British Aerospace HS-748-2A
Service difficulty reports · 190
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 = 'HS7482A' 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 = 'HS7482A' 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 CA190801002Cable · broken(CAN) DURING CLIMB THE GEAR WOULD NOT FULLY RETRACT. WHEN THE NORMAL GEAR DOWN SELECTION WAS DONE ONLY THE NOSE GEAR WENT TO LOCKED POSITION. AN EMERGENCY LOWERING WAS ATTEMPTED BUT MAINS STILL DID NOT LOCK. ALL HANDLES WERE RESET AND NORMAL GEAR DOWN SELECTEDSDR CA160304004Blade · damaged(CAN) DURING START THE ENGINE STOPPED ACCELERATING AND A LOUD THUMP WAS HEARD AND UPON FURTHER INVESTIGATION SMOKE WAS OBSERVED COMING FROM THE ENGINE AND THE ENGINE WOULD NOT ROTATE BY HAND. AFTER MAINTENANCE REVIEW ENGINE LOOKS TO HAVE FIRST STAGE BLADE DAMASDR CA151005001Wire · chafed(CAN) AIRCRAFT DECLARED AN EMERGENCY AFTER SHUTTING DOWN NR 1 ENGINE IN FLIGHT AFTER ENGINE FIRE WARNING LIGHT. CREW BLEW THE 2 FIRE EXTINGUISHER BOTTLES, BUT LIGHT REMAIN ON. THE PLANE LAND SAFELY. MAINTENANCE FOUND FIRE WIRE P/N D1384N TO BE THE FAULT. THEYSDR CA150528003Connector · shorted(CAN) DURING THE TAKEOFF ROLL THE FLIGHT CREW NOTICED THE FFP STOP REMOVED LIGHTS FOR BOTH ENGS REMAINED ILLUMINATED. THE FLIGHT CREW ABORTED THE TAKEOFF & TAXIED BACK TO THE HANGAR. DURING THE TAXI IT WAS NOTICED THAT THE BELOW FFP STOP LIGHT`S OR BOTH ENGSSDR CA141120026Wire · faulted(CAN) LT ENGINE FIRE BELL WENT OFF IN CRUISE. VISUALLY CONFIRMED FALSE INDICATION. LANDED, MAINTENANCE CONFIRMED FAULTY FIRE WIRE, SYS TESTED AND SERVICEABLE.SDR CA141003001Pump · failed(CAN) ON TAKEOFF ROLL AT 75 KTS, NR 2 ENGINE LOST POWER AND SHUTDOWN. CREW ABORT TAKEOFF WITH NO INCIDENT. FOUND NR 2 ENGINE FUEL PUMP FAULTY, PUMP REPLACED AND ACFT RETURN TO SERVICE. FUEL PUMP WILL BE SEND FOR STRIP REPORT.SDR CA140414008Skin · corroded(CAN) RIGHT MLG PIVOT BRACKET REMOVED DUE TO CRACK FOUND DURING PERIOD 19 INSPECTION. AFTER REMOVAL OF THE PIVOT BRACKET AND CLEANING OF THE LOWER WING SKIN HIDDEN BY THE PIVOT BRACKET, HEAVY CORROSION DAMAGE WAS FOUND.SDR CA131107008Line · leaking(CAN) HYDRAULIC PUMP AND LOW BRAKE PRESSURE LIGHT ILLUMINATED. COMPLETED EMERGENCY LANDING AND FOUND HYDRAULIC LINE LEAKING ON RT MAIN GEAR JACK UPLINE. ONCE TAXING THERE WAS NO FLUID FOR BRAKES.SDR CA130507002Probe · unknown(CAN) OVERHEAT AND FIRE WARNING LIGHTS WOULD NOT COME ON WITH HEAT TEST OF JANITROL HEATER SYS. FOUND THERE ARE 2 TYPES OF THERMOSTATS THAT CAN BE USED. 1 HAS A CASE GROUND AND ONE HAS NOT.SDR CA130430017Brake · failed(CAN) UPON LANDING FLIGHT CREW NOTICED THE AIRCRAFT WOULD NOT TAXI UNDER NORMAL TAXI POWER SETTINGS. THE AIRCAFT WAS SHUT DOWN ON THE RUNWAY AND TOWED BY MAINTENANCE PERSONEL. THE LEFT HAND INBOARD BRAKE UNIT WAS FOUND TO HAVE DISPLACED BRAKE