# Service difficulty reports: Raytheon HAWKER 1000

A list on [Raytheon HAWKER 1000](https://openairdocs.org/model/raytheon-hawker-1000.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 63 reports

- [SDR ZKFA20240701058](https://openairdocs.org/sdr/ZKFA20240701058.md): Filter Housing · pulled · Jul 2, 2024 · N261PA · Braero HAWKER1000 · Engine Oil System (Airframe Furnished)
  > DURING 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 HOLD
- [SDR ZKFA2024030600201](https://openairdocs.org/sdr/ZKFA2024030600201.md): Electronic Unit · overheated · Mar 5, 2024 · N261PA · Braero HAWKER1000 · Windshield/Door Rain/Ice Removal
  > PILOTS 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 ELE
- [SDR 2022F00364](https://openairdocs.org/sdr/2022F00364.md): None · none · Aug 5, 2022 · N261PA · Braero HAWKER1000 · Trailing Edge Flap Control System
  > AIRCRAFT IMPACTED A DEER ON LANDING AT KPYM. RIGHT TRAILING EDGE FLAP WAS DAMAGED BEYOND REPAIR AND WAS REPLACED.
- [SDR FUKA202201020001](https://openairdocs.org/sdr/FUKA202201020001.md): O-Ring · failed · Jan 2, 2022 · N8888H · Braero HAWKER1000 · Turbine Engine Oil System
  > WHILE 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 POS
- [SDR 2021FA0000311](https://openairdocs.org/sdr/2021FA0000311.md): Hinge · corroded · Nov 4, 2021 · N261PA · Braero HAWKER1000 · Aileron Tabs
  > RH 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 CA160216010](https://openairdocs.org/sdr/CA160216010.md): Engine · surges · Feb 10, 2016 · Braero HAWKER1000 · Engine (Turbine/Turboprop)
  > (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 R
- [SDR CA150602011](https://openairdocs.org/sdr/CA150602011.md): Engine · failed · May 17, 2015 · Braero HAWKER1000 · Engine (Turbine/Turboprop)
  > (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 2CJA20150528001](https://openairdocs.org/sdr/2CJA20150528001.md): Solenoid · intermittent · May 17, 2015 · N207K · Braero HAWKER1000 · Compressor Bleed Control
  > AT 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 CA140312001](https://openairdocs.org/sdr/CA140312001.md): Bleed Valve · malfunctioned · Feb 22, 2014 · Braero HAWKER1000 · Compressor Bleed Valve
  > DURING 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 IDEN
- [SDR ZKFR20130724001](https://openairdocs.org/sdr/ZKFR20130724001.md): Attach Fitting · corroded · Jul 24, 2013 · N261PA · Braero HAWKER1000 · Horizontal Stabilizer, Attach Fittings
  > DURING 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 2CJA2013F00139](https://openairdocs.org/sdr/2CJA2013F00139.md): Fire Warning · illuminated · Jul 1, 2013 · N207K · Braero HAWKER1000 · Fire Detection
  > AFTER 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 REMAIN
- [SDR CA130401012](https://openairdocs.org/sdr/CA130401012.md): Oil System · low pressure · Mar 23, 2013 · Braero HAWKER1000 · Engine Oil Indicating System
  > (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 WENT
- [SDR ZKFR20130117002](https://openairdocs.org/sdr/ZKFR20130117002.md): O-Ring · leaking · Jan 10, 2013 · N261PA · Braero HAWKER1000 · Wheel/Ski/Float
  > DURING 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 LEA
- [SDR ZKFR20130117001](https://openairdocs.org/sdr/ZKFR20130117001.md): O-Ring · leaking · Jan 10, 2013 · N261PA · Braero HAWKER1000 · Wheel/Ski/Float
  > DURING 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 NEA
- [SDR ZKFR20120605001](https://openairdocs.org/sdr/ZKFR20120605001.md): Check Valve · leaking · Jun 5, 2012 · N261PA · Braero HAWKER1000 · Crew Oxygen System
  > OXYGEN 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 ZKFR20120530001](https://openairdocs.org/sdr/ZKFR20120530001.md): Check Valve · leaking · May 30, 2012 · N261PA · Braero HAWKER1000 · Crew Oxygen System
