British Aerospace BAE 125-1000
Service difficulty reports · 43
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 = '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.
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
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 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 EMERGESDR 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 LANDINSDR 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 OSDR 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 WASDR 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 WITSDR 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 SDR 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 BOOSDR 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 OVERSDR 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.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 EVIDENSSDR 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 CAUSESDR 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 SATISFACTORSDR 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.SDR 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 OUTBSDR 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 ENGINESDR 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.SDR 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.SDR 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 FSDR 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 OSDR 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.SDR 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.SDR 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 CSDR 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.SDR AU971506O-Ring · failed(AUS) NO1 ENGINE HYDRAULIC PUMP HIGH PRESSURE FITTING `O' RING SEAL FAILED. LOSS OF HYDRAULIC FLUID.SDR 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 ARSDR 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. SDR 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, PAGSDR 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 INSDR 97ZZZX35Aux Valve · malfunctionAUX VALVE WILL NOT STAY OPEN. FOUND MALFUNCTIONING AUX VALVE.SDR 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)SDR 97DXTA087Control Valve · wrong positionAIRCRAFT WILL NOT PRESSURIZE IN FLIGHT. FOUND MANUAL CONTROL VALVE 'OPEN' DURING GROUND CHECK. REPOSITIONED VALVE TO 'CLOSED'. (X)SDR 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,SDR 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.SDR 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 PILOTSDR 96ZZZX3420Mask · tornRUBBER FACE CUP TORN. FOUR EACH PASSENGER FACE MASKS. ALL TORN IN THE SAME LOCATION. FOUND DURING 12-MONTH INSPECTION.SDR 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 SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.
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