British Aerospace BAE 125-1000

Service difficulty reports · 43

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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 = 'BAE1251000'
  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 2016120500007Actuator · malfunctionedDURING APPROACH, LT MLG, WHEN SELECTED DOWN, DID NOT SHOW DOWN AND SAFE INDICATION ON EITHER, NORMAL OR AUXILIARY, INDICATION SYSTEM. RT AND NLG BOTH SHOWED DOWN AND LOCKED. PILOT ATTEMPTED EMERGENCY EXTENSION UTILIZING AUXILIARY HYDRAULIC SYSTEM, IAW EMERGEDec 1, 2015 · N730CJ · Braero BAE1251000 · Landing Gear Retraction/Extension SystemSDR E0X2008F00007Rudder · lockedAFTER DEPARTED, GOING THROUGH APPROX 800 FT AGL THE F/O NOTED THAT THE RUDDER HAD LOCKED UP IN THE NEUTRAL POSITION. THE OAT AT THE TIME WAS +9C. ACFT CONTINUED TO CLIMB AND CAPTAIN INFORMED ATC THAT WOULD BE RETURNING TO DEPARTURE. ACFT WAS ABOVE MAX LANDINOct 25, 2008 · N505LR · Braero BAE1251000 · Rudder Control SystemSDR E0X2008F00004Engine · damagedAC DEPARTED AND SHORTLY AFTER DEPARTURE, SMOKE WAS NOTED IN CABIN WITH BAGGAGE SMOKE DETECTOR INDICATING SMOKE IN BAGGAGE COMPARTMENT. FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE, APPROACH AND LANDING WERE UNEVENTFUL WITH NO OTHER INDICATION OJun 6, 2008 · N513LR · Braero BAE1251000 · Engine (Turbine/Turboprop)SDR E0X2008F00005Starter Gen · failedIN CRUISE FLIGHT AT FL380, CREW FELT A VIBRATION, IT CONTINUED TO GET STRONGER. CREW REQUESTED ATC TO LAND AT NEAREST SUITABLE AIRPORT BUT DID NOT DECLARE AN EMERGENCY. FLIGHT CREW DETERMINED THAT NR 1 GENERATOR WAS GONG BAD AND DIVERTED THE AC. APPROACH WAJun 3, 2008 · N542LR · Braero BAE1251000 · Starter-GeneratorSDR E0X2007F00000Scavenge Port · wornDEPARTED, ENROUTE, AT 22,000FT THE FLIGHT CREW DECLARED AN EMERGENCY WHEN THE NR 1 (LT) ENGINE OIL PRESSURE STARTED FLUCTUATING AND ALL LOW PRESSURE LIGHT CAME ON. FLIGHT CREW SHUTDOWN NR 1 ENGINE AND MADE AN EMERGENCY LANDING. THE LANDING WAS UNEVENTFUL WITNov 19, 2007 · N515LR · Braero BAE1251000 · Turbine Engine Oil SystemSDR 2006FA0001159Pump · failedTHREE FUEL BOOST PUMPS IN OVERHAULED CONDITION, SAME PN, ORDERED FROM THE SAME VENDOR HAVE FAILED AFTER SHORT TIME ON SAME AIRCRAFT USED ON LT AND RT SIDES. 1) FUEL BOOST PUMP OVERHAULED CONDITION SN 11A557 FAILED 5/24/06 AFTER 247 HOURS. 2) FUEL BOOST PUMP Nov 17, 2006 · N46WC · Braero BAE1251000 · Fuel Boost PumpSDR 2006FA0001157Pump · failedTHREE FUEL BOOST PUMPS IN OVERHAULED CONDITION, SAME PART NUMBER, ORDERED FROM THE SAME VENDER HAVE FAILED AFTER SHORT TIME ON SAME AIRCRAFT USED ON LT AND RT SIDES. 1) FUEL BOOST PUMP OVERHAULED CONDITION SN 11A557 FAILED 5/24/06 AFTER 247 HOURS. 2) FUEL BOOMay 24, 2006 · N46WC · Braero BAE1251000 · Fuel Boost PumpSDR 2006FA0001158Pump · failedTHREE FUEL BOOST PUMPS IN OVERHAULED CONDITION, SAME PN, ORDERED FROM SAME VENDOR HAVE FAILED AFTER SHORT TIME ON SAME AIRCRAFT USED ON LT AND RT SIDES. 