Raytheon HAWKER 1000
Service difficulty reports · 63
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 = 'HAWKER1000' 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 = 'HAWKER1000' 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 ZKFA20240701058Filter Housing · pulledDURING A MAINTENANCE GROUND RUN, THE RT ENGINE DEVELOPED A MAJOR OIL LEAK AND WAS IMMEDIATELY SHUT DOWN. TECHNICIANS DISCOVERED THE OIL FILTER BOWL HAD BLOWN OFF. ONE HOLD DOWN STUD HAD COMPLETELY PULLED ITS THREADS OUT OF THE OIL FILTER HOUSING. A SECOND HOLDSDR ZKFA2024030600201Electronic Unit · overheatedPILOTS NOTICED SMOKE SMELL IN COCKPIT DURING CRUISE FLIGHT, ON TRIP KHYA-KAPF, FOLLOWED BY OBSERVING SMOKE. CONDUCTED EMERGENCY DESCENT AND LANDING AT KSAV. MAINT TECHNICIAN FOUND 2 AC CIRCUIT BREAKERS TRIPPED IN LEFT WINDSCREEN CIRCUIT AND LEFT WINDSCREEN ELESDR 2022F00364None · noneAIRCRAFT IMPACTED A DEER ON LANDING AT KPYM. RIGHT TRAILING EDGE FLAP WAS DAMAGED BEYOND REPAIR AND WAS REPLACED.SDR FUKA202201020001O-Ring · failedWHILE CRUISING AT 36,000 FT, CREW NOTED AN E1 LOW OIL PRESSURE INDICATION. ON CONFIRMING LOSS OF OIL PRESSURE ON THE ANALOG INDICATOR. THE CREW COMPLIED WITH QRH AND PERFORMED IN-FLT SHUTDOWN OF NR 1 ENGINE. LANDED WITH NO ISSUES, NO EMERGENCY DECLARED. ON POSSDR 2021FA0000311Hinge · corrodedRH AILERON SIGNIFICANT CORROSION FOUND AT CENTER TRIM TAB HINGE, AROUND BONDING STRAP ATTACHMENT HOLE, IN AFT SPAR STRUCTURE. TEXTRON ENGINEERING NOTIFIED AND NO REPAIR ALLOWED. NO NEW REPLACEMENT AILERONS AVAILABLE. ACQUIRED AS REMOVED RH AILERON S/N DHB1002 SDR CA160216010Engine · surges(CAN) DURING TAXIING, IN PREPARATION OF A REPOSITIONING FLIGHT, THE PILOT HEARD A LOUD NOISE REPORTED AS A COMPRESSOR SURGE. ENGINE POWER WAS PULLED BACK TO IDLE AND THEN SHUTDOWN. AIRCRAFT RETURNED TO THE HANGAR. THIS WAS THE SECOND EVENT. THE PREVIOUS TAXI RSDR CA150602011Engine · failed(CAN) CUSTOMER REPORTED THAT DURING TAKEOFF ROLL THE ACFT WAS SHAKING & ALL NR 2 ENG PARAMETERS WERE FLUCTUATING, ERRATIC. THE PILOT ELECTED TO PERFORM IFSD OF NR 2 ENG, TURNED AROUND & LANDED TO THE AIRPORT OF ORIGIN WITHOUT INCIDENT. AFTER LANDING, DURING SDR 2CJA20150528001Solenoid · intermittentAT 0915 LOCAL TIME THEY WERE POSITIONED ON AIRPORT HOLDING, SHORT OF RUNWAY 19. NOTICED AIR CONDITIONING WAS NOT MAINTAINING & CABIN WAS GETTING WARM. AFTER CLEARANCE WAS GIVEN FOR TAKEOFF, POWER WAS APPLIED & THE ACFT BEGAN TO SHAKE, FELT LIKE A COMPRESSOR SDR CA140312001Bleed Valve · malfunctionedDURING LANDING, THE ENGINE POWER REDUCED UNCOMMANDED TO BELOW IDLE POWER. THE ENGINE WAS SECURED AND THE TRIP COMPLETED WITHOUT FURTHER ISSUE. REPEATED ATTEMPTS TO RESTART THE ENGINE LATER WERE UNSUCCESSFUL. FSR IS IN CONTACT WITH THE CUSTOMER. PROBLEM IDENSDR