N275QS

ATA 3240

Part: PRESSURE SWITCH — LEAKING (PARKING BRAKE) · airframe 8,790 hrs · 5,456 cycles

AFTER TAKEOFF, MASTER CAUTION WITH PUMP HYD NR 2 ANNUNCIATOR ILLUMINATED. HYD NR 2 PSI CYCLED BETWEEN 1600/1800. RAN CHECKLIST RETURNS TO DEPARTURE UNEVENTFULLY- NOTED LOSS OF FLUID ON RAMP. REMOVED PARKING BRAKE PRESSURE SWITCH AND INSTALLED NEW PRESSURE SWITCH IAW MM 32-45-01 BLEED BRAKES LEAK AND OPS CHECK GOOD ALL WORK DONE IAW MM 32-419

ATA 2780

Part: WARNING LIGHT — ILLUMINATED (AUTO SLATS) · airframe 8,546 hrs · 5,294 cycles

ON TAKE OFF APPROX 2 SECONDS AFTER BRINGING THE THROTTLES TO TAKE OFF THE "AUTO SLATS" LIGHT ILLUMINATED. ABORTED TAKEOFF.

ATA 3417

Part: ADC — INOPERATIVE (NR 1) · airframe 8,546 hrs · 5,294 cycles

ON TAKEOFF APPROX 2 SECONDS AFTER BRINGING THE THROTTLES TO TAKEOFF THE "AUTO SLATS" LIGHT ILLUMINATED. REPLACED THE NR 1 AIR DATA COMPUTER WITH OVERHAULED UNIT IAW MM PROC 34-007. OPS AND LEAK CHECK WAS GOOD. REF FAS WO NR 08-3137. AND SLAT OPS CHECK IAW MM PROC 27-803 WAS GOOD.

ATA 2700

Part: UNKNOWN — UNKNOWN · airframe 8,543 hrs · 5,291 cycles

ACFT WAS DESCENDING THROUGH FL 380 WHEN FLYING PILOT MOMENTARILY LOST PITCH CONTROL.

ATA 5220

Part: LANYARD — MISSING (EMERGENCY WINDOW)

ACCESS COVER FOR THE EMERGENCY WINDOW HANDLE DOES NOT HAVE A LANYARD WHEN IT IS REMOVED. THE COVER HANGS BY THE WIRING THAT ILLUMINATES IT PUTTING STRESS ON THE SOLDERED CONNECTIONS TO BREAK CAUSING EITHER AN INOPERATIVE EMERGENCY LIGHT OR A SHORT CAUSING MORE THAN ONE EMERGENCY LIGHT TO NOT ILLUMINATE. THIS COVER IS REMOVED ROUTINELY FOR SECURITY PINNING OF THE EXIT HANDLE AND FOR EMERGENCY WINDOW HANDLE INSPECTION. THERE SHOULD BE A LANYARD TO PROVIDE STRESS RELIEF FOR THE ASSOCIATED WIRING MOUNTED ON THE COVER AND IN THE WINDOW ASSY. (K)

ATA 3417

Part: ADC — MALFUNCTIONED (NR 1) · airframe 7,938 hrs · 4,912 cycles

DURING TAKEOFF, TEN SECONDS AFTER FULL POWER WAS SET (AUTO SLATS) MESSAGE APPEARED. REPLACED ADC-850C AIR DATA COMPUTER NR 1 WITH AN OVERHAULED UNIT PER F2000 MM 34-103. COMPLETED LEAK CHECKS PER F2000 MM 34-100 & FAR 91.411 WITH NO LEAKS NOTED. OPS CHECKED GOOD PER F2000 MM 34-104. ASSISTED BY PRECISION STATIC TESTING CRS NO. QJAR856X REF. WO 4115. TRANSPONDER INTEGRATION CHECK GOOD PER FAR 43 APP F PARA B

