N284QS

Part: INVERTER — FAULTY (ELECTRICAL SYS) · airframe 12,399 hrs · 7,694 cycles

FA SMELLED A FIRE SMELL IN CABIN. GOT UP TO CHECK AND SMELLED SOMETHING HOT. UPON RETURNING TO COCKPIT NOTICED THE CAB AC MASTER CIRCUIT BREAKER HAD POPPED. OVEN WAS OFF AND PASSENGERS WERE NOT USING AC OUTLETS. REMOVED AND REPLACED STATIC INVERTER IAW MM 24-00-00. REMOVED 28VDC INVERTER PN SS120 SN 1456.

Part: SKIN — CORRODED (WING) · airframe 11,935 hrs · 7,383 cycles

DURING VISUAL INSPECTION, FOUND CORROSION ON THE WING SKIN BETWEEN RIBS 1A AND 1B. BLENDED AREA . COMPLIED WITH PATCH REPAIR INSTALLATION ON THE UPPER WING SKIN BETWEEN RIB 1A AND RIB 1B.

Part: MOTOR — FAILED (WINDSHIELD WIPER) · airframe 9,939 hrs · 6,156 cycles

SETTING SWITCH TO OFF WOULD NOT STOW WIPER. SHORTLY AFTER RECEIVED A STRANGE ODOR. 30 SECONDS LATER ODOR BECAME ELECTRICAL BURNING AND INCREASING IN INTENSITY. REMOVED FIRST OFFICER'S WINDSHIELD WIPER MOTOR AND INSTALLED A NEW WIPER MOTOR IAW MM 30-43-05-900-801. OPS CHECKED GOOD.

Part: BRAKE SYS — UNKNOWN (MLG) · airframe 9,906 hrs · 6,139 cycles

BRAKES AT SLOW SPEED TAXI & HIGH SPEED TAXI ARE LOCKING UP & PULLING TO THE RIGHT. JACKED STRUT & CHECKED FREEDOM OF WHEEL MOVEMENT, FOUND ACTION NORMAL. CHECKED TIRES FOR ANY EVIDENCE OF FLAT SPOTS, NONE NOTED. COMPLIED WITH TAXI CHECK, TAXI CHECKED NORMAL, NO PULLING NOTED. CHECKED FAULT HISTORY, NO HISTORY, NO HISTORY FOUND IN PRECEDING 6 MONTHS. NO FURTHER ACTION TAKEN. WORK PERFORMED IAW AMM 32-00.

Part: MOTOR — FAILED (WINDSHEILD WIPER) · airframe 7,454 hrs · 4,606 cycles

DURING ARRIVAL, DETECTED AN ELECRICAL ODOR OF SMOKE IN COCKPIT. POSSIBLY DUE TO CO-PILOT'S WINDSHIELD WIPER STICKING IN UP POSITION. REPLACED WINDSHIELD WIPER MOTOER IAW MM 24-000, 30-402, 30-407 34-003.

Part: BRAKE SYS — MALFUNCTIONED (MLG) · airframe 6,692 hrs · 4,159 cycles

WHILE AT A SLOW TAXI AFTER LANDING WITH BRAKE PRESSURE APPLIED, THE BRAKE PRESSURE SEEMS TO RELEASE TEMPORARILY. NO BREAK MONELCOS TRIPPED. BLED ALL BRAKES TO ENSURE SYS IS FREE OF AIR. TAXIED ACFT BEFORE AND AFTER BLEEDING BRAKES ALL OPS CHECKS GOOD. WORK PERFORMED IAW MM CHP 32-419. REF FAS W/O NR10-054.

Part: SERVO VALVE — INOPERATIVE (MLG BRAKES) · airframe 6,562 hrs · 4,077 cycles

BRAKES GRAB, BOTH LEFT & RIGHT. REMOVED AND REPLACED LEAKING NR1 LT BRAKE SERVO VALVE WITH REPAIRED VALVE IAW W/C 32-418. BLED BRAKES IAW W/C 32-419. OPS TEST GOOD. CREW TAXIED ACFT. BRAKING REPORTED TO BE NORMAL. FOR DETAILS REF FAS WO 09-2945.

Part: ACTUATOR — INOPERATIVE · airframe 5,565 hrs · 3,419 cycles

NORMAL TRIM SYS FAILED INFLIGHT AND WOULD NOT RE-ENGAGE, (ELEVATOR). REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR WITH A REPAIRED/MODIFIED ASSEMBLY PER MM W/C 27-406, 27-404.

