Raytheon HAWKER 900XP
Service difficulty reports · 141
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 = 'HAWKER900XP' 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 = 'HAWKER900XP' 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 2026FA0000839Bracket · out of positionRIGHT ENGINE (#2) REAR COWLING BRACE PIN CABLE CAUGHT AROUND THROTTLE LEVER AND WOULD NOT ALLOW THROTTLE MOVEMENT. CABLE AND BRACKET WERE ADJUSTED TO PREVENT FUTURE ISSUES. THIS OCCURRED AFTER ENGINE START ON THE GROUND.SDR E0YA2025FA0000081Engine · failedNUMBER 1 ENGINE FAILURE AT FL150. CREW HEARD A BANG, AIRCRAFT YAWED, ENGINE ROLLBACK, NO THRUST AVAILABLE, ITT STARTED TO RISE AND CREW SHUTDOWN. DIVERTED AND LANDED WITHOUT FURTHER ISSUE.SDR 3SRA20240425001Bearing · destroyedCREW INDICATED ON TAXI AFTER LANDING A VIBRATION/NOISE FROM L/H SIDE OF AIRCRAFT. AIRCRAFT WAS JACKED AND THE #1 MAIN WHEEL HAD SIDE TO SIDE PLAY IN THE WHEEL. UPON REMOVAL OF THE #1 WHEEL, INSPECTION REVEALED THE INNER BEARING SEPARATED WITH PART OF THE BEASDR 2023FA0000753None · noneANY HAWKER AIRCRAFT THAT HAS WINGLETS WILL RUN OUT OF NOSE DOWN TRIM IF IT IS NOT SET TO FULL AVAILABLE TRAVEL WITH THE TOLERANCE. TRAVELS AS STATED IN THE AMM ARE 1 DEGREE 45 MIN +/- 15 MIN. IF TRAVELS ARE SET TO NOMINAL (1 DEG 45 MIN) THEN IT WILL RUN OUT SDR 2023F00179Fitting · crackedCREW REPORTS AGGRESSIVE VIBRATION THROUGH THE MAIN LANDING GEAR UPON TOUCHDOWN. UPON PERFORMING VISUAL INSPECTION OF THE MAIN LANDING GEAR, DISCOVERED THE LEFT HAND SIDE STAY WING MOUNTED ATTACHMENT FITTING CRACKED.SDR Y9PA4202303210001Circuit Breaker · burnedDURING A CREW TRAINING SESSION THE DIRECTOR OF OPS FOUND 3 CIRCUT BREAKERS ON WINDOW HEAT TEST PANEL BEHIND THE CO-PILOT (SUB PANEL B)POPPED AND UPON FURTHER INVESTIGATION, FOUND ALL 3 CIRCUT BREAKERS HAD OVERHEATED AND MELTED THE PLASTIC EXTERNAL COVERS ANDSDR DBCA202212200010Fuel Nozzle · failedPRIOR TO POWER APPLICATION ON TAKEOFF THE NR 2 ENGINE ROLLED BACK. CREW EXITED THE RUNWAY AND RETURNED TO RAMP. MTN REMOVED AND INSPECTED ENGINE. FOUND FUEL NOZZLES UNSERVICEABLE.SDR DBCA202212070009Display · failedDURING TAKE-OFF ROLL PILOT'S PFD WENT BLANK. CREW EXECUTED A LOW SPEED ABORT AND RETURNED TO BED.MTN REMOVED AND REPLACED PILOT'S PFD WITH OVH UNIT. OPS CHECKED GOOD.SDR 9JLA2022080333655Pressure System · inoperativeTHE FLIGHT CREW DESCRIBED HAVING A PRESSURIZATION ISSUE DURING THE CLIMB AFTER TAKEOFF. THE FLIGHT CREW ELECTED TO RETURN BACK TO THE AIRPORT AND LAND FOR MAINTENANCE CONSIDERATIONS. THE BASE MAINTENANCE TEAM INSPECTED THE TAIL AREA AND FOUND THE WATER SEPARATSDR 2022FA0000521Compressor Blade · failedAIRCRAFT DEPARTED KHLN JULY 31 2022 AROUND 9:55 AM MDT