Garrett TFE731-5BR

Service difficulty reports · 328

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'TFE7315BR'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DXTA200701951Switch · inoperativeWHEN GEAR WAS RETRACTED AFTER TAKEOFF, THE LT MAIN INDICATED BOTH RED AND GREEN LIGHTS AND THE NOSE AND RT MAIN INDICATED RED LIGHTS. UPON PLACING THE LEVER IN THE DOWN POSITION 3 GREEN AND NO RED LIGHTS WERE OBSERVED. REMOVED U/C HANDLE SWITCH P/N 25-7NF859-Feb 16, 2007 · N816QS · Raythn HAWKER800XP · Landing Gear SelectorSDR DXTA200701927Computer · malfunctionedAUTO PILOT PITCHED OVER FROM LEVEL FLIGHT AT FL360 AND MACH .78 OR 260 KTS IND. WE LOST 450 FT UPON THE VIOLENT PITCHING MOMENT AND VERY ABRUPT TAIL FLUTTER. THIS HAPPENED ON THE L-AFCS, FLIGHT DIRECTOR VERY ERRATIC IN ALL MODES AFTER PITCHING MOMENT. REPLAFeb 9, 2007 · N838QS · Raythn HAWKER800XP · Autopilot SystemSDR DJFA2007018Seat · crackedDURING A SCHEDULED MAINTENANCE EVENT A CRACK WAS DISCOVERED ON THE COPILOT'S SEAT WEB. THE CRACK WAS APPROX 2.5 INCHES LONG AND EXCEEDED THE APPROVED REPAIR REQUIREMENTS OF 2.15 INCHES. THE SDR WILL BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION.Feb 9, 2007 · N813CW · Raythn HAWKER800XP · Flight Compartment EquipmentSDR DXTA200701893Fire Detector · malfunctionedBAGGAGE FIRE LIGHT FLASHES INTERMITTENTLY UPON LANDING. TESTED MWS AND LIGHT WOULD NOT COME ON. COULD NOT DUPLICATE SMOKE DETECTOR FAILURE. CLEANED CONTACTOR EYES & CONNECTORS FOR EACH OF THE THREE DETECTORS. RETESTED & FOUND NO DISCREPANCIES AT THIS TIME. Jan 30, 2007 · N875QS · Raythn HAWKER800XP · Fire DetectionSDR DJFA2007014Pin · bentDURING THE SCHEDULED REPLACEMENT OF THE SQUIBS AND FIRE BOTTLES MAINTENANCE DISCOVERED A PIN BENT OVER ON THE FORWARD FIRE BOTTLE SQUIB WHICH WOULD HAVE PREVENTED THE DISCHARGE OF THE BOTTLE DURING AN EMERGENCY. THE SDR WILL BE UPDATED UPON COMPLETION OF THE Jan 28, 2007 · N817TA · Raythn HAWKER800XP · Extinguishing SystemSDR DXTA200701881Warning System · activatedAT 300FT ON FINAL, GOT GPWS WARNING (TOO LOW GEAR, PULL UP). NOSE GEAR INDICATOR WENT BLANK. DID EMERG PROCEDURES INCLUDING PULLING GPWS AND HORN C/BS. DID LOW FLY BY TOWER TO CONFIRM GEAR DOWN. ON WAVEOFF DID AGRESSIVE PULLUP. NOSEGEAR INDICATOR WENT BLANK Jan 26, 2007 · N838QS · Raythn HAWKER800XP · Landing Gear Position and WarningSDR DJFA2007013Door Frame · crackedWHILE TROUBLESHOOTING A NOSE STEERING PROBLEM, MAINTENANCE FOUND THE LT NOSE GEAR DOOR FRAME CRACKED BEYOND THE LIMITS ACCEPTABLE IAW THE SRM. THE CRACK WAS APPROXIMATELY .5 INCHES IN LENGTH. MAINTENANCE PERFOMRED A REPAIR FROM ENGINEERING IAW EO 4731-187607Jan 26, 2007 · N843CW · Raythn HAWKER800XP · Landing Gear DoorsSDR DXTA200701878Flap System · malfunctionedWHEN FLAPS SET AT 15 DEG AIRPLANE BANKS RT AT 5000FT AT 190KTS. RAN AND OPERATED FLAPS WITH PROTRACTOR. HOOKED UP TO