrs · 17,929 cycles

AT CLT, CREW REPORTED LIGHTNING STRIKE ON CAPTAIN’S SIDE LOWER LEFT CENTER OF WINDSCREEN IN FLIGHT. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE FOLLOWING COMPONENTS: MDC (MAINTENANCE DIAGNOSTIC COMPUTER), LOWER TAIL NAV LIGHT ASSEMBLY, FORWARD UPPER VHF 1 ANTENNA AND VARIOUS STATIC WICKS. LIGHTNING STRIKE DAMAGE (BURNS) TO TAIL CONE WAS REPAIRED. CHECKS WERE PERFORMED. ALL WORK WAS ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BPSU — FAILED (TE FLAP) · airframe 17,265 hrs · 17,744 cycles

CREW REPORTED FLAPS FAILED CAUTION MESSAGE AFTER TAKEOFF FROM BTR. CREW RETURNED TO BTR AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BPSU — FAILED (TE FLAP) · airframe 17,226 hrs · 17,707 cycles

CREW REPORTED FLAPS FAIL CAUTION MESSAGE WHILE IN CRUISE FLIGHT EN ROUTE FROM CLT TO PGV. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: ECU — FAILED (TE FLAP) · airframe 17,215 hrs · 17,696 cycles

CREW REPORTED FLAPS FAIL CAUTION MESSAGE IN FLIGHT EN ROUTE FROM CLT TO ATL. CREW LANDED IN ATL WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FECU (FLAP ELECTRONIC CONTROL UNIT), RE-SECURED LOOSE BACKSHELL ON LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) CONNECTOR AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SEAL — BLOWN (OIL SYSTEM) · airframe 17,020 hrs · 17,509 cycles

CREW REPORTED LEFT ENGINE OIL PRESSURE MASTER WARNING AND TRIPLE CHIME SHORTLY AFTER TAKEOFF FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, FOUND SEAL BLOWN OUT OF LEFT ENGINE OIL PRESSURE TRANSDUCER, REMOVED AND REPLACED TRANSDUCER AND SEAL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WINGLET — DAMAGED (RT WING) · airframe 16,866 hrs · 17,358 cycles

CREW REPORTED LIGHTNING STRIKE DURING DESCENT INTO DAY. CREW LANDED IN DAY WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, REPAIRED DAMAGE TO RIGHT WINGLET, REMOVED AND REPLACED STATIC DISCHARGERS AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,188 hrs · 16,667 cycles

CREW REPORTED THE FORWARD CABIN CEILING EMERGENCY LIGHT TO BE INOPERATIVE AT CLT. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE FORWARD FLOODLIGHT AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 16,043 hrs · 16,533 cycles

ROW 9 TO 12 EMERGENCY LIGHTS WERE REPORTED NOT WORKING. MAINTENANCE USING THE AIRCRAFT MAINTENANCE MANUAL REMOVED AND REPLACED EMERGENCY BATTERY PACK. CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — FLAT (NLG) · airframe 15,742 hrs · 16,234 cycles

CREW ABORTED TAKEOFF BECAUSE OF NOSE VIBRATION. MAINTENANCE FOUND BOTH NOSE TIRES WERE FLAT. USING THE AIRCRAFT MAINTENANCE MANUALS, THE AIRCRAFT WAS INSPECTED, NOSE TIRES REPLACED AND AIRFRAME REPAIRED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DENTED (LT WING) · airframe 15,486 hrs · 15,985 cycles

AT CLT, CREW REPORTED A BIRD STRIKE ON THE LEFT WING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A DENT IN THE LEFT WING INBOARD LEADING EDGE SKIN RIGHT ABOVE THE TAXI AND LANDING LIGHT COVER. THE DENT WAS DETERMINED TO BE WITHIN LIMITS PER THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ANGLE — CRACKED (BS 559) · airframe 14,653 hrs · 15,183 cycles

DURING MAINTENANCE A CRACK AT FS 559 PRESSURE BULKHEAD CAP ANGLE WAS FOUND. AIRCRAFT WAS REPAIRED USING AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: WINDOW — CRACKED (COCKPIT) · airframe 13,863 hrs · 14,312 cycles

CREW REPORTED THE RT SIDE WINDOW CRACKED DURING CRUISE EN ROUTE FROM CLT TO GPT. AIRCRAFT DIVERTED TO PNS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT USING THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE REMOVED AND REPLACED THE RT SIDE WIDOW AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ELEVATOR — DAMAGED (RIGHT) · airframe 11,992 hrs · 12,354 cycles

CREW REPORTED LIGHTNING STRIKE IN PHL. MAINTENANCE REMOVED AND REPLACED THE RT ELEVATOR AND REPAIRED DAMAGED RIVETS. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — DAMAGED (RT MLG) · airframe 9,178 hrs · 9,354 cycles

