BMW Rolls BR700-710A220

Service difficulty reports · 189

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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 engine_model_key = 'BR700710A220'
  ORDER BY difficulty_date DESC"

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SDR CA100629003Generator · failedACFT HAD A VFG NR1 RUPTURED IN FLIGHT. OCCURRED AFTER APPROX 8 HRS OF FLIGHT. THE CREW HEARD A LOUD BANG FOLLOWED BY A GEN 1 FAILED MESSAGE ON EICAS. THEY LANDED AND AFTER A VISUAL INSP, THEY FOUND THE LT ENGINE LOWER COWLING PUNCTURED AND THE VFG DAMAGED. OJun 28, 2010 · Bombdr BD7001A10 · AC Generator-AlternatorSDR CA100611003Regulator · defectiveCYLINDER ASSY WAS RECEIVED FOR HYDROSTATIC TESTING. UPON REMOVAL OF REGULATOR FROM CYLINDER, VISUAL INSP OF THE REGULATOR DETECTED DEFORMATION OF THE REGULATOR BODY AT AND IN THE VICINITY OF THE THREADS USED TO SECURE THE REGULATOR TO THE CYLINDER. THE MFG Jun 11, 2010 · Bombdr BD7001A10 · Oxygen SystemSDR CA100611004Regulator · defective4 CYLINDER ASSEMBLIES WERE RECEIVED FOR HYDROSTATIC TESTING. UPON REMOVAL OF REGULATORS FROM CYLINDERS, VISUAL INSP OF THE REGULATORS DETECTED DEFORMATION OF THE REGULATOR BODIES AT AND IN THE VICINITY OF THE THREADS USED TO SECURE THE REGULATORS TO THE CYLINDJun 11, 2010 · Bombdr BD7001A10 · Oxygen SystemSDR CA100121009Counterbalance · separated(CAN) A SCREW SHEARED AND A COUNTER BALANCE WEIGHT FLEW OFF THE TURBINE WHILE TESTING IN FLIGHT. THE FLIGHT CREW DID NOT NOTICE THE FAILURE. UPON RETURN, AN INSP PRIOR STOWAGE OF TURBINE REVEALED THE MISSING WEIGHT. AFTER THAT FACT, AN INSP WAS CARRIED OUT ON Jan 20, 2010 · Bombdr BD7001A10 · Air Conditioning SystemSDR 2010FA0000058O-Ring · pinchedWHILE ACCOMPLISHING DISASSEMBLY FOR NR 2 BEARING HOUSING REPAIR (SB72-900500), A DEFECTIVE O-RING WAS FOUND ON THE FRONT PANEL ASSY. O-RING PN WAS AN SU-326. THE PACKING APPEARED PINCHED FROM ASSY OF THE NR1 BRG HSG ONTO THE FRONT PANEL ASSY.Jan 16, 2010 · Engine (Turbine/Turboprop)SDR CA090526001Circuit Card · burned(CAN) ON LANDING ROLL OUT, THE CREW STARTED THE APU, THE APU GEN CAME ON LINE AND THEN FAILED. THE CREW TRIED A RESET WITH NO LUCK SO KEPT RT ENGINE RUNNING AND SHUTDOWN THE APU. BY THIS TIME THE ACFT WAS ON PARKING BAY AND PASSENGERS WERE GETTING OFF. THERE May 22, 2009 · Bombdr BD7001A11 · AC Power Distribution SystemSDR CA090325005Receptacle · shorted(CAN) DURING FLIGHT, SOME 250 NM AFTER TAKEOFF, HOT CUP WAS INSERTED INTO ITS SOCKET. WHEN PLUG TERMINAL PINS TOUCHED THE POWER RECEPTACLE THEY WERE ALSO IN CONTACT WITH THE ALUMINIUM PANEL WHICH