British Aerospace HS748 SERIES 2B
Service difficulty reports · 48
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 = 'HS7482B' 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 = 'HS7482B' 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 CA141021012Elt · false activation(CAN) ELT ACTIVATED WHILE AIRCRAFT WAS ON THE APRON, REASON UNKNOWN.SDR CA140806005Elt · malfunctioned(CAN) ELT ACTIVATED WHILE ACFT WAS ON THE GROUND, REASON UNKNOWN.SDR CA140715001Elt · false activation(CAN) ELT ACTIVATED WHILE ON GROUND. REASON UNKNOWN.SDR CA140523007Elt · false activation(CAN) ELT ACTIVATED FOR UNKNOWN REASON WHILE ON GROUND.SDR CA140307006Elt · false activation(CAN) ELT ACTIVATED WHILE ON THE GROUND. REASON UNKNOWN.SDR CA050119009Heater · failed(CAN) SHORTLY AFTER DEPARTING, THE CABIN HEATER FAILED. THE CREW RETURNED THE AIRCRAFT TO POINT OF DEPARTURE. THE HEATER UNIT WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR CA050119007Landing Gear · unknown(CAN) ON TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT AFTER BEING SELECTED. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE AND LANDED NORMALLY. THE AIRCRAFT WAS HANGARED AND A GEAR SWING CARRIED OUT, THE FAULT COULD NOT BE DUPLICATED. THE AIRCRAFT WAS RETURNED TO SDR CA040531002Wire Harness · chafedAFTER DEPARTING, THE CREW OBSERVED ABNORMALLY LOW TGT VALUE ON NR 1 ENGINE. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE FOUND CHAFED WIRING AT THE TGT JUNCTION BOX, THE EXTERNAL CALIBRATION TEST CONNECTOR ASSY WAS REMOVED AND THE AIRCRAFT RETURNSDR CA021125001Oil Cooler · leaking(CAN) AIRCRAFT TOOKOFF FROM YZG FOR YUZ, AFTER TAKEOFF IN FLIGHT THE RT ENGINE OIL PRESSURE LIGHT CAME ON, OIL PRESSURE ZERO, PILOT SHUTDOWN ENGINE. ON ARRIVING TO YVP, INSPECTION WAS CARRIED OUT, AND RT OIL COOLER HONEYCOMB WAS LEAKING. RT OIL COOLER WAS REPSDR CA021030003Actuator · failed(CAN) NOSEWHEEL STEERING INTERMITTENTLY STIFF. NOSE WHEEL STEERING ACTUATOR WAS DISASSEMBLED. O-RING ON PISTON ROD WAS FOUND CUT, ALLOWING PRESSURE TO EQUALIZE ON EITHER SIDE OF THE RAM. BACKUP RINGS WHICH ARE INSTALLED ON EITHER SIDE OF THE O-RING WERE MISSINSDR CA020531009Supercharger · failed(CAN) DURING CRUISE FLIGHT, THE CREW NOTICED THAT THE CABIN PRESSURE WAS FLUXUATING ABNORMALLY. THE CREW SELECTED MANUAL OPERATION AND SELECTED THE NR 1 SOURCE AND CONTINUED THE FLIGHT TO DESTINATION. MAINTENANCE FOUND THAT THE NR 1 SUPERCHARGER HAD FAILED. BSDR CA011121006Rotor · damaged(CAN) DURING CRUISE, PILOTS SMELLED SMOKE IN COCKPIT. AT SAME TIME FLT ATTENDANT NOTIFIED COCKPIT THAT LAVATORY SMOKE DETECTOR HAD GONE OFF. A/C DEPRESSURIZED & EMERG DESCENT MADE, FOLLOWED BY UNSCHED LDG IN LA RONGE, SK. AIR-COND SYS OPERATED NORMALLY ON SUBSSDR CA010507011Hose · ruptured(CAN) DURING ENGINE START, A/C