  > OXYGEN 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 TH
- [SDR ZKFR2012040900001](https://openairdocs.org/sdr/ZKFR2012040900001.md): Skin · delaminated · Apr 9, 2012 · N261PA · Braero HAWKER1000 · Nacelle/Pylon, Plate/Skin
  > DURING 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 BO
- [SDR ZKFR201112163233](https://openairdocs.org/sdr/ZKFR201112163233.md): Controller · faulty · Dec 16, 2011 · N261PA · Braero HAWKER1000 · Cabin Temperature Control System
  > CABIN 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 CA110228001](https://openairdocs.org/sdr/CA110228001.md): Engine · shutdown · Feb 13, 2011 · Braero HAWKER1000 · Engine (Turbine/Turboprop)
  > (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. T
- [SDR S8A2009F00004](https://openairdocs.org/sdr/S8A2009F00004.md): Fire Loop · false activation · Jul 12, 2009 · N547LR · Braero HAWKER1000 · Fire Detection
  > ACFT 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 REPAI
- [SDR S8A2009F00001](https://openairdocs.org/sdr/S8A2009F00001.md): O-Ring · failed · Apr 15, 2009 · N548LR · Braero HAWKER1000 · Hydraulic System, Main
  > ACFT 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 DEPART
- [SDR CA090311007](https://openairdocs.org/sdr/CA090311007.md): Engine · flamed out · Mar 4, 2009 · Braero HAWKER1000 · Engine (Turbine/Turboprop)
  > (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 ESTABLISH
- [SDR S8A2008F00000](https://openairdocs.org/sdr/S8A2008F00000.md): Bypass Valve · stuck · Apr 16, 2008 · N547LR · Braero HAWKER1000 · Humidity Control System
  > ENROUTE, 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 EOX2008F00000](https://openairdocs.org/sdr/EOX2008F00000.md): Starter Gen · vibration · Jan 5, 2008 · N548LR · Braero HAWKER1000 · Starter-Generator
  > AIRCRAFT 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 DXTA200601612](https://openairdocs.org/sdr/DXTA200601612.md): Unknown · fumes · Sep 23, 2006 · N551QS · Braero HAWKER1000 · Air Distribution System
  > FUMES 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 DXTA200601543](https://openairdocs.org/sdr/DXTA200601543.md): Brake Assy · malfunctioned · Aug 7, 2006 · N552QS · Braero HAWKER1000 · Landing Gear Brake System
  > BRAKES 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 DXTA200601452](https://openairdocs.org/sdr/DXTA200601452.md): Tire · failed · Jun 23, 2006 · N552QS · Braero HAWKER1000 · Tire
  > BLOWN 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 DXTA200601414](https://openairdocs.org/sdr/DXTA200601414.md): Fluid · detected · May 31, 2006 · N552QS · Braero HAWKER1000 · Hydraulic System, Main
  > LT 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 DXTA200601369](https://openairdocs.org/sdr/DXTA200601369.md): Warning Light · unknown · Apr 30, 2006 · N546QS · Braero HAWKER1000 · Fuel Indicating System
  > AUX TRANSFER LIGHT ILLUMINATED, TAKE OFF ABORTED. ITEM IS UNDER INVESTIGATION.
- [SDR DXTA200601229](https://openairdocs.org/sdr/DXTA200601229.md): Unknown · unknown · Feb 2, 2006 · N550QS · Braero HAWKER1000 · Landing Gear Brake System
  > REPEAT WRITEUP, DURING NORMAL TAXI SPEED, WHEN BRAKES APPLIED AIRCRAFT VEERED LEFT.
- [SDR DXTA200601216](https://openairdocs.org/sdr/DXTA200601216.md): Brake Assy · hot · Jan 26, 2006 · N550QS · Braero HAWKER1000 · Main Landing Gear
  > REPEAT 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 CHEC
- [SDR DXTA200601201](https://openairdocs.org/sdr/DXTA200601201.md): Indicator · activated · Jan 17, 2006 · N550QS · Braero HAWKER1000 · Engine Fuel Indicating System
  > T/O ROLL ABORTED FOR ENG/FUEL LOOK UP LIGHT. ITEM IS UNDER INVESTIGATION.
