Raytheon HAWKER 800XP
Service difficulty reports · 916
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 = 'HAWKER800XP' 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 = 'HAWKER800XP' 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 Y9PA2026031100169Brake Assy · separatedNO. 4 BRAKE PAD SEPERATED WHEN AIRCRAFT WAS BEING TOWED OUT OF HANGAR CAUSING THE BRAKE TO LOCK UP.SDR 2026F00024Windshield · crackedPILOT'S "A" SCREEN OUTER LAYER CRACKED AT FL370. EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED TO KRDU. LANDING WAS SUCCESSFUL WITH NO FURTHER ISSUE.SDR MDGA202602100001Hanger Assy · fracturedAFTER DEPARTURE UPON SELECTION OF GEAR UP THE LEFT MAIN LANDING GEAR REMAINED EXTENDED. TOWER FLYBY CONFIRMED SINGLE LEG EXTENSION. THE DECISION WAS MADE TO DIVERT TO LISBON PORTUGAL FOR BETTER AVAILABILITY OF SERVICES. THE AIRCRAFT DIVERTED AND LANDED WITHOUTSDR Y9PA20251111001Display · inoperativeMFD DISPLAY INOPERATIVE. DOES NOT DISPLAY ANYTHING.SDR EXFA2025FA0000730Warning Message · false activationUPON REDUCING POWER FOR DESCENT FLIGHT CREW NOTICED HYDRAULIC LOW PRESSURE LIGHTS ON. COULD NOT DUPLICATE ON THE GROUND.SDR 2025FA0000730Hydraulic System · low pressure#1 AND #2 HYDRAULIC LOW PRESSURE LIGHT ON. HYDRAULIC @ 2300PSI. PERFORMED GEAR FREE LANDING PROCEDURE.SDR EXFA2025120800728Pipe · crackedWHILE IN CRUISE FLIGHT, CREW NOTED HYDRAULIC LOW PRESSURE LIGHTS ON, ENGINES 1 AND 2 WITH A HYDRAULIC PRESSURE OF 2300 PSI. CREW DIVERTED TO AN ALTERNATE AIRPORT EXTENDING LANDING GEAR MANUALLY PRIOR TO LANDING.SDR 2025FA0000728Hydraulic Line · leakingHYDRAULIC LOW PRESSURE LIGHTS #1 AND #2 FLIGHT LIGHTS IN HYDRAULIC PRESSURE INDICATOR READ 2300 PSI. CREW PERFORMED FREEFALLING LANDING GEAR PROCEDURE.SDR 2025FA0000729Instrument Panel · faultedSTANDBY INSTRUMENT INOPSDR 2RPA2025050100008Duct Clamp · looseON MAY 1, 2025, N80PK DEPARTED KBCT IN ROUTE TO KHPN WITH PAX. AT FL410 THE CREW NOTICED THE CABIN RATE BEGINNING TO CLIMB. SHORTLY AFTER, THE CABIN ALT LIGHT ILLUMINATED AND ALL O2 MASKS DEPLOYED. CREW ALERTED ATC OF THE ISSUE. THE CREW COMPLETED EMERGENCY CHSDR 2025F00049Squat Switch · inoperative“ AT FLIGHT LEVEL 380 IN NORMAL CRUISE FLIGHT WE RECEIVED AUDIBLE AND MWS PANEL WARNINGS OF LOSS OF PRESSURIZATION. WE DONNED MASKS AND IMMEDIATELY BEGAN AN EMERGENCY DESCENT TO 15K FEET, DECLARING AN EMERGENCY WITH ATC.”SDR UVCA202502210016Landing Gear · activeAIRCRAFT DEPARTED HVN IN LIGHT RAIN/ WINTRY MIX WEATHER TEMPERATURE 35 DEGREES HEADED OMA