N882QS

ATA 3420

Part: AHRS — INOPERATIVE (NR 2) · airframe 8,202 hrs · 5,761 cycles

NR 1 AND NR 2 EADI RED ATT FLAG WITH AMBER COMPUTER MON CAME ON CLIMBING THROUGH 10,000 FT. STAYED ON APPROX 4 MINUTES. R & R NR 2 AHRS IAW MM 34-20-15-401, TESTED NR 1 AND NR 2 AHRS IAW MM 34-20-15-501. NO FAULT FOUND.

ATA 2797

Part: WIRE — SHORTED (ELEVATOR/AILERON) · airframe 7,310 hrs · 5,153 cycles

ELEV/AIL TRIM LIGHT CAME ON AT FL360 CRUISE AND STAYED ON UNTIL PASSING THROUGH APPROX 8000 FT. FOUND WIRE C121E22 TO ELEV/AIL TRIM LIGHT SHORTED TO RT AFT KICK PANEL AISLE LIGHT SWITCH, ACTUATED BY SKI BOX LATCH. REPAIRED WIRE C121E22 AS REQUIRED AND REPAIRED INSULATION TO SKI BOX SWITCH. REPOSITIONED WIRE BUNDLES TO ELIMINATE RIDING CONDITION. ELEV/AIL TRIM OPS CHECK GOOD. ALL WORK ACCOMPLISHED IAW AMM 27-10-81 27-30-00 AND 20-10-50 PG 201.

ATA 3297

Part: WIRE — WRONG PART (WOW SWITCH) · airframe 7,242 hrs · 5,098 cycles

YELLOW ELE"AIL" TRIM ON MAIN MASTER WARNING PANEL ILLUMINATED IN FLIGHT WHEN ELEVATOR TRIM WHEEL POSITION OUTSIDE OF TAKEOFF RANGE. FOUND THAT WIRING WAS TERMINATED WITH SIZE 8 LUGS. TERMINAL POST IS A SIZE 6 STUD. RETERMINATED LT WOW WIRING WIRE FOR WIRE WITH THE PROPER SIZE TERMINAL LUG. APPLIED ACFT POWER AND PERFORMED THE ELEVATOR OUT OF TRIM ANNUNCIATOR FUNCTIONAL TEST-CHECKED GOOD WITH NO DEFECTS NOTED. WORK PERFORMED IAW MM. CHAPTER 27-30-00. PERFORMED THE AILERON OUT OF TRIM ANNUNCIATOR FUNCTIONAL TEST-CHECKED GOOD WITH NO DEFECTS.

ATA 2797

Part: LUG — WRONG PART (TERMINAL POST) · airframe 7,242 hrs · 5,098 cycles

YELLOW ELE"AIL" TRIM ON MAIN MASTER WARNING PANEL ILLUMINATED IN FLIGHT WHEN ELEVATOR TRIM WHEEL POSITION OUTSIDE OF TAKEOFF RANGE. FOUND THAT WIRING WAS TERMINATED WITH SIZE 8 LUGS. TERMINAL POST IS A SIZE 6 STUD AND THEREFORE A SIZE 6 TERMINAL LUG SHOULD BE USED. RETERMINATED LT WOW WIRING WIRE FOR WIRE WITH THE PROPER SIZE 6 TERMINAL LUGS. APPLIED ACFT POWER AND PERFORMED THE ELEVATOR OUT OF TRIM ANNUNCIATOR FUNCTIONAL TEST-CHECKED GOOD WITH NO DEFECTS NOTED. WORK PERFORMED IAW MM 27-30-00. PERFORMED THE AILERON OUT OF TRIM ANNUNCIATOR FUNCTIONAL TEST-CHECKED GOOD WITH NO DEFECTS NOTED. WORK PERFORMED IAW MM 27-10-00

ATA 3150

Part: WARNING LIGHT — ILLUMINATED · airframe 7,242 hrs · 5,098 cycles

YELLOW ELE"AIL" TRIM ON MAIN MASTER WARNING PANEL ILLUMINATED IN FLIGHT WHEN ELEVATOR TRIM WHEEL POSITION OUTSIDE OF TAKE OFF RANGE.

ATA 3150

Part: WARNING LIGHT — ILLUMINATED · airframe 7,242 hrs · 5,098 cycles

THE AMBER "ELE/AIL TRIM" ANNUNCIATOR (ON MWS) ILLUMINATES DURING FLIGHT OUTSIDE OF GREEN NORMAL BAND FOR TAKE OFF.

ATA 2210

Part: UNKNOWN — UNKNOWN (AUTOPILOT) · airframe 6,209 hrs · 4,372 cycles

WHILE CLIMBING THROUGH FL350 LT AFCS FAILED. COULD NOT ENGAGE R AFCS OR YAW DAMPER. COULD NOT SELECT BETWEEN L & R AFCS. NO A/P OR YAW DAMPER OPERATION. REMOVED AND REPLACED WITH INSPECTED UNITS, BOTH NR 1&2 FLIGHT GUIDANCE COMPUTERS. OPS CHECK OF SYSTEM SHOWS NO DEFECTS. ALL WORK PERFORMED IAW HAWKER 800XP MM CHP- 34-22.

ATA 3246

Part: WHEEL — OUT OF ROUND (NLG) · airframe 5,966 hrs · 4,190 cycles

AFTER GEAR RETRACTION THERE IS A VERY SIGNIFICANT VIBRATION THAT LASTS FOR ABOUT 2 MINUTES, COMING FROM THE NOSE GEAR. T/S WHEEL ASSEMBLY BY REMOVING & BALANCING, FOUND TIMES TO BE OUT OF ROUND FACILITATING REPLACEMENT, RECEIVED OVH WHEEL ASSEMBLIES FROM NETJETS, CHECKED BALANCE OF OVH WHEEL ASSY CHECK GOOD. INSTALLED ASSEM ON NOSE STRUT, TIRES INFLATED TO 100 PSI IAW 800XP CMM 32-44-49 / AMM 32-40-00 / AMM 12-00-00.

ATA 2821

Part: FUEL FILTER — LEAKING (NR 1 ENGINE) · airframe 3,469 hrs · 2,500 cycles

NR 1 ENGINE FUEL LIGHT CAME ON DURING TAKEOFF. INSPECTED BOTH ENGINES FOR EVIDENCE OF FUEL LEAK ETC. CHANGED BOTH FUEL FILTERS. LEAK CHECKED FILTERS, RAN BOTH ENGINES TO POWER SEVERAL TIMES, NO RED LOOK-UP LIGHT. ALL WORK IAW HONEYWELL MM CH 72-00-00.

ATA 7330

Part: WARNING LIGHT — ILLUMINATED (NR 2 ENG FUEL) · airframe 3,294 hrs · 2,377 cycles

AT BEGINNING OF TAKEOFF ROLL, ENGINE 1 FUEL LIGHT ILLUMINATED, REDUCED POWER AND LIGHT WENT OUT. REMOVED NR 1 ENGINE UNSERVICEABLE FUEL FILTER, NO FOREIGN MATERIAL WAS FOUND IN FILTER, INSTALLED NEW FUEL FILTER. AS A PRECAUTION, REMOVED NR 2 ENGINE FUEL FILTER, NO FOREIGN MATERIAL FOUND, INSTALLED A NEW FILTER ELEMENT. LEAK AND OPERATIONAL CHECK WAS FOUND TO BE SATISFACTORY, ALL WORK ACCOMPLISHED IAW TFE 731-5BR LMM CHAPTER 73-21-02.