N260JS

Part: UNKNOWN — ODOR (COCKPIT) · airframe 33,456 hrs · 33,457 cycles

CREW REPORTED AN ELECTRIC SMELL IN COCKPIT WHEN SWITCHING POWER FROM APU TO GROUND POWER. MX INSPECTED FLIGHT DECK AND SURROUNDING AREA FOR ELECTRIC SMELL. NO SMELL NOTED. PERFORMED OPS CHECKS OF GROUND POWER AND APU POWER WITH NO DEFECTS NOTED.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,932 hrs · 32,812 cycles

RT FLOOR SILL HAS AREA OF CORROSION AND SOME CHAFING, DAMAGE FROM FLOOR BOARD BETWEEN FS 559+112 TO FS 621. REMOVED AND REPLACED SILL IAW EO CL-600-2B19-53-L05666.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,932 hrs · 32,812 cycles

CLIP ANGLES AT FS 200 LBL6 AND RBL6 WL79 ARE CRACKED . REMOVED AND REPLACED CLIP ANGLES PN: 600-33101-89 AND CLIP ANGLE PN 600-33101-90 IAW SRM 51-42-06.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 33,932 hrs · 32,812 cycles

REPAIRED FS621 BULKHEAD IAW REO 601R-53-61-1240 REV D DATED 10/31/16. AND INCORPORATED DEVIATION REPAIR IAW REO 601R-53-61-6554 REV-- DATED 5/8/18 AT RBL 27.5 WL76-77, LBL27.5 WL 78-79, AND LBL9.5 WL76-79.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 33,932 hrs · 32,812 cycles

FS 280 CROSSBEAM IS CRACKED JUST O/B OF LBL 9. REPAIRED FS 280 CROSSBEAM IAW REO 601R-53-11-926 REV B DATED 2006/05/10.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 33,932 hrs · 32,812 cycles

PAX DOOR UPPER SILL (STR 3L) IS CRACKED JUST AFT OF FS 379.00. REPAIRED CRACKED STRINGER IAW REO 601R-53-21-2976. REV-- DATED 2018-04-28.

Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,932 hrs · 32,812 cycles

STGR 27 IS CORRODED BETWEEN FS 559+112 AND FS 574. REMOVED AND REPLACED ANGLE CLIP IAW SRM 200 51-42-06.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,932 hrs · 32,812 cycles

FORWARD FUSELAGE SKIN IS CRACKED AT THE LT TRU DOOR AFT LATCH LOCATION. REMOVED AND REPLACED DOOR LANDING IAW SRM 51-42-06 AND 51-42-13.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,932 hrs · 32,812 cycles

FUSELAGE FRAME FS574 IS CORRODED BETWEEN STGR 25L AND STGR 18R. REMOVED AND REPLACED FRAME SECTOR P/N 601R36024-61 IAW SRM 51-40-11, 51-42-06 AND 51-42-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,932 hrs · 32,812 cycles

INTERCOSTAL BETWEEN FS 621 AND FS 625 AT RBL45 WL 94 IS CRACKED. REMOVED AND REPLACED OBLIQUE ANGLE IAW SRM 51-42-06.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 33,932 hrs · 32,812 cycles

INTERCOSTAL BETWEEN FS 621 AND FS 625 AT LBL45 WL 94 IS CRACKED. REMOVED AND REPLACED OBLIQUE ANGLE IAW SRM 51-42-06.

Part: RIB — CRACKED (RT WING) · airframe 33,932 hrs · 32,812 cycles

RIGHT WING BATT RIB CAP ANGLE AT WS 48.30 IS CRACKED. REMOVED AND REPLACED CAP ANGLE IAW SRM 51-42-21.

Part: RIB — CRACKED (LT WING) · airframe 33,932 hrs · 32,812 cycles

LEFT WING BATT RIB CAP ANGLE AT WS 48.30 IS CRACKED. REMOVED AND REPLACED CAP ANGLE IAW SRM 51-42-21

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 32,788 hrs · 32,684 cycles

WHILE IN CRUISE FLIGHT, THE CREW NOTICED A CRACK ON THE CAPTAIN`S WINDSHIELD AND NOTICED A FEW SPARKS WHILE THE WINDSHIELD HEAT WAS ON. DECLARED AN EMERGENCY AND DIVERTED. REPLACED THE WINDSHIELD.

