Corporate Jets BAE 125-1000A
Service difficulty reports · 29
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 = 'BAE1251000A' 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 = 'BAE1251000A' 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 4USA20210709004Display · smokeSMOKE DETECTED COMING FROM CAPTAIN A SCREEN AT CRUISE ALTITUDE. CORRECTIVE ACTION: INSPECTED A SCREEN AND SURROUNDING WIRING. INSPECTED INSTRUMENT PANEL AND AVIONICS FANS. NO EVIDENCE OF ELECTRICAL DISCREPANCIES FOUND. PERFROMED OPERATIONAL CHECKS OF AVIONICS SDR 4USA04272021003Engine · surgesAFTER TAKEOFF FROM KOPF,WHILE CLIMBING THROUGH FLIGHT LEVEL 15000, RIGHT HAND ENGINE N2 BEGAN SURGING. THROTTLE WAS BROUGHT BACK TO IDLE AND ENGINE STABILIZED. AFTER APPROXIMATELY 20 MINUTES WHILE IN A HOLDING PATTERN, RH ENGINE N2 AGAIN BEGAN SURGING. LANDED SDR CA190604008Engine · malfunctioned(CAN) CUSTOMER REPORTED THAT THEY COULD NOT SHUT DOWN THE ENGINE NORMALLY, THEY HAD TO PULL THE T-HANDLE TO SHUT DOWN. WHEN ATTEMPTING TO SHUT THE ENGINE DOWN, PUT POWER LEVER IN CUT OFF, AND ENGINE OSCILLATED AND HUNG AROUND 30% N2. ITT WAS NEAR UPPER LIMIT ASDR CA140826003Oil System · low pressure(CAN) DURING FLIGHT, THE PILOT ELECTED TO SHUT DOWN THE LEFT ENGINE DUE TO LOW OIL PRESSURE. FLIGHT WAS DIVERTED TO VIE AIRPORT, VIENNA, AUSTRIA. UNEVENTFUL SINGLE ENGINE LANDING PERFORMED. AFTER LANDING THEY OIL FOUND LEAKED EXTERNALLY AND ENGINE LOST A LARGESDR CA131007001Engine · surges(CAN) DURING CRUISE FLIGHT, THE NR 2 ENGINE SURGED WHERE THE N2 AND FF IS FLUCTUATING AND N1 SPLIT OF 3 PERCENT.SDR CA130819006Engine · smoke(CAN) DURING CLIMB AT 3000 FEET, THE PILOT REPORTED TO HAVE SMOKE IN CABIN. AFTER A FEW ACTIONS FROM THE CREW TRYING TO ISOLATE THE ENGINE FROM WHICH THIS SMOKE WAS COMING FROM, POWER WAS REDUCED AND SMOKE STOPPED. ACFT LANDED SAFELY WHERE ADDITIONAL GROUND SDR CA130502002Engine · shutdown(CAN) THE CREW REPORTED THE LT ENGINE SPOOL BACK AND AN UNCOMMANDED SHUTDOWN AFTER 30 MINUTES OF FLIGHT DURING CRUISE AT FL 330. DURING THE SHUTDOWN, THE CREW PERFORMED THE EMERGENCY CHECK LIST AND DESCENDED TO FL210 WHERE THEY PERFORMED A START. THE DURATIOSDR BLUA2012F00026Computer · warning lightNR 2 ENGINE COMPUTER LIGHT ILLUMINATED IN FLIGHT.SDR E0X2009F00002Unknown · unknownAT FL 410 ECS INLET OVERHEAT LIGHT ILLUMINATED, CREW PUT MAIN AIR VALVES BOTH ON LB AND STARTED A DESCENT TO FL 350. APPROX 1 MINUTE AFTER START OF DESCENT THE CABIN BEGAN A RAPID CLIMB IN EXCESS OF 10,000 FT. CREW BEGAN AN EMERGENCY DESCENT AND DECLARED AN SDR E0X2008F00003Controller · defectiveON CLIMBOUT, FLIGHT CREW ELECTED TO TURN ON WINDSHIELD