1) FUEL BOOST PUMP OVERHAULED CONDITION SN 11A557 FAILED 5/24/06 AFTER 247 HOURS. 2) FUEL BOOST PUMP OVERMay 11, 2006 · N46WC · Braero BAE1251000 · Fuel Boost PumpSDR CA060425010Engine · malfunctionedDURING CRUISE, THE ENGINE SURGED FOLLOWED BY AN UNCOMMANDED POWER REDUCTION TO IDLE. THE WAS NO SUBSEQUENT RESPONSE TO THROTTLE INPUT. P&WC WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.Apr 8, 2006 · Braero BAE1251000 · Engine (Turbine/Turboprop)SDR CA060129015Line · fractured(CAN) FOLLOWING TAKEOFF, THE ENGINE FIRE WARNING ANNUNCIATED AND THE ENGINE WAS REPORTED TO BE (TRAILING SMOKE). THE ENGINE WAS SHUTDOWN IN FLIGHT, AN EMERGENCY DECLARED AND THE FLIGHT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED NO EVIDENSJan 3, 2006 · Braero BAE1251000 · Pneumatic Distribution SystemSDR CA051104011Engine · power loss(CAN) DURING A TRAINING TOUCH-AND-GO MANEUVER, THE ENGINE ROLLED BACK IN POWER AND THE LOW OIL PRESSURE WARNING ANNUNCIATED. THE ENGINE WAS SHUT DOWN IN FLIGHT AND AN UNSCHEDULED LANDING CARRIED OUT. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSEOct 22, 2005 · Braero BAE1251000 · Engine (Turbine/Turboprop)SDR DXTA200500718Proximity Switch · malfunctionedNOSE GEAR GREEN LIGHT WILL NOT ILLUMINATE WITH GEAR DOWN. REPLACED NOSE LANDING GEAR CHANGE OVER SWITCH. OPS CHECK GOOD IAW THE HAWKER 1000 MM 32-60-05. REPLACED NOSE LANDING GEAR CHANGE OVER MICRO SWITCH P/N WITH NEW P/N 1EN1-14N119. PERFORMED SATISFACTORMay 9, 2005 · N514QS · Braero BAE1251000 · Landing Gear Retraction/Extension SystemSDR CA050323005Line · cracked(CAN) DURING INSPECTION FUEL WAS FOUND LEAKING FROM A CRACKED HMU-TO-FUEL FLOW TRANSMITTER LINE. THE ENGINE HAD PREVIOUSLY EXPERIENCED AN AIRFRAME STARTER-GENERATOR FAILURE.Mar 7, 2005 · Braero BAE1251000 · Engine Fuel DistributionSDR DXTA200500535Blanket · looseFIVE SECONDS AFTER ADDING TAKEOFF POWER REAR BAY OVERHEAT LOOKUP LIGHT ILLUMINATED. LIGHT WENT OUT TWO SECONDS AFTER THROTTLE REDUCED TO IDLE. RAN ENGINES. CHECKED FOR LEAKS, NO LEAKS FOUND AT THIS TIME. FOUND HEAT BLANKET NOT SECURE ON EXPANSION PIPE OUTBJan 15, 2005 · N505QS · Braero BAE1251000 · Fuselage Miscellaneous StructureSDR DXTA200400472Odor · detectedAT FL370 A BURNING ODOR WAS DETECTED, LASTING ABOUT 3-5 MINUTES. ANOTHER DIFFERENT BURNING ODOR WAS DETECTED PASSING 15,000 FEET IN THE DESCENT, IT LASTED UNTIL THE BLEED AIR WAS TURNED OFF PASSING 10,000 FEET. RAN ENGINES AND CHECKED OIL LEVEL. NR 2 ENGINEDec 8, 2004 · N505QS · Braero BAE1251000 · Air Distribution SystemSDR DXTA200400391Coalescer Bag · dirtyON DESCENT WITH POWER LEVERS AT IDLE NOTICED EXHAUST FUME ODOR IN CABIN. REMOVED COALESOR SOCK AND INSTALLED NEW IAW MFG M/M CHAPTER 21-50-13. RAN AIRCRAFT AND LEAK