N298QS

ATA 5754

Part: SLAT — DAMAGED (RT WING) · airframe 9,113 hrs · 5,689 cycles

ON FLAP-SLAT RETRACTION AFTER TAKEOFF, THE YELLOW NIPS LIGHT REMAINED ON. IWA THE CHECKLIST, RE-EXTENDED SLATS-FLAPS, EXTENDED NORMALLY AND NIPS LIGHT WENT OUT. RETRACTED FLAPS-SLATS AND NIPS LIGHT REMAINED ON. UPON INVESTIGATION, THE RT SLAT HAS A WRINKLE IN IT. REMOVED DAMAGED RT WING SLAT AND INSTALLED REPAIRED RT WING SLAT. REF MM 57-503. PERFORMED OPS TEST OF RT WING ANTI-ICING SYS AND CHECKED FOR LEAKS AT TELESCOPIC TUBE CONNECTION REF MM 30-101. NO LEAKS NOTED.

ATA 3197

Part: WIRE HARNESS — MISROUTED · airframe 7,869 hrs · 4,944 cycles

STRONG SMELL OF AN ELECTRICAL TYPE BURNING ODOR AFTER TAKEOFF AND AGAIN AFTER LANDING. THE ODOR OCCURRED ON CLIMB OUT, CLEARED OUT EN ROUTE, AND CAME BACK WHEN PULLING ONTO RAMP. TROUBLESHOT AC ELECTRICAL AND PNEUMATIC SYS. FOUND PILOT MFD HARNESS ROUTED UNDER PILOT PFD POSSIBLE COOLING FAN IMPEDANCE REROUTED AND INSPECTED HARNESS WITH NO FAULT FOUND ALL WORK COMPETED IAW MM 34-001. COULD NO LONGER DUPLICATE FAULT.

ATA 3400

Part: DAU — INOPERATIVE (NOSE AVIONICS BA) · airframe 6,653 hrs · 4,206 cycles

WE GOT THE NO TAKE-OFF AURAL WARNING WITH NO TAKEOFF ANNUCIATE LIGHT ON TAKE OFF. REMOVED AND REPLACED DATA AQUISITION UNIT (DAU-4000) WITH OVERHAULED UNIT. PERFORMED OPS CHECK OF DAV AND TAKEOFF WARNING SYSTEM. OPS CHECK GOOD. WORK

ATA 2720

Part: YAW DAMPER — INOPERATIVE · airframe 5,997 hrs · 3,806 cycles

YAW DAMP IN DESCENT YAWS AIRCRAFT FROM SIDE TO SIDE. TURNED OFF AND BACK ON. THE UNCOMMANDED YAWING CONTINUED. TURNED OFF AND FLEW WITHOUT IT. REMOVED AND REPLACED YAW DAMPER IAW F-2000 M/M 22-105. OPERATIONAL TEST GOOD.

ATA 2530

Part: OVEN — ODOR (GALLEY) · airframe 5,764 hrs · 3,650 cycles

DURING FLIGHT, THE 115A INVERTER CB POPPED AS MICROWAVE WAS BEING USED. CREW NOTICED ELECTRICAL SMOKE/BURNED SMELL IN THE CABIN. OPERATED MICROWAVE OVEN FOR 15 MINUTES WITH NO DEFECTS NOTED. REPLACED MICROWAVE IAW F-2000 M/M 25-20-00. OPERATIONAL CHECK GOOD.

ATA 2120

Part: SMOKE — DETECTED (CABIN) · airframe 5,707 hrs · 3,620 cycles

THE F/A REPORTED SEEING SMOKE IN THE CABIN BY THE NR 2 SEAT AND THE SIDE WALL. SMELL STARTED ON SHORT FINAL AND STOPPED WHEN THE A/C TOUCHED DOWN. BOTH THE F/A & F/O REPORTED SMELLING "MODEL TRAIN LIKE - ELECTRICAL AND OZONE SMELL". ITEM IS UNDER INVESTIGATION.

ATA 3417

Part: PROBE — MALFUNCTIONED (PITOT HEAD) · airframe 5,575 hrs · 3,529 cycles

ON TAKE OFF ROLL NO AIRSPEED READOUT ON RIGHT SIDE. ERRONEOUS WIND READOUTS NOTED OF 40 -40 TO -60 KTS. TAKEOFF ABORTED. - REMOVED RT SIDE PITOT PROBE PN 50520 SN 1960 AND INSTALLED NEW PITOT PROBE P/N 50520 S/N 3772 IAW F2000 MM PROCEDURE 20-000. PERFORM OPERATIONAL CHECK OF HEATING ELEMENT OF RT SIDE PITOT PROBE I.A.W. F-2000 M.M.

ATA 3417

Part: ADC — FAILED (COCKPIT) · airframe 5,342 hrs · 3,373 cycles

DURING TAKEOFF ROLL, BELOW 50KTS, "AUTO SLATS" ANNUNCIATOR CAME ON, NO AIRSPEED OR ALTITUDE INFO ON NR 1 PFD. ADC MESSAGES ON EIED AFTER CLEARING THE RWY. TROUBLESHOT SYSTEM, REMOVED & REPLACED PILOTS ADC OPS CHECKS GOOD. PITOT/STATIC LEAK CHECK AND ADC FUNCTIONAL CHECK PERFORMED IAW FAR 91.411 AND PART 43.

ATA 2751

Part: POTENTIOMETER — FAILED (COCKPIT) · airframe 4,857 hrs · 2,084 cycles

FLAP CONTROL CIRCUIT BREAKER POPPED IN CRUISE FLIGHT. FLAP HANDLE WAS NOT MOVED AND REMAINED IN UP POSTION. INSTALLED REPAIRED LT POTENTIOMETER IAW FALCON 2000 M/M 27-509.

ATA 2750

Part: RESOLVER — MALFUNCTIONED (SLATS/FLAPS) · airframe 4,323 hrs · 2,734 cycles

AFTER T/O, FLAP ASYM LIGHT ON AND SLIGHT ROLLING. FLAP INDICATES SLIGHTLY DOWN AND SLATS EXTENDED. GAINED ACCESS TO FLAP ASYM RESOLVERS & FOUND LT RESOLVER CABLE LOOSE. RESET RESOLVER AS REQUIRED, OPS CHECK GOOD. ALL WORK PERFORMED IAW FALCON 2000 MM CHAPTER 27-502.

ATA 3260

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 3,838 hrs · 2,438 cycles

ON APPROACH LOWERED GEAR HANDLE AND DID NOT RECEIVE GREEN LIGHT, PERFORMED EMERGENCY GEAR EXTENSION AND DECLARED EMERGENCY. AIRCRAFT LANDED SAFELY. PLACED AIRCRAFT ON JACKS AND PERFORMED GEAR SWING, FOUND BOTH RT GREEN LIGHTS BURNED OUT, REPLACED BULBS AND SYSTEM OPS CHECKED GOOD IAW MM CHAPTER 32-002.