FOR A FUELING EVOLUTION, AIRCRAFT CLIMBED DIRECT TO THEIR ASSIGNED ALTITUDE 38,000 FT AND WAS THERE FOR 3.8 HRS. THE TEMPERATURE AT OMA WAS 12 DEGREES AT NOON. (PILOTS NASDR G13A20250214001Warning Message · illuminatedAT FL380 ENROUTE AN IAS AND MACH TRIM FAIL MESSAGE CAME ON WHICH DISABLED THE AUTOPILOT AND YAW DAMPENER. AFTER ESTABLISHING CONTROL WE BEGAN RUNNING THE CHECKLIST WHICH DIRECTED US TO REDUCE SPEED TO MACH .73. WE WERE UNABLE TO GET RID OF THE IAS FLAG WITHOUTSDR UVCA202501270017Outflow Valve · warning messageBETWEEN FLIGHT LEVEL'S 370 & 380 AT THE POINT OF LEVELING OFF AT 380 THE CABIN ALT RED ANNUNCIATOR ON THE MASTER WARNING PANEL ILLUMINATED AND THE AURAL HORN SOUNDED, AND THE PILOTS CHECKED THE PRESSURIZATION CONTROLLER AND NOTICED THE CABIN ALTITUDE GAUGE NEESDR 2025F00016Apu · contaminatedSMOKE IN COCKPIT CAUSED BY DEICING FLUID IN APU INTAKE DURIMNG DEICING PROCEDURES ON GROUND PRIOR TO TAKEOFFSDR 2RPA2024111800006Wire Harness · pinchedON LANDING IN BUF, AFTER GEAR EXTENSION AND FLAPS 45 NOTICED NO GREEN LANDING GEAR LIGHTS. NOSE GEAR PIN WAS OUT INDICATING DOWN AND LOCKED NOSE GEAR. PERFORMED GO AROUND, FOUND GEAR LIGHTS CB POPPED, TRIED TO RESET ONCE, WOULD NOT RESET. CREW FORGOT TO CHECK SDR OZTA202407190170Air Duct · buckledDURING CRUISE PORTION OF FLIGHT AT ALTITUDE 39,000 FT. FLIGHT CREW EXPERIENCED CABIN DECOMPRESSION, DONNED THEIR OXYGEN MASKS, DECLARED EMERGENCY, AND DIVERTED FROM DESTINATION TO KLBB. FAILURE OF CABIN PRESSURIZATION MIXER DUCT 25-8VF561-1A AND RUBBER COUPLINSDR 2024FA0000004Pitot System · blockedLOST AIRSPEED INDICATOR DURING DESCENT IN EXCESSIVE/SEVERE ICING. ALSO RECEIVING A PITOT/VANE HEAT FAILURE ANNUNCIATOR LIGHT. PERFORMED VISUAL INSPECTION OF PILOTS/COPILOT'S PITOT/STATIC PROBES. PERFORMED TEST OF PILOT/COPILOT PITOT PROBE AND STATIC PLATE HESDR 2024F00000Controller · failedON CLIMB OUT FROM DENVER, CENTENNIAL, (KAPA), THE AIRPLANE WOULD NOT PRESSURIZE. THE CREW ELECTED TO RETURN TO THE POINT OF DEPARTURE. MAINTENANCE WAS SUMMONED. IT WAS DETERMINED THAT THE PRESSURIZATION CONTROLLER HAD FAILED. AN OVERHAULED PRESSURIZATION CONTSDR 2023FA0000835Mixing Valve · stuckAS FLIGHT CREW BEGAN DESCENT FROM FL380 TO THEIR DESTINATION AIRPORT KBOW CABIN ALTITUDE BEGAN TO CLIMB AND HIGH CABIN ALTITUDE WARNING HORN CAME ON . CABIN OXYGEN MASKS DID DEPLOY AND FLIGHT CREW DID DON THEIR OXYGEN MASKS. FLT CREW BEGAN RAPID DESCENT TO BELSDR 2023F00336Unknown · unknownAFTER TAKEOFF FROM TETERBORO, NJ (KTEB), CLIMBING