BMW Rolls BR700-710A110
Service difficulty reports · 188
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 engine_model_key = 'BR700710A110' 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 engine_model_key = 'BR700710A110' 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 2008FA0000607Turbine Blades · crackedDURING A RECENT MID LIFE INSPECTION OF THIS ENGINE BY THE MFG, 58 OF 74 FIRST STATE TURBINE BLADES WERE FOUND CRACKED BEYOND SERVICEABLE LIMITS. THIS WAS A HIGH FAILURE RATE CONSIDERING THE LOW TOTAL ENGINE HOURS. A REPORT FROM THE MFG INTENDING TO PROVIDE ANSDR MWE2008F00000Battery Pack · inoperativeTWO LIGHT INOPERATIVE ON TAILCONE SLIDE EMERGENCY LIGHT. REPLACED BATTERY PACK ASSEMBLY. (K)SDR 2008FA0000224Sight Glass · crackedSIGHT GLASS CRACKED IN SEVERAL LOCATIONS AND LEAKS HYDRAULIC FLUID. THIS TANK IS ONE OF SEVERAL RETURNED FOR THE SAME DEFECT. (K)SDR 2008FA0000259Slat System · malfunctionedFLIGHT CREW REPORTED THAT SHORTLY AFTER ROTATION (AFTER T/O) THEY HAD A (FLICKERING) SLAT HALF SPD AND SLAT/FLAP HALF SPD EICAS MESSAGE. SHORTLY THEREAFTER THEY HAD AN AMBER SLAT FAIL, STALL WARN ADVANCE EICAS MESSAGE, C/B TRIP (E-2 SLAT/FLAP PWR 2) AND FLIGHSDR UG8A08P011002Line · bentHYDRAULIC LINE IN TAIL COMPARTMENT JUST AFT OF LT ELT IS BENT/DENTED.SDR UG8A08P011001Torque Tube · corrodedRUDDER TORQUE TUBE INNER AND OUTER TUBES ARE CORRODED AND PITTED.SDR UG8A08P011003Frame · crackedBAGGAGE DOOR FRAME IS CRACKED.SDR UG8A08P010901Bearing · corrodedRUDDER TORQUE TUBE BEARING CORRODED AND SEAL LOOSE.SDR N93A25122007Steering Sys · failedDURING GEAR EXTENSION, STEER BY WIRE FAIL MESSAGE ILLUMINATED. NO STEERING ON LANDING.SDR EOYA20080001Skin · dentedDURING LANDING APPROACH, AIRCRAFT STRUCK SECURITY FENCE, RESULTING IN DAMAGE TO FUSELAGE SKIN PANEL ON THE LT SIDE OF THE FUSELAGE. THE LOCATION OF THE DAMAGE IS AT FUSELAGE STATION 101.18, WATER LINE 73.50. DAMAGE SUSTAINED TO SKIN PANEL IS A DENT WITH GOUGESSDR UG8A07GM12041Warning System · false activationCREW RECEIVED A CAS (AIRCRAFT CONFIG) MESSAGE DURING THE TAKEOFF ROLL. THE LOADING AND WEIGHT OF THE AIRCRAFT REQUIRED THE PITCH TRIM TO BE SET, IAW THE AFM AT THE 8 DEGREE LIMIT. IF SET AT THIS LIMIT NORMAL SYSTEM COULD CAUSE THE CONFIG WARNING TO ANNUNCIASDR N93A04122007Valve · faultyNOSE LANDING GEAR DID NOT EXTEND NORMALLY AFTER GEAR WAS SELECTED DOWN, AFTER ABOUT 45 SECONDS GEAR EXTENDED NORMALLY, FOUND NOSE LANDING GEAR DOOR CONTROL VALVE AT FAULT.SDR 2007FA0001092Oven · failedFLIGHT CREW REPORTED THE ODOR OF ELECTRICAL SMOKE IN THE GALLEY. THE ODOR WAS COMING FROM THE OVEN, THEN THE OVEN CB OPENED (POP). THE OVEN WAS REMOVED