Raytheon HAWKER 800
Service difficulty reports · 83
Newest first. General aviation reporting is voluntary.
Query with SQL
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 aircraft_model_key = 'HAWKER800' 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.
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 aircraft_model_key = 'HAWKER800' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR Y9PA2025060900392Brake Assy · seizedRIGHT MAIN TIRE LOST PRESSURE AFTER TAXI IN AT HOBBY. NOTICED THAT DURING TAXI IN AFTER LANDING ON LEG 1 OF 4 THAT BRAKES SEEMED TO ENGAGE WITHOUT PEDDLES BEING DEPRESSED AS IF ANTI SKIT WAS ACTIVATING BUT SPEED WAS UNDER 5 KNOTS.SDR 2023FA0000594Controller · failedCABIN TEMPERATURE CONTROL SYSTEM FAILED IN FULL HOT CAUSING CABIN TEMP TO CLIMB AND EVENTUALLY CAUSED SMOKE IN THE CABIN.SDR MY5A202308030729Switch · failedENGINE #2 FUEL LIGHT ILLUMINATED AFTER 25 MINUTES OF FLIGHT AT FL320. FOLLOWED CHECKIST PROCEDURE. REDUCED POWER TO IDLE AND LIGHT WENT OUT. DIVERTED TO DEPARTURE AIRPORT, SCOTTSDALE, AZ (KSDL). CALLED MAINTENANCE FOR SUPPORT. REPLACED #2 ENGINE FUEL HIGH TEMPSDR 2022F00273None · none#1 (LEFT) MAIN BOOST PUMP FAILEDSDR 2021F00032Oil System · fluctuatesAFTER DEPARTURE FROM KJVL DURING CLIMB OUT THE CREW NOTICED THE RH ENGINE OIL PRESSURE FLUCTUATING. THE CREW FOLLOWED CHECKLIST PROCEDURES AND SHUT THE ENGINE DOWN AS A PRECAUTION.SDR FVJA20181214001Starter Gen · failedDURING CRUISE FLIGHT AT AN ALTITUDE OF FL380 ENROUTE FROM TORONTO-PEARSON INTERNATIONAL AIRPORT (CYYZ) TO MCCARREN INTERNATIONAL AIRPORT (KLAS) THE CREW EXPERIENCED INTERMITTENT FOLLOWED BY CONTINUOUS TO MODERATE VIBRATION ACCOMPANIED BY A LOW FREQUENT "HUMMINSDR G73R201808225587Cabin Pressure · malfunctionedDURING CRUISE AT FL360, WITH CABIN CONTROLLER SET TO FL380 AND NORMAL PRESSURIZATION. AT TOP OF DESCENT REDUCED POWER SLIGHTLY AND AT THE SAME TIME THE CABIN RATE KNOB TURNED TO MIN AND CABIN CONTROLLER MOVED SLIGHTLY TOWARD FIELD ELEVATION. WITHIN SECONDS SDR G73R20180515445Bushing · wornDURING ARRIVAL, AFTER LEVELLING OFF AT 10,000 FT AN ABNORMAL VIBRATION WAS NOTICED. MOVING EACH THRUST LEVER INDEPENDENTLY INDICATED THAT THE VIBRATION WAS ASSOCIATED WITH THE NR 2 THRUST LEVER MOVEMENT. NR 2 ENGINE WAS REDUCED TO IDLE UNTIL LANDING, AND THESDR C40A201803050001Hinge Bracket · crackedDURING CLIMB, THE LEFT GEAR UNSAFE, IN TRANSIT INDICATION ILLUMINATED WITH NOTICEABLE DECREASE IN PERFORMANCE. DIVERTED WITH UNEVENTFUL FULL STOP LANDING. VISUAL INSPECTION REVEALED LEFT MLG DOOR AFT HINGE BRACKET HAD BROKEN AND REAR OF INBOARD DOOR WAS HANGINSDR 2018F00097Starter Gen · failedENROUTE, ABOUT 3 HOURS INTO FLIGHT, HAD A SMALL VIBRATION THAT