LOST OUTBOARD BRAKE PRESSURE: MARSHALER NOTICED HYDRAULIC FLUID COMING FROM RIGHT NACELLE, & APPROPRIATELY SIGNALLED A/C CREW. ENG SHUTDOWN, & HYDRAULIC LEAK INVESTIGATED. RUPTURED HOSE FOUND AT TOP OF RT MAIN GEAR SHOCK STRUT.SDR CA010511024Pin · dislodged(CAN) WHEN CLIMBING THROUGH 12,000 FEET, PILOT REALIZED THERE WAS NO RUDDER TRIM INPUT WHEN WHEEL WAS TURNED. AIRCRAFT RETURNED TO BASE AND LANDED OVERWEIGHT. TAPER PIN THAT HOLD RUDDER WHEEL WAS FOUND DISLODGED. PIN WAS RE INSTALLED AN SECURED. OVERWEIGHT LANSDR CA010425005Contactor · intermittent(CAN) ON APPROACH, CREW SELECTED FLAPS TO APPRAOCH FROM 15 DEGREES. FLAPS FAILED TO MOVE. HANDLE SELECTED & DE-SELECTED SEVERAL TIMES, FLAPS OPERATED NORMALLY. FOUND UP SIDE OF REVERSING CONTACTOR FAILING INTERMITTENTLY. REPLACED CONTACTOR, NO FURTHER PROBLEMSSDR AU010022Hose · cracked(AUS) RT GEARBOX MOUNTED HYDRAULIC PUMP OUTLET HOSE END FITTING CRACKED ON FLARED OLIVE.SDR CA010205023Bolt · broken(CAN) CREW ON LANDING DECLARED AN EMERGENCY DUE TO RED LIGHT ON RT MAIN GEAR. INVESTIGATION AFTER LANDING REVEALED THAT TRIP BOLT OPERATING MICROSWITCH ON DOWNLOCK WAS BROKEN P/N 100021303 LEADING TO FALSE INDICATION. TRIP BOLT P/N 100021303 WAS REPLACED AND RSDR CA010118004Block · misinstalled(CAN) PRECAUTIONAERY INSPECTION OF FLAP LEVER ASSEMBLY SLIPPER BLOCK FOR INCORRECT PRESENCE OF A SHIM UNDER, THE HEAD OF THE SLIPPER BLOCK, RETAINING BOLTS, SHIMS WERE FOUND LT SIDE STATION 0 IB BLOCK, STAION 91 IN AND OB BLOCK, STATION 296 OB AN IB BLOCK, RT SDR CA001030009Radar · failed(CAN) ON DEPARTURE, DURING CLIMB RADAR INDICATOR EMITTED SMOKE AFTER SELECTED ON. ELECTRICAL FIRE CHECK LIST CARRIED OUT AIRCRAFT RETURNED TO POINT OF DEPARTURE. THE INDICATOR WAS VERIFIED AS THE SOURCE OF THE PROBLEM AND NO WIRING ANOMOLIES WERE OBSERVED. THESDR CA000804022Case · cracked(CAN) DURING HOT SECTION INSPECTION, COMPRESSOR OUTLET CASING FOUND TO BE CRACKED BEYOND MAINTENANCE MANUAL LIMITS. CIRCUMFERENTIAL CRACK 7 IN , MAX ALLOWABLE IS 6 IN. AS VIEWED FROM REAR OF ENGINE THROUGH COMPRESSOR NR 1 OUTLET, WITH COMBUSTION CHAMBER REMOVESDR CA000606022Window · separated(CAN) THE CREW REPORTED HEARING AN UNUSUAL ONE TIME NOISE WHILE THEY WERE ENROUTE YYH TO YZF. AFTER ARRIVING YZF A PORTION OF THE RT EMERGENCY EXIT OUTER WINDOW PANE WAS OBSERVED TO HAVE DEPARTED THE AIRCRAFT. DAMAGE TO THE RT HORIZONTAL STABILIZER LEADING EDGSDR CA000427019Brush Block · failed(CAN) PROP BRUSH BLOCK FAILURE EXPERIENCED. SLIP RINGS WERE SEVERELY PITTED ALONG WITH SIGNS OF BURING AND MELTING OF BRUSH GEAR. NO CURCUIT PROTECTION WAS ACTIVATED. INSPECTION SCHEDULE REQUESTED FROM OPERATOR. MAINTENANCE INSPECTIONS OF BRUSH BLOCK ARSDR CA991209063Fire Detector · failed(CAN) ON TAXI, NR 1 ENGINE FIRE WARNING ILLUMINATED. INVESTIGATION REVEALED