N893QS

Part: WARNING LIGHT — ILLUMINATED (NR 1 COMPUTER) · airframe 8,171 hrs · 5,881 cycles

NR 1 COMPUTER LIGHT ILLUMINATED ON TAKEOFF ROLL AT APPROX 60KTS. ABORTED TAKEOFF.

Part: COMPUTER — MALFUNCTIONED (NR 1) · airframe 8,171 hrs · 5,881 cycles

NR 1 COMPUTER LIGHT ILLUMINATED ON TAKEOFF ROLL AT APPROX 60KTS. ABORTED TAKEOFF. DOWNLOAD DEEC AND FOUND ECTM DATA BUFFERS FULL. CLEANED ECTM DATA. PERFORMED IDLE RUN AND OPS CHECKS IAW MM.

Part: FIRE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 7,605 hrs · 5,474 cycles

CARGO FIRE WARNING LIGHT COME ON DURING APPROACH. VISUALLY CHECKED THE FWD, UNDERSINK AND AFT SMOKE DETECTORS MOUNTING AREAS FOR SIGN OF BURNED/HEATING PARTS OF THE AC, CHECKED WIRES AND CONNECTORS OF THE SMOKE DETECTORS, NO FAULTS FOUND. CHECKED VISUALLY THE SMOKE DETECTOR AMPLIFIER AND SLIGHTLY TAPPED THE AMPLIFIER, NO FAULT FOUND. CHECKED THE SWITCHES TERMINALS, NO FAULT NOTED. PERFORMED SMOKE DETECTION SYS FUNCTIONAL TEST, CHECKED GOOD, IAW MM ADDENDA ATA 26-11-00. WORK DONE IAW DWG NR A8-8R-100. REFER TO WO SC1823 ITEM 1.9 FOR DETAILS.

Part: INDICATION SYS — MALFUNCTIONED (MLG) · airframe 7,556 hrs · 5,444 cycles

WITH GEAR SELECTED UP AFTER T/O ALL 3 GEAR INDICATED UNSAFE WITH RED LIGHTS. JACKED AIRCRAFT CYCLED NOSE ONLY THEN UNPINNED MAINS COMPLETED 2 MORE COMPLETE CYCLES WITH NO FAULTS. WORK COMPLETED IAW MM 29-10-00.

Part: DOWNLOCK SWITCH — INTERMITTENT (MLG) · airframe 7,448 hrs · 5,387 cycles

DURING T/O AS THE NLG LEAVES THE GRD, A NOSE LIKE SHIMMY OR A TIRE IMBALANCE IS HEARD FOR APPROX. 3 SEC. THEN DURING RETRACTION THE NLG LIGHTS DIMLY FLICKER (BOTH RED & GREEN) UNTIL THE GEAR IS RETRACTED FULLY. MLG LIGHT ARE NORMAL. ALSO AT APPROX 20 MIN INTO THE FLIGHT DURING CLIMB WE NOTICED THE NLG LIGHTS FLICKER LIKE BEFORE. REMOVED & REPLACED NOSE WHEEL DOWN LOCK SWITCH WITH NEW SWITCH OPS CHECKS GOOD PER 800XP MM 32-60-00 & WD 32-60-10-04.

Part: LANDING GEAR — FALSE INDICATION (MAINS) · airframe 7,443 hrs · 5,382 cycles

UPON GEAR RETRACTION, (3) RED LIGHTS ALONG WITH 1 GREEN FOR THE NOSEWHEEL ARE INDICATED FOR 1 MINUTE AFTER SELECTING GEAR UP. INSPECTED GEAR AND CYCLED SEVERAL TIMES IAW MM 29-10-00-501. NO DEFECTS NOTED AT THIS TIME.

Part: FAN BLADE — DAMAGED (RT ENGINE) · airframe 6,959 hrs · 5,009 cycles

RT ENGINE HAS FOD DAMAGE TO MULTIPLE ENGINE FAN BLADES. [SUP 4-19-07] ALL MAINTENANCE ACCOMPLISHED. IAW HONEYWELL LMM 731-5 AND HAWKER MM. 800XP.

Part: ENGINE — UNKNOWN · airframe 6,172 hrs · 4,444 cycles

DURING TAKEOFF ROLL, NR 1 ENGINE N2 FLUCTUATES 10 PERCENT AND ACTUATED APR. ABORTED TAKEOFF AT 90 KTS. LATER NR 1 ENGINE COMPUTER LIGHT CAME ON.

Part: THROTTLE CONTROL — OUT OF ADJUST (FUEL CONTROL SYS) · airframe 6,127 hrs · 4,420 cycles

RIGHT ENGINE TAKEOFF THRUST AT 13 DEG CELSIUS ONLY PRODUCING 94.1% N-1. MADE MINOR ADJUSTMENT TO FCU AND MADE ADJUSTMENT TO THROTTLE COLLAR ON THE NR 2 SIDE. RAN AIRCRAFT AND CHECKED IDLE, POWER OF THE DAY, ACCELERATION AND DECEL CHECKED GOOD. WORK DONE IAW CHAP 72-00-00 OF THE HONEYWELL TFE731 LMM AND CHAP 76-10-00 OF THE HAWKER 800XP MM.