PADS, CAUSING THESDR CA130422007Spar · corroded(CAN) LOCALIZED CORROSION FOUND DURING INSPECTION, EXFOLIATION OF FWD FACE UPPER REAR SPAR, BOOM, ANGLE.SDR CA130304009Blade · missing(CAN) ENGINE SN 13370, FOUND HP TURBINE BLADE MISSING DURING VISUAL INSPECTION. THERE SEEMS TO BE A TREND AS THIS IS THE 4TH HP TURBINE BLADE FOUND MISSING OVER THE PAST YEAR. INVESTIGATION INTO THIS PROBLEM HAS STARTED WITH O/H FACILITY AND INTERNAL COMPANY SDR CA130210001Case · damaged(CAN) DURING CRUISE FLIGHT, 16,000 FT, THE PILOTS OBSERVED THE PORT HYD SYS LOW FLOW LIGHT ILLUMINATED, FOLLOWED BY THE STARBOARD HYD SYS LOW FLOW LIGHT ILLUMINATING. THE ACFT RETURNED, CARRIED OUT AN UNEVENTFUL LANDING AND TAXIED TO THE HANGER USING NORMAL NSDR CA130125008Line · leaking(CAN) DURING CRUSE AT 14,000 FT, THE PORT LOW FLOW HYDRAULIC LIGHT ILLUMINATED, FOLLOWED WITHIN 60 SECONDS BY THE STARBOARD LOW FLOW HYDRAULIC LIGHT. APPROXIMATELY FIVE MINUTES LATER THE PORT D.C. GENERATOR FAILED. THE PILOTS TURNED BACK, DECLARED AN EMERGENCYSDR CA121109015Generator · seized(CAN) DURING THE TAKEOFF ROLL, ENGINE NR 1 DC GENERATOR TRIPPED DROPPED OFF LINE. THE PILOTS ABORTED THE TAKEOFF AND RETURNED TO THE TERMINAL. ATTEMPTS TO PUT THE GENERATOR ON LINE WERE UNSUCCESSFUL. MAINTENANCE REPLACED THE DC GENERATOR AND RAN THE ENGINE SDR CA121109014Oil Cooler · leaking(CAN) ACFT DEPARTED AIRPORT, APPROXIMATELY 15 MINUTES AFTER TAKEOFF, ENGINE NR 2 OIL PRESSURE GAUGE STARTED TO FLUTTER AND THE LOW OIL PRESURE LIGHT ILLUMINATED INTERMITTENTLY. THE PILOTS SHUTDOWN ENGINE NR 2, FEATHERED THE PROPELLER AND RETURNED TO DEPARTURESDR CA120525008Switch · malfunctioned(CAN) DURING TAKEOFF ROLL, THE RT ENGINE AUTOFEATHERED AT LOW SPEEED. MAINTENANCE FOUND THE LOW TORQUE SWITCH HAD FAILED, CAUSING THE PROPELLER TO AUTOFEATHER. THE TORQUE SWITCH IS A TIME-CONTROLLED PART AND HAD ACCUMULATED 15.9 HRS & 11 CYCLES SINCE LAST O/SDR CA120301003Valve · leaking(CAN) FLIGHT CREW EXPERIENCED TOTAL LOSS OF HYD PRESSURE DURING FLIGHT. THE ACFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND THE HYDRAULIC CUT OUT VALVE IN THE RT WHEEL WELL TO BE BYPASSING OR INTERNALLY LEAKING. THE VALVE WAS REPLACED AND THE ACFTSDR CA110803022Valve · crackedUPON LANDING GEAR EXTENSION IN PREPERATION FOR LANDING, CREW NOTICED A PRESSURE DROP IN THE HYD SYS. AFTER NORMAL LANDING, WHEN ACFT WAS PARKED ON RAMP, HYD FLUID WAS NOTICED UNDER THE RT NACELLE AREA. MX PERSONEL FOUND THE HYD CUT OUT VALVE HAD A CRACKED HSGSDR CA110405003Impeller · cracked(CAN) HIGH PRESSURE IMPELLER FAILURE, SECTION APPROX 40 X 40 MM RELEASED FROM QTY 1 VANE. DOWNSTREAM IMPACT DAMAGE TO ADDITIONAL VANES. ITEM HAS BEEN REMOVED FROM SERVICE & MFG HAS BEEN CONTACTED FOR FURTHER INFORMATION.SDR CA110208006Landing Gear · failed(CAN) UPON LANDING THE MAIN GEAR HAD TO BE