Raytheon HAWKER 850XP

Service difficulty reports · 30

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 = 'HAWKER850XP'
  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 G13A2026012016206Oil Cap · mechanic errorDURING CLIMB OUT APPROACHING FL180, THE PF NOTICED THE OIL PRESSURE ON THE LEFT ENGINE FLUCTUATING PLUS OR MINUS 6 PSI (36-42PSI). CONTINUED THE CLIMB WHILE MONITORING, THE OIL PRESSURE CONTINUED TO FLUCTUATE BUT WORSENED AS WE REACHED OUR CRUISE OF FL330. WE Jan 16, 2026 · N921PK · Raythn HAWKER850XP · Turbine Engine Oil SystemSDR 2025F00178Elec Connector · dirtyCREW REPORTED OBSERVING THE #2 ENGINE OIL PRESSURE DECREASE STEADILY ON THE GAUGE FROM NORMAL TO APPROXIMATELY 16 PSI CREW DID NOT NOTE A MASTER WARNING INDICATION LIGHT FOR OIL PRESSURE UNTIL AFTER COMPLETING THE ENGINE SHUTDOWN.. CREW INITIATED AN ENGINE SHUAug 10, 2025 · N921PK · Raythn HAWKER850XP · Nacelle/Pylon System WiringSDR 2024FA0000983Engine · power lossPILOTS FELT LOSS OF POWER ON TAKEOFF ROLL BEFORE V1. TAKEOFF ABORTED OUT OF PRECAUTION. NO WARNING INDICATIONS NOTED ON ANNUNCIATOR PANEL. TAXIED TO RAMP AND PERFORMED GROUND RUN TO TRY DUPLICATING SQUAWK. GROUND RUN PRODUCED NO FAULTS. MAINTENANCE SUMPED BOTHDec 27, 2024 · N188B · Raythn HAWKER850XP · Engine (Turbine/Turboprop)SDR 2RPA2024120400007Windscreen · delaminatedIN CRUISE AT FL 410 IN SMOOTH CLEAR CONDITIONS THE LEFT WINDSCREEN OUTER LAYER OF GLASS STARTED TO DELAMINATE. THE WINDSCREEN WAS OPERATING NORMALLY. THE CREW IMMEDIATELY CHECKED THE CABIN PRESSURE WHICH REMAINED NORMAL WITH A CABIN ALTITUDE OF 8000 FEET AND CDec 1, 2024 · N459J · Raythn HAWKER850XP · Flight Compartment WindowsSDR WWQA2024F00118Switch · failed"UPON GEAR RETRACTION, THE RIGHT MAIN LANDING GEAR IN TRANSIT LIGHT FAILED TO EXTINGUISH. THE CREW RECYCLED THE GEAR FIVE TIMES" AIRCRAFT RETURNED TO TEB. MAINTENANCE REPLACED THE RH MLG DOOR MICROSWITCH WITH NEW AND OPS CHECKED GOOD BY SWINGING THE LANDING GEApr 17, 2024 · N720T · Raythn HAWKER850XP · Landing Gear Position and WarningSDR 2HGR20231121001Sequence Valve · out of sequencePLANE DEPARTED FROM KHDN, AFTER TAKE OFF CREW NOTICED GEAR RED UNSAFE LIGHT, CREW CONTACTED TOWER TO VERIFY GEAR WAS UP, TOWER CONFIRMED THE LEFT GEAR WAS DOWN, CREW LOWERED GEAR DID A LOW APPROACH TO KHDN TO CONFIRM ALL 3 GEAR WERE DOWN & DECIDED TO DIVERT TONov 8, 2023 · N806MC · Raythn HAWKER850XP · Landing Gear Retraction/Extension SystemSDR 2023FA0000347Engine · abnormalLH ENGINE FAILED IN FLIGHT AND FLAMED OUT.Jun 30, 2023 · N816KY · Raythn HAWKER850XP · Engine (Turbine/Turboprop)SDR 9JLA2023021731472None · noneTHE FLIGHT CREW REPORTED THE PILOT'S "A" PANEL HEATING ELEMENT INOPERATIVE. THE WINDSHIELD HEAT SYSTEM WAS PLACED ON MEL FOR CONTINUED OPERATIONS. THE MAINTENANCE PROVIDER REPLACED THE PILOT "A" PANEL WITH NEW WINDSHIELD. OPS CHECKS WERE SATISFACTORY. AIRCRAFTNov 28, 2022 · N999SS · Raythn HAWKER850XP · Window/Windshield SystemSDR E0YA2021010400001Autopilot Sys · failedAUTO PILOT FAILURE DURING CLIMB. CREW DEVIATED FLIGHT PLAN.Jan 2, 2021 · N359BC · Raythn HAWKER850XP · Autopilot SystemSDR 3SRA20201026002Valve · out of adjustDURING LANDING GEAR RETRACTION, THE RIGHT MAIN LANDING GEAR RED LIGHT REMAINED ILLUMINATED. THE CREW RECEIVED A CALL FROM TOWER THAT THE RIGHT LANDING GEAR WAS NOT RETRACTED. THE CREW DIVERTED TO KIND AND LANDED WITHOUT INCIDENT.Oct 23, 2020 · N850TK · Raythn HAWKER850XP · Landing Gear Retraction/Extension SystemSDR 3SRA20201026001Uplock Switch · failedDURING LANDING GEAR RETRACTION, THE RT MAIN LANDING GEAR RED LIGHT REMAINED ILLUMINATED. THE CREW REPORTED NO NOISE TO INDICATE THAT THE GEAR DID NOT RETRACT.Oct 21, 2020 · N850TK · Raythn HAWKER850XP · Landing Gear Position and WarningSDR E0YA2020081280003Pitot Head · obstructedAIRSPEED INDICATION MISCOMPARE FROM LT TO RT. DEBRIS FOUND IN LT PITOT, REMOVED, AND LEAKED CHECKED.Aug 8, 2020 · N359BC · Raythn HAWKER850XP · Pitot/Static SystemSDR CA160317001Pump · malfunctioned(CAN) STBD ENGINE MASTER WARNING FOR LOW OIL PRESSURE ON SHORT FINAL. SHUT DOWN ENGINE ON RUNAWAY. TROUBLESHOOT AND FOUND OIL PUMP TO BE SUSPECT. SOAP SAMPLE TAKEN AND OIL FILTER REPLACED. REPLACED PUMP IAW 79-20-03 AND ADJUSTED TO 44PSI IAW TR-174-72-00-00. Mar 6, 2016 · Raythn HAWKER850XP · Turbine Engine Oil SystemSDR UG8A2015 1207 01Packing · leakingDURING PILOTS PREFLIGHT, PILOT DISCOVERED FUEL DRIPPING FROM APU ENCLOSURE. REPLACED PACKING ON OUTLET FITTING OF APU FUEL CONTROL UNIT IAW GTC 36-150 MM CHAPTER 49 30 52. LEAK CHECKED GOOD.Dec 7, 2015 · N97KL · Raythn HAWKER850XP · APU Engine Fuel and ControlSDR 7GER20151023001Rivet · failedTHE RIVET ATTACHING THE BRAKE WEAR PAD TO BRAKE PRESSURE PLATE FAILED, CAUSING THE WEAR PAD TO BECOME DISLODGED FROM ITS CORRECT LOCATION AND BECOME LODGED BETWEEN THE PRESSURE PLATE AND THE STATIONARY DISC RESULTING IN THE BRAKE NOT BEING ABLE TO ROTATE, CAUSOct 23, 2015 · Raythn HAWKER850XP · Landing Gear Brake SystemSDR CA150703002Rib · corroded(CAN) DURING THE 8 YEAR INSPECTION, WE FOUND RIB 16 ON BOTH WING CORRODED. DAMAGE WAS OUT OF THE SRM REPAIR AUTHORITY, REPAIRED IAW ENGINEERING.Jun 8, 2015 · Raythn HAWKER850XP · Wing, Rib/BulkheadSDR CA150703001Rib · corroded(CAN) DURING THE 8 YEAR INSPECTION, WE FOUND RIB NR 16 ON BOTH WING CORRODED. DAMAGE WAS OUT OF THE SRM REPAIR AUTHORITY, REPAIRED.May 1, 2015 · Raythn HAWKER850XP · Wing, Rib/BulkheadSDR 2015F00057Smoke Detector · false activationCHECK "BAG FIRE" SMOKE DETECTORS - THE "BAG FIRE" ANNUNCIATOR FOR THE SMOKE DETECTOR SYSTEM, FLASHED 3 TIMES THEN EXTINGUISHED. THE CREW VISUALLY VERIFIED THAT NO SMOKE OR FIRE WAS EVIDENT AT EACH SMOKE DETECTOR LOCATION'S, FWD BAGGAGE, AFT BAGGAGE AND LAV BAGApr 12, 2015 · N770CC · Raythn HAWKER850XP · Smoke DetectionSDR EBVR2014041400001Tube · corrodedFUEL LINE FLANGE FOUND BROKEN ACROSS ONE CORNER OF THE FLANGE FLAT. FURTER INVESTIGATION REVEALED PART HAS BEEN CORRODED WHICH LEAD TO A WEAKENING OF THE FLANGE AND SUBSEQUENT BREAKAGE.Apr 14, 2014 · N542M · Raythn HAWKER850XP · Fuel StorageSDR ABFA2014022800001Starter Gen · failedNR 2 ENGINE STARTER/GENERATOR HAD A CATASTROPHIC BEARING FAILURE, ON THE FRONT SHAFT MOUNT OF THE STARTER/GENERATOR. THIS CAUSED A PRONOUNCED ENGINE VIBRATION ON THE NR 2 ENGINE, PROMPTING THE FLIGHT CREW TO SHUT THE ENGINE DOWN IN FLIGHT. COMPONENT WAS O/H,Apr 14, 2014 · N914CE · Raythn HAWKER850XP · Starter-GeneratorSDR T17A201402178005Connector · looseNUMBER 1 ENG FAILED INFLIGHT, COMPLETE ENG SHUTDOWN. ENG N1, 2 FUEL FLOW STARTED TO FLUCTUATE DURING CRUISE. ENG BECAME UNRESPONSIVE & STUCK AT 90%, N1 ITT 908C. ENG FAILED DURING EMERGENCY DECENT AT 17000'. DOWNLOADED THE NR 1 ENG N1 DEEC, DIGITAL ELECTRONFeb 12, 2014 · N403CT · Raythn HAWKER850XP · Engine Fuel System WiringSDR CA120914001Cable · lack of lube(CAN) ON DESCENT, NR 2 ENGINE UNABLE TO RETARD THRUST BELOW 51 PERCENT N1. ACFT WAS DIVERTED, LANDED WITHOUT INCIDENT, NR 2 ENGINE SHUTDOWN USING LP FUEL COCK. RT ENGINE CONTROL TELEFLEX INSPECTION, CHECK AND LUBRICATION CARRIED OUT IAW AMM. ENGINES GROUND RSep 13, 2012 · Raythn HAWKER850XP · Power LeverSDR 9PVA2012F00176Pump · defectiveAFTER LEVEL OFF AT FL380 AND APPROX 18 MINUTES INTO THE FLIGHT THE "ENG 1 FUEL" CAUTION LIGHT ON THE OVERHEAD PANEL ILLUMINATED, INDICATING "EITHER FUEL FILTER BLOCKED OR FUEL OVERHEAT" IAW THE AIRPLANE FLIGHT MANUAL THE NR 1 ENGINE THRUST LEVER