- [SDR DXTA200601180](https://openairdocs.org/sdr/DXTA200601180.md): Fire Warning · illuminated · Jan 3, 2006 · N548QS · Braero HAWKER1000 · Fire Detection
  > DURING 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 DXTA200501129](https://openairdocs.org/sdr/DXTA200501129.md): Master Cylinder · malfunctioned · Dec 5, 2005 · N552QS · Braero HAWKER1000 · Master Cylinder/Brake Valve
  > UPON 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. O
- [SDR 2005FA0001528](https://openairdocs.org/sdr/2005FA0001528.md): Extinguisher · incorrect · Nov 8, 2005 · N551QS · Braero HAWKER1000 · Fire Bottle, Portable
  > REMOVING 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 DISCHARGI
- [SDR DXTA200500898](https://openairdocs.org/sdr/DXTA200500898.md): Landing Gear · inoperative · Aug 14, 2005 · N546QS · Braero HAWKER1000 · Landing Gear Retraction/Extension System
  > RED 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 DXTA200500893](https://openairdocs.org/sdr/DXTA200500893.md): Warning Light · malfunctioned · Aug 10, 2005 · N546QS · Braero HAWKER1000 · Landing Gear Position and Warning
  > RED 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 DEF
- [SDR DXTA200500788](https://openairdocs.org/sdr/DXTA200500788.md): Position Switch · malfunctioned · Jun 19, 2005 · N551QS · Braero HAWKER1000 · Landing Gear Position and Warning
  > DEPARTING 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 SW
- [SDR DXTA200500734](https://openairdocs.org/sdr/DXTA200500734.md): Wire · broken · May 21, 2005 · N549QS · Braero HAWKER1000 · Autopilot System
  > AFTER 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 SATISFAC
- [SDR DXTA200500699](https://openairdocs.org/sdr/DXTA200500699.md): Strut · damaged · Apr 26, 2005 · N544QS · Braero HAWKER1000 · Rudder Control System
  > THRU 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 MM
- [SDR DXTA200500660](https://openairdocs.org/sdr/DXTA200500660.md): Warning Light · illuminated · Apr 3, 2005 · N503QS · Braero HAWKER1000 · Landing Gear Position and Warning
  > ON 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 S
- [SDR DXTA200500594](https://openairdocs.org/sdr/DXTA200500594.md): Line · leaking · Feb 15, 2005 · N545QS · Braero HAWKER1000 · Hydraulic System, Main
  > ON 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 DXTA200500587](https://openairdocs.org/sdr/DXTA200500587.md): Quick Disconnect · contaminated · Feb 11, 2005 · N549QS · Braero HAWKER1000 · Engine Fuel and Control
  > ON 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 FOUND
- [SDR DXTA200500576](https://openairdocs.org/sdr/DXTA200500576.md): Control Cable · out of adjust · Feb 3, 2005 · N545QS · Braero HAWKER1000 · Control Column Section
  > CONTROLS 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 MO
- [SDR DXTA200400503](https://openairdocs.org/sdr/DXTA200400503.md): Oil System · overserviced · Dec 30, 2004 · N544QS · Braero HAWKER1000 · Turbine Engine Oil System
  > IMMEDIATELY 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 REINSPECTIO
- [SDR DXTA200400468](https://openairdocs.org/sdr/DXTA200400468.md): Warning System · activated · Dec 7, 2004 · N551QS · Braero HAWKER1000 · Engine Fuel Indicating System
  > ON TAKEOFF ROLL AT APPROX 65-70 KTS FUEL/ENG LOOK UP LIGHT WITH ASSOCIATED AUX TRANSFER FAULT ILLUMINATED. ITEM IS UNDER INVESTIGATION.
- [SDR DXTA200400457](https://openairdocs.org/sdr/DXTA200400457.md): Odor · detected · Nov 22, 2004 · N549QS · Braero HAWKER1000 · Air Distribution System
  > AFTER 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 DXTA200400428](https://openairdocs.org/sdr/DXTA200400428.md): Brake Assy · malfunctioned · Oct 17, 2004 · N548QS · Braero HAWKER1000 · Landing Gear Brake System
  > WHEN 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 INVESTI
- [SDR DXTA200400352](https://openairdocs.org/sdr/DXTA200400352.md): Odor · detected · Aug 2, 2004 · N550QS · Braero HAWKER1000 · Air Distribution System
  > WHILE 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 10
- [SDR DXTA200400271](https://openairdocs.org/sdr/DXTA200400271.md): Tape · loose · Mar 19, 2004 · N550QS · Braero HAWKER1000 · Wing Miscellaneous Structure
  > CLIMBING 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

Next page: https://openairdocs.org/model/raytheon-hawker-1000/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/model/raytheon-hawker-1000/reports

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