LASTED TWO SECONDS AND WENT AWAY. AT FL360 M.72 KEPT GETTING SMALL VIBRATIONS, ENGINE INDICATIONS WERE STANDARD. AT THIS POINT, THOUGHT IT COULD BE A PRESSURE PROBLEM DUE TO RUMBLE IN THE FLOOR OFSDR C40A20171206001Switch · false activationTAKEOFF ROLL AT 50-60KTS, AIRBRAKES OPEN WARNING ILLUMINATED WITH ASSOCIATED WARNING HORN. PILOTS EXECUTED TAKEOFF ABORT AND SAFELY RETURNED TO RAMP AT ATLANTIC AVIATION (KOPF). TROUBLESHOOTING REVEALED FAILED RH AIRBRAKE MICROSWITCH, PART NUMBER 1322ZMK3. REMSDR ZP7A2017080200001Cabin Pressure · malfunctionedCLIMBING THROUGH APPROXIMATELY 17,500 MSL A POPPING SOUND WAS HEARD, THEN THE CABIN ALTITUDE BEGAN TO CLIMB APPROXIMATELY 2000FT PER MINUTE. PROCEDURES IN THE QRH WERE COMPLETED BUT RESULTED IN NO CHANGE TO THE SITUATION. AN EMERGENCY WAS DECLARED AND THE DECISDR G73R2016080400001Controller · inoperativeRIGHT WINDSCREEN GOES INTO OVERHEAT.SDR G73R2016060300001Thermal Switch · defectiveAPU FIRE BELL AND LIGHT SOUNDED AND ILLUMINATED DURING AIRCRAFT ROLL OUT ON LANDING WITH APU OFF.SDR C40A20150924001Plunger · obstructedCRUISE AT FL360, ACFT EXPERIENCED A REAR BAY DOOR MWS INDICATION IMMEDIATELY FOLLOWED BY CABIN ALTITUDE. CREW & PAXS DONNED 02 MASKS. CREW DESCENDED TO SAFE ALTITUDE & RETURNED TO BASE. INSPECTION REVEALED TRASH ON PLUNGER FOR TOILET PREVENTING PROPER SEAL.SDR 9JLA201506247566Controller · defectiveCREW REPORTED THAT DURING FLIGHT THE RT ENG DEEC LIGHT CAME ON AT 86% N1. THE CREW INDICATED THAT THE ENG DIVERTED TO MANUAL MODE. TROUBLE SHOT THE DISCREPANCY & FOUND THAT THE ENG SYNC CONTROLLER WAS DEFECTIVE. THE UNIT WAS R & R WITH AN EXCHANGE UNIT PN 2SDR 9JLA201504227550Jack · contaminatedDURING FLIGHT, FL 330 & 300, THE LT & RT AUTO PILOT SYS DISENGAGED. ABLE TO REENGAGE THE SYS FOR ONLY 2 MIN BEFORE THE SYS DISENGAGED AGAIN. THE SYS WAS TROUBLE SHOT & IT WAS FOUND THAT MOISTURE WAS IN THE GREASE WITHIN THE ELEVATOR TRIM JACKS. THE SERVICE SDR 9JLA201504227561Position Switch · shortedDURING FLIGHT THE AIRBRAKE, OPEN, INDICATION ANNUNCIATION REMAINED ILLUMINATED WITH AIRBRAKES IN THE SHUT POSITION. THE POSITION INDICATOR CB WAS TRIPPED. TROUBLESHOOTING OF THE AIRBRAKE INDICATOR CIRCUIT FOUND THE RT AIRBRAKE MICRO-SWITCH TO BE SHORTING OUTSDR 9JLA201504227560Skin Panel · crackedDURING THE POST-FLIGHT INSPECTION THAT THE RT UPPER AIRBRAKE HAD A 4 INCH CRACK ON THE TOP SKIN ALONG THE TE. NO CAUSE FOR THE CRACK WAS FOUND. REMOVED THE DAMAGED RT UPPER AIRBRAKE PN 25-8WB5-2A. INSTALLED AN OVERHAULED AIRBRAKE PANEL IAW THE AMM & RIGGED.SDR BWVR201503200002Clamp · disengagedDURING ROUTINE MX, ONE OF OUR TECHNICIANS WAS TASKED TO TAKE A SOAP SAMPLE FROM THE ACFT APU. WHILE TAKING THE SAMPLE HE NOTICED