THROUGH FL 250, THE UPPER AND LOWER NAVIGATIONAL SCREENS ON THE CAPTAINS SIDE (LEFT), WENT BLANK. ON THE FIRST OFFICER SIDE (RIGHT), THERE WAS NO FLIGHT DIRECTOR, NO AUTOPILOT AND NO LNAV. THE FIRST OFFICER FLESDR 2023F00330Unknown · unknownON CLIMB OUT LEFT ENGINE SHUT DOWN WITH OIL SMELL IN CABIN. AFTER LANDING NOTED NO OIL INDICTING IN SIGHT GAGESDR 1JAA20231011004Unknown · unknownAIRCRAFT DEPRESSURIZED DURING CLIMB FROM KBCT. CREW INITIATED DECENT TO 10000FT., PERFORMED THE DEPRESSURIZATION CHECKLIST, AND HELD TO BURN OFF FUEL AS REQUIRED. LANDED AIRCRAFT SAFELY AT KPBI FOR MAINTENANCE.SDR 2023FA0000468Mount · crackedTHE LOWER ENGINE MOUNT WAS FOUND TO BE CRACKED DURING MAJOR ENGINE INSPECTION NDT TASK 530017.SDR 9JLA2023022140523None · noneTHE FLIGHT CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE IN AUTOMATIC MODE CONTROL. THE MAINTENANCE PROVIDER TROUBLESHOT THE SYSTEM TO A CLOGGED JET PIPE AND JET PUMP REQUIRING CLEANING. FOR WORK PERFORMED REF HAWKER AMM. OPS CHECKS WERE PERFORMED AND FOUND SDR 2023F00048Tire · damagedUPON LANDING AT BURLINGTON, WA (KBVS) THE #1 AND #2 TIRES SCUFFED BEYOND SERVICEABILITY., THE #1 AND #2 TIRES AND WHEELS WERE REPLACED AND THE AIRPLANE WAS RETURNED TO SERVICE. SDR 2RPA2023011700002Engine · stalledWHILE CLIMBING OUT A HIGH FREQUENCY SOUND OCCURRED AT ABOUT 10,000FT. AT ABOUT 25,000FT A STRONG VIBRATION DEVELOPED AND THE SOUND INTENSIFIED AND CABIN AND COCKPIT BEGAN TO FILL WITH SMOKE. ALL ENGINE INSTRUMENTS LOOKED NORMAL ALTHOUGH CLIMB PERFORMANCE SEEMESDR 9JLA2022122939632Rmu · defectiveTHE FLIGHT CREW REPORTED THAT THE CO-PILOTS INTERPHONE WAS INOP, CONTINUOUS STATIC WAS EMITTED FROM SPEAKERS AND CO-PILOTS OXYGEN MASK MICROPHONE WAS INOP DURING FLIGHT. THE MAINTENANCE PROVIDER TROUBLESHOT AND DETERMINED THAT THE NR 2 RADIO MANAGEMENT UNIT (RSDR YQKA202211290001Seal · damagedREAR BAY OVERHEAT ILLUMINATED DURING DEPARTURE CLIMB TO CRUISE ALTITUDE.SDR 9JLA2022092039607Computer · failedTHE FLIGHT CREW REPORTED THAT THE AOA INDEXER WAS STUCK AT 1.0 WHILE IN FLIGHT. THIS DISCREPANCY WAS DEFERRED UNDER MEL 34-20-5 AND OPERATIONS WERE ABLE TO CONTINUE. DURING THE MAINTENANCE EVENT THE MAINTENANCE PROVIDER REMOVED THE AOA COMPUTER/INDICATOR AND ISDR MDGA8733081722Fuel Control · power lossENGINE POWER REDUCED FOR DESCENT AND UPON LEVEL OFF ENGINE WOULD NOT ACCELERATE ABOVE FLIGHT IDLE. ENGINE WOULD NOT RESPOND IN MANUAL MORE. ENGINE SECURED AND AIRCRAFT LANDED WITHOUT FURTHER ISSUE. FUEL CONTROL REPLACED.SDR 