AND REPLACED WITH A NEW UNIT. (K)SDR 2007FA0001015Connector · crackedBACK SHELL IS BROKEN/CRACKED AND SEPARATED FROM CONNECTOR PLUG ASSY. POSSIBLE CAUSE IS WIRE BUNDLE TO CONNECTOR PLUG STRESSES AND PULLING ON BACK SHELL. BACK SHELL IS MADE ON PLASTIC NOT METAL. IF BACK SHELL WAS MADE OF METAL IT WOULD HOLD UP AS A STRAIN RELSDR 2007FA0000816Socket · burnedTHE SOCKET ON ONE OF THE (2) LAMPS BURNED CAUSING AN ELECTRICAL ODOR IN THE BAG BIN WHERE THE STERILIZER IS LOCATED. THE 2 AMP CIRCUIT BREAKER WHICH CONTROLS THE POWER TO THE STERILIZER DID NOT POP.SDR 2007FA0000759Fairing · crackedDURING INSPECTION OF THE AIR INTAKE ROTATING FAIRING, WE FOUND A CRACK BETWEEN THE MOUNT BOLT HOLE AND THE ADJACENT ALIGNMENT PIN HOLE.SDR UG8A2007GM07SSkin · chafedDURING COMPLIANCE WITH POST FLIGHT INSPECTION IT WAS NOTED THAT THE LT AND RT WING A FLAP TRACK ISLAND HAT PANELS WERE CHAFING THROUGH THE WING TRAILING EDGE FIXED COVE PANEL. MFG ENGINEERING DISPOSITION NR CS117877 RELEASED OUTLINING REPAIR FOR CONDITION. RSDR UG8A2007GM05SSkin · chafedDURING COMPLIANCE WITH POST FLIGHT INSPECTION IT WAS NOTED THAT THE LT AND RT WING A FLAP TRACK ISLAND HAT PANELS WERE CHAFING THROUGH THE WING TRAILING EDGE FIXED COVE PANEL. MFG ENGINEERING DISPOSITION NR CS117877 RELEASED OUTLINING REPAIR FOR CONDITION. RSDR 2007FA0000860Connector · corrodedEXCESSIVE CORROSION AT CONNECTOR PINS CAUSING NWS FAIL MSG. SUGGEST PERIODIC INSPECTION AND CLEANING OR IMPROVED CONNECTOR SEALING FROM MOISTURE. (K)SDR GM07004Seat Track · corrodedCORROSION DISCOVERED ON ALL SEAT TRACKS AFT OF FS 426.5.SDR GM07003Floorboard · corrodedCORROSION DISCOVERED ON ALL FLOORBOARD INSERTS AFT OF FS 426.5.SDR N93A04072007Tiller · unknownNOSE STEERING INOPERATIVE.SDR N93A26062007Tiller · unknownON TOUCHDOWN, CREW RECEIVED NOSE WHEEL STEERING FAIL MESSAGE.SDR UG8A2007PA01OEjector · icedDURING CRUISE THE CREW REPORTED GETTING AN AMBER FUEL TANK TEMP ILLUM WITH ACTUAL TEMP -4/-5 FOLLOWED BY L-R FUEL LOW LEVEL WITH MORE THAT 9000 LBS REMAINING. AN EMERGENCY LANDING WAS MADE. UPON ACCESSING THE FUEL EJECTOR PUMPS IN BOTH WINGS, ICE WAS FOUND SDR N93A30012007Bleed Valve · stickingENGINE VIBRATION ABOVE IDLE, ACRID SMELL IN CABIN. ENGINE WAS BORESCOPED WITH NO DISCREPANCY FOUND. MAINTENANCE FOUND BLEED AIR VALVE STICKING AND REPOSITIONED TWO (V) BAND CLAMPS.AIRCRAFT WAS DISPATCHED ON AN EVALUATION FLIGHT WITH NO FURTHER DISCREPANCIES.SDR N93A20061221Contactor · faultyACRID SMELL IN COCKPIT DURING PREFLIGHT. MAINTENANCE DETERMINED ODOR WAS FAULTY AC CONTACTOR.SDR UG8APA06007Pitot Tube · blockedNR 1MADC HAD AN ALTITUDE COMPARATOR AT 15000 FT AND A 400 FT SPLIT