CLIMBING THROUGH 25,000FT PILOT REPORTED LOUD BANG FROM #2 ENGINE AND THEN THE ENGINE ROLLED BACK AND SHUTDOWN. THEY THEN TURNED BACK AROUND AND LANDED AT KHLN.SDR 3SRA20220110001Fuel Control · inoperativePHYSICAL ROLLBACK OF #1 ENGINE FOLLOWED BY THE AMBER #1 ENGINE COMPUTER LIGHT ILLUMINATING. ENGINE CONTINUED TO OPERATE IN MANUAL MODE. AIRCRAFT RETURNED TO KSUSSDR 9JLA2021120812616Tcas System · intermittentTHE FLIGHT CREW REPORTED OF A INTERMITTENT TCAS FAIL ON THE PDF. THE MAINTENANCE TEAM DETERMINED THE TCAS PROCESSOR WAS DEFECTIVE AND WAS REMOVED AND REPLACED WITH AN OVERHAULED UNIT. OPS CHECKS WERE SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICESDR 9JLA2021120612616Tcas System · defectiveTHE FLIGHT CREW REPORTED ON FLIGHT LEG #2 THE TCAS FAIL INTERMITTENT ON PRIMARY FLIGHT DISPLAY. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE TCAS RECEIVER WAS DEFECTIVE. THE DEFECTIVE UNIT WAS REMOVED AND AN OVERHAULED UNIT WAS INSTALLED. OPS CHECKS WERSDR 9JLA2021120634618None · noneTHE FLIGHT CREW NOTED FUEL LEAKING FROM THE VENTRAL FUEL TANK AFTER LANDING. OPERATIONS WERE CONTINUED PER MEL 28-22-1-2. THE MAINTENANCE TEAM DISCOVERED THE REFUELING COUPLING CONNECTOR WAS AT FAULT FOR LEAK. THE O-RINGS ON THE PRESSURE REGULATING VALVE WAS RSDR 2021FA0000261Bushing · migratedTHE HAWKER 900XP MAINTENANCE MANUAL "POWER PLANT (ENGINE CHANGE) - REMOVAL/INSTALLATION" CHAPTER XP-71-00-01-401 PARAGRAPH 4. B. (3) (A) (B), (5) (A) (B) READS TO INSTALL THE FWD TOP AND BOTTOM MOUNT BOLTS THE OPPOSITE DIRECTION AS THE FIGURE 410. NEITHER THE SDR 3SRA20210922001Pressure System · inoperativeAFTER TAKEOFF CREW REPORTED THAT THE AIRCRAFT WAS NOT PRESSURIZING. PIC RETURNED TO AIRPORT AND LANDED WITH NO PROBLEMS.SDR 9JLA2021081025962Switch · defectiveTHE FLIGHT CREW REPORTED THAT DURING LANDING THE RIGHT THRUST REVERSER GREEN REVRS LIGHT FLASHES INTERMITTENTLY AND EXTINGUISHES WITH TR ACTIVATION. THEREFORE NOT ALLOWING THE RIGHT TR TO POWER UP. OPERATIONS WERE CONTINUED ON MEL. THE MAINTENANCE TEAM TROUBLESDR 9JLA2021080227994Terminal · dirtyTHE FLIGHT CREW REPORTED THAT AFTER STARTING THE NO1 ENGINE THE NO2 ENGINE WOULD NOT START. NO1 ENGINE START SELECT DID NOT ILLUMINATE AND THERE WAS NO ENGINE ROTATION. THE MAINTENANCE VENDOR FOUND THE "B4" CIRCUIT BREAKER ON THE ZL PANEL FOR MAIN START CONTROSDR 9JLA2021072825960Warning Message · false activationTHE FLIGHT CREW REPORTED A "TCAS FAIL" ANNUNCIATION ON THE PDF AND TCAS TEST FAIL AURAL ANNOUNCEMENT DURING PREFLIGHT TESTING. OPERATIONS WERE CONTINUED PER MEL. THE MAINTENANCE VENDOR RESET THE TCAS CIRCUIT BREAKER AND PERFORMED FAULT DIAGNOSTIC CHECKS, COULDSDR UG8A21P04261349JFI/O Module · malfunctionedRED