Part: TARGET — LOOSE (PROXIMITY SENSOR) · airframe 32,094 hrs · 32,065 cycles

CREW RECEIVED GEAR DISAGREE MESSAGE AFTER DEPARTING CAE, DUE TO THE RIGHT MAIN GEAR NOT RETRACTING. MX INSPECTED AND FOUNG THE RT MAIN GEAR UPLOCK PROXIMITY SENSOR TARGET WAS LOOSE. SECURED THE TARGET, LANDING GEAR RETRACTION AND EXTENSION SYSTEM OPS CHECKED GOOD.

Part: CARBON SEAL — DEFECTIVE (RT ENGINE) · airframe 30,678 hrs · 30,713 cycles

RED RIGHT ENGINE OIL PRESSURE WARNING. REMOVED AND REPLACED THE ACCESSORY DRIVE GEARBOX’S CARBON SEAL ASSEMBLIES.

Part: PROXIMITY SENSOR — INOPERATIVE (PAX DOOR) · airframe 29,482 hrs · 29,546 cycles

AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE PASSENGER DOOR OUTER HANDLE PROXIMITY SENSOR PS2MB AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 28,656 hrs · 28,722 cycles

FLAPS FAIL MESSAGE, MAINTENANCE TROUBLESHOT, R & R THE FLAPS ELECTRONIC CONTROL UNIT, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: SENSOR — FAILED (BLEED AIR) · airframe 26,313 hrs · 26,409 cycles

CREW REPORTED RT 14TH DUCT, RED WARNING MESSAGE ON TAKEOFF. QRH WAS RUN AND MESSAGE PERSISTED. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT 14TH STAGE PYLON SENSING ELEMENT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (BS 589-621) · airframe 24,680 hrs · 24,751 cycles

DURING SCHEDULED MAINTENANCE A CREASE WAS FOUND BELOW THE BAGGAGE BAY SCUFF PLATE AT BS 605. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 24,680 hrs · 24,751 cycles

DURING SCHEDULED MAINTENANCE, CABIN SEAT TRACK BS 409+40 WAS FOUND CORRODED. SEAT TRACK R & R IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: POST — CRACKED (BS 409) · airframe 24,680 hrs · 24,751 cycles

DURING SCHEDULED MAINTENANCE THE RT VERTICAL POST BS 409+128 WAS FOUND CRACKED. VERTICAL POST R & R IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: SKIN — CRACKED (WING) · airframe 24,680 hrs · 24,751 cycles

DURING SCHEDULED MAINTENANCE, LOWER WING PLANK AFT FASTENER WAS FOUND CRACKED. REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: SKIN — CRACKED (BS 235) · airframe 24,680 hrs · 24,751 cycles

DURING SCHEDULED MAINTENANCE, THE AFT RIGHT CORNER OF THE NLG CUTOUT SKIN, BS 235 WAS FOUND CRACKED. INSPECTED AND REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — MALFUNCTIONED (COCKPIT) · airframe 24,539 hrs · 24,599 cycles

CREW REPORTED ICE ACCUMULATION INSIDE BLACK AREA OF LT SIDE ON CAPTAIN’S FRONT WINDSHIELD. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LEFT FORWARD WINDSHIELD AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: IDG — FAILED (NR 1) · airframe 21,968 hrs · 22,208 cycles

DURING CRUISE, NR 1 GENERATOR FELL OFF LINE. ACFT RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MX TROUBLESHOT, R & R NR 1 IDG IAW ACFT MANUALS. CHECKS WERE PERFOMED IAW THE ACFT MANUALS AND ACFT WAS RELEASED FOR SERVICE.

Part: RIB — CRACKED (RT MLG WW) · airframe 21,524 hrs · 21,815 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND AT THE RIGHT RIB IN RIGHT WHEEL WELL. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSING ELEMENT — FAULTY (LT ENGINE) · airframe 20,892 hrs · 21,260 cycles

CREW REPORTED LEFT 14TH STAGE BLEED DUCT WARNING MESSAGE WITH ANTI-ICE TURNED ON AND APU STARTED. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MESSAGE WENT OFF 15 TO 20 MINUTES LATER. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT ENGINE 14TH STAGE PYLON SENSING ELEMENT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: TIRE — SEPARATED (NLG) · airframe 20,749 hrs · 21,135 cycles

ON CLIMBOUT, SHORTLY AFTER TAKEOFF, CREW HEARD THUMPING NOISE AROUND NOSE GEAR. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND TREAD SEPARATION ON RIGHT NOSE LANDING GEAR TIRE. MAINTENANCE REMOVED AND REPLACED RIGHT AND LEFT TIRE / WHEEL ASSEMBLIES. NOSE LANDING GEAR AFT DOOR WAS REMOVED AND REPLACED DUE TO DAMAGE AND FUSELAGE DENTS WERE REPAIRED. CHECKS WERE PERFORMED AND AIRCRAFT RELEASED FOR SERVICE. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS.