BOTH FLAP'S. BOTH FLAPS WITHIN .1 DEGREE DURING OPERATION. RAN SPOILERS AND LIFT DUMP SEVERAL TIMES. NO PROBLEMS NOTED. IAW M/M 27-10 AND 27-50Jan 25, 2007 · N836QS · Raythn HAWKER800XP · Trailing Edge Flap Control SystemSDR DXTA200701871Bearing · damagedSTRONG FUMES IN THE COCKPIT, NO VISIBLE SMOKE. FUMES STRONGEST WITH ENGINE POWER HIGH. FUMES ARE LOCALIZED IN COCKPIT AREA NOT NOTICEABLE IN CABIN AREA. NO DIVERT. INSTALLED LT ENGINE NEW FAN SHAFT, BEARING AND SEAL IAW ROLLS ROYCE MM 72-21-20. RAN AIRCRAJan 21, 2007 · N936QS · Cessna 750 · Turbine Engine Compressor SectionSDR DXTA200701870Control Valve · faultyWHEN BRAKING NOTHING HAPPENS UNTIL BRAKE HYD PRESSURE GAUGES READ 200 PSI THEN BRAKES GRAB HARD. SEEMS THE CAPTAINS BRAKE PEDALS ARE BAD, CO-PILOT'S SIDE BRAKES SEEM NORMAL.REMOVED AND REPLACED BRAKE CONTROL VALVE. ALL WORK DONE IAW MM.Jan 18, 2007 · N805QS · Raythn HAWKER800XP · Landing Gear Brake SystemSDR DXTA200701857Squat Switch · failedAFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. SNOW AND SLUSH ALL GROUND SURFACES. RETURNED TO DEPARTURE. JACKED AC AND ACCOMPLISHED GEAR SWINGS, NO DEFECTS WERE NOTED ACCESSED GEAR SELECTOR VALVE IN NOSE WHEEL WELL AND CHECKED FOR FREEDOM OF MEASUREMENT OF LIJan 16, 2007 · N870QS · Raythn HAWKER800XP · Landing Gear Position and WarningSDR DXTA200701841Brake · wornBRAKES FEEL MUSHY AFTER LANDING AND DURING TAXI. REPLACED NR 1 AND 2 BRAKE ASSEMBLIES. BLED SYSTEM. OPS CHECKED OK IAW HAWKER 800XP M.M. 32-40-00Jan 8, 2007 · N805QS · Raythn HAWKER800XP · Landing Gear Brake SystemSDR DXTA200701840Smoke Detector · malfunctionedRED FIRE ANNUNICATOR ILLUMINATES, FLASHES INTERMITTENTLY IN FLIGHT. VISUALLY INSPECTED ALL BAGGAGE COMPARTMENTS. CLEANED AND INSPECTED FORWARD, AFT AND LAV SMOKE DETECTORS. REMOVED LINT AND DUST FROM AFT AND LAV SMOKE DETECTORS. OPS CHECK GOOD IAW MM 26-10-Jan 6, 2007 · N875QS · Raythn HAWKER800XP · Smoke DetectionSDR DJFA2006368Seat Track · crackedDURING A SCHEDULED MAINTENANCE EVENT, MAINTENANCE FOUND THE COPILOT'S SIDE SEAT RAIL WEB CRACKED. THE CRACK WAS APPROXIMATELY 1.5 INCH LONG AND WAS LOCATED ON THE SEAT RAIL WEB FORWARD OF FRAME 7. THE CRACK WAS REPAIRED USING A DOUBLER IAW MFG STANDARD REPAIDec 21, 2006 · N830LX · Raythn HAWKER800XP · Fuselage, Seat/Cargo Attach FittingsSDR DJFA2006363Frame · crackedDURING A SCHEDULED MAINTENANCE EVENT, MAINTENANCE REPORTED THE FLOOR BOARDS NEAR THE ENTRANCE WAY WERE SPONGY. UPON FURTHER INSPECTION, FRAME 10 WAS FOUND CRACKED. THE CRACK WAS APPROXIMATELY 1 INCH LONG AND BEGAN AT THE FORWARD NUTPLATE AND EXTENDED FROM LTDec 18, 2006 · N824LX · Raythn HAWKER800XP · Fuselage Main, FrameSDR DJFA2006360Web · crackedDURING A SCHEDULED MAINTENANCE EVENT, MAINTENANCE FOUND THE STRUCTURAL WEB UNDER THE COPILOTS SEAT RAIL SHELF CRACKED. THE CRACK WAS APPROXIMATELY 1.5 INCHES LONG LOCATED FORWARD