9JLA2022081233201Controller · faultyTHE FLIGHT CREW REPORTED A PRESSURIZATION ISSUE ON TAKEOFF , THE CABIN CLIMBED TO 2000 FT AND THE DESCENDED TO 5000 FT. THEY INDICATED THE PRESSURIZATION FLUCTUATED WITH ENGINE POWER CHANGES DURING DESCENT. THE BASE MAINTENANCE TEAM TROUBLESHOT AND SUSPECTED SDR 2022FA0000401Brake · misoverhauledHAD THE #3 BRAKE ASSY FAIL DURING TOWING OPERATIONS CAUSING THE BRAKE TO LOCK UP AND SHED PARTS. UPON INSPECTION AFTER REMOVAL AND A SECOND FAILURE IN THE FLEET WE NOTED THAT IT APPEARS THAT THE RIVETS THAT HOLD THE BRAKE FRICTION MATERIAL WERE INSTALLED INCORSDR 2022F00300Brake · binding#2 BRAKE ASSEMBLY LOCKED UP WHEN TOWING AIRCRAFT INTO HANGAR. UPON REMOVAL AND INSPECTION OF BRAKE ASSEMBLY IT WAS FOUND THAT BRAKE PADS HAD SEPARATED FROM THE STATOR ASSEMBLY'S. THIS APPEARS TO BE CAUSED BY IMPROPER INSTALLATION OF THE RIVETS. BRAKE UNIT HAS SDR 2022F00254Pump · failed#2 (RIGHT) HYDRAULIC PUMP FAILURE.SDR 6RNA2022F00135Flap System · failedUPON APPROACH TO LAND, FLAPS FAILED TO MOVE FROM ZERO. CREW PERFORMED ZERO FLAP LANDING PROCEDURE AND DECLARED EMERGENCY AS A PRECAUTION.SDR CWQA20220119001Rod End · out of limitsDURING APPROACH FLAPS FAILED TO DEPLOY. CHECKLIST FOLLOWED, EMERGENCY DECLARED, AND UNEVENTFUL LANDING PERFORMED. MAINTENANCE EVALUATION FOUND CUT-OFF LEVER TO FLAP SYNCHRONIZER RECEIVER UNIT TO BE SLIGHTLY OUT OF LIMITS. ADJUSTED CUT-OFF LEVER ROD END. PESDR OZCA25854509JUL21Windshield · crackedLEFT WINDSHIELD CRACKEDSDR 9JLA2021060230522Computer · faultedTHE FLIGHT CREW REPORTED THAT DURING FLIGHT THE ALTITUDE SELECT FAILED, COULD NOT SELECT ALTITUDE. RED ASEL INDICATION WAS ILLUMINATED. THE MAINTENANCE PROVIDER TROUBLESHOT AND DETERMINED THAT THE RIGHT FLIGHT GUIDANCE COMPUTER WAS FAULTY. THE FAULTY UNIT WAS SDR 2021F00053Sleeve · detachedSYSTEM TROUBLE SHOT AND FOUND HOSE/SLEEVE UP STREAM OF WATER SEPARATOR DETACHED. ACCESS GAINED BY REMOVING DUCT INSTALLATION AIR CONDITION SYSTEM ASSY PN 25-8VF773-1 TO ACCESS AND RE-SECURE HOSE/SLEEVE CONNECTION PN BAS169B3-550-030. HOSE/SLEEVE CONNECTION PN SDR 9JLA2021020430507Relay · defectiveDURING MAINTENANCE GROUND CHECKS THE MAINTENANCE TEAM DISCOVERED THAT THE ELECTRICAL EXTERNAL GROUND POWER WOULD NOT ENERGIZE AIRCRAFT SYSTEMS. TROUBLESHOOTING DETERMINED THAT THE GROUND POWER CONTACTOR RELAY WAS DEFECTIVE. REMOVED AND REPLACED WITH A NEW GROUSDR 9JLA2021011830500Adc · intermittentTHE FLIGHT CREW REPORTED THAT IN FLIGHT FL280 THE AUTOPILOT STARTED AN UNCOMMANDED CLIMB, 300' WHEN