ATA 3200

Part: UNKNOWN — UNKNOWN (MLG) · airframe 7,319 hrs · 4,524 cycles

BIRD STRIKE ON NOSE GEAR IMPROPER RETRACTION CYCLE EVENTUALLY DID RETRACT. JACKED AIRCRAFT AND INSPECTED NOSE GEAR AREA FOR DAMAGE DUE FROM BIRD STRIKE. NO DAMAGE WAS FOUND. APPLIED POWER TO AIRCRAFT AND CYCLED LANDING GEAR SEVERAL TIMES TO CHECK FOR PROPER OPERATION. GEAR OPS CHECK CHECKED GOOD. PERFORMED A VISUAL INSPECTION AROUND AIRCRAFT STRUCTURE, FLIGHT CONTROLS AND ENGINE INTAKES WITH NO DEFECTS NOTED. WORK DONE IAW DASSAULT FALCON 2000 MM CHAPTER 32-300, 05-102 AND 32-214.

ATA 3220

Part: LANDING GEAR — NOISY (NOSE) · airframe 7,172 hrs · 4,427 cycles

ON TAKEOFF GEAR RETRACTION, LOUD NOISE HEARD FROM NOSE AREA LIKE GEAR DOOR NOT CATCHING OR BINDING SHOOK NOSE OF AIRPLANE. ON GEAR EXTENSION LOUD NOISE THIS TIME GRINDING SOUND LIKE WHEN TWO GEARS NOT MESHING TOGETHER RIGHT. POSITIONED AIRCRAFT IN HANGAR. INSPECTED GEAR, GEAR DOORS NOSE CONE. NO DEFECTS NOTED. PERFORMED NUMEROUS GEAR SWINGS. NO DEFECTS NOTED. INSPECTED NOSE WHEEL WELL ACCESS PANEL SEAL. FOUND SEAL WORN.REMOVED OLD SEAL P/N FGFB291600003 FROM WHEEL WELL ACCESS PANEL AND CLEANED PANEL. NOTE ALL WORK DONE IAW F-2000 M/M CH 52-40-00-3/11/07.

ATA 5312

Part: SEAL — WORN (NLG WW PANEL) · airframe 7,163 hrs · 4,419 cycles

LOUD GRINDING NOISE DURING GEAR DOWN CYCLE. DURING CYCLE, 20 SECOND WARNING LIGHT STARTED FLASHING. 3 GREEN/ NO RED WAS INDICATED APPROXIMATELY 10 SECONDS AFTER 20 SECOND WARNING FLASHER. INSPECTED MLG, MLG DOORS NOSE CONE. NO DEFECTS NOTED. PERFORMED MLG SWINGS. NO DEFECTS NOTED. INSPECTED NLG WW ACCESS PANEL SEAL. FOUND SEAL WORN. PLACED SEAL. NLG WHEEL WELL PANEL PLACED. ALL WORK DONE IAW F-2000 M/M CH 52-40-00-3/11/07.

ATA 5270

Part: ACCESS DOOR — WARNING LIGHT · airframe 5,958 hrs · 3,719 cycles

DOOR WARNING LIGHT CAME ON DURING THE TAKEOFF ROLL. TAKEOFF WAS ABORTED AND ALL DOORS WERE VERIFIED CLOSED. DEFERRED IAW NJA FALCON 2000 MEL, FERRIED AIRCRAFT TO CMH FOR REPAIR. COMPLETED DOOR INDICATION TEST IAW F2000 MM 52-701. NO DEFECTS NOTED.

ATA 3417

Part: ADC — INOPERATIVE (NR 1) · airframe 5,645 hrs · 3,527 cycles

ON TAKEOFF ROLL. EXPERIENCED AN ADC FAILURE. TAKEOFF WAS ABORTED. REMOVED AND REPLACED NR 1 ADC, SYSTEM OPERATIONALLY CHECKS NORMAL IN ACCORDANCE WITH FALCON 2000 MAINTENANCE MANUAL CHAPTER 34-100 AND 34-104. ALL WORK PERFORMED BY DUNCAN AVIONICS TEB.