OF FRAME 7 ON THE SEAT RAIL WEB. THE CRACK WAS REPAIRED BY REMOVING THE DAMAGEDDec 15, 2006 · N848CW · Raythn HAWKER800XP · Fuselage Miscellaneous StructureSDR DJFA2006355Floor Support · crackedDURING A SCHEDULED MAINTENANCE EVENT, MAINTENANCE FOUND THE FLOOR SUPPORT AT FRAME 10 BELOW THE FLOOR AT THE GALLEY CRACKED. THE 1.5 INCH CRACK WAS LOCATED LT OF CENTER ON THE LIGHTNING HOLE. MAINTENANCE PERFORMED FRAME 10 REPAIR IAW SRM 51-71-07 , 53-20-11.Dec 6, 2006 · N816LX · Raythn HAWKER800XP · Fuselage Miscellaneous StructureSDR DJFA2006350Turbine Blades · brokenTRIP NR: 1110547 - ENROUTE AT FL350, CREW REPORTED SMELL OF SMOKE IN THE COCKPIT FOLLOWED BY GRINDING NOISE AND A LOUD BANG AFTER WHICH A VIBRATION WAS FELT IN CONTROLS. CREW DECLARED AN EMERGENCY AND DIVERTED. ON APPROACH, VIBRATION WOULD INCREASE W/ THRODec 4, 2006 · N780TA · Raythn HAWKER800XP · Turbine SectionSDR DJSA20061202Engine · failedUNCONTAINED ENGINE FAILURE DURING CLIMB AT 600 FEET AGL. AIRCRAFT RETURNED, MAKING AN UNEVENTFUL LANDING. ENGINE HAS BEEN RETURNED TO MANUFACTURER FOR TEARDOWN AND EVALUATION TO DETERMINE CAUSE OF FAILURE.Dec 2, 2006 · N531FL · Amd FALCON20C5 · Engine (Turbine/Turboprop)SDR DXTA200601771Flap System · malfunctionedWHEN FLAPS 15 DEGREES WERE SELECTED FOR LANDING (A/S 190 KTS) THE FLAPS ONLY EXTENDED 3 TO 4 DEGREES. (STALL INDENT) LIGHT ILLUMINATED HYD PSI NORMAL, ALL OTHER SYSTEMS NORMAL. PERFORMED FLAPS UP LDG. GAINED ACCESS TO FLAP SYNCHRONIZER MECHANISM AND PERFORMED Nov 30, 2006 · N836QS · Raythn HAWKER800XP · Trailing Edge Flap Control SystemSDR DJFA2006346Frame · crackedDURING SCHEDULED MAINTENANCE A CRACK WAS LOCATED AT THE FRAME 10 RIB, UNDER THE CENTER ISLE FLOOR AT THE GALLEY. REPAIRED FRAME 10 IAW SRM 51.71.11.Nov 25, 2006 · N817LX · Raythn HAWKER800XP · Fuselage Main, FrameSDR DXTA200601740Water Separator · contaminatedWHILE LEVEL AT 10000 AND INDICATING 310KIAS A LOUD BANG AND WIND NOISE OCCURRED, APPARENTLY FROM THE NOSE AREA. SPEED WAS REDUCED TO 200KIAS AND NOISE SUBSIDED. ALL HANDLING CHARACTERISTICS WERE NORMAL. FLOOR AREA SEEMED TO BE VIBRATING ASSOCIATED WITH WIND NONov 19, 2006 · N855QS · Raythn HAWKER800XP · Humidity Control SystemSDR DJFA2006342Frame · crackedDURING A SCHEDULED MAINTENANCE VISIT, A 1 INCH CRACK WAS FOUND ON LT SIDE OF THE LIGHTNING HOLE AT FRAME 10 UNDER THE CENTER ISLE FLOOR AT THE GALLEY. REPAIRED FRAME 10 IAW SRM 51.71.11Nov 16, 2006 · N728TA · Raythn HAWKER800XP · Fuselage Main, FrameSDR DXTA200601671Engine · bird ingestionON TAKEOFF ABOUT 20 SECONDS AFTER MAVS SELECTED OPEN (700 MSL) A CHEMICAL ODOR FOLLOWED BY A BURNING OF THE EYES AT 1500 MSL. THE MAV'S WERE SELECTED CLOSED AND THE APU BLEEDS ON. THE CHEMICAL ODOR WENT AWAY SHORTLY AFTER THAT. ISOLATED ODOR TO LEFT ENGINE Oct 19, 2006 · N815QS · Raythn HAWKER800XP · Engine (Turbine/Turboprop)SDR DJFA2006329Mount · crackedWHILE PERFORMING A NON-DESTRUCTIVE TEST ON THE AIRCRAFT ENGINE MOUNTS, A CRACK WAS FOUND IN THE LT FWD UPPER ENGINE MOUNT. THE ENGINE MOUNT WAS REPLACED IAW THE MM.Oct 12, 2006 · N817TA · Raythn HAWKER800XP · Engine Mount SectionSDR 2006FA0001024Turbine Wheel · fracturedIN FLIGHT, CREW FELT SLIGHT TO MODERATE VIBRATION FROM NR 2 ENGINE. AFTER LANDING FURTHER INSPECTION FOUND APPROX ONE INCH OF ONE OF THE 3 LPT DISK BLADES MISSING. REASON FOR FAILURE AT THIS TIME UNDER INVESTIGATION BY MFG, SB 72-3689. (K)Oct 2, 2006 · N6NR · Raythn HAWKER800XP · Turbine SectionSDR 2006FA0000992Engine · failed(REF NR: 2006-1001) 30,000 FT, ENGINE BANG, ENGINE WAS SHUTDOWN AND FLIGHT DIVERTED. NR 2 ENGINE TURBINE WHEEL FAILURE, UNCONTAINED. INITIAL VISUAL INSPECTION POSSIBLE TURBINE WHEEL FAILURE. INVESTIGATION IN PROCESS WITH ASSISTANCE FROM MFG. PORTION OF ESep 7, 2006 · N800WW · Raythn HAWKER800XP · Engine (Turbine/Turboprop)SDR 2006FA0001110Blade · damagedTHE INFLIGHT SHUTDOWN OCCURED ON SEPT 7, 2006, AFTER LEVELING OFF AT 30,000 FT THE CREW REPORTED A LOUD BANG FROM THE NR 2 ENGINE. THE CREW SECURED THE ENGINE, DIVERTED AND LANDED WITHOUT INCIDENT. VISUAL INSPECTION OF THE AC REVEALED DISPLACED MATERIAL ON TSep 7, 2006 · N800WW · Raythn HAWKER800XP · Turbine SectionSDR 2006FA0000923Carbon Seal · deteriorated(NR 4 CARBON SEAL, PN30745732, SN 010515810208), (NR 5 CARBON SEAL, PN 30745742, SN 0119368002352) PILOTS REPORT HIGH OIL PRESSURE. OIL PRESSURE FOLLOWED THROTTLE HIGH GEARBOX PRESSURE CAUSED BY DETERIORATION OF NR 4 AND NR 5 CARBON SEALS.Aug 23, 2006 · N922JW · Amd FALCON900 · Turbine Engine Oil SystemSDR 2006FA0000924Carbon Seal · deteriorated(NR 4 CARBON SEAL, PN30745732, SN 010515810208) (NR 5 CARBON SEAL, PN30745742, SN 011936802352) PILOTS REPORT HIGH OIL PRESSURE. OIL PRESSURE FOLLOWED THROTTLE HIGH GEARBOX PRESSURE CAUSED BY DETERIORATION OF NR 4 AND NR 5 CARBON SEALS. (K)Aug 23, 2006 · N922JW · Amd FALCON900 · Turbine Engine Oil SystemSDR DJSA20060002Elt · activatedELT ACTIVATED IN FLIGHT.Aug 3, 2006 · N531FL · Amd FALCON20C5 · Emergency Locator BeaconSDR DJFA2006295Engine · fodKIND TRIP ID# 1053869 DURING CLIMB OUT THE CREW REPORTED THAT THE # 1 ENGINE LOST POWER. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT WAS RETURNED TO KIND. AFTER LANDING ALL FAN BLADES WERE FOUND DAMAGED ON THE # 1 ENGINE. FOUR FIRST STAGE FAN BLADES WERE Jul 28, 2006 · N893CW · Raythn HAWKER800XP · Engine (Turbine/Turboprop)SDR 062006CVMA01AEngine · vibrationCLIMBING FL350 HEARD A LOUD BANG/POP SOUND FOLLOWED BY VIBRATION. INDICATION OF ENGINE PROBLEM, FLASHING RED OUT OF LIMITS ITT ON RT ENGINE. PULLED BACK RT ENGINE THROTTLE TO IDLE. ALL OTHER ENGINE PARAMETERS NORMAL. A MILD BURNT OIL SMELL OBSERVED IN CABIJun 25, 2006 · N799S · Raythn HAWKER800XP · Engine (Turbine/Turboprop)SDR CVM2006F00000Wire Harness · chafedDURING ROUTINE REPLACEMENT OF THE MAIN ENGINE FIRE BOTTLES, IT WAS DISCOVERED THAT THE WIRE BUNDLE NEXT TO THE DISCHARGE PIPE FOR THE AFT MAIN ENGINE FIRE EXTINGUISHER HAD CHAFFED THROUGH THE INSULATION OF A 14 GAUGE WIRE AND ARKED ON THE NR4 DISCHARGE PIPE. Jun 8, 2006 · N799S · Raythn HAWKER800XP · Fire Protection System WiringSDR CVM2006F00001Wire Harness · chafedREF: 060003 - AFTER A DISCREPANCY OF WIRE BUNDLE CHAFING ON THE AFT MAIN ENGINE FIRE EXTINGUISHER DISCHARGE LINE WAS FOUND ON LIKE MODEL AC IN OUR FLEET, AN INSPECTION OF THE SAME WIRE BUNDLE WAS PERFORMED ON THIS AIRFRAME. THE INSPECTION FOUND THAT THE WIREJun 1, 2006 · N8186 · Raythn HAWKER800XP · Fire Protection System WiringSDR 2006FA0000652Gauge · brokenTHIS THE THIRD FIRE BOTTLE FOUND, ON 2 DIFFERENT AIRCRAFT WITH THE PRESSURE GAUGE SCALE BROKEN FREE FROM ITS MOUNTED POSITION. THE RESULT WAS A FALSE INDICATION OF AGENT (HALON CBRF3) PRESENT INSIDE THE BOTTLE. THE LOCAL QA MANAGER IS LAUNCHING A FORMAL INVEJun 1, 2006 · N456Q · Lear 45LEAR · Extinguishing SystemSDR CA060516001Inverter · failedAIRCRAFT DEPARTED AND DURING CLIMB-OUT AN INDICATION OF XS1 BUS FAILURE. THE CREW COMPLETED THE COCKPIT ABNORMAL CHECK LIST FOR THE ITEM AND RETURNED TO DEPARTURE. MAINTENANCE WAS ADVISED AND MET THE AIRCRAFT UPON ITS RETURN. INVESTIGATION FOUND THE ODOR OFMay 14, 2006 · Raythn HAWKER800XP · AC InverterSDR DJFA2006232Controller · burnedTRIP ID NR 995418 DURING INITIAL CLIMB TO ALTITUDE WHILE PASSING FL 260, THE CREW HEARD A SINGLE (POP) SOUND FOLLOWED SHORTLY BY A BURNING ELECTRICAL ODOR AND LIGHT SMOKE COMING FROM THE CO-PILOTS WINDSCREEN BASE NEAR THE GLARE SHIELD. AN EMERGENCY WAS DECLAApr 18, 2006 · N817TA · Raythn HAWKER800XP · Flight ControllerSDR DXTA200601332Engine · unknownDURING 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.Apr 5, 2006 · N893QS · Raythn HAWKER800XP · Power Indicating SystemSDR CA060410001Adc · malfunctioned(CAN) THE FLIGHT CREW HAD SNAGGED THE NEUTRAL FUEL TANK FULL INDICATION AS NOT SHOWING FULL WHEN THE TANK WAS ACTUALLY FULL. IN CONJUNCTION WITH THIS DEFECT THEY ALSO REPORTED THAT THE L/VMO TEST WAS NOT FUNCTIONING. BOTH THESE DEFECTS WERE ACTIONED AND DURIApr 4, 2006 · Raythn HAWKER800XP · Air Data ComputerSDR DXTA200601306Throttle Control · out of adjustRIGHT 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 IAWMar 18, 2006 · N893QS · Raythn HAWKER800XP · Fuel Controlling SystemSDR CA060316001Clamp · failedDURING INSPECTION, RT ENGINE COWLING WAS OPENED AND TECHNICIAN FOUND PARTS OF RUBBER HOSE INSIDE COWLING. FURTHER INVESTIGATION LEAD TO OPENING OF THE RT LOWER ACCESS PANEL WHERE THE CLAMP FOR THE RT LOW PRESSURE BLEED AIR TO THE MIXING VALVE DUCT WAS FOUND BMar 9, 2006 · Raythn HAWKER800XP · Engine Air Intake SystemSDR DXTA200601196Filter · unknownENG 2 FUEL ANNUNCIATOR ILLUMINATES AT TAKEOFF