N433JS

Part: BLEED VALVE — FAILED · airframe 19,559 hrs · 17,238 cycles

DURING TAKE OFF, THE CREW RECEIVED A BLEED SHUT OFF VALVE CAS MESSAGE AND ABORTED TAKE OFF. WHILE THE AIRCRAFT WAS CLEARING THE RUNWAY THE MESSAGE CLEARED. THE CREW WAS THEN NOTIFIED THAT THERE WAS TWO PASSENGERS THAT WERE ON THE WRONG FLIGHT AND WANTED TO GET OFF THE PLANE. ONCE THE PLANE WAS BACK AT THE GATE THE CREW FOUND OUT THEY JUST WANTED TO GET OFF THE PLANE BECAUSE OF THE ABORTED TAKE OFF. FLIGHT 4043 WAS THEN CLEARED FOR ANOTHER TAKE OFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 19,171 hrs · 16,931 cycles

DURING TAKEOFF, THE CREW RECEIVED A LEFT HAND GENERATOR AND ECU FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE MESSAGE CLEARED. FLIGHT 4064 WAS THEN CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4064 THEN DEPARTED WITH NO FURTHER INCIDENTS.

Part: PSEU — FAILED · airframe 19,084 hrs · 16,854 cycles

DURING TAKE OFF, THE CREW RECEIVED A PROXY SYSTEM CAS MESSAGE AND A DOOR SWITCH FAIL AND ABORTED TAKE OFF. MAINTENANCE INSPECTED AND RERACKED THE PSEU IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STALL WARNING — MALFUNCTIONED (COCKPIT) · airframe 17,864 hrs · 15,906 cycles

DURING TAKEOFF, THE CREW RECEIVED A PUSHER, SHAKER CAS MESSAGE AND ABORTED TAKEOFF. WINDS WERE GUSTING TO 40 KNOTS. AS THE AIRCRAFT EXITED THE RUNWAY, THE MESSAGE CLEARED. FLIGHT 4083 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND THEN DEPARTED WITH NO FURTHER INCIDENTS.

Part: STALL WARNING — MALFUNCTIONED (COCKPIT) · airframe 17,812 hrs · 15,861 cycles

DURING TAKEOFF, THE CREW RECEIVED A STICK SHAKER FAIL AND ABORTED TAKEOFF. THE WINDS WERE GUSTING TO 18 KNOTS. AS THE AIRCRAFT EXITED THE RUNWAY, THE MESSAGE CLEARED BY ITSELF. THE CREW CALLED MAINTENANCE CONTROL WHO ADVISED THE CREW TO ATTEMPT ANOTHER TAKEOFF. FLIGHT 4028 THEN DEPARTED WITH NO FURTHER INCIDENTS.

Part: SENSOR — MALFUNCTIONED (STALL WARNING) · airframe 17,444 hrs · 15,558 cycles

DURING TAKEOFF, THE CREW RECEIVED AN ANGLE OF ATTACK CAS MESSAGE AND ABORTED TAKEOFF. AS THE AIRCRAFT CLEARED THE RUNWAY THE MESSAGE CLEARED BY ITSELF, THE CONDITIONS WERE EXTREMELY WINDY. FLIGHT 4049 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 17,402 hrs · 15,523 cycles

AT 80 KNOTS THE CREW RECEIVED A PUSHER-SHAKER FAIL CAS MESSAGE AND ABORTED TAKEOFF. AFTER EXITING THE RUNWAY THE MESSAGE CLEARED ITSELF. FLIGHT 4015 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 17,234 hrs · 15,382 cycles

DURING TAKEOFF, THE CREW RECEIVED A PUSHER FAIL CAS MESSAGE AND ABORTED TAKEOFF. AFTER EXITING THE RUNWAY THE MESSAGE CLEARED. FLIGHT 4021 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 17,227 hrs · 15,374 cycles

DURING TAKEOFF, THE CREW RECEIVED A PITOT HEAT FAIL INDICATION AND ABORTED TAKEOFF. AS THE AIRCRAFT CLEARED THE RUNWAY THE INDICATION WENT OUT BY ITSELF. FLIGHT 4055 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4055 THEN DEPARTED WITH NO FURTHER INCIDENTS.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 17,183 hrs · 15,342 cycles

DURING TAKEOFF, THE CREW RECEIVED AN ANGLE OF ATTACK FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE CREW CLEARED THE RUNWAY AND THE INDICATION CLEARED BY ITSELF. THERE WERE WINDY CONDITIONS AT THIS TIME. FLIGHT 4059 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4059 DEPARTED WITH NO FURTHER INCIDENTS.