WAS REDUCED TOAug 28, 2012 · N850ME · Raythn HAWKER850XP · Engine Fuel PumpSDR 2012F00087Lever · corrodedCOMPONENTS (LEVERS AND ASSOCIATED RODS) FOUND CORRODED. NO CORROSION PREVENTATIVE MATERIAL FOUND ON PARTS. CORROSION EXTENSIVE BUT ONLY ON THESE PARTS IN PARTICULAR. SURROUNDING AREAS IN BETWEEN THE WHEEL WELLS APPEAR TO BE CLEAN AND FREE FROM CORROSION. AApr 6, 2012 · N776RS · Raythn HAWKER850XP · Landing Gear SystemSDR 2010FA0000160Door · frozenACFT WAS ON APPROACH. WHEN THE GEAR WAS EXTENDED THE NOSE GEAR DID NOT COME DOWN. THE CREW DIVERTED TO AND AFTER SOME HIGH "G" MANEUVERS GOT THE NOSE GEAR TO EXTEND. THE ACFT MADE A NORMAL LANDING. THE ACFT WAS JACKED AND A GEAR SWING AND INSP WAS PERFORMED. Feb 9, 2010 · N853CC · Raythn HAWKER850XP · Landing Gear Door Retract SectionSDR 2010FA0000010Valve · malfunctionedTHE ACFT DEPARTED AFTER ROUTINE MX. UPON OPENING THE MAIN AIR VALVES, THE PILOTS NOTICED SMOKE IN THE CABIN, DECLARED AN EMERGENCY AND RETURNED TO THE AIRPORT. INVESTIGATION FOUND HYD FLUID IN THE BLEED AIR DUCTING. DURING SERVICING, HYD FLUID BYPASSED THE Dec 18, 2009 · N255RB · Raythn HAWKER850XP · Hydraulic System, MainSDR DJFA2009007None · noneON GEAR RETRACTION, AFTER TAKEOFF, CREW HEARD A LOUD BANG IN THE NOSE GEAR WELL AREA AND NOTED A RUBBER BURNING ODOR. AIRCRAFT RETURNED TO THE DEPARTURE AIRPORT AND LANDED SAFELY. MAINTENANCE PERFORMED SEVERAL GEAR SWINGS BUT COULD NOT DUPLICATE THE DISCREPAFeb 10, 2009 · N826LX · Raythn HAWKER850XP · Landing Gear SystemSDR T17A081022001Control Valve · inadequateLEFT MAIN LANDING GEAR BRAKES WERE LOCKED UP ON LANDING. THE NR 1 AND NR 2 WHEEL AND TIRE ASSEMBLIES WERE DISTROYED. AFTER REPLACING THE WHEELS, NO DEFECTS COULD BE FOUND WITH THE BRAKE SYSTEM. AS A PRECAUTION THE BRAKE CONTROL VALVE WAS REPLACED AS IT WAS Oct 2, 2008 · N403CT · Raythn HAWKER850XP · Landing Gear Brake SystemSDR V0J2008F00000Eec · inoperativeNEW DIGITAL ELECTRONIC ENGINE COMPUTER WAS INOPERABLE UPON INSTALLATION. (S)Jun 25, 2008 · N1776A · Raythn HAWKER850XP · Fuel Control/Turbine EnginesSDR CA070927004Line · chafed(CAN) DURING SCHEDULE INSPECTION FOUND 2 OIL LINES CHAFING. THE SAME PROBLEM WAS ON BOTH ENGINES.THE PROBLEM COMES FROM THE FACTORY SINCE THE AIRCRAFT IS NEW AND LOW TIME. THE AIRCRAFT HISTORY DOES NOT SHOW ANY MAINTENANCE ACTION BEING PERFORMED IN THAT AREA SSep 26, 2007 · Raythn HAWKER850XP · Turbine Engine Oil System
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