Part: LEVER — OUT OF POSITION (COCKPIT) · airframe 6,014 hrs · 4,352 cycles

AFTER TAKEOFF DURING GEAR RETRACTION, HAD 3 RED LIGHTS ILLUMINATED AND TWO MAIN GEAR GREEN LIGHTS ILLUMINATED. GEAR DOWN EXTENDED NORMALLY AND 3 GREEN LIGHTS (M2B). FOUND AUX HYD PUMP LEVER UP DOWN BY THE PILOT'S RIGHT FOOT AND THE AUX HYD LEVER PULLED UP A LITTLE WHICH WOULD NOT GO ALL THE WAY DOWN DUE TO THE PUMP LEVER BEING UP PUSHED PUMP LEVER DOWN AND THEN PUSHED AUX HYD LEVER DOWN ALSO, SWUNG GEAR AND OPS CHECKED SEVERAL TIMES. OPS CHECKED GOOD.

Part: UNKNOWN — UNKNOWN (LANDING GEAR)

AFTER TAKEOFF, DURING GEAR RETRACTION HAD 3 RED LIGHTS ILLUMINATED AND TWO MAIN GEAR GREEN LIGHTS ILLUMINATED. GEAR DOWN EXTENDED NORMALLY AND 3 GREEN LIGHTS.

Part: APU — ODOR (APU BAY) · airframe 5,709 hrs · 4,154 cycles

TEN SECONDS AFTER STARTING THE APU ON SHORT FINAL, RECEIVED A MASTER WARNING AND SMELLED A HOT ELECTRICAL ODOR AND THE APU DID NOT AUTO SHUTDOWN. SHUTDOWN THE APU MANUALLY, THE ODOR WENT AWAY. ITEM IS UNDER INVESTIGATION.

Part: STRUT — INOPERATIVE (RUDDER) · airframe 5,562 hrs · 4,041 cycles

RUDDER BIAS ACTIVATES WITH BOTH POWER LEVERS AT T/O POWER. GOT FULL RIGHT DEFLECTION OF THE RUDDER, ABORTED AT 50 KTS. - REMOVED AND REPLACED RIGHT HAND RUDDER BIAS STRUT PERFORMED FUNCTION TEST. FUNCTION TESTED GOOD ALL WORK PERFORMED IAW HAWKER 800XP MM 27-20-51.

Part: CONNECTOR — LOOSE (CARGO BAY) · airframe 5,546 hrs · 2,049 cycles

CARGO BAY FIRE LIGHT ANNUNICATOR ILLUMINATED STEADY IN FLIGHT (APPROX 5 SECONDS). REMOVED ACCESS PANELS TO FOM ON FWD AFT SMOKE DETECTORS. VISUALLY INSPECTED SMOKE DETECTORS (3EA). FOUND FWD CONNECTOR LOOSE. TIGHTENED PLUG. CLEANED SCREEN. RE-INSTALLED ACCESS PANELS. INSPECTED AREA AROUND SMOKE DETECTORS. NO DEFECTS AT THIS TIME. OPS CHECK GOOD IAW HAWKER 800XP AMM. REMOVED ACCESS PANELS TO FOM ON FWD AFT SMOKE DETECTORS. VISUALLY INSPECTED SMOKE DETECTERS (3EA). FOUND FWD CONNECTOR LOOSE. TIGHTENED PLUG. CLEANED SCREENS. PERFORMED OPS CHECK, GOOD. TIGHTENED CONNECTORS. RE-INSTALLED ACCESS PANEL. INSPECTED AREA AROUND SMOKE DETECTOR. NO DEFECTS AT THIS TIME IAW HAWKER 800XP AMM.

Part: STARTER — FAILED (APU) · airframe 5,162 hrs · 3,759 cycles

UPON LANDING CREW SMELLED ELECTRICAL BURNING OF UNKNOWN ORIGINAL IN COCKPIT, NO SMOKE OBSERVED. NO SMELL IN CABIN, WINDSCREEN HEAT OFF. APU STARTER GENERATOR FOUND TO BE CAUSE OF PROBLEM.

Part: WARNING LIGHT — ILLUMINATED (FUEL FILTER) · airframe 4,408 hrs · 3,252 cycles

ON TAKE OFF ROLL AT 40 KNTS "ENGINE NR 1 FUEL" LIGHT ILLUMINATED, ABORTED TAKE OFF - SUMPTED FUEL FROM AIRCRAFT AND CHECKED FOR WATER CONTAMINATION, NONE FOUND. INSPECTED THE LEFT ENGINE FUEL FILTER AND NO DEBRIS NOTED. REPLACED FILTER AND PERFORMED ENGINE GROUND RUN, SYSTEM OPS AND LEAK CHECKED GOOD IAW RAYTHEON MM CHAPTER 71-00-00.