Part: STICK SHAKER — MALFUNCTIONED (COCKPIT) · airframe 17,175 hrs · 15,336 cycles

DURING TAKEOFF, THE CREW RECEIVED A SHAKER AND PUSHER FAIL MESSAGE AND ABORTED TAKEOFF, THE MESSAGE CLEARED BY ITSELF. THERE WAS CONSIDERABLE WIND GUSTS. FLIGHT 4020 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT AND DEPARTED WITH NO FURTHER INCIDENTS.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 16,921 hrs · 15,120 cycles

DURING TAKEOFF, THE CREW RECEIVED A CHIME AND PUSHER FAIL CAS MESSAGE AND ABORTED TAKEOFF. THE MESSAGE CLEARED BY ITSELF AND FLIGHT 4169 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4169 THEN DEPARTED WITH NO FURTHER INCIDENTS.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 16,911 hrs · 15,107 cycles

DURING THE TAKEOFF, THE CREW RECEIVED A SHAKER AND PUSHER FAIL MESSAGE AND ABORTED TAKEOFF. AS FLIGHT 4023 CLEARED THE RUNWAY THE MESSAGE CLEARED AND FLIGHT 4023 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4023 THEN DEPARTED WITH NO FURTHER INCIDENTS.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 16,766 hrs · 14,973 cycles

DURING THE TAKE ROLL, THE CREW RECEIVED LEFT HAND SHAKER FAIL CAS MESSAGE AND ASSOCIATED AMBER CAS MESSAGES AND ABORTED TAKEOFF. AS THE AIRCRAFT DECELERATED THE INDICATIONS CLEARED. THE CREW CONTACTED MAINTENANCE CONTROL WHO CLEARED THE FLIGHT FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4168 DEPARTED WITH NO FURTHER INCIDENTS.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 15,268 hrs · 13,630 cycles

FLIGHT 4009 BEGAN THE TAKEOFF ROLL AND THE CREW RECEIVED A LEFT HAND ANGLE OF ATTACK FAIL CAS MESSAGE AND A SHAKER FAIL CAS MESSAGE. THE CREW ABORTED TAKEOFF AND CLEARED THE RUNWAY. AFTER FLIGHT 4009 CLEARED THE RUNWAY THE INDICATION EXTINGUISHED. FLIGHT 4009 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT. FLIGHT 4009 DEPARTED WITHOUT ANY FURTHER INCIDENTS.

Part: CONTROL UNIT — FAILED (ALTERNATOR) · airframe 14,581 hrs · 13,035 cycles

THE CREW RECEIVED A RIGHT HAND ALTERNATOR FAIL CAS MESSAGE AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE ALTERNATOR CONTROL UNIT IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 24-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — DIRTY (EECU) · airframe 14,409 hrs · 12,899 cycles

DURING TAKEOFF, THE CREW RECEIVED A RIGHT HAND ELECTRONIC CONTROL UNIT AND RIGHT HAND ALTERNATING CURRENT VOLT FAIL MESSAGES AND ABORTED THE TAKEOFF. THE CREW CONSULTED THE QUICK REFERENCE HANDBOOK AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND CLEANED THE ELECTRONIC CONTROL UNIT CANNON PLUG IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 73-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT)

FLT 4008 - DAY - AFTER TAKING THE RUNWAY, RECEIVED STANDBY PITOT HEAT FAIL CAS MESSAGE. THE AIRCRAFT TAXIED BCK TO THE GATE AND MAINTENANCE RESET THE CIRCUIT BREAKER AND THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT. (M)

Part: COVER — LEAKING (RT ENGINE) · airframe 12,427 hrs · 11,278 cycles

WHILE CLIMBING OUT OF PHILADELPHIA, THE RIGHT HAND ENGINE OIL STARTED TO FLUCTUATE IN THE NORMAL RANGE. CONTINUING ON TO KNOXVILLE, THE OIL PRESSURE STARTED TO FLUCTUATE IN THE AMBER RANGE. THE CREW DECLARED AN EMERGENCY AND DIVERTED TO WASHINGTON NATIONAL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TORQUED THE FRONT INLET CASE COVER IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 72-10-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PCU — LEAKING (RT PROPELLER) · airframe 12,427 hrs · 11,278 cycles

WHILE ON APPROACH, THE CREW DECLARED AN EMERGENCY DUE TO LOW AND FLUCTUATING OIL PRESSURE ON THE RIGHT HAND ENGINE. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND PITCH CONTROL UNIT QAD IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BATTERY — DISCHARGED (ROW 4 & 6)

A SECTION OF EMERGENCY FLOOR LIGHTING AT ROWS FOUR AND SIX WAS NOTED TO BE INOPERATIVE DURING THE PRE-FLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT BATTERY AT POSITION 5LK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-00. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (BS 564)

A GASH IN THE FUSELAGE, STATION 564, WAS FOUND BY THE CREW DURING THE POST FLIGHT INSPECTION. MAINTENANCE INSPECTED AND REPAIRED THE DAMAGE IN ACCORDANCE WITH DORNIER SRM 53-00-11 AND 53-22-00.