ALSO HAS A METAL HONEYCOMB STRUCTURE. A SHORT CIRCUIT TO GROUND Mar 10, 2009 · Bombdr BD7001A11 · Electrical Power SystemSDR CA090130003Bracket · looseQUANTITY 2 BOLTS LOOSE ON BRACKET GD417-1579-3 QUANTITY 2 BOLTS INSTALLED BUT NOT SECURED AND TORQUED BOLT ARE NAS 6203-3 THE ELEVATOR BRACKET ASSY IS MOVING UP OR DOWN .375 INCH LOCATION: RT ELEVATOR PULLEY BRACKET ASSY REAR FUSELAGE F/S 955.Jan 27, 2009 · Bombdr BD7001A10 · Fuselage Main, Attach FittingsSDR CA090130005Support · loose3 BOLTS NAS6203-3 MISSING ONTO PULLEY SUPPORT GD417-1570-3 AND 3 BOLTS NAS6203-3 MISSING ONTO PULLEY SUPPORT GD417-1573-3. 1 BOLT NAS6203-3 MISSING ONTO CHANNEL GD417-1580-3. HOLES ON CLEAT GD417-1661-1 DO NOT LINE UP WITH PULLEY SUPPORT GD417-1570-3 AND HOLEJan 27, 2009 · Bombdr BD7001A10 · Fuselage Main, Attach FittingsSDR CA081219001Controller · malfunctioned(CAN) AIRCRAFT SUFFERED A RAPID DEPRESSURIZATION AT 47 000 FT AND COULD NOT CONTROL THE CABIN PRESSURE IN EITHER MANUAL OR AUTO MODES. OXYGEN MASKS DEPLOYED AND EMERGENCY DESCENT WAS PERFORMED. A/C LANDED SAFELY AT SAO PAULO, BRAZIL. NO CAIMS MESSAGE WERE Dec 9, 2008 · Bombdr BD7001A10 · Cabin Pressure ControllerSDR CA081112004Spoiler Sys · malfunctioned(CAN) AFTER TAKEOFF AND DURING CLIMB, A LATERAL CONTROL MOVEMENT TO THE LT WAS NOTICED . ONE SPOILERON DEPLOYED ON THE LT WING (2 PAIR OF MULTI-FUNCTION SPOILER (MFS) IAW WING ON THIS ACFT). THE LT NR 2 MFS WAS AMBER LINE ON THE FLIGHT CONTROL SYNOPTIC PAGE. SNov 10, 2008 · Bombdr BD7001A10 · SpoilersSDR UG82008F00000Shaft · failedDUMP HANDLE SLIPS ON SHAFT. THE SHAFT SEEMS TO BE UNDER SIZE. (K)Jun 4, 2008 · N551KF · Gulstm GVSP · Water and Waste SystemSDR UG82008F00001Shaft · failedDUMP HANDLE SLIPS ON SHAFT. THE SHAFT SEEMS TO BE UNDERSIZE. (K)Jun 4, 2008 · N940DC · Gulstm GVSPG550 · Water and Waste SystemSDR CA080423003Eec · unserviceable(CAN) THE AIRCREW REPORTED THE FOLLOWING, AC WAS CRUISING AT FL450 AND CREW REALIZED THAT THE LT ENGINE SPOOLED DOWN TO IDLE WITHOUT PILOT INPUT. CREW ATTEMPTED TO MOVE THE THROTTLE IN EPR AND N1 MODE AND THERE WAS NO REACTION FROM THE LT ENGINE. EICAS MESSAGApr 21, 2008 · Bombdr BD7001A10 · Fuel Controlling SystemSDR CA071130002Inverter · overheated(CAN) DURING MAINT AND AFTER THE AC HAD BEEN POWERED WITH EXTERNAL GROUND POWER FOR APPROX 4 HOURS, THE CREW NOTICED A BURNING SMELL AROUND THE AC. NO ABNORMAL INDICATIONS WERE DISPLAYED ON THE CREW ALERTING SYS (CAS) MESSAGE AND THE ELECTRICAL MGMT SYS CONTRONov 29, 2007 · Bombdr BD1001A10 · AC InverterSDR CA070418001Potable Water · leaking(CAN) FOLLOWING THE ADVISORY