ZKFR20130724001Attach Fitting · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON LT SIDE OF VERTICAL TO HORIZONTAL STABILIZER ATTACH FITTING. CORROSION IS INTERGRANULAR, AND IS LOCATED AROUND 12 FASTENER HEADS.SDR 2CJA2013F00139Fire Warning · illuminatedAFTER TAKEOFF AND MAKING TURN NORTH. AT ROUGHLY 3500 FT, NR 2 ENGINE FIRE ALARM VERY BRIEFLY SOUNDED AND THE RESPECTIVE ENGINE FIRE LIGHTS CAME ON VERY BRIEFLY. ABOUT A HALF SECOND LATER IT SOUNDED AGAIN WITH ALL THE RESPECTIVE LIGHTS ILLUMINATED AND REMAINSDR CA130401012Oil System · low pressure(CAN) AFTER LANDING, WHILE ON TAXI, THE OIL PRESSURE WENT DOWN, THE ENGINE ROLLED BACK AND SHUTDOWN BY ITSELF. THE PILOT CONTINUED TAXIING AND THE FIRE WARNING CAME ON. THE PILOT PULLED THE FIRE HANDLE, BUT DID NOT DISCHARGE BOTTLES, AS THE WARNING LIGHT WENTSDR ZKFR20130117002O-Ring · leakingDURING PREFLIGHT, FLIGHT CREW NOTICED LT OTBD TIRE LOOKED LOW. MX DISCOVERED TIRE ALMOST COMPLETELY DEFLATED BUT NOT BLOWN. WHEEL ASSYS ONLY HAD 9 CYCLES SINCE IT WAS O/H. REMOVED AND REPLACED WHEEL/TIRE ASSY. INSPECTED REMOVED WHEEL ASSY AND FOUND AIR LEASDR ZKFR20130117001O-Ring · leakingDURING PREFLIGHT, FLIGHT CREW NOTICED LT INBD TIRE LOOKED LOW. MX DISCOVERED TIRE ALMOST COMPLETELY DEFLATED BUT NOT BLOWN. WHEEL ASSYS ONLY HAD 9 CYCLES SINCE IT WAS O/H. R & R WHEEL/TIRE ASSY. INSPECTED REMOVED WHEEL ASSY AND FOUND AIR LEAKING FROM RIM NEASDR ZKFR20120605001Check Valve · leakingOXYGEN SYS NON-RETURN VALVE LEAKING ALLOWING OXYGEN TO FLOW BACKWARDS AND LEAK OUT OF FILLER PORT. THIS WAS A BRAND NEW CHECK VALVE FROM MFG. REMOVED AND REPLACED UNIT.SDR ZKFR20120530001Check Valve · leakingOXYGEN SYSTEM LEAKING: FOUND OXYGEN SYSTEM NON-RETURN VALVE INOP AND ALLOWING OXYGEN TO FLOW BACKWARDS AND LEAKING OUT OF FILLER PORT. REMOVED AND REPLACED NON-RETUEN VALVE AND LEAK CHECKED GOOD. THIS NON RETURN VALVE WAS JUST INSTALLED 9 MONTHS AGO FOR THSDR ZKFR2012040900001Skin · delaminatedDURING ENGINE CHANGE, CORE COWL SEGMENT FOUND DELAMINATED. MFG HAS A REPAIR FOR THIS PROBLEM BUT UNFORTUNATELY THE EXTENT OF DAMAGE TO THIS CORE COWL IS BEYOND ALL LIMITS OF REPAIR. THE REPAIR IS USUALLY FOR A SMALL AMOUNT OF LIFTING AT THE CORNERS OF THE BOSDR ZKFR201112163233Controller · faultyCABIN TEMPERTURE UNCONTROLLABLE IN AUTO MODE. FOUND CABIN TEMPERTURE CONTROLLER NOT PROVIDING ANY OUTPUT VOLTAGE. CONTROLLLER GIVES MOMENTARY PULSES ONLY VISIBLE USING A TEST LAMP WHICH CAUSES TEMP CONTROL VALVE TO "CLICK" BUT NOT ENOUGH TO MOVE VALVE. R & SDR CA110228001Engine · shutdown(CAN) IFSD DURING TAXI AFTER LANDING, THE PILOT NOTICED AN UNCOMMANDED ENGINE SHUTDOWN. THE ACFT CONTINUED TO THE HANGAR AND ATTEMPTED ENGINE RE-START WAS UNSUCCESSFUL. TSDR S8A2009F00004Fire Loop · false activationACFT DEPARTED ENROUTE