Part: UNKNOWN — MULTIPLE FAIL (STAB CONTROL) · airframe 5,525 hrs · 3,398 cycles

DURING DESCENT, AP TRIM FAIL LIGHT ILLUMINATED WITH ASSOCIATED AMBER CAS MESSAGE. REPLACED STAB CONTROL RELAYS- 504CH, 505CH, 506CH & 507CH. REPLACED STAB CONTROL PCB'S 502CH & 503CH. OPS CHECKED STAB CONTROL RELAY BOX DUE TO RELAY AND PCB REPLACEMENT. INSPECTED HORIZONTAL STAB CONTROL BUSS. ALL ABOVE WORK ACCOMPLISHED PER MM 27-405-OPS CHECK GOOD.INSPECTED PILOT AND CO-PILOT TRIM SWITCHES IAW WDM27-41-00-CHECKED GOOD. PERFORMED AUTO-PILOT TRIM OPERATIONAL CHECK PER MM 22-100- OPS CHECK GOOD.

Part: TRIM SYSTEM — MALFUNCTIONED · airframe 5,525 hrs · 3,398 cycles

DURING DESCENT AP TRIM FAIL LIGHT ILLUMINATED WITH ASSOCIATED AMBER (E).

Part: CIRCUIT BOARD — DAMAGED (MLG) · airframe 5,360 hrs · 3,301 cycles

BRAKES DO NOT WORK PROGRESSIVELY. THEY GRAB OR RELEASE SUDDENLY WHEN PRESSED OR RELEASED. INSPECTED ALL GEAR UPLOCK SWITCHES WIRING, NO DEFECTS NOTED. CHECKED UPLOCK SWITCHES ADJUSTMENTS AND GEAR UPLOCK LINKAGE, NO DEFECTS NOTED. REPLACED LANDING GEAR CONTROL PCB (A162) WITH NEW PCB (A162). CYCLED LANDING GEAR NUMEROUS TIMES, OPS CHECK GOOD. VERIFIED THAT RED TRANSIT LIGHT EXTINGUISHES AFTER CYCLE. ALL WORK IAW 400XP WDM 32-31-01 AND 400XP MM 32-20-00, 32-30-00.

Part: BRAKE — MALFUNCTIONED (MLG) · airframe 4,912 hrs · 3,031 cycles

WHEN MAIN A/C BRAKES ARE APPLIED BRAKES WILL GRAB THEN RELEASE, THEN GRAB WHILE BRAKES ARE APPLIED SMOOTHLY. [07-23-07] PERFORMED BRAKE PRESSURE CHECKS AND FOUND NO ABNORMAL PRESSURES. IAW F2000 MM 32-412. FOUND FAULT CODES FOR BSCU NR 1 AND 2 AND FOUND CODE 335 AND 435. REMOVED (DEFECTIVE) 4 EACH WHEEL GENERATOR SLEEVES P/N A35005, INSTALLED 4 EACH NEW GENERATOR SLEEVES P/N A35005 IAW 32-415 OPERATIONAL CHECK GOOD.

Part: TRANSDUCER — MALFUNCTIONED (WHEEL SPEED) · airframe 4,825 hrs · 2,965 cycles

WHEN BRAKING AT LOW TAXI SPEEDS THE LT BRAKE RELEASES AND THE AIRCRAFT WILL PULL TO THE RT. PERFORMED FUNCTIONAL CHECK OF ANTI-SKID SYSTEM, BOTH CHANNELS AND BOTH SYSTEMS ARE WORKING IAW M/M 32-414 CHECKED WIRING FROM BOTH BSCU'S TO ALL TRANDUCERS AND SERVO VALVES WITH NO DEFECTS NOTED. CLEARED ALL FAULT SFROM AIRCRAFT COMPUTERS AND EICAS DISPLAYS AND RESET ALL MINELCOS. REMOVED NR1 AND NR2 WHEEL SPEED TRANSDUCERS AND OPS CHECKED ANTI-SKID SYSTEM GOOD IAW MM 32-414.

Part: CONTROL UNIT — INTERMITTENT (BRAKE SYSTEM) · airframe 4,808 hrs · 2,955 cycles

WHEN BRAKING THE AIRCRAFT TO A FULL STOP AT LOW TAXI SPEEDS, LT BRAKE RELEASED AS PRESSURE ON THE BRAKE PEDALS IS LESSENED TO PREVENT NOSE DIP. IS MOST PRONOUNCED WHEN PARKING OR HOLDING SHORT. REMOVED OLD NR 2 BSCU AND REPLACED WITH REPAIRED UNIT. OPERATIONAL TEST PASSED IAW CH 32-446 OF THE F-2000 MM. ALL WORK PERFORMED IAW CH'S 45-001, 29-000, 24-000, AND 29-112 OF THE F-2000 MM.