LOWERED BY EMERGENCY SELECTION. ON LANDING THE CREW HAD 3 GREEN INDICATION.SDR CA100603004Flex Hose · ruptured(CAN) AFTER TAKEOFF, THE CREW OF ANT 207 SELECTED THE LANDING GEAR TO RETRACT. THE LANDING GEAR RETRACTED PART WAY AND THE HYDRAULIC PUMP LOW PRESSURE LIGHTS ILLUMINATED. A CHECK OF THE PRESSURE GAUGE INDICATED ALMOST NO HYDRAULIC PRESSURE. THE CREW DIVERTESDR CA090615010Engine · making metal(CAN) DURING CLIMB, RT OIL PRESSURE LIGHT ILLUMINATED AND OIL PRESSURE WAS CONFIRMED TO BE LOW. ENG WAS SHUTDOWN AS A PRECAUTIONARY MEASURE. ACFT WAS LANDED WITHOUT INCIDENT. MX INVESTIGATION REVEALED METAL PARTICLES IN THE OIL FILTERS AND ENGINE WAS REMOVSDR CA090605009Bolt · broken(CAN) BOLT THAT ACTUATED THE SWITCH FOR GEAR DOWN AND LOCKED, BROKE. THE BOLT BREAKING CAUSED THE MLG INDICATION TO SHOW IN TRANSIT AND THE MECHANICAL LANDING GEAR FLAG ARM TO BECOME DETACHED NOT SHOWING "DOWN AND LOCKED". THE GEAR WAS DOWN AND LOCKED.SDR CA090519009Oil Cooler · leaking(CAN) DURING THE CLIMB, RT ENGINE LOST OIL PRESSURE WITH ILLUMINATION OF THE WARNING LIGHT. THE CREW SHUTDOWN THE RT ENGINE AND RETURNED TO BASE. UPON INVESTIGATION BY MX, THE OIL COOLER WAS RUPTURED. THE OIL COOLER WAS REPLACED AND THE ENGINE RETURNED TO SERVSDR CA090213004Indicator · leaking(CAN) SHORTLY AFTER DEPARTURE, THE CREW OBSERVED A PORT HYD PUMP INDICATION LIGHT WHICH REMAINED ILLUMINATED WITH THE MAIN SYS CYCLING EVERY 5 SECONDS. THE ACFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. MX IDENTIFIED THAT THE STARBOARDSDR CA090211001Cone · crackedVISUAL INSPECTION DURING "A-CHECK" (WITH FLASHLIGHT) REVEALED LARGE CRACK IN CIRCUMFERENCE OF EXHAUST UNIT INNER CONE. CLOSER INSPECTION (CRAWLED UP JET-PIPE) INDICATED APPROX, 2/3 OF INNER CONE CIRCUMFERENCE CRACKED. DAMAGED AREA NORMALLY RESTS WITHIN 1/8 -SDR CA081215001Door · obstructed(CAN) AFTER DEPARTURE, THE CREW OBSERVED A PRESSURE LOCK NOT ENGAGED INDICATION FOR THE MAIN PAX DOOR. THE ACFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT INCIDENT. MX FOUND ICE IN THE DESICCANT CARTRIDGE. THE ICE WAS REMOVED AND HEAT APPLIED AFTER WHSDR CA090604004Blades · failed(CAN) DURING NORMAL COMPANY OPERATIONS A VIBRATION WAS DETECTED COMING FROM RT ENG. UPON INVESTIGATION IT WAS FOUND THAT 1ST STAGE TURBINE ASSY HAD EXPERIENCED SOME KIND OF FAILURE. LARGE SECTIONS WERE MISSING FROM SEVERAL BLADES. SECOND STAGE TURBINE SHOWESDR CA080919007Supercharger · inoperative(CAN) WHILE IN CRUISE FLIGHT, ENROUTE, CREW NOTICED A STRANGE ODOR COMING FROM THE CABIN. CREWMAN ONBOARD WENT TO LOOK IN THE CABIN AND NOTICED TEMPERATURE IN THE CABIN WAS VERY HOT AND THERE WAS LIGHT HAZE OR SMOKE IN SAFELY. MX INSPECTED THE ACFT AND FOUNDSDR CA080729006Cover · leaking(CAN) WHILE ENROUTE FROM YBK TO YTH FAMO EXPERIENCED LOSS OF HYDRAULIC PRESSURE. AN EMERGENCY WAS