THE APU STARTER GEN WAS LOOSE. AFTER FURTHER INVESTIGATION HE FOUND THE CLAMP THAT SECURES THE STARTER GEN TO THE APU WAS SAFETIESDR 9JLA2014101307187Diode · defectiveTHE MULTIFUNCTION DISPLAY WENT BLANK. TROUBLESHOOTING FOUND THAT THE SG WAS INOPERATIVE. FURTHER TROUBLESHOOTING FOUND DIODES CR79 & CR80 DEFECTIVE. IT’S UNCLEAR IF THE DEFECTIVE SG TOOK OUT THE DIODES OR DIODES TOOK OUT THE SG. THE DIODES WERE REPLACED WISDR 9JLA2014040907167Inverter · failedCREW REPORTED THAT THE NR 1 INVERTER FAILED IN FLIGHT. THE FAILED INVERTER WAS REMOVED PN 140-380010-7, SN SG1347 & A REPAIRED INVERTER WAS INSTALLED.SDR 9JLA2014042107165Windshield · defectiveTHE FLIGHT CREW REPORTED THAT THE RIGHT B SCREEN WOULD NOT HEAT IN FLIGHT. TROUBLESHOOTING DISCOVERED THE RT B PANEL WINDSCREEN DEFECTIVE. THE DEFECTIVE WINDSCREEN WAS REMOVED & NEW WINDSCREEN WAS INSTALLED. LEAK & FUNCTIONAL CHECKS GOOD AT THIS TIME.SDR 9JLA2014030406397Window · failedTHE PILOT, SIC, REPORTED THAT WHILE CLIMBING OUT OF FL320 TO FL360, HE HEARD A LOUD BANG. THE SIC STATED THAT HE LOOKED OVER HIS SHOULDER TO THE CABIN & THE PAX ADVISED THAT THE NR 3 LT CABIN WINDOW HAD CRACKED. THE SIC ADVISED THE PIC OF THE EVENT. THE PIC SDR VPQA2014FA0000083Throttle Switch · weakNR 2 T/R FAILED TO DEPLOY UPON LANDING. FOUND NR 2 T/R PIGGY BACK POSITION SWITCH, PN 25-8CX213-1A, HARNESS WIRES BROKEN AT ADEL SECURING POINT DEEP WITHIN THE CENTER PEDESTAL. THE WIRES APPEAR TO HAVE BEEN EXPOSED TO THE ELEMENTS FOR SOMETIME DUE TO DISCOLORSDR 9JLA2014011507160Adc · defectiveTHE FLIGHT CREW REPORTED THAT THE NR 2 ADC INDICATED AN INTERMITTENT OVER SPEED WARNING INFLIGHT & ON THE GND. TROUBLESHOOTING OF THE NR 2 FOUND IT TO BE DEFECTIVE. THE DEFECTIVE ADC WAS REMOVED PN 7000700-668, SN 00078756 & A REPAIRED UNIT WAS INSTALLED & TSDR 9JLA2013110406378Pump · failedFLIGHT CREW REPORTED THAT THE RT ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT CAME ON IN FLIGHT. TROUBLESHOT AND IDENTIFIED THE RT ENGINE DRIVEN HYDRAULIC PUMP AS DEFECTIVE. REMOVED PUMP, AND INSTALLED AN O/H PUMP. LEAK AND OPS CHECKED SATISFACTORY.SDR 9JLA2013110406377Gcu · defectiveDURING THE TAKEOFF ROLL, CREW REPORTED THAT THE NR 1 DC GENERATION SYS FAILED PRIOR 80 KNOTS AND THE TAKEOFF WAS ABORTED. TROUBLESHOOTING IDENTIFIED THE NR 1 GENERATOR CONTROL UNIT AS DEFECTIVE. THE DEFECTIVE GCU WAS R & R WITH A REPAIRED UNIT.SDR 9JLA2013072206365Fire Loop · defectiveTHE FLIGHT CREW REPORTED THAT DURING THE PREFLIGHT INSPECTION THE NR 2 ENGINE FIRE DETECTION SYSTEM FAILED TO TEST. TROUBLESHOOTING DETERMINED THAT THE ZONE 2 FIRE LOOP WAS DEFECTIVE PN 3001-133-900-500-6. INSTALLED NEW FIRE LOOP IAW THE LMM CHAPTER 72-00-05SDR 2013FA0000371Tire · damagedINSTALLED REPAIRED WHEEL ASSY WITH NEW TIRE, AFTER ONE LANDING, ACFT PULLED TO RT DURING TAXI. NOSE WHEEL STEERING OPS CHECKED GOOD, SWAPPED NOSE WHEELS ACFT PULLED TO THE LEFT. REMOVED NOSE WHEELS ASSEMBLIES AND INSTALLED TWO NEW TIRES. TAXI CHECKED GOODSDR 9JLA2013042405688Fan · defectiveCREW REPORTS THE CABIN RECIRCULATING FAN WAS DEFECTIVE. REMOVED THE DEFECTIVE CABIN FAN PN 0901-2, SN 0696. INSTALLED AN O/H UNIT. THIS IS THE THIRD FAN ASSY REPLACED IN ABOUT A YEAR.SDR 9JLA2013011803545Indicator · defectiveDURING THE POST FLIGHT INSPECTION, THE NR 1 ENGINE OIL FILTER BYPASS INDICATOR WAS NOTED IN THE BYPASS POSITION. A SOAP WAS TAKEN AND RESULTS WERE NORMAL. THE BYPASS INDICATOR, PN 3070246-4 ON THE ENGINE WAS SUSPECT TO BE DEFECTIVE AND WAS REPLACED IAW SB TFSDR 9JLA2012110706339Controller · defectiveTHE CREW REPORTED THAT THE RT WINDSCREEN WOULD OVERHEAT WITH THE LT AND RT WINDSHIELD HEATS ON. TROUBLESHOOTING IDENTIFIED THE RT TEMP CONTROL UNIT AS DEFECTIVE PN ND0075-2011. REPLACED UNIT WITH NEW TEMP CONTROL, FUNCTIONAL CHECKS SATISFACTORY.SDR UVVR2012101700025Scissor Link · bentTHE RT MLG UPPER SCISSOR LINK WAS FOUND BENT CLOSE TO THE CENTER PIVOT AREA DURING A PHASE INSPECTION. NO COMPLAINTS FROM THE PILOTS OR OPERATOR THAT THE ACFT HAD ANY GEAR VIBRATION BEFORE THE SCHEDULED MX.SDR 9JLA2012040905660Inverter · failedCREW REPORT THE NR 2 INVERTER FAILED. FOUND INVERTER TO BE DEFECTIVE.SDR 9JLA2012032806316Pump · failedTHE CREW REPORTED THAT THE RT WING FUEL BOOST PUMP FAILED. THE FAILED FUEL BOOST PUMP WAS INSTALLED 8 MONTHS PRIOR AND LASTED ONLY 283.5 HRS AND WAS O/H.SDR 9JLA2012032324205Inverter · failedCREW REPORTED THAT THE NR 1 MAIN INVERTER FAILED. FOUND UNIT TO BE DEFECTIVE. PN 501-1235-01, SN 1170SDR 9JLA2011122806314Pump · defectiveTHE CREW REPORTED THAT THE "HYD 2 LO PRESS" ANNUNCIATOR ILLUMINATED DURING LANDING. TROUBLESHOOTING IDENTIFIED THE NR 2 ENGINE HYD PUMP AS DEFECTIVE. THE PUMP WAS REMOVED FROM SERVICE AND REPLACED WITH O/H UNIT ALONG WITH THE HYD SUCTION FILTER.SDR 9JLA2011120706313Pressure Switch · defectiveTHE CREW REPORTED THE HYDRAULIC PRESSURE NR 2 LOW PRESSURE ANNUNCIATOR ILLUMINATED. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE HYDRAULIC LOW PRESSURE SWITCH DEFECTIVE. REMOVED THE DEFECTIVE SWITCH S/N 6005TW AND INSTALLED A NEW LOW PRESSURE SWITCH P/N 211CSDR 9JLA20110829001Pump · low pressureTHE CREW HAS BEEN REPORTING DURING APU START THAT IT WOULD HANG AT ABOUT 45% FOR ABOUT 5-6 SECONDS AND THEN LET OUT A LOUD "POP" AND THEN CONTINUE ONTO START AND RUN NORMALLY, NOTE: DURING THE START SEQUENCE IT WAS NOTED A FOG OF FUEL WAS BEING EXPELLED FROM TSDR 9JLA20110801001Pump · defectiveTHE CREW REPORTED