N861QS

ATA 3310

Part: BULB — BURNED OUT (COCKPIT) · airframe 7,568 hrs · 5,334 cycles

CLIMBING THROUGH ABOUT FL300 A BURNING ODOR WAS IN THE COCKPIT (PAX COULD NOT ODOR SMOKE IN CABIN). M2B- INSPECTED BEHIND INSTRUMENT PANELS AND UNDER GLARESHIELD PANELS WITH NO FAULTS NOTED. RAN AIRCRAFT FOR .5 HRS WITH NO SMELL OF SMOKE. TALKED WITH TECH REPS AND WAS TOLD TO CHECK FOR BURNED OUT BULBS IN ANNUNCIATOR PANEL DUE TO HISTORY OF SMOKY ODOR WHEN BULBS BURN OUT. FOUND 4 INDIVIDUAL BULBS OUT IN THE UPPER AC POWER ANNUNCIATOR PANEL. REPLACED BULBS WITH NEW AND RAN AIRCRAFT FOR .5 HRS WITH NO SMELL OF SMOKE NOTED. WORK DONE IAW MM CHP 33-10-00.

ATA 2700

Part: CONTROL PANEL — SHORTED (FLT CONTROLS) · airframe 7,561 hrs · 5,329 cycles

10 MIN INTO FLT AT NIGHT, 12000 MSL, IN AND OUT OF CLOUDS AND RAIN, AREA ABOVE RT- SIDE FLT CONTROL PANEL SPARKED W/POPPING NOISE AND BRIEF BURNED SMELL ACCOMPAINIED BY BOTH MASTER WARNING LTS FLASHING. RAN A/C APU AND ENGINES TO VERIFY DISCREPANCY, COULD NOT DUPLICATE SPARKING SMELL OR WIRING ACTUATION. PERFORMED GENERAL INSPECTION OF COCKPIT FLIGHT CONTROL PANELS AND PILOT AND CO-PILOT WINDSHIELDS. FOUND 4 STATIC DISCHARGE DRAINS NOT SECURED. REPAIRED STATIC DRAIN WEDGES IAW SRM CHAPTER 56-10-11.

ATA 3297

Part: WIRE — MISINSTALLED (LT MLG) · airframe 7,448 hrs · 5,244 cycles

AFTER TAKEOFF, THE LEFT MAIN GEAR RED LIGHT STAYED ILLUMINATED AFTER GEAR RETRACTION. JACKED A/C AND TROUBLESHOT SYSTEM, FOUND WIRE JK2L WAS LOCATED ON TERMINAL JK3L. CORRECTED MISWIRE AND PERFORMED EXTENSION AND RETRACTION SEVERAL TIMES WITH NO DEFECTS NOTED. ALL WORK PERFORMED IAW HAWKER 800XP MM CHP 32-30-01.

ATA 3244

Part: TIRE — BLEW OUT (LT MLG) · airframe 6,453 hrs · 4,582 cycles

BOTH LEFT MAIN GEAR TIRES BLOWN ON TAKEOFF. INSPECTED AIRCRAFT AND FOUND ON THE LEFT HAND SIDE FLAP WELL AREA AND THE WHEEL WELL AREA DAMAGED, PERFORMED INTERIM REPAIR TO FLAP AND WHEEL WELL STRUCTURE, REPLACED HYDRAULIC LINE AND BRACKET. REMOVED AND REPLACED BRAKE LINES P/N: SA7670024-005, SA7670024-006, SA7670024-014, SA7670024-007, SA7670024-008, SA7670024-015 25SW129-85. REPLACED NR 1 (S/N KY027) AND NR 2 (S/N YC162) MAIN WHEEL ASSEMBLES, PERFORMED GEAR SWING ALL WORK IAW HAWKER 800XP AMM 32-40-12 AND 32-40-00 OPS CK LEAK CHECK GOOD. AIRCRAFT TO BE FERRIED TO MAINTENANCE FACILITY FOR REPAIR.

ATA 2611

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 5,547 hrs · 3,960 cycles

BAG FIRE LIGHT ILLUMINATED DURING CLIMBOUT AND EXTINGUISHED AFTER APPROX 10 SECS. LIGHT ILLUMINATED AGAIN AFTER A FEW MINS AND EXTINGUISHED AGAIN AFTER 10 SECS. REMOVED AND REPLACED FWD CABIN SMOKE DETECTOR. PERFORMED SMOKE DETECTION SYSTEM TEST, SYSTEM OPS CHECK GOOD. WORK DONE IAW RAYTHEON A/C HAWKER 800XP MM ADDENDA CH 26-11-00.

ATA 2821

Part: FILTER — OBSTRUCTED (FUEL SYSTEM) · airframe 5,021 hrs · 3,617 cycles

NUMBER ONE ENGINE FUEL LIGHT CAME ON DURING TAKEOFF ROLL, EXTINGUISHED AFTER REJECTED TAKEOFF. REMOVED AND REPLACED NR 1 AND NR 2 ENGINE FUEL FILTER ELEMENTS WITH NEW ELEMENTS PER HONEYWELL TECH SUPPORT REQUEST, NOTED SMALL AMOUNTS OF LINT ON EACH FILTER. RAN BOTH ENGINES AT 5 PERCENT BELOW TAKEOFF POWER FOR 5 MINUTES, COULD NOT DUPLICATE DISCREPANCY. ALL WORK DONE IAW HONEYWELL TFE731-5BR MM CHAPTER 73-21-02.

ATA 2611

Part: CONNECTOR — LOOSE (SMOKE DETECTOR) · airframe 4,199 hrs · 3,071 cycles

DURING FLIGHT TOILET SMOKE DETECTION LIGHT AND BAGGAGE FIRE DETECTION LIGHT CAME ON ERRONEOUSLY, SYSTEMS WILL NOT TEST. GAINED ACCESS TO THE FORWARD AND AFT BAGGAGE COMPARTMENT SMOKE DETECTORS, FOUND BOTH CONNECTORS LOOSE, TIGHTEN BOTH CONNECTORS. GAINED ACCESS TO THE LAVATORY SMOKE DETECTOR, INSPECTED AND FOUND CONNECTOR IS SECURED. ALL WORK DONE IAW HAWKER 800XP MM CHAPTER 26-11-00.