DECLARED AND THE ACFT DIVERTED TO YTH WHERE AN UNEVENTFUL LANDING WAS MADE. DURING THE FLIGHT HYDRAULIC PRESSURE WAS SEEN TO RISE AND FALL A NR OF TIMES. EMERGENCSDR CA080801001Flex Line · chafed(CAN) ON APPROACH, THE CREW OBSERVED A LOSS OF HYDRAULIC PRESS AFTER GEAR WAS SELECTED DOWN. THE ACFT LANDED WITHOUT FURTHER INCIDENT. MAINT IDENTIFIED THE HYDRAULIC LINE FROM THE PUMP THE HIGH PRESSURE FILTER AS THE SOURCE OF THE LEAK. THE LINE WAS REPLACED SDR CA080313004Engine · malfunctionedDURING APPROACH IN ICING CONDITIONS AND HEAVY PRECIPITATION, WHEN THE PILOT THROTTLED BACK, ENGINE NR 2 FLAMED OUT AND AUTO FEATHERED. THE PILOT DID NOT ATTEMPT TO RE-LIGHT AND LANDED WITH ONE ENGINE OPERATING. MAINTENANCE CHECKED THE OIL SCREEN, FUEL SCREEN ASDR CA071112003Fire Loop · faulty(CAN) AFTER TAKEOFF, ENGINE NR 1 FIRE-WARNING ALARM WENT OFF. THE FLIGHT CREW INFORMED TOWER AND RETURNED TO AIRPORT. A HOLE WAS FOUND IN THE FLEXIBLE DUCT AT THE SUPERCHARGER OUTLET. ALSO, (2) FIRE DETECTION LOOPS WERE REPLACED BECAUSE THEY FAILED THE RESISSDR CA071001005Impeller · damaged(CAN) WHILE ON CLIMB AFTER DEPARTING, THE WAS A BANG FROM THE RT ENGINE, TOTAL LOSS OF POWER AND FIRE WARNING. THE FWD PART OF THE ENGINE WAS SEEN TO BE ON FIRE, WHICH WAS EXTINGUISHED BY (2) SHOTS OF THE EXTINGUISHER SYSTEM. THE AIRCRAFT RETURNED TO DEPARTURESDR CA070910003Line · ruptured(CAN) 10 MINUTES PRIOR TO LANDING, THE PORT AND STARBOARD HYDRAULIC PUMP LIGHTS ILLUMINATED WITH MAIN PRESSURE DEPLETING AND STOPPING AT ACCUMULATOR PRESSURE. THE CREW CARRIED OUT THE APPROPRIATE PROCEDURES AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUNSDR CA070905005Lever · failed(CAN) AFTER ARRIVING AT AIRPORT, THE AIRCRAFT ROLLED FORWARD AFTER THE PARK BRAKE WAS APPLIED WITH ENGINES STILL RUNNING AND THEN CONTACTED GROUND EQUIPMENT. MAINTENANCE DETERMINED THAT THERE WAS A FAULT WITH THE PARK BRAKE SYSTEM AND THE HANDLE ASSEMBLY WAS SDR CA070905002Alternator · inoperative(CAN) AFTER DEPARTING AND ENROUTE, THE CREW OBSERVED NR 2 ALTERNATOR HAD TRIPPED OFFLINE AND DID NOT RESET. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE REPLACED THE NR 2 ALTERNATOR. THE AIRCRAFT COMPLETED A SATISSDR CA070824005Line · leaking(CAN) WHILE FLYING BOTH HYDRAULIC PUMP LIGHTS CAME ON. THE AIRCRAFT LANDED USING ITS BACKUP SYSTEM. IT WAS FOUND THAT THE HYDRAULIC LINE THAT RUNS BETWEEN THE PUMP AND FILTER ON THE LT NACELLE. THE LINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CA070712002Line · perforated(CAN) AFTER DEPARTING, THE CREW OBSERVED BOTH THE LT AND RT HYDRAULIC PRESSURE LOSS INDICATION LIGHTS WERE ILLUMINATED. THE AIRCRAFT DIVERTED AND LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE NR 2 HYDRAULIC PRESSURE RETURN LINE TO THE HP FILTER IN THESDR CA070507011Wire Harness · damaged(CAN) DEPARTING THE LANDING GEAR SELECT LEVER WOULD NOT MOVE TO THE GEAR UP POSITION. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE DETERMINED THE SOURCE OF THE PROBLEM WAS IN THE LT GEAR HARNESS WHEELWELL CONNECTOSDR CA070319001Pressure Switch · malfunctioned(CAN) DURING DEPARTURE THE AIRCRAFT`S HEATER FAILED AND THE CREW WAS UNABLE TO RESTART THE HEATER. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED WITHOUT FURTHER PROBLEM. MAINTENANCE REPLACED THE HEATER PRESSURE SWITCH AND THE AIRCRAFT RETURNED TO SERVSDR CA070309001Valve · malfunctioned(CAN) AC WAS IN CRUISE FLIGHT, WHEN THE FLIGHT CREW OPENED THE FUEL CROSSFEED VALVE TO BALANCE THE FUEL LOAD. WHEN THE FLIGHT CREW SELECTED THE LT BOOST PUMPS TO OFF, THE NR 1 ENGINE FLAMED OUT. THE FLIGHT CREW FEATHERED ENGINE NR 1. THE PILOT THEN CLOSED THE SDR CA070131008Line · leaking(CAN) IN CRUISE FLIGHT (30 MINUTES AFTER DEPARTURE THE FLIGHT CREW OBSERVED NR 1 AND NR 2 LOW HYDRAULIC PRESSURE LIGHTS ILLUMINATED. THE FLIGHT CREW RETURNED TO DEPARTURE, USED ALTERNATE MEANS FOR EXTENDING THE LANDING GEAR AND LANDED UNEVENTFUL. MAINTENANCE SDR CA070130002Indicator · inoperative(CAN) ON TAKEOFF ROLL THE CREW REJECTED THE TAKEOFF AT 85 KTS WITH NO INDICATION ON FIRST OFFICERS SIDE. MAINTENANCE CONDUCTED A PURGE OF THE SYSTEM AND CARRIED OUT A PITOT/STATIC SYSTEM TEST.THE SYSTEM WAS VERIFIED SERVICEABLE AND THE AIRCRAFT RETURNED TO SERSDR CA070111012Window · cracked(CAN) DURING CLIMB THE FIRST OFFICERS MAIN WINDOW CRACKED. THE AIRCRAFT RETURNED TO POINT OF DEPARATURE WITHOUT FURTHER PROBLEM. MAINTENANCE REPLACED THE WINDOW AND THE AIRCRAFT WAS RETURNED TO SERVICE. (TC NR 20070111012)SDR CA070119003Indicator · leaking(CAN) ENROUTE, THE CREW OBSERVED BOTH HYD SYSTEMS INDICATING APPROXIMATELY 1200 PSI WITH LOW FLOW LIGHTS ON. THE CREW CONTINUED WHERE ON APPROACH THE HYDRAULIC PRESSURE RECOVERED AND THE FLOW LIGHTS EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEM. MASDR CA061219029Fuel · contaminated(CAN) PILOT OBSERVED ENGINE NR 1 FUEL FILTER DE-ICING WARNING LIGHT ILLUMINATED IN CRUISE FLIGHT. SHORTLY AFTER APPLYING FUEL HEAT, ENGINE NR 1 QUIT. PILOT FEATHERED PROPELLER AND LANDED UNEVENTFUL. MAINT REMOVED ENGINE NR 1 LOW PRESSURE FUEL FILTER AND FOUNDSDR CA061128002Indicator · failed(CAN) DURING DEPARTURE THE CAPTAINS HORIZON FAILED ON CLIMB OUT. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE WITHOUT FURTHER PROBLEM. MAINTENANACE REPLACED THE NO1. GYRO AND THE AIRCARFT WAS RETURNED TO SERVICE. (TC# 20061128002)SDR CA061122007Indicator · failed(CAN) DEPARTING THE CAPT`S HORIZON FAILED DURING TAKE-OFF. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE WITHOUT INCIDENT. MAINTENANCE REPLACED THE GYRO AND THE AIRCRAFT WAS RETURNED TO SERVICE. (TC# 20061122007)
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