TRIM ANNUNCIATOR ILLUMINATED CONTINUOUSLY DURING ALL MODES OF FLIGHT, CLIMB, CRUISE AND DESCENT. THE LIGHT WOULD ILLUMINATE SHORTLY AFTER AP WAS ENGAGED. WE VERIFIED AIRCRAFT WAS PERFECTLY TRIMMED PRIOR. THE AP KEPT ADDING NOSE-UP TRIM, EVEN WHEN NOT RESDR 9JLA2021041627971Controller · defectiveTHE FLIGHT CREW REPORTED THAT DURING FLIGHT THE COPILOTS A WINDSCREEN DID NOT HEAT. THE MAINTENANCE TEAM DETERMINED THAT THE THERMAL CONTROLLER WAS DEFECTIVE. THE DEFECTIVE CONTROLLER WAS REMOVED AND A NEW UNIT WAS INSTALLED. OPERATIONAL CHECKS WERE SATISFACTOSDR 9JLA2020110929419Wire Harness · defectiveTHE FLIGHT CREW REPORTED THAT THE NR 1 ENGINE N2 INDICATIONS WERE ERRATIC IN FLIGHT. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THAT THE NR 1 ENGINE HARNESS WAS DEFECTIVE. THE MX VENDOR REPLACED THE WIRING HARNESS WITH A NEW HARNESS. OPERATIONS CHECKSDR 9JLA2020110929404Wire Harness · defectiveTHE FLIGHT CREW REPORTED THAT THE NO 1 ENGINE N1 FLUCTUATED AT CRUISE AND ALSO RECEIVED AN AMBER COMPUTER NO 1 ANNUNCIATOR. THE MAINTENANCE VENDOR TROUBLESHOT, PER HONEYWELL TECH SUPPORT AND DETERMINED THAT THE P1-16 ENGINE WIRING HARNESS WAS DEFECTIVE. THE SDR 2020F00325Window · damagedRIGHT DV WINDOW OUTER PANE SEPARATED AFTER TAKE-OFF NO INDICATION BEFORE SEPARATION P/N 25-8FN353-44A. AIRCRAFT HAD JUST TAKEN OFF AT 2,000 FEET WINDOW DELAMINATED AND SEPARATED FROM THE AIRCRAFTSDR 9JLA2020110921237Wire Harness · defectiveTHE FLIGHT CREW REPORTED THAT THE NUMBER 1 ENGINE N2 INDICATIONS WERE ERRATIC CAUSING A FLIGHT DIVERSION. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THAT THE NUMBER 1 ENGINE WIRING HARNESS WAS DEFECTIVE. THE HARNESS WAS REPLACED WITH A NEW HARNESS. OSDR 2GYR201912190007Trunnion · damagedWHILE INSTALLING THE RIGHT MLG LEG WE NOTICED THAT THE FWD UPPER AND LOWER TRUNNION ATTACH POINTS, WHERE THE BARREL NUTS SLIDE INTO, BOTH HAD GROOVES WORN INTO THEM AND CHAFFED REALLY BAD ALL AROUND. TOP BARREL NUT HOLE HAD A GROOVE THAT MEASURED ABOUT .035" ISDR 2GYR201910240001Bolt · failedWHEN THE AIRCRAFT TOUCHED DOWN ON LANDING, THE CREW NOTED A LARGE VIBRATION THROUGHOUT THE AIRFRAME. THE VIBRATION LESSENED IN INTENSITY AS THE AIRCRAFT SLOWED AND WENT AWAY WHEN STOPPED. TAXI TO THE RAMP WAS REPORTED AS NORMAL. IT WAS DISCOVERED THAT THE LEFTSDR 2GYR20191023004Bolt · brokenUPON LANDING AT KGYY AT APPROX. 