WITH (4) PASSENGERS AND (2) CREW. AT CLIMB OUT AT APPROX 2000 FT AGL NR 1 ENG HAD FIRE INDICATION. CREW DECLARED AN EMERGENCY WITH ATC AND RETURNED TO DEPARTURE AIRPORT WITH AN UNEVENTFUL LANDING. OMP WAS CONTACTED TO INSPECT AND REPAISDR S8A2009F00001O-Ring · failedACFT DEPARTED ON REPO LEG WITH ONLY CREW ON BOARD. ON CLIMBOUT NOTICED NR 2 SYS LOW PRESSURE LIGHT CAME ON FOLLOWED BY MAIN HYD LOW LEVEL LIGHT AND NR. 1 SYS LO-PRESSURE LIGHT. SEVERAL MINUTES LATER AUX LO-LEVEL LIGHT CAME ON. FLIGHT CREW RETURNED TO DEPARTSDR CA090311007Engine · flamed out(CAN) DURING DESCENT, THE STARTER GENERATOR (OUT) WARNING CAME ON FOLLOWED BY ENGINE FLAMEOUT. THE CREW LANDED THE ACFT SINGLE ENGINE AT DESTINATION. TROUBLESHOOTING IS ON-GOING. MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHSDR S8A2008F00000Bypass Valve · stuckENROUTE, AIRCRAFT N547LR AT 22,000 FT EXPERIENCED A UNCOMMANDED LOSS OF PRESSURIZATION FROM 16,000 TO 6,000 FT. THE AIRCRAFT MADE A DIVERSION, WITH AN UNEVENTFUL APPROACH AND LANDING. THIS WAS REPOSITIONING FLIGHT WITH ON PASSENGERS ON AIRCRAFT AND TWO FLIGHT SDR EOX2008F00000Starter Gen · vibrationAIRCRAFT WAS FL360 ENROUTE, FLIGHT CREW NOTED A VIBRATION IN THE RT ENGINE AND DID A PRECAUTIONARY SHUTDOWN OF THE RT ENGINE. THE AIRCRAFT DIVERTED AND MADE AN UNEVENTFUL LANDING WITH NO INJURIES TO PASSENGERS OR CREW. INSPECTED THE RT ENGINE AND FOUND THAT SDR DXTA200601612Unknown · fumesFUMES IN CABIN WHEN AIRCRAFT ON THE GROUND AND APU RUNNING WITH APU AIR VALVE OPENED. RAN LT AND RT ENG, APU IAW H/S M/M 49-20 + HS1000 M/M CHAP 80-10-00. OPS CHECK GOOD. NO DEFECTS NOTED.SDR DXTA200601543Brake Assy · malfunctionedBRAKES ARE MUSHY, ALMOST 3/4 TRAVEL ON PILOTS SIDE BEFORE BRAKES BEGIN TO TAKE EFFECT. ABOUT 1/2 TRAVEL ON CO-PILOTS SIDE. PERFORMED BRAKE BLEED PROCEDURE TO ALL FOUR BRAKE ASSEMBLIES IAW HAWKER 1000 MM 32-40-00. BRAKES OPS CHECK GOOD.SDR DXTA200601452Tire · failedBLOWN RT MAIN OUTBOARD TIRE INBOARD RT MAIN + OUTBOARD LT MAIN HAVE FLAT SPOT WITH 6 CORDS SHOWING. FOUND RT MAIN OUTBOARD TIRE BLOWN, RT MAIN INBOARD TIRE FLAT SPOTTED. REMOVED & REPLACED W/OVERHAULED UNITS PER H1000 M/M CH 32-40-05, SERVICED PER H1000 M/M SDR DXTA200601414Fluid · detectedLT IB TIRE VERY HOT AFTER LANDING. STREAM OF SMOKE FROM THE 12 O'CLOCK IB POSITION. PLANE PULLS TO LT WHEN BRAKES ARE APPLIED GENTLY. SUSPECT DRAGGING IB PORT BRAKE ASSY. POSSIBLE BLOWN FUSE PLUG PORT IB TIRE. INSPECTED TIRE, BRAKE ASSEMBLY, NO DEFECTS NOTED,SDR DXTA200601369Warning Light · unknownAUX TRANSFER LIGHT ILLUMINATED, TAKE OFF ABORTED. ITEM IS UNDER INVESTIGATION.SDR DXTA200601229Unknown · unknownREPEAT WRITEUP, DURING NORMAL TAXI SPEED, WHEN BRAKES APPLIED AIRCRAFT VEERED LEFT.SDR DXTA200601216Brake Assy · hotREPEAT WRITE-UP. AFTER LOW SPEED 