HEAT, SOMETIME AFTER THAT AND BEFORE REACHING CRUISE ALT. THE FLIGHTCREW NOTED THE FO`S RT REAR WINDSHIELD DELAMINATING, LITERALLY COOKED, STATED BY CAPTAIN. FLIGHT CREW LEVELED AT 12,000 FT, DECLARED AN ESDR E0X2008F00002Engine · failedNR 1 ENGINE QUIT AS AC WAS CLIMBING THROUGH FL370 WITH NO WARNING. FIRST INDICATION WAS LOSS OF OIL PRESSURE AS ENGINE SPOOLED DOWN. DIVERTED AND DECLARED AN EMERGENCY. THEIR WAS NOT AN ATTEMPT MADE TO AIRSTART THE FAILED ENGINE. SINGLE ENGINE LANDING WAS UNESDR E0X2008F00001Unknown · unknownON APPROACH, AT 3000 FT, EXPERIENCED A PARTIAL PANEL FAILURE ON THE CAPT EADI, EHSI, MFG. TRANSFERRED CONTROL OF AC TO THE F/O. SELECTED THE NR 2 AFSC AND 30 SECONDS THE AC DEPARTED LEVEL FLIGHT AND STARTED AN UNCOMMANDED DESCENT. AT 2700 FT BOTH FLIGHT CRESDR CA071128009O-Ring · leaking(CAN) CREW REPORTED OIL PRESSURE FLUCTUATIONS AND ILLUMINATION OF THE LOW OIL PRESSURE WARNING INDICATOR. THE ENGINE WAS SHUTDOWN AND THE FLIGHT DIVERTED. INVESTIGATION REVEALED DEFECTIVE O-RINGS ON THE NR4 BEARING TRANSFER TUBES (TC NR 20071128009)SDR 2005FA0001481Drain · chafedRT HYDRAULIC PUMP CASE DRAIN HYDRAULIC LINE RUPTURED IN FLIGHT, DRAINING HYDRAULIC FLUID FROM THE AIRCRAFT SYSTEM. FOUND RT HYDRAULIC PUMP CASE DRAIN LINE CRACKED WHERE LINE HAS BEEN CHAFING. INSPECTED AIRCRAFT AND FOUND SIMULAR CHAFE IN SAME LINE IN SAME LOSDR DXTA200500519Engine · overheatedOVERTEMP NR 2 ENGINE ON TAKEOFF, TEMPERATURE WENT TO 797 DEGREES FOR 2 SECONDS. ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION.SDR DXTA200400498Cdu · faultyBURING ELECTRICAL SMELL IN COCKPIT, NO OTHER INDICATIONS. GEN 1 AMPS 80/ GEN 2 AMPS 120. REMOVED NR 1 FMS CDU DUE TO NO DISPLAY AND FAINT BURNING ELECTRICAL SMELL. REPLACED WITH SERVICEABLE FMS CDU OPS CHECK GOOD IAW HAWKER 1000 MM CH 34-61-00 REV 27 10/04.SDR DXTA200400478Sequence Valve · malfunctionedIMMEDIATELY AFTER TAKEOFF AND GEAR RETRACTION, THE RT GEAR IN TRANSIT LIGHT (RED LIGHT) REMAINED ILLUMINATED. PRIOR TO LOWERING GEAR REQUESTED (2) LOW FLIGHT PASSES WITH LIT TOWER FOR VISUAL VERIFICATION, TOWER ADVISED THE RIGHT MAIN GEAR DOOR WAS SLIGHTLY OPSDR 2005FA0000260Alternator · failedAIRCRAFT WAS SQUAWKED WITH NR 1 ALTERNATOR DROPPING OFF IN FLIGHT. DURING TROUBLESHOOTING THE TECHNICIAN FOUND SMOKE TRAILS ON THE (GG PANEL), LOCATED ON THE AFT SIDE OF THE REAR FACE OF THE PRESSURE BULKHEAD. A MORE CLOSE INSPECTION REVEALED A DESTROYED FUSDR 2005FA0000088Holder · destroyedAIRCRAFT WAS SQUAWKED WITH NR 1 ALTERNATOR DROPPING OFF IN FLIGHT. DURING TROUBLESHOOTING THE TECHNICIAN FOUND SMOKE TRAILS ON THE GG PANEL. LOCATED ON THE AFT SIDE OF THE REAR