CHECKED, NO LEAKS NOTED, COULD NOT DUPLICATE SMELL AT IDLE ON GROUND.Sep 14, 2004 · N505QS · Braero BAE1251000 · Humidity Control SystemSDR DXTA200400389Smoke · detectedDURING TAXI OUT FOR A REPOSITION FLIGHT, THE AUX AND PAC WARNING LIGHT CAME ON, FOLLOWED BY THE REAR BAGGAGE SMOKE WARNING LIGHT. SMOKE BEGAN TO FILL THE CABIN AREA, PERFORMED EMERGENCY EVACUATION FOR FLIGHT CREW. ITEM IS UNDER INVESTIGATION.Sep 11, 2004 · N520QS · Braero BAE1251000 · Air Distribution SystemSDR DXTA200400319A/C Pack · malfunctionedNOTICED FUMES AND SLIGHT SMOKE COMING FROM THE CO-PILOTS AIR CONDITIONING VENT DURING DEPARTURE, ODOR WAS STRONGEST WHEN MAIN AIR VALVES WERE FIRST OPENED AND WENT AWAY AFTER THE VALVES WERE PLACED TO LOW PRESSURE. RAN BOTH ENGINES AND APU WITH BLEED AIR ON FJun 5, 2004 · N514QS · Braero BAE1251000 · Cabin Cooling SystemSDR DXTA200300090Wire · brokenAFTER TAKE-OFF COULD NOT RETRACT LANDING GEAR, ACCOMPLISHED AIR TURN BACK TO TPA AND LANDED OVERWEIGHT. - REPAIRED BROKEN WIRE AT KAPIS BY INSTALLING SPLICE P/N D436-36, OPS CHECKED GOOD I/A/W HAWKER 1000 MM CHAPTER 32-30-00. C/W PRESSURIZE CHECK ON GROUND OAug 15, 2003 · N514QS · Braero BAE1251000 · Landing Gear System WiringSDR DXTA200300056Engine · malfunctionedDURING TAKEOFF ROLL AT APPROX 100KTS A/C STARTED YAWING TO THE RIGHT ENGINE GUAGES REVEALED LEFT N1 98.4 PERCENT RIGHT N1 94 PERCENT LEFT ENGINE FUEL FLEW 2300 LBS/HR AND RIGHT 1900 LB/HR APR ARMED.Jul 3, 2003 · N514QS · Braero BAE1251000 · Fuel Flow IndicatingSDR UXF2002F00000Lamp · inoperativeFLUORESCENT LAMP 22 INCHES LONG, MODEL F00100 HAS EVIDENCE OF SEVERE OVERHEATING (CHARRING) AT ONE END OF LAMP. LAMP USED IN GALLEY/CABIN LIGHTING SYSTEM.Nov 16, 2001 · N119U · Braero BAE1251000 · Passenger Compartment LightingSDR 98ZZZX4206P3 Line · brokePILOTS DISCREPANCY WAS NR 1 ENGINE TEMPORARILY LIMITED ABOVE CRUISE DETENT. REMOVED THE OUTBOARD INNER BYPASS ACCESS TO CHECK BLEED VALVES. UPON INVESTIGATION, FOUND THE BLEED AIR (P3 LINE) BROKEN AT B-NUT, P/N 3081695. IT APPEARED THE FIT OF THE LINE HAD COct 6, 1998 · N530QS · Braero BAE1251000 · Fuel Controlling SystemSDR 98ZZZX3222Tube · brokenRIGHT HAND ENGINE OUTBOARD BLEED AIR VALVE P3 LINE FOUND BROKEN AT WELDED 'L' FITTING. BY VISUAL INSPECTION, SUSPECTED CAUSE IS VIBRATION AND FATIGUE AND POSSIBILITY OF FLAW IN WELD.Aug 1, 1998 · N513QS · Braero BAE1251000 · Compressor Bleed ControlSDR AU971506O-Ring · failed(AUS) NO1 ENGINE HYDRAULIC PUMP HIGH PRESSURE FITTING `O' RING SEAL FAILED. LOSS OF HYDRAULIC FLUID.Nov 25, 1997 · Braero BAE1251000 · Hydraulic Pump (Electric/Engine), MainSDR 97ZZZX2089Line · chafed throughFOUND LEFT PITOT HEAD (P1) LINE 'SAWED THROUGH' BY LEFT ELEVATOR CONTROL CABLE DURING INVESTIGATION OF AN AIRSPEED DISCREPANCY. REMOVED AND REPLACED LINE. LINE IS PART OF A 4-GANG CLUSTER RUNNING