DURING CLIMBOUT THAT THE ENG 2 FUEL ANNUNCIATOR ILLUMINATED. THE FUEL FILTER HAD BEEN REPLACED 2 DAYS PRIOR WITH SATISFACTORY OPERATIONAL CHECKS. TROUBLSHOOTING FOUND THAT THE ENGINE DRIVEN FUEL PUMP WAS DEFECTIVE. P/N 3070850-57 S/N 396995SDR CA110614011Turbine Blades · damaged(CAN) ON CLIMB-OUT THROUGH 25,000 FT A LARGE BANG WAS HEARD AND MODERATE VIBRATION FELT THROUGH THE REAR OF THE ACFT FOLLOWED BY AN EXHAUST ODOR. AIRCRAFT LEVELLED OUT AT 26,000 FT. ALL INDICATIONS WERE WITHIN LIMITS, BUT THERE WAS A LOWER ITT, N1, N2 AND SDR 9JLA2650Switch · intermittentCREW REPORTED THAT THE AIRBRAKE INDICATOR WAS INOP. REQUIRED SYSTEM TO BE DEFERRED. TROUBLESHOT SYSTEM AND FOUND THE LT AIRBRAKE SWITCH TO BE INTERMITTENT. REMOVED THE DEFECTIVE SWITCH AND INSTALLED A NEW SWITCH P/N 1322ZMK3.SDR 9JLA03503Pressure Switch · defectiveTHE FLIGHT CREW REPORTED THE "HYD 1 LO PRESS" ILLUMINATED AFTER THE FINAL FLAP SETTING AND REMAINED ON. TROUBLESHOOTING FOUND THE NR 1 HYD PRESSURE SWITCH P/N 15185-4SN1 TO BE DEFECTIVE. A NEW SWITCH WAS INSTALLED, FUNCTIONAL CHECKS SATISFACTORY.SDR V0JA041176HOil System · low pressureDURING TAXI TO RUNWAY THE CREW WAS ALERTED TO LOW OIL PRESSURE IN THE NR 1 ENGINE BY THE MWS ANNUNCIATORS. THE LOW OIL PRESSURE WAS VERIFIED BY THE NR 1 ENGINE OIL PRESSURE GAUGE AND THE ENGINE WAS SHUTDOWN FOR PRECAUTIONARY MEASURES. TECH WAS CALLED IN TO TSDR 2011F00036Starter Gen · failedACFT EXPERIENCED MODERATE VIBRATION IN CRUISE, FLIGHT CREW FELT VIBRATION WAS FROM NR 2 ENGINE, FOLLOWED SHORTLY AFTER WITH GEN 2 FAIL INDICATION, CREW SHUTDOWN NR 2 ENGINE, FLIGHT DIVERTED FOR NON-EVENTFUL SINGLE ENGINE LANDING. MX REMOVED NR 2 ENGINE STARTESDR 2011F00040Cooling Turbine · defectiveCREW REPORTED NOISE IN THE AIR CONDITIONING SYS, TROUBLESHOOTING FOUND THE COOLING TURBINE ASSY TO HAVE A BAD VIBRATION WHILE OPERATING. REMOVED THE DEFECTIVE COOLING TURBINE ASSY PN 203880-2-2, SN 68-885 AND INSTALLED AN O/H UNIT.SDR 9JLA20110107001Position Switch · shortedTHE FLIGHT CREW DISCOVERED DURING THE PREFLIGHT CHECKS A SSU/FLAP FAULT INDICATION. MX TROUBLESHOT THE FAULT AND FOUND BOTH THE RT INBD/OTBD FLAP POSITION FLAP SWITCHES SHORTED TO GROUND AND THE F5 3AMP FUSE FOR THE NR2 SSU WAS OPEN. BOTH FLAP POSITION SWITCHSDR 2010F00226Annunciator · activatedCREW REPORTED THE "ENG 2 FUEL" ANNUNCIATOR ILLUMINATED DURING FLIGHT.SDR BKEA201008011Valve · openDURING REPOSITION FLIGHT WITH NO PASSENGERS ON ACFT, AFTER TAKEOFF. DURING CLIMB OUT, ACFT EXPERIENCED IN FLIGHT SMOKE IN CABIN. ACFT RETUREND TO DEPARTURE, HAVING DECLARED AN EMERGENCY, COCKPIT AUX HEAT VALVE WAS FOUND PARTIALLY OPEN AFTER MX, THIS WAS THE F
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