Part: UNKNOWN — UNKNOWN (DOOR) · airframe 4,571 hrs · 2,807 cycles

RED DOOR MASTER WARNING CAME ON JUST PRIOR TO V1- ABORTED TAKEOFF AND LIGHT WENT OUT WHILE DECELERATING. ADJUSTED BAGGAGE DOOR MICRO SWITCHES 43MW & 47 MW IN ACCORDANCE WITH F2000 MM 52-700. OPERATIONAL CHECK GOOD.

Part: HMU — FLUCTUATES (NR 2 ENGINE) · airframe 4,396 hrs · 2,701 cycles

ENROUTE FROM EGE TO SNA THE (FUEL 2) LIGHT ILLUMINATED. THE LOW BOOSTER PUMP PRESSURE CHECKLIST WAS APPLIED THE LIGHT REMAINED ILLUMINATED. DUE TO NO INDICATION OF A FUEL LEAKS AND NO CHECKLIST REQUIREMENT TO LAND IMMEDIATELY THE FLIGHT WAS CONTINUED. APPROXIMATELY 15 MINUTES LATER THE NR 2 ENGINE IGNITION LIGHT BEGAN TO ILLUMINATE INTERMITTENTLY. DURING IGNITION ILLUMINATION THE NR 2. N2 WOULD FLUCTUATE FROM 99.1 TO 100.4 WITH MILD AIRFRAME BUFFET. DURING THE ENGINE IGNITION CYCLE THE NR 2 ENGINE REMAINED ON THE (A) CHANNEL. LATER YET, THE NR 2 ENGINE FUEL FLOW INDICATOR WENT TO (0), WITH ALL OTHER ENGINE INDICATIONS NORMAL. SHORTLY THEREAFTER THE NR 2 ENGINE POWER BEGAN TO ROLL BACK AND FORTH WITHOUT PILOT

Part: POSITION SWITCH — MALFUNCTIONED (MLG) · airframe 2,992 hrs · 1,847 cycles

AFTER TAKEOFF GEAR HANDLE WAS SELECTED UP, GEAR STARTED TO RETRACT WITH THREE RED LIGHTS, GEAR THEN STOPPED INTRANSIT WITH MAIN GEAR RED AND GREENS SEEN AND GEAR HANDLE FLASHING. AFTER SELECTING GEAR DOWN, GEAR WENT DOWN NORMALLY. TROUBLESHOT FOR LANDING GEAR FAILURE TO RETRACT NORMALLY INTERFACED WITH AIRFRAME SYSTEM COMPUTERS AND FOUND NO FAULTS, OPERATIONALLY TESTED LANDING GEAR SEVERAL TIMES WITH NO FAULTS. AT THE OPERATOR REQUEST THE MLG DOOR ACTUATOR PROXIMITY SWITCHES, LEFT P/N 803602, S/N 1391, RIGHT P/N 803682, S/N 1243 WERE REPLACED WITH NEW SWITCHES OF SAME P/N, LEFT S/N 1224, RIGHT 1220 IN ACCORDANCE WITH FALCON 2000 MM 32-811. PERFORMED MLG OPERATIONAL CHECK AND FOUND T/O OPS CHECK NORMAL.

Part: PCB — INOPERATIVE (MLG) · airframe 2,983 hrs · 1,841 cycles

UPON GEAR EXTENSION, GOT THE FOLLOWING INDICATIONS, THE 3 RED LIGHTS NO GREEN THE EXTENSION PROCESS THEN STOPPED. HEARD A CLICKING SOUND COMING FROM BEHIND US. JUST AS THE GEAR HANDLE STARTED FLASHING THE EXTENSION PROCESS FINISHED. REMOVED PCB 10GW AND INSTALLED SERVICEABLE PCB 10 GW PERFORMED FULL FUNCTIONAL EXTEND/RETRACT TEST OF L/G AND DOORS NUMEROUS TIMES. OPS CHECK GOOD IAW DASSAULT F2000 M/M 32-300.

Part: WARNING LIGHT — ILLUMINATED (RT BRAKES) · airframe 2,389 hrs · 1,451 cycles

ON TAXI OUT AMBER BRAKE LIGHT ILLUMINATED AND RT BRAKE MINELCO TRIPPED. COMPUTER SHOWS CODE 424 RIGHT PEDAL SWITCH. ITEM IS UNDER INVESTIGATION.