60KT ABORTED TAKEOFF, LEFT BRAKE ASSEMBLY WAS VERY HOT AND SMOKING. LARGE TEMP DIFFERENCE BETWEEN LEFT (HOT) AND RIGHT (COOLER) BRAKES. NO DRAG OR SWERVE FELT AS BRAKES WERE APPLIED. PERFORMED ALL MAINTENANCE PROCEDURE CHECSDR DXTA200601201Indicator · activatedT/O ROLL ABORTED FOR ENG/FUEL LOOK UP LIGHT. ITEM IS UNDER INVESTIGATION.SDR DXTA200601180Fire Warning · illuminatedDURING ROTATION NR 2 ENG FIRE LIGHT ILLUMINATED WITH MASTER WARNING LIGHT & FIRE BELL. DURING EMERGENCY PROCEDURE FIRE LIGHT WENT OUT WHEN HANDLE WAS PULLED. FIRE BOTTLE WAS NOT DEPLOYED. ITEM IS UNDER INVESTIGATION.SDR DXTA200501129Master Cylinder · malfunctionedUPON LANDING, CAPTAINS BRAKE PEDALS ARE SPONGY & PEDALS TEND TO GO TO THE FLOOR IN ORDER TO STOP THE AIRCRAFT. BRAKES CHECKED NORMAL ON TAXI OUT PRIOR TO DEPARTURE. BLED (4) BRAKE MASTER CYLINDERS TO THE BRAKE CONTROL VALVE, NJA CREW PERFORMED TAXI CHECK. OSDR 2005FA0001528Extinguisher · incorrectREMOVING HAND HELD FIRE EXTINGUISHER FROM THE COCKPIT FOR ROUTINE INSPECTION IT WAS NOTED THAT THE HANDLE DID NOT APPEAR TO BE CORRECT. FURTHER INSPECTION SHOWED THAT THERE ARE TABS ON THE LOWER HANDLE THAT WOULD HAVE PREVENTED THE EXTINGUISHER FROM DISCHARGISDR DXTA200500898Landing Gear · inoperativeRED LANDING GEAR LIGHT ON THE RIGHT SIDE (RIGHT MAIN) STAYED ON AFTER GEAR RETRACTION, WITNESS ON THE GROUND REPORTED THAT THE RIGHT MAIN GEAR NEVER RETRACTED. ITEM IS UNDER INVESTIGATION.SDR DXTA200500893Warning Light · malfunctionedRED LANDING GEAR UNSAFE LIGHT ON THE RIGHT SIDE STAYED LIT AFTER GEAR RETRACTION. EXCESS WIND NOISE AND SLIGHT VIBRATION WAS NOTICED WHILE AIRBORNE. VISUALLY INSPECTED RT MAIN GEAR, INSPECTED MICRO SWITCHES & WIRING HARNESS AT SWITCH & TERMINAL BLOCK, NO DEFSDR DXTA200500788Position Switch · malfunctionedDEPARTING LIT GEAR SELECTED UP L MAIN GEAR UNSAFE LIGHT ILLUMINATED. 400FT AGL SELECTED FLAPS UP AND GEAR LIGHT EXTINGUISHED. CYCLED LANDING GEAR OPS GOOD. AT 15000 MSL, L MAIN GEAR LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. ADJUSTED LT MLG DOOR UPLOCK SWSDR DXTA200500734Wire · brokenAFTER TAKEOFF, THE MACH TRIM YAW DAMPER AND AUTO-PILOT WOULD NOT ENGAGE ON THE FGC PANEL. REPAIRED BROKEN WIRES AT LAFGS ANNUNCIATOR TRANSFER BUTTON. CLEANED BUTTON CONTACTS IAW ARKANSAS AERO DWG A1-44-001 REV B AND A1-44-003 REV B. OPERATIONAL CHECK SATISFACSDR DXTA200500699Strut · damagedTHRU V1, RUDDER BECAME EXTREMELY STIFF AND REMAINED STIFF UNTIL AFTER AIRCRAFT CAME TO A TAXI. YAW DAMPER WAS CYCLED ON THEN OFF TWICE AND APPEARED TO FUNCTION NORMALLY. REMOVED FAULTY LT AND RT RUDDER BIAS STRUTS. INSTALLED LT AND RT UNIT IAW HAWKER 1000 MMSDR DXTA200500660Warning Light · illuminatedON CLIMBOUT, AFTER GEAR SELECTED UP, THREE RED UNSAFE LIGHTS SHOWED (LM, NOSE, RM) AS