8:00 P.M. ON THE NIGHT OF OCTOBER 21, 2019 AIRCRAFT N163DK FELT A ABNORMAL VIBRATION FORM THE LEFT MLG. THE AIRCRAFT TAXIED TO THE JET CENTER AND DISCOVERED THAT THE LEFT MLG UPPER AND LOWER TORQUE LINKS WERE SEPARATED FROM EACHSDR ZESA201942301Duct · looseDURING CRUISE AT 40,000FT A LOUD BANG WAS HEARD AND THE CABIN STARTED TO DEPRESSURIZE, PILOTS FOLLOWED THEIR CHECKLIST AND DESCENDED AND LANDED ASAP. THE PROBLEM WAS THAT THE PRESSURIZATION DUCT AT THE WATER SEPARATOR CAME LOOSE FROM THE DUCT ASSY AIR TURBINE SDR 3FPY201810078004Seat Track · corrodedLT INBOARD SEAT RAIL CORRODED - FOUND DURING C1-C12 INSPECTION. ASSESSED BY STRUCTURES AND SUPPORTS CONTINUED AIRCRAFT OPERATION FOR ANOTHER 100 FLIGHT HOURS WITH RESPECT TO CURRENT AIRFRAME TOTAL TIME (I.E. 1608.8+100.00 HOURS), OR UNTIL 3 JANUARY 2019, WHICHSDR 3FPY201810078003Stator Vane · damagedDURING ROUTINE ENGINE INSPECTIONS, THE LT ENGINE FAN STATOR VANES - LEADING EDGE SCREENS WERE FOUND DAMAGED - QTY 13 NEW VANE FAN STATORS INSTALLED.SDR 3FPY201810078002Control Cable · corrodedELEVATOR CONTROL CABLE CORRODED AT REAR FUSELAGE - FOUND DURING C1-C12 INSPECTION.SDR 3FPY201810078001Lever · corrodedFUEL SYSTEM LOW PRESSURE VALVE LEVER FOUND CORRODED DURING C1-C12 INSPECTION.SDR ZESA10280724001Sensor · faultyAIRCRAFT LEFT KLBE WITH NORMAL TAKE OFF AND CLIMB, AT CRUISE THE ENGINE WENT INTO MANUAL MODE, CHECK LIST WERE FOLLOWED AND PILOTS RETURNED TO BLOCK AT KLBE AND LANDED WITHOUT INCIDENT. A DOWNLOAD WAS PERFORMED ON THE DEECS AND THEY WERE SENT TO ENGINE AOG SERSDR XCGA201804160001Fuel Control · failedPILOT REPORTED THAT WHILE DESCENDING THROUGH 24,000 FEET ON APPROACH, THE LEFT ENGINE ROLLED BACK AND FAILED. NO RESTART WAS ATTEMPTED, THE AIRPLANE MADE AN UNEVENTFUL LANDING. MAINTENANCE VISUALLY INSPECTED THE FUEL FILTER, NO CONTAMINATION WAS NOTED. THE FUESDR 2018F00099Rib · corrodedLIGHT CORROSION FROM LT WING OTBD RIB 16. REPAIRED IAW FR-HA-0019-3819, REV 1.SDR DXTA2018012100499Transducer · inoperativeDURING CRUISE, THE RIGHT ENGINE N1 ROLLED BACK APPROX 5 TO 7 PERCENT. SIGNIFICANT YAWING WAS NOTICED AS THE ENGINE ROLLED BACK AND THEN RESUMED NORMAL POWER. FELT LIKE WHEN ONE ENGINE COMPUTER GOES OFFLINE AND THEN RESUMES. DEEC DOWNLOADS REVEALED FAULT CODESDR 9JLA2018012612392Starter Gen · defectiveTHE FLIGHT CREW REPORTED THAT DURING FLIGHT THAT THEY WERE SHOWING A AMP SPLIT BETWEEN GENERATORS AND THE RH SIDE WAS LOWER THAN NORMAL. MAINTENANCE TROUBLESHOT AND DETERMINED THERE WAS A DEFECT IN THE NO2 STARTER/GENERATOR. 23080-064 SN P2288 TOTAL TIME IN SESDR 9JLA2018012612584Spigot · brokenDURING THE PRE-FLIGHT INSPECTION CHECKS, THE TOP AFT MAIN CABIN DOOR SPIGOT PIN ASSEMBLY WAS FOUND TO BE BROKEN. THE PIN WAS REPLACED AND THE DOOR SYSTEM RIG CHECKED.SDR 9JLA2018012612583Gcu · failedDURING FLIGHT, THE FLIGHT CREW REPORTED THAT THEY LOST THE NR 2 AC ALTERNATOR. THE SYSTEM WAS SECURED AND THE FLIGHT CONTINUED. TROUBLESHOT AND DETERMINED THAT THE NR 2 AC ALTERNATOR GCU HAD FAILED . THE GCU WAS REPLACED. RETURNED TO