Part: PIN — NOT REMOVED (RT MLG)

AFTER TAKEOFF, THE RIGHT HAND MAIN LANDING GEAR FAILED TO RETRACT WHEN SELECTED. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO THE FIELD AND LANDED. MAINTENANCE INSPECTED AND FOUND A GEAR SAFETY PIN INSTALLED ON THE GEAR LEG. MAINTENANCE REMOVED THE GEAR PIN AND RETURNED THE AIRCRAFT TO SERVICE.

Part: CONNECTOR — DIRTY (RT PROP GOV)

THE RIGHT HAND PROPELLER OVERSPEED TEST FAILED TO FUNCTION WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND CLEANED THE OVERSPEED GOVERNOR CANNON PLUG. OPERATIONAL CHECKS WERE COMPLETED, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-04.

Part: POWER LEVER — LACK OF LUBE (LEFT)

THE LEFT HAND POWER LEVER WOULD NOT ADVANCE PAST THE FLIGHT IDLE POSITION WHEN THE TAKEOFF WAS ATTEMPTED. THE TAKEOFF WAS ABORTED, AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND LUBRICATED THE LEFT HAND POWER LEVER FLIGHT IDLE DETENT, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 76-11-11. FUNCTION CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SELECTOR — FAILED (FLIGHT DECK)

THE LANDING GEAR FAILED TO EXTEND WHEN SELECTED, DURING THE APPROACH. THE CREW FOLLOWED THE CHECK LIST AND MANUALLY PUMPED THE LANDING GEAR DOWN. A NORMAL LANDING WAS PERFORMED WITHOUT FURTHER INCIDENT. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT FOR REPAIR. THE FERRY WAS COMPLETED WITHOUT ANY PROBLEMS. PIT MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR SELECTOR HANDLE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 32-31-01. OPERATIONAL CHECKS WERE COMPLETED.

Part: WIRE — BROKEN (RT ENGINE)

DURING THE TAXI FOR TAKEOFF, THE RIGHT HAND PROPELLER OVERSPEED TEST FAILED TO OPERATE WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REPAIRED BROKEN WIRES AT THE OVERSPEED GOVERNOR CANNON PLUG CONNECTOR, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 61-21-04. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — FAILED (CABIN)

DURING THE PRE-FLIGHT INSPECTION, THE FLOOR PATHWAY EMERGENCY LIGHTING AT ROWS FIVE AND SIX WERE NOTED TO BE INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND BATTERY FOR THE AFFECTED LIGHTS. OPERATIONAL CHECKS WERE COMPLETED IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER LEVER — LACK OF LUBE (COCKPIT)

WHEN THE POWER LEVERS WERE ADVANCED FOR TAKEOFF, THE RIGHT HAND POWER LEVER WOULD NOT MOVE PAST THE FLIGHT IDLE POSITION. THE AIRCRAFT ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND LUBED THE RIGHT HAND POWER LEVER FLIGHT IDLE LOCK GATE, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 76-11-21. NO OTHER DEFECTS WERE NOTED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING THE PRE-FLIGHT INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS 4,5, AND SIX WERE NOTED TO BE INOPERATIVE. OUTSTATION MAINTENANCE INSPECTED AND APPROVED THE AIRCRAFT FOR A FERRY FLIGHT TO PIT. THE FERRY FLIGHT TOOK PLACE WITHOUT ANY FURTHER PROBLEMS. PIT MAINTENANCE INSPECTED AND REPLACED THE 5LK BATTERY PACK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER LEVER — LACK OF LUBE (LEFT)

WHEN THE AIRCRAFT TOOK THE ACTIVE RUNWAY, THE CREW ADVANCED THE POWER LEVERS FOR TAKEOFF. THE LEFT POWER LEVER WOULD NOT ADVANCE PAST THE FLIGHT IDLE DETENT. THE AIRCRAFT RETURNED TO THE GATE. OUTSTATION MAINTENANCE INSPECTED AND LUBED THE LEFT POWER LEVER RELEASE AND LOCK SYSTEM. OPERATIONAL CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING ENGINE START PRIOR TO TAKEOFF, SEVERAL EMERGENCY FLOOR LIGHTS WERE NOTED TO BE INOPERATIVE. MAINTENANCE WAS CALLED OUT TO TROUBLESHOOT THE PROBLEM. MAINTENANCE INSPECTED AND REPLACED THE 5LK EMERGENCY POWER PACK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATIONAL CHECKS WERE COMPLETED.

