N290QS

Part: LANDING GEAR — MALFUNCTIONED · airframe 7,470 hrs · 4,605 cycles

LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. 3 RED LIGHTS DISPLAYED ON GEAR PANEL. GEAR EXTENDED NORMALLY.

Part: INDICATION SYS — MALFUNCTIONED (MLG) · airframe 7,470 hrs · 4,604 cycles

AFTER WEIGHT CAME OFF OF WHEELS, STALL WARNING STARTED AND COULD NOT BE SILENCED. ALL 3 RED MOVING LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. UPON GEAR EXTENSION, ALL 3 RED MOVING LIGHTS EXTINGUISHED. AMBER GRND PROX WAS DISPLAYING IN THE ATTITUDE INDICATOR AS WE DESCENDED TO LAND. AFTER LANDING THE STALL WARNING STOPPED.

Part: CONTROL PANEL — MALFUNCTIONED (MLG) · airframe 7,469 hrs · 4,602 cycles

ALL THREE RED MOVING LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. UPON GEAR EXTENSION, ALL THREE RED MOVING LIGHTS THEN EXTINGUISHED. REPLACED CONFIGURATION PANEL (30C2) WITH A REPAIRED PANEL IAW MM 34-003. LANDING GEAR EXTENSION LOCATIONED TESTED GOOD IAW MM 32-300. OPS CHECK REQUIRED IAW INSTALLING PROCEDURE GOOD IAW MM 27-505 27-605, 27-805 AND 33-101.

Part: CONTROL UNIT — INOPERATIVE (EXTERIOR LIGHTS) · airframe 6,404 hrs · 3,946 cycles

SHORTLY AFTER TAKEOFF THE LT EXT LIGHT AND RT EXT LIGHTS CIRCUIT BREAKERS POPPED AND THE ODOR OF ELECTRICAL SMOKE WAS NOTICED. T/S SYS. FOUND PULSE LIGHT CONTROL UNIT TO HAVE FAILED DUE TO EXPOSURE TO WATER. REMOVED AND REPLACED CONTROL UNIT WITH MODIFIED UNIT. OPS CHECK OF LANDING LIGHTS AND PULSE LIGHT SYS, GOOD AT THIS TIME. IAW MM TASK 33-300.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 6,312 hrs · 3,888 cycles

DURING AIRCRAFT EXTERIOR INSPECTION FOUND 3" BOLT LODGED IN RT IB FLAP. BOLT PENETRATED THROUGH UPPER AND LOWER SKIN OF FLAP. REMOVED RIGHT INBD FLAP FOR REPAIR. INSTALLED NEW SKIN PANEL IAW SRM 51-10-04, 51-30-05, 51-30-07, AND MM 20-321. APPLIED PAINT FINISH TO REPAIR AREA IAW MM 20-601 AND 20-611. REINSTALLED REPAIRED FLAP IAW MM 57-603. PERFORMED FUNCT TEST OF FLAP CONTROL AND INDICATING SYSTEM PER MM 27-503 WITH NO DISCREPANCIES NOTED.

Part: UNKNOWN — SMOKE (COCKPIT) · airframe 5,849 hrs · 3,610 cycles

SMOKE IN COCKPIT ORIGINATING FROM CENTER CONSOLE/FMS NR 2 AREA.

Part: CDU — SHORTED · airframe 5,849 hrs · 3,610 cycles

SMOKE IN COCKPIT ORIGINATING FROM CENTER CONSOLE/FMS NR 2 AREA. INSPECTED CENTER CONSOLE FOR ACTUAL ORIGIN OF SMOKE. FOUND AT 3 FMS CDU AS THE SOURCE AS INDICATED BG THE PRESENCE OF A BURNED PLASTIC ODOR EMITTING FROM THE UNIT. INSPECTED ALL CONSOLE WIRING FOR SIGNS OF DAMAGE, INSPECTED AVIONICS COOLING SQS. FOR PROPER OPERATION AND VERIFIED PROPER VOLTAGES PRESENT AT THE FMS CDU. NO FURTHER DEFECTS NOTED. THE NR 2 FMS CDU WAS REPLACED ON A SQUAWK IN THE SAME W/O. ALL DAMAGE WAS CONFINED WITHIN THIS UNIT REF MM 05-102.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 5,460 hrs · 3,360 cycles

DOORS LIGHT ON MWP CAME ON AT 80 KTS DURING TAKEOFF. ADJUSTED SECONDARY CATCH ON BAGGAGE DOOR PERFORMED A DOOR WARNING CHECK, OPS CHECK GOOD REF FALCON 2000 MM 52-701

Part: SWITCH — OUT OF ADJUST (CARGO DOOR) · airframe 5,251 hrs · 3,238 cycles

RED DOOR LIGHT CAME ON DURING T/O ROLL, APPROXIMATELY 100 YRDS AFTER BRAKE RELEASE AND FULL POWER. INSPECTED CONDITION AND ADJUSTMENT OF ALL DOOR SWITCHES AND PROX SENSORS, FOUND BAGGAGE BAY FWD SWITCH (43MV) OUT OF ADJUSTMENT AND STICKING. ADJUSTED AND CLEANED IAW MM CH 52-700, OPERATIONAL CHECK GOOD. NO FURTHER DEFECTS FOUND.

Part: OVEN — ODOR (GALLEY) · airframe 4,633 hrs · 2,858 cycles

WHITE ODORLESS SMOKE POURS OUT OF THE GALLEY CONVECTIVE OVEN WHEN OPERATING. CLEANED OUT INSIDE OF OVEN. OPERATED AT HIGHEST TEMPERATURE SETTING FOR 15 MINUTES. VERY MINIMAL SMOKE NOTED AFTER CLEANING. IAW F2000 M/M 20-314

Part: FAN — ODOR (NR 4 PDU) · airframe 2,447 hrs · 1,495 cycles

MODERATE TO STRONG BURNING ODOR WAS NOTICED IN COCKPIT AFTER DEPARTURE, ODOR BECAME FAINT AND THEN STRONGER SEVERAL TIMES. REMOVED AND REPLACED NR 4 PDU COOLING FAN ASSY. WITH A NEW FAN ASSEMBLY. OPS CHECK GOOD NO ODOR NOTED IN CABIN. WORK PERFORMED IAW FALCON 2000 MM 34-001.

Part: LEG ASSY — VIBRATION (NLG) · airframe 1,922 hrs · 1,190 cycles

NOSE GEAR SCISSORS NOT PINNED PRIOR TO TAKE OFF, NLG WOULD NOT RETRACT INTO WHEEL-WELL, SEVERE VIBRATION FROM NOSE WHEEL WAS NOTED ON TOUCHDOWN. REMOVED NOSE LANDING GEAR LEG ASSY PN- D23332000-4 SN- B147. INSTALLED AN OVERHAULED NOSE GEAR LEG ASSY PN D233320004, SN B2. WORK DONE PER THE FOLLOWING F2000 WORK PROCEDURES : 32-203, 32-213, 32-201, 32-214, 32-401, 32-200, 32-300, AND 32-501.