UNDER THE CENTER COCKPIT FLOOR. SUBMITTER STATED THE LINES ARApr 1, 1997 · N514QS · Braero BAE1251000 · Pitot/Static SystemSDR 97ZZZX1757Switch · faultyKISP - ON APPROACH (PART 91 - NO PASSENGERS) WHEN GEAR HANDLE LOWERED, DID NOT GET A GREEN LIGHT FOR THE NLG. WITH GEAR HANDLE DOWN AND NO GREEN LIGHT FOR THE NLG, THE ALTERNATE INDICATOR (PIN POSITION ON CENTER CONSOLE) WAS CHECKED. IT INDICATED NLG DOWN. Mar 25, 1997 · N81HH · Braero BAE1251000 · Landing Gear Position and WarningSDR 97ZZZX1321Lever Arm · gougedDURING A ROUTINE INSPECTION, FOUND ELEVATOR LEVER ARM (IPC 55-20-05-01, ITEM 370) GOUGED ON THE OUTBOARD SIDE APPROXIMATELY .5 INCH ABOVE ELEVATOR ROD ATTACHEMENT BOLT. DURING REMOVAL AND INSTALLATION OF THE TAIL ASSEMBLY BULLET FAIRING, (IPC 55-30-10-01, PAGMar 5, 1997 · N514QS · Braero BAE1251000 · Elevator Control SystemSDR 97ZZZX597Line · cracked80 INCH LONG GALLEY DRAIN LINE WAS FOUND CRACKED FROM WATER EXPANSION. THIS LINE RUNS FROM GALLEY ALONG LOWER SIDE PLATES INSIDE CABIN AREA. ATTACH POINTS FOR LINE ONLY ALLOW A LEVEL INSTALLATION UNTIL JUST BEFORE IT ANGLES BELOW THE CABIN. THE CRACK WAS INJan 10, 1997 · N525QS · Braero BAE1251000 · Waste Disposal SystemSDR 97ZZZX35Aux Valve · malfunctionAUX VALVE WILL NOT STAY OPEN. FOUND MALFUNCTIONING AUX VALVE.Nov 11, 1996 · N520QS · Braero BAE1251000 · Cabin Pressure Control SystemSDR 97DXTA088Duct · leakingFLT 68798 - AIRCRAFT WILL NOT PRESSURIZE IN FLIGHT WITH MAIN AIR VALVE, BUT WILL WITH AUX VALVE. FOUND CABIN AIR FLOW DUCT LEAKING. REMOVED AND REPLACED DUCT. (X)Nov 5, 1996 · N525QS · Braero BAE1251000 · Air Distribution SystemSDR 97DXTA087Control Valve · wrong positionAIRCRAFT WILL NOT PRESSURIZE IN FLIGHT. FOUND MANUAL CONTROL VALVE 'OPEN' DURING GROUND CHECK. REPOSITIONED VALVE TO 'CLOSED'. (X)Nov 1, 1996 · N540QS · Braero BAE1251000 · Cabin Pressure ControllerSDR 96ZZZX4387Longeron · crackedFOUND CRACK ON LEFT ENGINE THRUST REVERSER UPPER DOOR INBOARD LONGERON ASSEMBLY ABOUT TWO INCHES FROM BUMPER. LONGERON ASSY IS WEAK IN MACHINED AREA WHICH IS WHERE THE CRACK IS LOCATED. SUBMITTER STATED IF THE BUMPER IS MODIFIED TO EXTEND PAST THE WEAK AREA,Aug 15, 1996 · N514QS · Braero BAE1251000 · Engine Thrust ReverserSDR 96ZZZX3724Longeron Assy · crackedFOUND CRACK ON LEFT ENGINE THRUST REVERSER UPPER DOOR INBOARD LONGERON ASSEMBLY, ABOUT 2 INCHES FROM BUMPER. LONGERON ASSEMBLY IS WEAK IN MACHINED AREA WHICH IS WHERE THE CRACK IS LOCATED.Jul 3, 1996 · N513QS · Braero BAE1251000 · Engine Thrust ReverserSDR 98ZZZX118Wire · damagedHOSE CLAMP HOLDING CUSTOM MADE AIRBOX TO PILOTS SIDE PANEL WAS POSITIONED SO THAT WORM SCREW OF CLAMP FOR SCREWDRIVER SLOT END WAS CUTTING INTO WIRES ON TERMINAL BLOCK MOUNTED BELOW BOX CAUSING FAILURE OF AUTOPILOT TRIM SYSTEM. THIS CONDITION EXISTED ON PILOTJun 28, 1996 · N548QS · Braero BAE1251000 · Auto Flight System WiringSDR 96ZZZX3420Mask · tornRUBBER FACE CUP TORN. FOUR EACH PASSENGER FACE MASKS. ALL TORN IN THE SAME LOCATION. FOUND DURING 12-MONTH INSPECTION.Jun 20, 1996 · N81AB · Braero BAE1251000 · Passenger Oxygen SystemSDR 96ZZZX1154Bolt · wrong lengthDURING A RECENT 2,400 HOUR-INSPECTION, THE LT ELEVATOR UPPER MID-ATTACH HINGE SEAL BOLTS WERE REPLACED WITH 5 EACH, DHS 1465-2DD, PER MOD 253410A DRAWING. AT 84 HRS FROM INSP DURING A PILOT PREFLT CHECK, A BINDING, AND SUBSEQUENT INSP REVEALED AT EXTREME AFT Feb 26, 1996 · N100U · Braero BAE1251000 · Elevator StructureSDR 96ZZZX968Relief Valve · leakingTHE AIRCRAFT WAS DETERMINED TO HAVE LEAKING THERMAL RELIEF VALVE. ORDERED REPLACEMENT PART. RECEIVED 4 EACH NEW RELIEF VALVES. ALL 4 EACH LEAKED. SUBMITTER SUSPECTS SPRING IS WEAK OR POOR FIT OF PISTON.Jan 26, 1996 · N533QS · Braero BAE1251000 · Fuel StorageSDR 96ZZZX19Mask · tornMASK RUBBER FACE CUP IS TORN. ON THIS ACFT, 6 MASKS WERE FOUND UNSERVICABLE. ALL MASKS HAD THE SAME DISCREPANCY. ONE NEW MASK WAS FOUND TORN PRIOR TO INSTALLATION, ITS MFG DATE WAS 6-95. P/N WAS SAME, BUT AT REV. U.Dec 13, 1995 · N544QS · Braero BAE1251000 · Passenger Oxygen SystemSDR 95ZZZX756Hose · burnedFUEL FEED LINE FOR APU FOUND DURING INSPECTION. OUTSIDE FUEL SLEEVEING HAD 2 HOLES BURNED THROUGH. FIRE RETARDANT SLEEVE HAD ONE HOLE BURNED IN RED RUBBER COVERING. WAS NOT BURNED TO HOSE AT THIS TIME.Jan 9, 1995 · N535QS · Braero BAE1251000 · APU Engine Fuel and ControlSDR 95ZZZX755Line · burnedAPU FUEL FEED LINE FOUND BURNED ON INSPECTION. OUTSIDE FUEL SLEEVEING HAD A HOLE BURNED THROUGH. FIRE RETARDANT SLEEVE HAD A HOLE BURNED INTO THE RED RUBBER COVERING. WAS NOT BURNED TO FUEL HOSE AT THIS TIME.Jan 9, 1995 · N539QS · Braero BAE1251000 · APU Engine Fuel and ControlSDR 95ZZZX754Line · burnedFOUND DURING PRE-FLIGHT - APU HOSE (FUEL FEED) WAS BURNED THROUGH THE PLASTIC SHIELD, AND THROUGH THE RUBBER INSULATION HALF WAY. CAUSE: LEFT ENGINE BLEED AIR AT MIXER VALVE IS BURNING THROUGH THE APU FUEL FEED LINE. NEED LINE ROUTED TO A DIFFERENT PATH.Jan 4, 1995 · N541QS · Braero BAE1251000 · APU Engine Fuel and ControlSDR 95ZZZX753Hose · burnedFOUND DURING PRE-FLIGHT. APU HOSE (FUEL FEED) WAS BURNED THROUGH THE PLASTIC SHIELD. THE FIRE RETARDANT COATING HAD NOT BEEN DAMAGED. CAUSE: HOSE LOCATED TOO CLOSE TO HOT AIR LINE. FIX: ROUTE LINE IN NEW POSITION.Jan 4, 1995 · N533QS · Braero BAE1251000 · APU Engine Fuel and ControlSDR 95ZZZX518Feed Line · burnedFOUND DURING PRE-FLIGHT. APU FUEL FEED HOSE WAS BURNED THROUGH THE PLASTIC SHIELD AND INTO THE HOSE INSULATION. BLEEDAIR FROM LEFT MIXER VALVE IS BURNING THE APU FUEL FEED LINE. NEED LINE ROUTED AWAY FROM BLEED AIR.Jan 4, 1995 · N520QS · Braero BAE1251000 · APU Engine Fuel and Control
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