WELL AS THE GREEN RIGHT MAIN LIGHT. RETURNED FOR LANDING GEAR SELECTED DOWN THREE GREEN INDICATED AS WELL AS BOTH GREEN STANDBY LIGHTS AND NOSE GEAR PIN WAS EXTENDED FOR A SSDR DXTA200500594Line · leakingON LANDING BRAKES WERE VERY SOFT AND MADE STOPPING THE AIRPLANE DIFFICULT. ALSO CO-PILOTS BRAKES CONFIRMED THE BRAKE ISSUE. LEFT PEDAL ON CO-PILOTS SIDE WENT TO FULL TRAVEL. BLED CO-PILOT BRAKES IAW HAWKER 1000 MM 32-40-00. OPERATIONAL CHECK SATISFACTORY.SDR DXTA200500587Quick Disconnect · contaminatedON A ROLLING TAKEOFF NR 1 ENGINE DID NOT SPOOL UP TO FULL POWER I FIRST NOTICED A SPLIT IN N2 RPM THEN SAW N1 RPM ON NR 1 ENGINE WAS ABOUT 5 PERCENT BELOW TAKEOFF POWER. RAN FADEC CODES AND IT IS SHOWING KB ON CHANNEL B ON ALL LINES. TROUBLESHOT SQUAWK FOUNDSDR DXTA200500576Control Cable · out of adjustCONTROLS ARE BINDING. WHILE MOVING THE CONTROLS LT & RT THERE IS A NOISE AND FEELING OF BINDING IN PILOT CONTROL COLUMN. AT HIGHER SPEED MORE PRONOUNCED, AT SLOWER SPEED LESS PRONOUNCED. AFTER PERFORMING DETAIL INSPECTION DETERMINE THAT SLIGHT RATCHETING MOSDR DXTA200400503Oil System · overservicedIMMEDIATELY AFTER AIRBORNE & SELECTING MAIN AIR VALVE TO ON, SMOKE BEGAN TO BELLOW THROUGHOUT THE COCKPIT AND CABIN AREAS. MAIN AIR VALVES WERE IMMEDIATELY SELECTED OFF AND RAM AIR SELECTED TO FULL ON, TO HELP CLEAR THE COCKPIT. ON THE GROUND, ON REINSPECTIOSDR DXTA200400468Warning System · activatedON TAKEOFF ROLL AT APPROX 65-70 KTS FUEL/ENG LOOK UP LIGHT WITH ASSOCIATED AUX TRANSFER FAULT ILLUMINATED. ITEM IS UNDER INVESTIGATION.SDR DXTA200400457Odor · detectedAFTER TWO HOURS OF FLIGHT BOTH PILOTS SMELLED STRONG ELECTRICAL / BURNED OIL FUMES WHICH IRRITATED EYES. NO VISIBLE FUMES MAIN AIR VALVES SELECTED TO LOW PRESSURE FUMES DISAPPEARED. AIRCRAFT RUN UP SYSTEMS OPS CHECKED GOOD. DUCTS WORK INSPECTED (LOW PSI) SDR DXTA200400428Brake Assy · malfunctionedWHEN APPLYING THE BRAKES FROM THE LT SEAT, THE FIRST APPLICATION RESULTS IN ALMOST NO BRAKING ACTION. THE PEDALS GO TO THE STOPS WITH VERY LITTLE RESULTS. BREAKING ACTION RETURNS TO NORMAL AFTER THE PEDALS ARE RELEASED AND RE-APPLIED. ITEM IS UNDER INVESTISDR DXTA200400352Odor · detectedWHILE CLIMBING THROUGH FL250 SELECTED ENGINE ANTI ICE ON, SHORTLY THEREAFTER NOTICED A STRONG BURNING SMELL IN THE COCKPIT. DE-SELECTING ANTI ICE, SMELL WENT AWAY, NO VISIBLE SMOKE WAS NOTICED. OPS CHECKED ANTI ICE SYSTEM, SYSTEM OPS CHECK GOOD IAW HAWKER 10SDR DXTA200400271Tape · looseCLIMBING THROUGH APPROXIMATELY FL280, EXPERIENCED A SEVERE LONGITUDINAL OSCILLATION. THE YOKE OSCILLATED LEFT AND RIGHT RAPIDLY AND WINGS WERE FLEXING 4 TO 6 INCHES, DISCONNECTED AUTOPILOT WITH NO POSITIVE AFFECT, CONDITION IMPROVED BY SLOWING DOWN THE AIRCRAF
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