Part: SMOKE DETECTOR — FALSE ACTIVATION (LAVATORY) · airframe 20,360 hrs · 20,789 cycles

CREW REPORTED LAVATORY SMOKE ALARM SOUNDED ABOUT 7 MINUTES INTO FLIGHT. NO SMELL OR SMOKE SEEN. NO MESSAGES WERE DISPLAYED. AIRCRAFT RETURNED TO AIRPORT LANDING WITHOUT ISSUE. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR. OPERATIONAL CHECKS WERE PERFORMED USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: HANDLE — OPEN (CARGO DOOR) · airframe 19,852 hrs · 20,347 cycles

CREW REPORTED CARGO DOOR CAUTION MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. HANDLE WAS CONFIRMED OPEN BY GROUND PERSONNEL. MAINTENANCE CLOSED CARGO DOOR HANDLE AND INSPECTED CARGO DOOR USING AIRCRAFT MAINTENANCE MANUALS. NO DEFECT FOUND. AIRCRAFT RELEASED FOR SERVICE.

Part: SENSING ELEMENT — FAULTY (RT PYLON) · airframe 17,420 hrs · 18,064 cycles

CREW REPORTED RIGHT 14TH DUCT RED CAS MESSAGE IN FLIGHT EN ROUTE FROM DAY TO DCA. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT PYLON SENSING ELEMENT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 16,784 hrs · 17,444 cycles

DURING SCHEDULED MAINTENANCE THE FS 280.0 FLOOR TRAVERSE BEAM WAS FOUND CRACKED AND CORRODED. THE FS 280.0 FLOOR TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE. REVISED UNIQUE NUMBER.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 16,784 hrs · 17,444 cycles

DURING SCHEDULED MAINTENANCE THE FS 280.0 FLOOR TRAVERSE BEAM WAS FOUND CRACKED AND CORRODED. THE FS 280.0 FLOOR TRAVERSE BEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POST — CRACKED (FUSELAGE) · airframe 16,784 hrs · 17,444 cycles

DURING SCHEDULED MAINTENANCE FS409+128 RBL 18 AND LBL POST WERE CRACKED. REPAIRS WERE MADE. INSPECTION AND REPAIRS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — CORRODED (LT WING) · airframe 167,484 hrs · 17,444 cycles

DURING SCHEDULED MAINTENANCE LEFT WING LOWER PLANK ACCESS HOLE (540BB) WAS PITTED. REPAIRS WERE MADE. INSPECTION AND REPAIRS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TRIM SWITCH — DIRTY (COCKPIT) · airframe 16,579 hrs · 17,246 cycles

CREW REPORTED STAB TRIM CAS MESSAGE OCCURRED REPEATEDLY AFTER TAKEOFF FROM CVG. CREW RETURNED TO CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, CLEANED FIRST OFFICER’S STAB TRIM DISCONNECT SWITCH AND PERFORMED CHECKS USING AIRCRAFT MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 15,162 hrs · 15,845 cycles

DURING SCHEDULED MAINTENANCE DAMAGE WAS FOUND FROM FS605 TO FS621 SKIN. DAMAGE WAS REPAIRED USING AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,162 hrs · 15,845 cycles

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

Part: OIL SYSTEM — LOW (APU) · airframe 12,988 hrs · 13,606 cycles

CREW REPORTED AN APU OIL TEMP AMBER MESSAGE DURING CRUISE EN ROUTE FROM CLT TO XNA. AIRCRAFT DIVERTED TO BNA BECAUSE THE RT ENGINE INTEGRATED DRIVE GENERATOR (IDG) WAS ALREADY DEFERRED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE APU OIL LEVEL AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FAN BLADE — DAMAGED (LT ENGINE) · airframe 12,262 hrs · 12,787 cycles