Part: GATE LOCK — LACK OF LUBE (LT POWER LEVER)

THE LEFT HAND POWER LEVER WOULD NOT MOVE PAST THE FLIGHT IDLE POSITION WHEN SELECTED, DURING THE TAKEOFF. THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND LUBRICATED THE POWER GATE LOCK, IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 76-11-04. OPERATION CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

DURING THE ENGINE START UP, THE EMERGENCY FLOOR LIGHTS WERE NOTED TO BE INOPERATIVE. OUTSTATION MAINTENANCE INSPECTED THE AIRCRAFT, AND APPROVED IT FOR A FERRY FLIGHT TO OUR CAK MAINTENANCE BASE. THE FERRY WAS CARRIED OUT WITHOUT ANY PROBLEMS. CAK MAINTENANCE INSPECTED AND REPLACED THE EMERGENCY BATTERY PACK , IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 33-51-01. OPERATION CHECKS WERE COMPLETED, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: POWER LEVER — LACK OF LUBE (LEFT)

DURING TAXI PRIOR TO TAKEOFF, THE LEFT HAND POWER LEVER WOULD NOT ADVANCE ABOVE THE FLIGHT IDLE POSITION, WHEN SELECTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED AND LUBRICATED THE POWER LEVER CONTROL LOCK GATE IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 76-11-06. OPERATION CHECKS WERE SATISFACTORY, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: CIRCUIT BREAKER — TRIPPED (PROP OVERSPEED)

DURING TAXI, THE CREW ATTEMPTED A PROP OVERSPEED TEST. THE TEST FAILED, AND THE AIRCRAFT RETURNED TO THE GATE . PIT MAINTENANCE INSPECTED AND RESET THE OVERSPEED CIRCUT BREAKER. OPERATION CHECKS WERE COMPLIED WITH IN ACCORDANCE WITH DORNIER MAINTENANCE MANUAL 71-01-00, AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — FAILED (RT MLG BRAKE)

DURING TAXI, THE CREW NOTED A BRAKE TEMPERATURE WARNING INDICATION FOR THE RT OUTBOARD BRAKE. THE ACFT RETURNED TO THE GATE. MX INSPECTED AND FOUND THE BRAKE TEMPERATURE TO BE WITHIN NORMAL LIMITS FOR SERVICE. MX IN TYS, DEFERRED THE RT BRAKE TEMPERATURE INDICATION, IAW THE DORNIER 328 MINIMUM EQUIPMENT LIST. THE ACFT WAS RETURNED TO SERVICE. LATER WHEN THE ACFT ARRIVED IN PIT ON 17 DEC 97 , MX INSPECTED AND REPLACED THE RT INBOARD BRAKE TEMP SENSOR, IAW DORNIER MM 32-42-09. THE DEFERRAL WAS REMOVED, AND THE ACFT WAS RETURNED TO SERVICE.

Part: CONTROL UNIT — FAILED (RT MLG)

DURING TAXI FOR T/O, NOTED UNUSUAL VIBRATION FROM THE RT MLG. CREW NOTED THAT WITH THE ANTI SKID SYSTEM DE-SELECTED, VIBRATIONS WOULD CEASE. THE A/C RETURNED TO THE GATE. MX CLEANED AND INSPECTED THE RT WHEEL SPEED TRANSDUCER AND RE-RACKED THE ANTI- SKID CONTROL UNIT, IAW DORNIER MM 32-42-13 AND 32-42-11. THE FUNCTION CHECK WAS UNSATISFACTORY. A/C WAS ISSUED A FERRY FLT PERMIT TO PIT. PIT MX, INSPECTED AND REPLACED THE BRAKE METERING CONTROL UNIT, IAW DORNIER MM 32-42-03. OPS AND LEAK CHECKS WERE COMPLETED, AND THE A/C WAS RETURNED TO SERVICE.

Part: DE-ICE VALVE — FAILED (LT ENGINE)

LEFT ENGINE DE-ICE FAILED, AIRCRAFT RETURNED TO THE FIELD WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE EJECTOR FLOW CONTROL VALVE, OPERATIONAL CHECKED GOOD.