FROM MADC AND STDBY AT FL230. IT ALSO HAD A 5 CKAS SPLIT IN AIRSPEED. BLOCKAGE FOUND IN LT UPPER PITOT/STATIC PROBE, OF UNKNOWN ORIGIN. BLEW OUT STATIC LINES USING DRY NITOGEN. INSTALLED NESDR 65810262006Steering Sys · failedNOSE WHEEL STEERING FAIL CASS MESSAGE AS AIRCRAFT LINED UP FOR TAKEOFF.SDR 2006FA0000502Shutoff Valve · malfunctionedDURING A SCHEDULED INSPECTION, OPERATIONAL CHECK OF THE AILERON HARD OVER PROTECTION TEST. BOTH LT AND RT AILERON HYD SHUT OFF CIRCUIT BREAKERS POPPED. REPLACED RT AILERON , LT HYD SYSTEM SHUTOFF VALVE AND LT AILERON, LT HYD SYS SHUTOFF VALVE. (K)SDR 2006FA0000374Stop · brokenDURING SCHEDULED TAIL INSPECTION LT ELEVATOR UP AND DOWN STOP WAS FOUND BROKEN OFF AND LAYING IN ELEVATOR ATTACH/HINGE AREA. (K)SDR N93A20060328Shutoff Valve · malfunctionedDURING DESCENT AT FL 200 BLUE CAS MESSAGE BAGG COMPT LO PRESS ILLUMINATED. UNABLE TO OPEN INTERIOR BAGGAGE DOORSDR N93A20060325Shutoff Valve · stuckUNABLE TO OPEN INTERIOR BAGGAGE DOOR IN FLIGHT, DUE TO BAGGAGE COMPARTMENT SHUTOFF VALVE BEING STUCK. (ACTIVATES ABOVE SPECIFIC ALTITUDE AND RELEASES BELOW SPECIFIC ALTITUDE.SDR 2006FA0000382Lamp · inoperativeDURING ROUTINE LAMP REPLACEMENT, IT WAS DISCOVERED THAT ONE END OF THE REMOVED UNIT WAS DISCOLORED. THE DISCOLORATION WAS THOUGHT TO BE DUE TO OVERHEATING. THE LOCATION OF THE FAILED LAMP WAS IN THE GALLEY OVERHEAD. INSTALLED NEW UNIT OF SAME MFG AND PN. OSDR 2006FA0000174Computer · failedDURING A RECENT FLIGHT DISPLAY UNITS 1,2, AND 3 BLINKED ON AND OFF. DISPLAY UNITS 1, 2 CYCLED ON AND OFF DISPLAY UNIT 3 WAS RED X`D. DURING THAT TIME AN AMBER (MAU 3A FAIL) MESSAGE DISPLAYED AND A BLUE (DATABASE CONFIG) MESSAGE ALSO DISPLAYED. AFTER 5-8 SECSDR PA06001Eec · malfunctionedDURING CRUISE, THE LEFT ENGINE ROLLED BACK AND FLAMED OUT. EICAS MESSAGE -LEFT ENGINE FAILED- DISPLAYED. UNSCHEDULED LANDING MADE. THE LT ENGINE ELECTRONIC ENGINE CONTROLLER (EEC) WAS FOUND TO HAVE VARIOUS FADEC SYSTEM FAULTS WHEN INTERROGATING THE MDAU. TSDR UG82006F00000Attach Bracket · failed(REF: GM06-001) NO TONE OR RUDDER LIMIT ANNUNCIATIONS RECEIVED DURING CONTROL CHECK. UPON INSPECTION OF THE RUDDER ACTUATOR IT WAS NOTICED THAT THE FORWARD RUDDER ATTACH FITTING HAD FAILED. SUSPECT INCORRECT HARDWARE STACK UP OR OUT OF PLACE BUSHING TO HAVE SDR 62512082005Unknown · unknownWHILE TAXING AIRCRAFT RT MAIN GEAR DEPARTED TAXI WAY.SDR 2005FA0001566Blade · debondedDURING ROUTINE ENGINE A-CHECK INSPECTION, FOUND 15 OUT OF 24 (CHOCKING PADS) ON BASE OF ENGINE FAN BLADE TO HAVE MIGRATED AFT OF NORMAL POSITION DUE TO DEBONDING OF (CHOCKING PAD). THIS CONDITION WAS CAUSING ABNORMAL ENGINE VIBRATION DURING