FACE OF THE PRESSURE BULKHEAD. A MORE CLOSE INSPECTION REVEALED A DESTROYED FUSESDR DXTA200400419Computer · failedNR 2 FMS WENT BLANK AND A ELECTRICAL BURNING ODOR WAS NOTICED SHORTLY AFTERWARDS IN COCKPIT. REPLACED NR 2 FMS IAW HAWKER 1000 AMM CHAPTER 34-61-00, OPS CHECK GOOD IAW HAWKER 1000 AMM CHAPTER 34-61-00.SDR DXTA200300205Controller · malfunctionedDURING FLIGHT FROM TEB TO ADS DURING DESCENT FLAPS WILL NOT LOWER WHEN SELECTED TO 15, 25, OR 45 DEGREES. DIVERTED TO DFW AND LANDED SAFELY. ITEM IS UNDER INVESTIGATION.SDR DXTA200300121Coalescer Bag · contaminatedON CLIMB OUT AT 15,000 FT BROUGHT THRUST LEVERS TO IDLE AND CABIN BEGAN FILLING WITH SMOKE. REPLACED WATER SEPARATOR SOCK, AND LOWERED NR 2 ENG OIL PRESS IAW HAWKER 1000 M/M, CHAPTER 71-00-00 AND CHAPTER 21-50-15. AIR CONDITIONING SYSTEM FUNCTIONAL CHECKED SDR DXTA200300109Indicator · erraticON TAKEOFF ROLL FLAP POSITION INDICATOR HAD ERRATIC MOVEMENT, FROM THE SET POSITION OF 15 DEGREES THEN MOVED TO 20 DEGREES THEN TO 25 DEGREES AND THEN BACK TO 15 DEGREES, FOLLOWED IMMEDIATELY BY IT MOVING BACK TO 25 DEGREES AND THEN CONTINUING DOWN TO 45 DEGRESDR DXTA200300093Engine · failedON SHORT FINAL WITH A REDUCTION IN POWER NR 2 ENG FAILED AND MASTER CAUTION ILLUMINATED. OIL PRESSURE CAUTION LIGHT CAME ON NOTICED OIL PRESSURE GAUGE READ 10 PSI, ENGINE SHUTDOWN UNCOMMANDED. - REMOVED RT THROTTLE RDVT AND INSTALLED A NEW RDVT AND RIGGED IAW SDR DXTA200300035Master Cylinder · overservicedNO BRAKING ACTION FROM CO-PILOT'S RIGHT BRAKE PEDAL (ONLY 300-400 PSI REGISTERED ON BRAKE PRESS. GAUGE). - BLED HYDRAULIC SYSTEM AND SERVICED MASTER CYLINDER TO PROPER FLUID LEVEL.SDR 20001102SH031Bolt · failedDUNLOP WHEEL CMM TIE BOLT RUNNING TORQUE CHECK DOES NOT CHECK FULL LENGTH OF THE THREADS. THE TIE BOLTS APPEAR TO BE STRETCHING FARTHER TOWARD THE SHANK OF THE BOLT. WHEN RUNNING TORQUE WAS CHECKED OVER, THE FULL LENGTH OF THE THREAD, 5 BOLTS FAILED. (X)SDR VJ1R2000002Turbine Wheel · failedTURBINE WHEEL FAILURE. TURBINE WHEEL, P/N M167222-1, S/N V16-H329N. TSN: 661.9 HOURS. CSN: 2,311. SUBMITTER STATED THIS TURBINE WHEEL INSTALLED IN THIS APU 5-9-97. (X)SDR 98ZZZX4648Line · brokenPILOT'S DISCREPANCY WAS NR 1 ENIGNE IS TEMP LIMITED ABOVE CRUISE DETENT. REMOVED THE OUTER AND 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 CAUSDR 99ZZZX889Eec · failedENGINE UNRESPONSIVE TO THROTTLE MOVEMENT. TROUBLESHOT FADEC FAULT 'TE' (ENGINE SPEED LIMITED AT IDLE WHEN INTRANSIT DISCRETE). FADEC 'SEES' THRUST REVERSER INTRANSIT, HOLDS ENGINE AT IDLE. FOUND ELECTRONIC ENGINE CONTROL AT FAULT. REPLACED EEC. OPS CHECK
Back to Corporate Jets BAE 125-1000A