CREW REPORTED, INGESTED SMALL BIRD(S) IN LEFT ENGINE. AIRCRAFT RETURNED TO DAY WITHOUT INCIDENT. MAINTENANCE INSPECTED LT ENGINE PER THE MANUFACTURER MAINTENANCE MANUAL AND REPLACE FAN BLADES. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 11,172 hrs · 11,656 cycles

CREW REPORTED 10 MIN AFTER T/O AUTO XFLOW INHIBIT WHITE STATUS MSG APPEARED AND THE FUEL QTY INDICATORS LEFT SIDE AS WELL AS TOTAL FUEL WERE BLANK W/AMBER DASHES. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE DEFERRED SYSTEM PER MEL 28-41-01-1. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROBE — FAILED (FUEL TANK) · airframe 11,044 hrs · 11,519 cycles

CREW REPORTED THE FUEL QUANTITY INDICATOR SHOWED DASHES ON LT SIDE AND TOTAL FUEL SYNOPTIC PAGE. AIRCRAFT RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED, AND REPLACED LT NR 6 FUEL QTY PROBE. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: APU — HUNG START · airframe 10,397 hrs · 10,834 cycles

CREW REPORTED ON DESCENT INTO DAY, APU EXPERIENCED A HUNG START. MOMENTS LATER THE CREW TRIED TO START APU AND WAS SUCCESSFUL. BLEED AIR WAS SELECTED TO APU AND A STRONG FUEL SMELL WAS EVIDENT IN COCKPIT AND CABIN. APU WAS SHUTDOWN AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED APU AND APU COMPARTMENT FOR LEAKS. NO LEAKS WERE EVIDENT. NO OTHER DEFECTS WERE NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE. NOTE: RESIDUAL FUEL WAS EVIDENT IN THE APU EXHAUST DRAIN. THIS WAS SUSPECTED TO BE EXCESS FUEL FROM THE HUNG START.

Part: NONE — NONE (NONE) · airframe 9,495 hrs · 9,867 cycles

CREW REPORTED THE PDF SHOWED FLAPS EXTENDED TO 2 DEG UNCOMMANDED AT 30,000FT WITH NO AURAL WARNING AT CRUISE. THE CREW DIVERTED TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND NO DEFECTS. AIRCRAFT WAS RETURNED TO SERVICE. (A)

Part: TIRE — SEPARATED (LT MLG) · airframe 7,499 hrs · 7,667 cycles

CREW REPORTED THE LEFT HAND INBOARD MAIN TIRE TREAD HAD PARTIALLY SEPARATED AND SHREDDED UPON LANDING. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE LEFT HAND FLAP. MAINTENANCE REMOVED AND REPLACED THE LEFT HAND INBOARD MAIN TIRE. MAINTENANCE ISSUED TEMP REPAIR 10861 PER REO 601R-57-52-658 FOR THE FLAP DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — SEPARATED (NLG) · airframe 7,369 hrs · 7,522 cycles

CREW REPORTED THE RIGHT HAND NOSE TIRE TREAD SEPARATED ON TAKEOFF. CREW DECLARED AN EMERGENCY AND CONTINUED ON TO CLT WHERE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CONFIRMED THE RIGHT HAND NOSE TIRE TREAD HAD SEPARATED AND CAUSED DAMAGE TO THE AFT NOSE LANDING GEAR DOOR. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE REMOVED AND REPLACED THE AFT NOSE LANDING GEAR DOOR ALONG WITH REPAIRING ALL DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: IDG — FAILED (NR 1) · airframe 6,076 hrs · 6,156 cycles

CREW REPORTED AN IDG CAS MESSAGE ON TAKEOFF ROLL. CREW REJECTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 IDG IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR SEAL — DIRTY (PAX DOOR) · airframe 4,822 hrs · 4,827 cycles

THE CREW REPORTED THE MAIN CABIN DOOR SQUEALS IN FLIGHT. MAINTENANCE CLEANED AND INSPECTED THE SEAL AND PRESSURE HOLES. NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 4,676 hrs · 4,677 cycles

CREW REPORTED NR 2 IDG AMBER CAS MESSAGE ON TAKEOFF. TAKEOFF WAS ABORTED WITHOUT INCIDENT. MAINTENANCE INSPECTED, SERVICED, OPERATIONALLY AND LEAK CHECKED NR 2 IDG. OPERATIONAL AND LEAK CHECKS BOTH GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SECU — FAILED (NR 2) · airframe 4,648 hrs · 4,645 cycles