WIRE FROM MFG, THE WATER SYSTEM VENT VALVES (6) WHERE REPLACED IN MFG. ON THE NEXT CUSTOMER FLIGHT, ONE VENT VALVE FROM THE GALLEY HAS STARTED TO LEAK. END RESULT, AVIONICS BAY FLOODED, BLACK BOXES FULL OF WATER. INVESTIGATION SHOWApr 16, 2007 · Bombdr BD7001A10 · Potable Water SystemSDR CA070111016Fan Blade · separated(CAN) DURING CLIMB AT APPROXIMATELY 35,000 FEET, THE CREW HEARD A LOUD BANG AND THE LT ENGINE SHUTDOWN. THE CREW DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. AN INSPECTION OF LT ENGINE REVEALED ONE FAN BLADE HAD FRACTURED JUST ABOVE THE ROOT. THE BLADE ROODec 19, 2006 · Bombdr BD7001A10 · Turbine Engine Compressor SectionSDR CA070117001Servo · malfunctioned(CAN) THE OPERATOR REPORTED AILERON CONTROL DIFFICULTIES AT FL470 WHILE ENROUTE. THE AIRCRAFT DEPARTED IN HEAVY RAIN. THE PILOT-IN-COMMAND (PIC) DISCONNECTED THE AUTOPILOT AFTER AN AP TRIM IS LWD CAS MESSAGE WAS ANNUNCIATED AND NOTED THAT THE AILERON CONTROLDec 16, 2006 · Bombdr BD7001A10 · Autopilot Main ServoSDR CA070118007Probe · malfunctioned(CAN) DURING CRUISE AT 43,000 FEET, CREW HAD EICAS MESSAGE AIR DATA COMPUTER (ADC) 3 MISCOMPARE ANNUNCIATED FOR 2 MINUTES FOLLOWED MOMENTARILY BY ADC 1 MISCOMPARE AND THEN ADC 2 MISCOMPARE MESSAGES. AFTER THE MESSAGES WENT OUT, COCKPIT INDICATIONS STARTED TO Dec 7, 2006 · Bombdr BD7001A10 · Air Data ComputerSDR YNO2006F00001Tube · crackedON AUGUST 2, 2006, AC WAS PREPARING TO DEPART AIRPORT. FOLLOWING A SUCCESSFUL NR 1 ENG START, PILOTS NOTICED NR 1 HYD SYSTEM QUANITY DROPPING RAPIDLY A FEW MINUTES AFTER START. PILOTS IMMEDIATELY SHUTDOWN BOTH ENGINES TO INVESTIGATE THE PROBLEM. UPON INSPECAug 2, 2006 · N917R · Bombdr BD7001A10 · Hydraulic System, MainSDR CA060407008Access Panel · missing(CAN) THE AIRPLANE LANDED AT IT`S DESTINATION WHEN CREW EXITED THE PLANE, THEY NOTICED THAT THE AFT RT BELLY ACCESS PANEL WAS MISSING. NOTHING WAS NOTICED BY CREW WHILE IN FLIGHT (VIBRATIONS). (TC NR 20060407008)Mar 31, 2006 · Bombdr BD7001A10 · Nacelle/Pylon, Plate/SkinSDR CA051213002Tire · failedA/C DEPARTED, NR 2 TIRE BLOW OUT ON LANDING. SHORTLY AFTER LANDING, CREW REPORTED LOST NR 2/3 HYD SYSTEMS. AS A RESULT OF THIS, LOST ALL BRAKING AND STEERING AND RT T/R WAS STUCK IN DEPLOYED POSITION. A/C DRIFTED TO RT AND EXITED RUNWAY INITIALLY ONTO A HIGDec 9, 2005 · Bombdr BD7001A10 · TireSDR CA041124001Indicator · broken(CAN) DURING STRAIGHT AND LEVEL FLIGHT, THE ISI (STANDBY ADI) SHUTDOWN AND CAME BACK ONLINE BY ITSELF. THE ISI WAS REPLACED.Nov 19, 2004 · Bombdr BD7001A10 · Altimeter, Barometric/EncoderSDR CA040930007Control Unit · burned(CAN) DURING ROUTINE MAINTENANCE, THE CREW REPORTED THAT THE NR 2 SFCU CIRCUIT BREAKER POPPED TWICE AND WERE RESET TWICE. THEY THEN SMELLED SMOKE COMING FROM THE AVIONICS BAY. THE SOURCE OF SMOKE WAS TRACED BACK TO THE SFCU. THE SFCU WAS REMOVED AND WAS FOUNSep 28, 2004 · Bombdr BD7001A10 · Trailing Edge Flap Control SystemSDR CA041004006Connector · burned(CAN) THE CREW SMELLED SMOKE IN THE COCKPIT AND RETURNED TO THE AIRPORT JUST AFTER TAKEOFF. THEY HAD SEVERAL CIRCUIT BREAKER TRIPPED FOR THE DC BUS 1 ON THE EMSCDU AND EVENTUALLY THE DC BUSS 1 FEED 4, WHICH FEED SPDA 4 TRIPPED AS WELL. SEVERAL ANOMALIES WERESep 8, 2004 · Bombdr BD7001A10 · Electrical Power System WiringSDR CA040408012Torque Tube · disconnected(CAN) ON APPROACH THE CREW SELECTED SLATS TO GO OUT AND GOT A FAIL MESSAGE ON EICAS. POST LANDING INSPECTION REVEALED THAT THE LT SLAT PARTIALLY DEPLOYED AND THE RT SLAT WAS STOWED. MAINTENANCE CREW FOUND THE RT TORQUE TUBE DISCONNECTED FROM THE SLAT POWER DRApr 1, 2004 · Bombdr BD7001A10 · Leading Edge Slat Control SystemSDR CA040408001Eec · malfunctioned(CAN) OPERATOR REPORTED A RECENT IN-FLIGHT OCCURRENCE WHERE, AFTER APPROXIMATELY 2 HOURS INTO THE FLIGHT, AT 41,000 FT, THE RT ENGINE SHUTDOWN AND AN AMBER FADEC FAIL.Mar 26, 2004 · Bombdr BD7001A10 · Fuel Controlling SystemSDR CA040216008Visor · separated(CAN) PILOT WAS MOVING HIS VISOR BACK FROM EXTREME RT SIDE OF VISOR RAIL TO LT, WHEN VISOR FELL OFF RAIL ONTO THROTTLE QUADRANT. LT ENGINE RUN SWITCH ON QUADRANT WAS INADVERTENTLY MOVED TO OFF POSITION BY VISOR IMPACT AND ENGINE STARTED TO SHUT DOWN. PILOT Feb 13, 2004 · Bombdr BD7001A10 · Flight Compartment EquipmentSDR CA031216006Control Unit · failed(CAN) AFTER TAKE OFF, (BRAKE FAULT) AND (GND LIFT DUMP) ADVISORY CAS MESSAGE WERE POSTED UPON GEAR RETRACTION AND REMAIN POSTED THROUGHOUT THE FLIGHT. ON TOUCHED DOWN, THE PILOT NOTICED THAT THERE WAS NO DECELERATION FELT WHEN APPLYING THE PEDALS. THE THRUSTNov 16, 2003 · Bombdr BD7001A10 · Landing Gear Brake SystemSDR CA030520004Controller · malfunctioned(CAN) AFTER 10 LANDINGS A STAB TRIM MSG. ATTEMPTED 2 RESETS OF CHANNELS 1 & 2 STAB STUCK AT 5.8 UNITS. LANDED IN OUT OF TRIM CONDITION AT CYUL. INVESTIGATION ON GOING.May 20, 2003 · Bombdr BD7001A10 · Elevator Tab Control SystemSDR CA030203003Display · intermittent(CAN) ON CLIMB OUT, CO-PILOT'S PRIMARY DISPLAYS LOST ALL VIDEO DATA, AND SCREENS HAD A RED X. THIS WAS QUICKLY FOLLOWED BY THE SAME LOSS OF DATA AND RED X ON PILOT'S PRIMARY DISPLAYS. EICAS BEGAN TO FILL UP WITH NUMEROUS AMBER MESSAGES, THEN PILOT'S ANDCO-PILFeb 2, 