THRUST, ABORTED TAKEOFF. REMOVED THE NR 2 ENGINE FUEL FILTER ELEMENT AND REPLACED WITH A NEW FILTER ELEMENT. PERFORMED ENGINE POWER RUNS AND LEAK CHECKS, ALL CHECKS SATISFACTORY. WORK PERFORMED IAW THE HAWKER 80Jan 13, 2006 · N876QS · Raythn HAWKER800XP · Engine Fuel Indicating SystemSDR DXTA200701846Master Cylinder · lowBRAKES FEEL SOFT. THEY SEEM TO WORK FINE BUT PEDALS HAVE TO BE PRESSED ALMOST ALL THE WAY. FOUND FLUID LEVELS IN ALL 4 MASTER CYLINDERS TO BE LOW. SERVICED ALL FOUR MASTER CYLINDERS. CHECKED MUTING OF ALL BRAKE LINES AND ACCUMULATOR PRESSURES. OP CHECKED BRAKJan 9, 2006 · N855QS · Raythn HAWKER800XP · Master Cylinder/Brake ValveSDR DJFA2006185Switch · intermittentDURING DESCENT, FL 350, AC EXPERIENCED A RAPID DEPRESSURIZATION. (MAIN AIR VALVE), (CABIN PRESS), (STALL IDENT) LIGHTS ILLUMINATED. EMERGENCY DESCENT WAS INITIATED. CREW DONNED THEIR OXYGEN MASKS AND SQUAWKED CODE 7700 ON TRANSPONDER. USING FLT DECK HEAT Jan 4, 2006 · N813CW · Raythn HAWKER800XP · Landing Gear Position and WarningSDR BLU2006F00000Engine · failedSOON AFTER TAKEOFF, A NOISE WAS HEARD AND THERE WAS AN IMMEDIATE SPOOLDOWN OF THE LEFT ENGINE. A RETURN WAS EXECUTED AN UNEVENTFUL SINGLE ENGINE LANDING WAS MADE. THE ENGINE IS CURRENTLY BEING REMOVED FROM THE AIRCRAFT AND WILL BE SHIPPED TO MFG FOR EVALUATIJan 2, 2006 · N800NJ · Raythn HAWKER800XP · Engine (Turbine/Turboprop)SDR DXTA200501166Coalescer Bag · odorREPEAT WRITE UP, SHORTLY AFTER TAKEOFF WE SMELLED SMOKE FUMES AND BAGGAGE FIRE/SMOKE LIGHT CAME ON. ALL BAGGAGE COMPARTMENT LIGHTS WERE VERIFIED OFF PRIOR TO DEPARTURE. REMOVED WATER SEPARATOR SEAL, CHECKED FOR CLEANLINESS. CLEANED AND REINSTALLED SOCK. RAN Dec 20, 2005 · N833QS · Raythn HAWKER800XP · Humidity Control SystemSDR DXTA200501164Light · hotSHORTLY AFTER TAKEOFF (APPROX 3000 FT MSL) THE BAG RED SMOKE /FIRE LIGHT ON THE FO'S FOWARD PANEL CAME ON AND WENT OUT AND SMELLED SMOKE AT THE SAME TIME. FOUND SUITCASE ON LIGHT AND LIGHT ON IN BAGGAGE COMPARTMENT, MOVED SUITCASE. SYSTEM OPS CHECKS GOOD AT TDec 19, 2005 · N833QS · Raythn HAWKER800XP · Cargo CompartmentsSDR DJFA2005162Connector · looseCREW REPORTED THAT DURING DESCENT THE LEFT ENGINE BEGAN SURGING UP AND DOWN. THE FUEL FLOW RANGED FROM 400 TO 1,300 LBS / HR. PRIORITY HANDLING WAS REQUESTED AND FIRE RESCUE RESPONSE WAS GIVEN FOLLOWING A NORMAL LANDING IN KMSP. THE ENGINE CONTINUED TO SURGNov 16, 2005 · N829LX · Raythn HAWKER800XP · Engine Fuel System WiringSDR CA051020003Filter · unknown(CAN) THE INDICATORS ON THE PUMP ASSEMBLIES ARE SHOWING A BYPASS CONDITION. WHEN EXAMINED THE FILTERS ARE CLEAN. THESE FILTERS CAN BE LEFT IN SERVICE UP TO 600 HR. BUT ARE NOW TRIPPING THE INDICATOR ANY WHERE FROM 5 TO 500 HRS. WITH THE TYPICAL TIME BEING LESSOct 20, 2005 · Amd FALCON900 · Engine Fuel Distribution
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