FAILED FIRE WIRE AND FERRULE. PARTS REPLACED.SDR CA990521031Bearings · wrong part(CAN) SPILL VALVE IN FOR OVERHAUL. BEARINGS ON ARMATURE FOUND TO DIFFER FROM ONES LISTED IN IPL. BEARINGS WILL BE REPLACED.SDR CA990308010Gearbox · making metal(CAN) DURING REMOVAL OF THE ALTERNATOR, FERROUS METAL WAS FOUND IN THE ALTERNATOR AREA. THE GEARBOX WAS REPLACED.SDR AU990416021Seal · leaking(AU) UPON INSTALLATION IN AIRCRAFT SEAL DRAIN BEGAN LEAKING. UPON INVESTIGATION BY R&O SHOP LEAK HAD DISSAPPEARED. THREE SIMILAR INSTANCES HAVE LED TO CONCLUSION THAT EVEN IN A SHORT PERIOD OF TIME THIS SEAL WILL DRY OUT. SUBMITTER SUGGESTS THAT THESE PUMPSDR CA981230020Line · leaking(CAN) HYDRAULIC FLOW LIGHTS CAME ON IN-FLIGHT, EMERGENCY DECLARED. WHEN U/C LOWERED, THE STANDBY LIGHT WENT OUT, HYDRAULIC PRESSURE WAS NORMAL. AIRCRAFT LANDED OK. STANDBY HYD PUMP BLEED NIPPLE LEAKING, RESEALED, PUMPS BLED AND FLUID REPLENISHED. ON APPROASDR CA980916055Tire · ruptured(CAN) ON DEPARTURE, GROUND PERSONNEL REPORTED DEBRIS ON RUNWAY, AIRCRAFT MADE LOW PASS AND NR 2 POSITION TIRE APPEARED FLAT. AIRCRAFT LANDED AND NR 1 AND NR 2 WHEELS REPLACED. DIAMOND SHAPE SECTION OF RUBBER 18 BY 11 MISSING FROM TIRE.SDR CA980529006Shaft · damaged(CAN) GENERATOR WOULD NOT COME ON LINE. INSPECTION FOUND THE GENERATOR DRIVE (FEMALE) IN THE ACCESSORY GEARBOX NOT TURNING. GEARBOX REMOVED FOR REPAIR.SDR CA980529005Selector · sticking(CAN) ON GEAR DOWN, SELECTION HANDLE DID NOT GO ALL THE WAY DOWN, SELECTOR RECYCLED AND OPERATED PROPERLY. SYSTEM CHECKED, LUBED, TESTED AND NO FAULT FOUND. PROBLEM OCCURRED AGAIN. TELEFLEX CABLE REPLACED, TESTED OK, OCCURRED AGAIN AND SELECTOR REPLACED SBSDR CA980415018Seal · leaking(CAN) LEAK OCCURRED WHEN WATER METHANOL PUMPS TURNED ON PRIOR TO DEPARTURE. A/C INFORMED OF LEAK WHILE HOLDING SHORT. ENGINE SHUTDOWN AND A/C TOWED. SEAL LEAKING AT FIREWALL DISCONNECT SUPPLY LINE. SEAL REPLACED.SDR CA980325041Resevoir · cracked(CAN) HYDRAULIC RESERVOIR CRACKED AT FOOT WELD AREA. REPLACED. PART TC: 11,438.SDR CA970822004Contactor · burnt(CAN) AFTER LANDING CREW REPORTED NO ANTI-ICE ON NR1 ENGINE INTAKE. INSPECTION OF CONTINUOUS LIP HEAT RELAY FOUND THE UNIT SEVERELY OVERHEATED WITH INDICATIONS OF LOCAL FIRE IN THE AREA OF THE NACELLE WHERE THE UNIT IS LOCATED. REPLACED.SDR CA970715027Supercharger · failed(CAN) WHILE IN CRUISE SMOKE ENTERED THE CABIN THROUGH THE HEATING DUCTS. THE AIRCRAFT MADE AN EMERGENCY DESCENT AND LANDING. POST FLIGHT INSPECTION FOUND THE #1 ENGINE HARD TO ROTATE PRODUCING A GRINDING SOUND. THE #1 SUPERCHARGER WAS REPLACED AND THE AIRCRAFTSDR CA970624002Supercharger · shaft sheared(CAN) LH ACCESSORY GEARBOX LOW ON OIL. THE OIL SUPPLY LINE TO THE CABIN SUPERCHARGER WAS BROKEN OFF AT THE FITTING. THE SUPERCHARGER WAS REMOVED, THE QUILL