CREW CORRECTED. IN THE DESCENT IN VNAV AS IT WAS LEVELING IN AGAIN INITIATED AN UNCOMMANDED CLIMB 500' GAIN BEFORE BEING CORRECTED. THE MAINTENANCE VENDOR TROSDR 3WTR20210104Wire Harness · chafedFOUND WIRE BUNDLE CHAFING INTO LOWER OUTBOARD WING SKIN LOCATED BETWEEN RIB 15 AND RIB 16 IN THE AFT BAY. THIS AREA IS DIFFICULT TO INSPECT AND THIS PROBLEM WAS DISCOVERED AFTER WING TIPS WERE REMOVED FOR WINGLET INSTALLATION (INCORPORATION OF STC ST01411SE).SDR 9JLA2020120929950Actuator · leakingTHE FLIGHT CREW REPORTED THAT DURING POST FLIGHT CHECKS HYDRAULIC FLUID LEAKING FROM BOTH SIDES OF THE VERTICAL STAB AND UNDERNEATH THE HORIZONTAL STAB. THE MAINTENANCE VENDOR DISCOVERED THAT THE RUDDER SERVO ACTUATOR WAS LEAKING EXTERNALLY. THE SERVO WAS RESDR MDGA873311072020Lamp · inoperativeWHILE LANDING AT KPHL, THE NOSE LANDING LIGHT DID NOT ILLUMINATE AND A GO-AROUND WAS INITIATED. AFTER COMPLETION OF THE QRH, A LOW FLY-BY OVER THE RUNWAY WAS CONDUCTED AND THE CONTROL TOWER INDICATED THAT THE LANDING GEAR APPEARED TO BE IN THE DOWN POSITION. SDR 9PMA2020121500538Link · lack of lubePILOT REPORTS FUEL TRANSFER HANDLE HARD TO PULL INTO TRANSFER MODE. UPON FURTHER INSPECTION FOUND FUEL TRANSFER LINKAGES IN BELLY WERE HARD TO MOVE DUE TO LACK OF LUBRICATION. CLEANED AND LUBRICATED ALL LINKAGES IN BELLY PANEL, ONCE COMPLETED FUEL TRANSFER HSDR MDGA2020030500000Cdu · malfunctionedTHE AIRCRAFT SMELLED SMOKE, THE CREW LANDED THE AIRCRAFT IN MCI WITHOUT INCIDENT. MAINTENANCE WAS SENT TO THE AIRCRAFT AND REPORTED THAT THE SMELL CAME FROM THE #1 CDU UNIT. THE UNIT STARTED TO WORK BUT WE DECIDED TO REPLACE THE UNIT. THE UNIT IS AT COLLINS ANSDR P6UR2020010298001Circuit Breaker · burnedDURING ACCOMPLISHMENT SCREEN HEAT CIRCUIT BREAKERS INSPECTION (F6 INSPECTION) OVERHEATING/MELTING OF THE CIRCUIT BREAKER BODY WAS DETECTED.SDR CDNA20191226002Mixing Valve · bentPILOTS REPORT "REAR BAY OVERHEAT" ANNUNCIATOR ILLUMINATED DURING CRUISE FLIGHT. DESCENT WAS REQUESTED BUT NOT AUTHORIZED BY ATC, SO AN EMERGENCY WAS DECLARED IN ORDER TO DESCEND. WARNING LIGHT EXTINGUISHED A SHORT TIME AFTER DESCENT WAS COMPLETED. INSPECTIONSDR MDGA202012045254Warning Message · false activationON ROLL OUT THE AIRCRAFT SHOWED THAT THE OIL PRESSURE WAS LOW THE PILOT ABORTED AND RETURNED TO THE RAMP. UPON FURTHER INVESTIGATION THE CREW DETERMINED THAT AFTER AN ENGINE RUN ON THE RAMP THAT THE OIL PRESSURE WAS READING WITH I LIMITS AND CONTINUED THE TRIP
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