2003 · Bombdr BD7001A10 · Central ComputersSDR CA021015008Wire · pinched(CAN) DURING RETURN TO SERVICE TESTING AFTER A MAINTENANCE DOWNTIME, THE FLAPS WERE OPERATED AND WHEN THEY REACHED APPROXIMATELY 30 DEGREES, AN AVIONICS SMOKE MESSAGE WAS OBSERVED. PRIOR TO POWER BEING REMOVED FROM THE A/C, A SLAT/FLAP HALF SPEED MESSAGE WAS Oct 10, 2002 · Bombdr BD7001A10 · Flight Control System WiringSDR CA020905007Slat Track · worn(CAN) DURING A 'C' CHECK, PREMATURE WEAR OF THE SLAT TRACK PLATING WAS DISCOVERED (PLATING WORN). IT APPEARS THE WORN SURFACE PLATING PROCESS WAS USED. TRACK AFFECTED RAIL : LT SLAT NR 1, RAIL NR 2, RT SLAT NR 1, RAIL NR 2, RT SLAT NR 3, RAIL NR 3Aug 23, 2002 · Bombdr BD7001A10 · Wing, Control SurfacesSDR CA021209001Ribbon Heater · melted(CAN) RIBBON HEATERS INSTALLED ON FORWARD CABIN LINES WERE INOPERATIVE. ON INVESTIGATION IT WAS FOUND THAT THE HEATERS WERE BURNED AND MELTED CAUSING OPEN CIRCUITS.May 21, 2002 · Bombdr BD7001A10 · Water/Waste System WiringSDR CA020215009Rivet · jammed(CAN) DURING A/C 20002 FLT 26, AM ELEVATOR BINDING EXPERIENCED BY CREW DURING HANDLING TESTS. AIRCREW TOOK NECESSARY PRECAUTIONS TO EVALUATE FLT CONTROL AVAILABILITY TO PERFORM SAFE LDG W/O HAVING TO DISCONNECT ELEVCCT. FOLLOWING AIR ASSESSMENT, CREW PROCEEDFeb 4, 2002 · Bombdr BD7001A10 · Elevator StructureSDR 2003FA0000218Battery · faultyAIRCRAFT WAS CONNECTED TO EXTERNAL AIRCRAFT POWER CART, AND POWERED UP. A LOUD POP WAS HEARD COMING FROM AFT EQUIPMENT BAY OF AIRCRAFT. DURING INVESTIGATION, ANOTHER POP WAS HEARD. ACCESSED APU BATTERY. FOUND IT TO BE DAMAGED AND SMOKING. FOUND SEVERAL CESep 5, 2001 · N226HD · Bombdr BD7001A10 · Airborne Auxiliary Power Unit (APU) SystemSDR CA001129009Blade · broken(CAN) DURING A FLIGHT TEST OF THIS AIRCRAFT AND DURING DESCENT THE ENGINE VIBRTION (NH) HAS GONE ABOVE LIMIT. ENGINE HAS BEEN REMOVED SENT TO RRC FOR BORESCOPIC INSPECTION. BORESCOPE INSPECTION REVEALED ONE OFF STAGE 1 BLADE BROKEN OFF AT APPROXIMATELY MID SPAOct 9, 2000 · Bombdr BD7001A10 · Turbine SectionSDR 2000ZZZX71Housing · cracked(CAN) CRACK FOUND ADJACENT TO HYDRAULIC PUMP MOUNTING POSITION FORWARD FACE ON ACCESSORY GEARBOX. PART TOTAL CYCLES: 34. (X)Oct 13, 1999 · Bombdr BD7001A10 · Turbine Engine Accessory DriveSDR CA990125014Gearbox · cracked(CAN) ENGINE OIL WAS VISIBLE ON HI-POWER RUN-UP. INSPECTION FOUND OIL COMING FROM A 0.400 INCH LONG LINE ON THE ACCESSORY GEARBOX . NO VISIBLE CRACK DETECTED. FURTHER REPORT TO FOLLOW. PART TC: 9.Jan 12, 1999 · Turbine Engine Accessory Drive
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