DUE TO MULTIPLE PREVIOUS WRITE UPS MAINTENANCE PERFORMED FURTHER TROUBLESHOOTING ON THE SPOILERS. FAULT (FAULT CODE) WAS FOUND RELATING TO THE NR 1 SECU. SECU WAS SWAPPED TO THE NR 2 POSITION. TROUBLE FOLLOWED. NR 2 SECU WAS REMOVED AND REPLACED. OPERATIONAL CHECKS WERE COMPLETED. OPERATIONAL CHECKS GOOD. SYSTEM BYTE CHECKS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 4,376 hrs · 4,347 cycles

DURING TAKEOFF ROLL - TAKEOFF CONFIG WARNING SPOILERS CAME ON. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLIGHT SPOILER SYSTEM. NO FAULTS WERE FOUND AND ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — LIGHTNING STRIKE (RT WING) · airframe 4,079 hrs · 4,035 cycles

AFTER LANDING THE CREW REPORTED THE AIRCRAFT HAD TAKEN A LIGHTNING STRIKE. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. MINOR PITTING DAMAGE WAS FOUND ON THE TOP FUSELAGE AND RIGHT WING. ALL DAMAGE WAS REPAIRED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SHUTOFF VALVE — FAILED (LT WING) · airframe 3,502 hrs · 3,453 cycles

DURING APPROACH THE CREW RECEIVED A WING OVERHEAT WARNING MESSAGE AND AURAL WARNING. FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT 14TH STAGE BLEED AIR SHUTOFF VALVE. THE SYSTEM LEAK AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TARGET — LOOSE (PROX SENSOR) · airframe 3,070 hrs · 3,026 cycles

AFTER TAKEOFF WITH THE GEAR HANDLE SELECTED UP THE GEAR DISAGREE WARNING MESSAGE ILLUMINATED. THE RIGHT MAIN LANDING GEAR DID NOT SHOW LOCKED IN THE UP POSITION. THE CREW FOLLOWED THE QRH, RETURNED TO TYS, AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE FOUND THE RT MLG UPLOCK PROX SENSOR TARGET LOOSE. THE TARGET WAS ADJUSTED AND SECURED IAW CRJ200 AMM 32-61-05. A LANDING GEAR EXTENSION/RETRACTION FUNCTIONAL TEST WAS PERFORMED IAW CRJ 200 AMM 32-30-00-720-801. THE SYSTEM CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: DOOR — OPEN · airframe 2,806 hrs · 2,759 cycles

SHORTLY AFTER TAKEOFF THE CREW REPORTED A LOUD POPPING NOISE NEAR THE NOSE OF THE AIRCRAFT. THE FLIGHT RETURNED TO CLT AND LANDED SAFELY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE EXTERNAL SERVICES PANEL DOOR OPEN AND A HEADSET PLUG ADAPTOR PLUGGED INTO THE AUDIO JACKS. THE ADAPTOR WAS REMOVED. NO DAMAGE WAS FOUND ON THE EXTERNAL SERVICES PANEL OR DOOR. PAINT WAS FOUND SCRATCHED ON AN 8 X 4 AREA OF SKIN AFT OF THE PANEL. THE PAINT DAMAGE WAS WITHIN LIMITS AND TRANSFERRED TO THE DAI LIST. THE DOOR WAS SECURED CLOSED AND THE AIRCRAFT RELEASED FOR SERVICE.

Part: UNKNOWN — UNKNOWN (NLG) · airframe 1,985 hrs · 1,927 cycles

UPON POWER APPLICATION FOR TAKEOFF THE AIRCRAFT VEERED LEFT WITH NO RESPONSE TO RUDDER INPUT. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED THE NOSE LANDING GEAR AND FOUND NO DEFECTS. A HIGH SPEED TAXI WAS PERFORMED WITH THE CREW AND THE PROBLEM COULD NOT BE DUPLICATED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 1,265 hrs · 1,222 cycles

THE CREW OF FLIGHT 2396 REPORTED THAT THE FLAPS FAILED AT ZERO DEGREES ON APPROACH TO BTV. THE CREW DECLARED AN EMERGENCY, PREPPED THE CABIN, AND MADE AN UNEVENTFUL ZERO FLAP APPROACH AND LANDING AT BTV. CONTRACT MAINTENANCE RESET THE FLAP CONTROL UNIT IAW RSSL00-001. THE FLAP SYSTEM OPERATIONALLY CHECKED GOOD. NO DEFECTS WERE NOTED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.