ENGINE GROUND OPERSDR 2005FA0001561Blades · debondedDURING ROUTINE ENGINE A-CHECK INSPECTION, FOUND 15 OUT OF 24 (CHOCKING PADS) ON BASE OF ENGINE FAN BLADE TO HAVE MIGRATED AFT OF NORMAL POSITION DUE TO DEBONDING OF (CHOCKING PAD). THIS CONDITION WAS CAUSING ABNORMAL ENGINE VIBRATION DURING ENGINE GROUND OPERSDR 2005FA0001550Cowl Door · crackedDURING ROUTINE INSP, FOUND 25 INCH CRACK, SEVERE DELAMINATION WITHIN THE LT ENG LOWER COWL DOOR. AFFECTED AREA IS LOCATED JUST AFT OF FWD SIDE, BETWEEN THE 4 & 8 O'CLOCK POSITION. INITIAL INSPECTION REVEALS DEBOND ON CARBON FIBER SKIN TO CORE AT 375 SQUARE SDR GM05010Actuator · inoperativeCREW REPORTED RECEIVING A (FLAP STAB INOP) MESSAGE DURING CLIMB, AFTER SELECTING FLAPS TO THE UP POSITION. IT WAS DISCOVERED THAT THE HORIZONTAL STABILIZER ACTUATOR NO-BACK MECHANISM HAD TRIPPED CAUSING THE ACTUATOR TO OPERATE IN THE DOWN DIRECTION ONLY. INCSDR 2005FA0001501Connector · disconnectedDURING SCHEDULED MAINTENANCE, CREW NOTED SEVERAL CABIN LIGHTS WENT INOPERATIVE. WIRE PX601A8 AT CONNECTOR 394A1J1/369A1P1 BEHIND AUX CB PANEL AT RT RADIO RACK WAS FOUND WITH EVIDENCE OF OVERHEATING AND ARCING. SOLDERED CONNECTION TO CORRESPONDING PIN HAD FAISDR 2005FA0001502Connector · disconnectedDURING SCHEDULED MAINTENANCE, CREW NOTED SEVERAL CABIN LIGHTS WENT INOPERATIVE. WIRE PX601A8 AT CONNECTORS 394A1J1/394A1P1 BEHIND AUX CB PANEL AT RT RADIO RACK WAS FOUND WITH EVIDENCE OF OVERHEATING AND ARCING. SOLDERED CONNECTION TO CORRESPONDING PIN HAD FASDR 62309302005Rib · damagedON POST FLIGHT DAMAGE NOTED TO FAIRING ON OUTSIDE PORTION OF RT STABILIZER LOWER SURFACE.SDR AT0500025Line · crackedLOSS OF HYD PRESSURE AND QUANTITY AFTER TAKE OFF. FOUND CRACKED END ON GROUND SRV RETURN/PRESS LINE. REPAIRED END OF TUBING WITH PERM-A-SWAGE FITTING REF M/M 20-10 SERVICED HYD LEAK AND OPS CK GOOD. RAN NR 2 ENG, OPS CK EDP, OPS CK GOOD.SDR MWEA050059Transceiver · inoperativeAFTER DEPARTURE LOST COMUNICATION ON NR 1 AND NR 2 COMM. REMOVED AND REPLACED NR 1 VHF TRANCEIVER.SDR 647062705Regulator · failedCLIMBING OUT CARGO BAY LOW PRESSURE INDICATION ILLUMINATED.SDR 637041005Fuel Control · failedENG MAINT AMBER CAS MESSAGE.SDR AT0500012Engine · inoperativeLEFT ENGINE COMPRESSOR STALLS AND ROLL BACK AT FL310. REMOVED AND REPLACED LEFT ENGINE.SDR MWEA050022Engine · false indicationLEFT AND RIGHT ENGINE SYSTEM FAIL ALERT ANNUNCIATED. ENGINE ELECTRONIC CONTROLLER (EEC) INTERROGATION DISPLAY MAINTENANCE MESSAGES (FAULTS) 73211, 732138. PERFORMED FAULT ISOLATION MANUAL (FIM) TASKS, RETURN TO SERVICE (RTS), FUEL MATERING UNIT (FMU), EEC P2
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