SERVICE.SDR 2017FA0000299Windshield · crackedPILOTS WINDSHIELD CRACKED DURING FLIGHT FROM KIAH TO KCAK. THE AIRCRAFT DEPARTED KIAH AT 0707 CDST AND LANDED AT KCAK AT 1046 CDST. THE CREW DECLARED AN EMERGENCY AND LANDED AT KCAK WITHOUT INCIDENT. THERE WAS NO ADDITIONAL DAMAGE TO THE AIRCRAFT AND NO INJURISDR DXTA2017070406420Connector · dirtyLEFT ENGINE ROLLED BACK. AT 38,000 APX 5 MIN INTO CRUISE PHASE. LEFT ENGINE ROLLED BACK 10% PLUS. OBSERVED LEFT ENGINE GAUGE AND CONFIRMED WITH AIRCRAFT YAWNING MOMENT. CLEANED AND INSPECTED N2 MONOPOLE CONNECTOR OF DEBRIS. PERFORMED VERIFICATION OF DEEC OPESDR UVVR2017052300045Stud · shearedLEFT MLG FAILED TO RETRACT AFTER TAKEOFF. RT MLG AND NLG RETRACTED NORMALLY. LG EXTENDED NORMALLY. JACKED AIRCRAFT & PERFORMED FUNCTIONAL TEST OF MLG SYSTEM WITH NO DISCREPANCIES NOTED. EXTENSION & RETRACTION NORMAL WITH PROPER INDICATIONS. REMOVED & REPLASDR ZESA20170131001Lamp · burned outDURING A FLIGHT, THE PILOTS DIVERTED DUE TO THE LANDING GEAR DOWN AND LOCK INDICATION DID NOT ILLUMINATE. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE GEAR INDICATION LAMPS WERE FOUND TO BE BURNED OUT AND WERE REPLACED.SDR DXTA2017012606363Line · leakingSTRONG ODOR OF HYDRAULIC FLUID COMING FROM VENTS WITH MAIN AIR VALVES SELECTED ON IN FLIGHT. CLEANED RESIDUAL HYDRAULIC FLUID FROM HYDRAULIC RESEVOIR AIR CHARGE PORT, HYDRAULIC HEAD PRESSURE GUAGE AND LINE, REMOVED AND REPLACED THE LT AND RT ENGINE BLEED AIRSDR P6UR201701173249Cable · brokenDEFECTIVE AIRBRAKE CONTROL CABLE FOUND BROKEN AT PULLEY JUST AFT OF COCKPIT CENTER PEDESTAL.SDR 2016FA0000569Control Panel · malfunctionedPILOT COULD NOT SELECT AN ALTITUDE ON THE AUTO-PILOT ALTITUDE PRESELECT FUNCTION. THE CONTROLLER KEPT CHANGING ALTITUDES INSTEAD OF THOSE SELECTED. TWO MORE FLIGHT GUIDANCE PANELS FAILED.SDR BKEA20161031Warning Message · false activationDURING CLIMB, PASSING THRU APPROXIMATELY FL 280, RECEIVED A YELLOW CAUTION MESSAGE HYD 2 LOW PRESSURE WARNING. AFTER RUNNING APPROPRIATE CHECK LISTS, DETERMINED TO RETURN TO DEPARTURE. DECLARED THE EMERGENCY. LANDING WAS UNEVENTFUL, ALL SYSTEMS FUNCTIONED ASDR DXTA2016092406310Sensor · failedDURING CRUISE AT FL 400, THE RIGHT ENGINE ROLLED BACK THEN WENT BACK TO NORMAL. ROLL BACK WAS ENOUGH TO MAKE THE PLANE YAW. RETURNED TO DEPARTURE. REPLACED INLET PRESSURE AND TEMPERATURE SENSOR.SDR DXTA2016092106304Connector · dirtyAT 40,000 FT APPROXIMATELY 200 MILES FROM DESTINATION, -48C IS A+8. RIGHT ENGINE ROLLED BACK 2 TIMES IN APPROXIMATELY 30 SECONDS. FIRST ROLL BACK UNABLE TO RECORD PARAMETERS. SECOND ROLL BACK APPROXIMATELY 97.6 N1, 92.4 N2, CRUISE. ONLY ABLE TO CATCH N1 BE
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