CREW REPORTED THE RIGHT INBOARD MAIN TIRE SHREDDED UPON LANDING IN PHL. MAINTENANCE REMOVED AND REPLACED BOTH RIGHT HAND MAIN GEAR TIRES IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS FERRIED TO DAY FOR FURTHER EVALUATION AND TO REPAIR DAMAGE. MAINTENANCE ISSUED TEMP REPAIR 10995. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSOR — DAMAGED (STALL WARNING) · airframe 7,358 hrs · 7,424 cycles

CREW REPORTED A LIGHTNING STRIKE ON CLIMBOUT. MAINTENANCE PERFORMED AN ENROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. AIRCRAFT WAS FERRIED TO DAYTON FOR REPAIR. MAINTENANCE INSPECTED AND REPAIRED ALL DAMAGE. MAINTENANCE ALSO REMOVED AND REPLACED THE RIGHT HAND ANGLE OF ATTACK IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 27-35-05-000/400-801. OPS CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 4,956 hrs · 4,881 cycles

DURING CLIMBOUT THE -FLAPS FAIL- CAUTION MESSAGE ILLUMINATED WITH FLAPS STUCK AT 13 DEGREES. THE CREW FOLLOWED THE QRH, RETURNED TO FAY, AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM. NO FAULTS WERE FOUND AND ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FCU — FAILED (TE FLAPS) · airframe 4,936 hrs · 4,860 cycles

DURING INITIAL DEPARTURE THE -FLAPS FAIL- CAUTION MESSAGE ILLUMINATED WITH FLAPS STUCK AT 15 DEGREES. THE CREW FOLLOWED THE QRH, RETURNED TO CLT, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLAP ELECTRONIC CONTROL UNIT. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 4,886 hrs · 4,809 cycles

ON APPROACH THE -FLAPS FAIL- CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 16 DEGREES. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM. NO FAULTS WERE FOUND AND ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACCESS PANEL — PUNCTURED (LT NOSE COWL) · airframe 3,227 hrs · 3,166 cycles

A BELT LOADER HIT THE LT ENGINE NOSE COWL LOWER ACCESS PANEL. DAMAGE AT THE 5 O'CLOCK POSITION WAS A 6 X 2 HOLE. AFTER INSPECTION AND TEMPORARY REPAIR THE AIRCRAFT WAS FERRIED TO CKB WHERE MAINTENANCE REMOVED & REPLACED THE PANEL WITH A SERVICEABLE UNIT IAW CRJ200 AMM 71-14-01-000(400)-801. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: TRIM SYSTEM — UNKNOWN (STAB) · airframe 2,457 hrs · 2,366 cycles

STABILIZER TRIM FAILED IN FLIGHT AND THE MACH TRIM DISENGAGED. MAINTENANCE OPERATIONALLY CHECKED THE STAB TRIM SYSTEM IAW BOMBARDIER RJ-SL-00-001. THE SYSTEM CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — ACTIVATED (ANTI ICE SYS) · airframe 1,994 hrs · 1,913 cycles

MULTIBLE TIMES DURING THE FLIGHT THE CREW RECEIVED ANTI-ICE DUCT WARNING MESSAGES. THE CREW OF FLIGHT 2471 FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING AT DESTINATION. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE BLEED-AIR LEAK DETECTION AND WARNING SYSTEM IAW CRJ-200 AMM 36-21-00-710-801. ALL TESTS WERE GOOD. NO DEFECTS WERE NOTED AT THIS TIME. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 1,988 hrs · 1,906 cycles

DURING TAKEOFF ROLL AT DAY THE CREW RECEIVED ANTI-ICE DUCT WARNING MESSAGES. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. PSA MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE WING ANTI-ICE CONTROL & INDICATION SYSTEM IAW CRJ 200 AMM 30-12-00-710-801. THE SYSTEM CHECKED GOOD AND NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE INDICATION (GROUND SPOILERS) · airframe 1,769 hrs · 1,704 cycles

AT THE START OF TAKEOFF ROLL AT DCA THE CREW REPORTED A TAKEOFF CONFIG WARNING AND THE GND SPLR DEPLOY CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2428 ABORTED THE TAKEOFF AND RETURNED TO THE GATE. CONTRACT MAINTENANCE PERFORMED TAKEOFF CONFIG OPERATIONAL CHECKS IAW CRJ 200 FIM 22-12-00. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: CONNECTOR — LOOSE (APU FIRE BOTTLE) · airframe 685 hrs · 672 cycles

THE CREW REPORTED THAT THE APU FIRE BOTTLE ARMED PUSH TO DISCHARGE GREEN LIGHT WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED AND FOUND CONNECTOR 1PS1WA LOOSE. MAINTENANCE THEN RESECURED CONNECTOR 1PS1WA IN ACCORDANCE WITH SMP. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.