Part: SELECTOR VALVE — FAILED (PARKING BRAKE)

PARKING BRAKE ACCUMULATOR PRESSURE LOW CAS MESSAGE CAME ON INFLIGHT. LANDED AT NEAREST SUITABLE AIRPORT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY PARK BRAKE SELECTOR VALVE, OPERATIONAL CHECKED GOOD.

Part: INTAKE DE-ICE — INOPERATIVE (RT ENGINE)

RT INTAKE DE-ICE INOP. DIVERTED TO CLT DUE TO ICING CONDITIONS. MAINTENANCE CYCLED THE NR 1 IAC CIRCUIT BREAKER, OPERATIONAL CHECK GOOD.

Part: FUEL PRESS WARN — ACTIVATED (COCKPIT)

CREW ABORTED TAKEOFF AFTER BEING ALERTED BY A FUEL LOW PRESSURE CAS MESSAGE. AIRCRAFT RETURNED TO THE TAXI WAY. CREW CLEARED THE CAS MESSAGE, CONDUCTED ENGINE FULL POWER CHECKS IAW AFM, CAS MESSAGE DID NOT ILLUMINATE. ALL SYSTEMS CHECKED GOOD CREW CONTINUED ON WITH THE FLIGHT.

Part: RELAY — DEFECTIVE (LT AVIONIC RACK)

SHORTLY AFTER CLIMBOUT, RECEIVED AN AMBER CAS MESSAGE PAK OVERHEAT ASSOCIATED WITH A SWEET SMELL IN THE CABIN. AIRCRAFT DIVERTED TO PIT WHERE MX REPLACED THE LEFT BLEED SHUT OFF VALVE TIME DELAY RELAY IAW MM 31-14-00. GROUND CHECKED GOOD.

Part: BULB — DEFECTIVE (GEAR HANDLE)

FLT 4149 - ON APPROACH AFTER LANDING GEAR WAS SELECTED 'DOWN', CREW REPORTED 'NO' DOWN AND LOCKED INDICATION FOR THE LEFT MAIN GEAR. CREW CONDUCTED A TOWER FLY-BY TO CONFIRM A GEAR DOWN CONDITION. ATC DECLARED AN EMERGENCY, EQUIPMENT ROLLED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. OUT STATION MAINTENANCE REPLACED BULBS IN THE LANDING GEAR POSITION INDICATOR IAW MM 32-00-00. GROUND CHECK 'GOOD'. AIRCRAFT RETURNED TO SERVICE. (X)

Part: WINDSHIELD — DAMAGED (LT COCKPIT)

FLT 4045 - CAPTAIN'S WINDSHIELD (OUTER PANE) CRACKED DURING DESCENT INTO PIT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MX REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-11-00. GROUND CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE.

Part: BRK TEMP SENSOR — DEFECTIVE (MLG BRAKES)

FLT 4166 - CREW REPORTED A BRAKE OVER TEMP IN-FLIGHT. CREW ADVISED TO RETURN TO FIELD. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. PIT MAINTENANCE REPLACED LT BRAKE TEMPERATURE SENSOR IAW MM 32-42-09. GROUND CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: HP FUEL PUMP — CONTAMINATED (RT ENGINE)

PHL/CVG - FLT 4010 - EN ROUTE, APPROXIMATELY 80 MILES EAST OF CVG, FLIGHT CREW WAS ALERTED BY A FUEL FILTER BYPASS CAS MESSAGE. CREW WAS ADVISED TO DIVERT TO DAY. AIRCRAFT LANDED IN DAY WITHOUT FURTHER INCIDENT. DAY MAINTENANCE INSPECTED THE RT ENGINE HP FUEL PUMP FILTER AND FOUND IT WAS CONTAMINATED. DAY MAINTENANCE REMOVED AND REPLACED HP FUEL PUMP FILTER AND FOUND IT WAS CONTAMINATED. DAY MAINTENANCE REMOVED AND REPLACED RT ENGINE HP FUEL PUMP IAW MM 73-11-03. GROUND RUNS CHECKED GOOD, AIRCRAFT RETURNED TO SERVICE. (X)

Part: TQ CONNECTORS — DIRTY (LT ENGINE)

FLT 1002 - CREW ELECTED TO RETURN TO FIELD AFTER EXPERIENCING TORQUE FLUX, LT ENGINE. SHUT DOWN LT ENGINE, AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED CONNECTORS ON NP AND TQ SENSORS IAW STANDARD MAINTENANCE PRACTICES. GROUND CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.