SHAFT WAS FOUND SHEARED AND THE SCROLLS BINDING. THE SUPERCHARGER DRIVE BEARINGS LOCATED ON THE GEARBOX SDR CA970609015Stringer · cracked(CAN) APPROXIMATELY 6" OUTBOARD OF LH RIB 20.0 STRINGERS 4, 6, 8 CRACKED, SKIN CRACKED BENEATH STRINGERS, EXTENDING FORWARD O.5 INCH AT STRINGERS 4 AND 6; EXTENDING AFT 1" AT STRINGERS 4 AND 6. SLIGHT DOWNWARD BUCKLING AT DAMAGED AREAS. REPAIRED IN ACCORDANCE SDR CA970326010Bolts · loose(CAN) AFTER LANDING OIL WAS OBSERVED LEAKING FROM #1 ENIGNE COWLING. THE OIL QUANTITY WAS TOPPED UP AND A GROUND RUN WAS CARRIED OUT. MAINTENANCE FOUND THE BOLTS WHICH RETAIN THE FORWARD BEARING HOUSING FOR THE COUPLING SHAFT (OUTPUT SHAFT) WERE LOOSE. THE BOLSDR CA970305004Starter · failed(CAN) #2 ENGINE FAILED TO START AFTER DE-ICING. STARTER REPLACED.SDR CA970210001Hose · leaking(CAN) AIRCRAFT LOST HYDRAULIC SYSTEM PRESSURE ON DESTINATION. LANDED NORMALLY. TOWED OFF RUNWAY. HYDRAULIC LINE TO RH MAXARET LEAKING, REPLACED.SDR CA970203011Comb Chamber · broken(CAN) DURING INSPECTION THE NOSE CONE OF ONE OF THE COMBUSTION CHAMBERS WAS FOUND BROKEN AWAY FROM THE COMBUSTION CHAMBER BODY.SDR CA970117003Accumulator · leaking(CAN) AFTER DEPARTURE AIRCRAFT HYDRAULIC PRESSURE DROPPED TO 400 PSI. PRESSURE DROP DUE TO ACCUMULATOR FAILURE. REPLACED.SDR CA970115004Engine · making metal(CAN) ENGINE WAS SHUTDOWN DURING APPROACH DUE TO ILLUMINATED OIL PRESSURE WARNING LIGHT. POST FLIGHT INSPECTION FOUND METAL IN THE OIL FILTER. THE ENGINE WAS REMOVED.SDR CA961223005Connector · dirty(CAN) PRIOR TO DEPARTURE, BOTH ENGINES RUNNING, FIRE INDICATION WAS OBSERVED ON NO.1. NO EVIDENCE OF FIRE. OIL CONTAMINATED CONNECTOR PLUG. CLEANED. SERVICEABLE.SDR CA961203012Bearing · failed(CAN) FORWARD TUNNEL SHAFT BEARING FAILED CAUSING FORWARD END CAP OF SHAFT TO DISCONNECT FROM INPUT SHAFT. SUSPECT BEARING FAILURE ATTRIBUTED T OIL STARVATION; PLUGGED JET AND/OR PUMP FAILURE. GEARBOX SHIPPED FOR TEARDOWN.SDR CA960916013Fire Wire · shorted(CAN) ON DESCENT FIRE INDICATION ON #1 ENGINE BOTTLES DISCHARGED AND ENGINE SHUT DOWN. INTERNALLY SHORTED FIRE WIRE. BOTTLES AND WIRE REPLACED.SDR CA960916012Bearing · failed(CAN) ON ROLL OUT AIRCRAFT WAS PULLING TO THE LEFT AND DIFFICULT TO STEER. LH OUTER WHEEL BEARING HAD DISINTEGRATED CAUSING INNER RACE TO SEIZE TO SPACER AND AXLE. REPLACED.SDR CA960812019Fuel Trimmer · failure(CAN) IN CRUISE #2 ENGINE FUEL TRIM FAILED. AIRCRAFT RETURNED TO BLOCKS. FUEL TRIM REPLACED.SDR CA970609032Cover · damaged(CAN) DURING TRAINING FLIGHT THE GEAR WAS SELECTED DOWN IN THE EMERGENCY MODE. THE LH GEAR WOULD NOT LOCK DOWN WITH HAND PUMP PRESSURE BUT WOULD LOCK DOWN WITH NORMAL SYSTEM PRESSURE. AIRCRAFT LANDED WITH 3 GREEN. THE UPPER SEAR COVER WAS FOUND BENT UPWARDS IN
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