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 PA03004Controller · malfunctionedABNORMAL AUTOTHROTTLE DISENGAGMENT OCCURRED AFTER TAKEOFF. PERFORMED AUTOTHROTTLE OPERATIONAL CHECK IAW MM. NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE.SDR MA2982323Gasket · damagedDURING MAINTENANCE, CABIN CARPET AND PADDING WAS FOUND TO BE WATER SOAKED. AFTER REMOVAL, SEVERE CORROSION WAS FOUND ON THE SEAT TRACKS IN THE PRESSURE BOARD AREA BETWEEN FS 426-576.5 AT LBL 30.5, LBL AND RBL 18.5 AND ALSO LBL 6.0. STRUCTURAL EVALUATION DETESDR GMC2002F00000Brake Assy · damagedLOUD CHATTER WAS NOTICED AS AIRCRAFT WAS BEING TOWED. LT INBOARD AND OUTBOARD BRAKE ASSEMBLY WERE FOUND TO HAVE DAMAGED ROTATING DISC DRIVE KEY SLOTS DAMAGE WAS ALSO FOUND ON WHEEL ASSEMBLY. BRAKES AND WHEELS WERE REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR HALA0200609Relay · inoperativePRIMARY TRIM INOPERATIVE. REPLACED PRIMARY TRIM DOWN BRAKE RELAY IAW MM. GROUND CHECK, OK.SDR UG82002F00010Control Unit · malfunctionedTAKEOFF WAS ABORTED, DUE TO A RED LT LOOP "B" OVERHEAD LEGEND AND ASSOCIATED CAS MESSAGE. PERFORMED ENGINE FIRE WARNING SYSTEM MALFUNCTION CHECKLIST. SYSTEM CHECKED PROPERLY. LT FIRE CONTROL BOX MALFUNCTIONED, REPLACED LT FIRE CONTROL BOX. OPERATION NORMALSDR V9M2002F00000Brace · failedUPON EXTENSION OF LANDING GEAR, AN UNSAFE GEAR ECAS MESSAGE AND LT MAIN GEAR SHOWED UNSAFE INDICATION. FAILED PROX SENSOR TARGET WITH IN BRACE. MODIFICATION TO BRACE UNDER REVIEW AT MFG.SDR LD22002F00001Pump · failedFLUID SAMPLE TAKEN AT 100 HOUR INTERVAL SHOW THAT THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP AND BLED SYSTEM WITH SIGHT GAUGE INSTALLED IN RETURN LINE OF HYDRAULIC RIG TO HELP EVALUATE AIR REMOVAL FROM SYSTEM. WE WILL CONTINUE TO MONITOR FLUID SAMPLES. FASDR LD22002F00002Pump · failedFLUID SAMPLE TAKEN AT 100 HOUR INTERVAL SHOW THAT THE PUMP NEEDS TO BE REPLACED. REPLACE PUMP AND BLED SYSTEM WITH SIGHT GAUGE INSTALLED IN RETURN LINE OF HYDRAULIC RIG TO HELP EVALUATE AIR REMOVAL FROM SYSTEM. WE WILL CONTINUE TO MONITOR FLUID SAMPLES. FAISDR LD22002F00000Pump · contaminatedFLUID SAMPLE TAKEN AT 100 HOUR INTERVAL SHOWS THAT THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP WILL CONTINUE TO TAKE FLUID SAMPLES AT 100 HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED.SDR 2002FA0000259Fitting · crackedAFTER GEAR EXTENSTION, CREW HAD A LOUD BANG, AND NOTICED LOSS OF LEFT HAND HYDRAULIC FLUID. AFTER LANDING INSPECTION SHOWED NOSE GEAR SWIVEL FITTING CRACKED AT FORGED SEAM.SDR BTV2001F00004Bearing · crackedDURING A ROUTINE, SCHEDULED LANDING GEAR INSPECTION, THE MECHANIC NOTED WHAT APPEARED TO BE A CRACK ON THE LOWER MOUNT BALL OF THE RIGHT HAND SHOCK ABSORBER. UPON REMOVAL OF THE SHOCK ABSORBER, VISUAL INSPECTION CONFIRMED THAT THE SPHERICAL BALL PORTION OF THSDR KW32002F00000Jackscrew · galledUPON INSPECTION OF HORIZONTAL STABILIZER PITCH TRIM ACTUATOR, THE PITCH TRIM ACTUATOR JACK SCREW THREADS WERE FOUND TO HAVE EXCESSIVE GALLING.SDR UG82001F00006Pump · damagedENGINE DRIVEN HYDRAULIC PUMP, DAMAGED.SDR UG82001F00007Pump · damagedENGINE DRIVEN HYDRAULIC PUMP, DAMAGED.SDR 2001FA0000484Thermoswitch · wrong partFOUND THERMAL SWITCH PN 512T130B150001 INSTALLED. REMOVED SWITCH AND INSTALLED PN GAS850DF512-250 REV B. THIS SWITCH CORRECTED PROBLEM. THE REMOVED SWITCH CAUSED (FIRE WARNING LIGHT FOR THE LEFT AFT DUCT) TO COME ON. NO LEAKS NOTED. THE SWITCH REMOVED WASSDR LD22001F00002Disk · crackedWHILE COMPLETING THE RECURRING NDT INSPECTION OF THE FAN DISC, A CRACK WAS FOUND. THERE WERE NO VISUAL INDICATIONS OF A CRACK. (ATTACHED SHEET FOR LOCATION OF CRACK ON FAN DISC.) THE FAN DISC HAD BEEN NDT 117 CYCLES PREVIOUS TO THIS NDT THAT REVEALED A CRACKSDR LD22001F00001Rotor · crackedSMALL CRACKS WERE FOUND IN THE NR 1 ROTOR DURING PREFLIGHT INSPECTION. BRAKE WAS REPLACED WITH NEW UNIT. WHILE REPLACING UNIT WE NOTICED THAT THE BOLT HOLES APPEAR LARGER THAN NEEDED. MEASURED HOLES, ALL ARE WITHIN SPECS.SDR LD22001F00009Relay · overheatedLEFT FRONT AND RIGHT WINDSHIELD HEAT WILL NOT SHUT OFF WHEN DESELECTED. FOUND LEFT FRONT WINDSHIELD HEAT CONTROL RELAY AND SOCKET OVERHEATED. THE WIRES CONNECTED TO CONTACTS A1, A2, B1 AND B2 WERE BROWN FROM OVERHEATING. THE PLASTIC ON THE SOCKET HAD STARTESDR LD22001F00010Socket · overheatedLEFT AND RIGHT FRONT WINDSHIELD HEAT WILL NOT SHUT OFF WHEN DESELECTED. FOUND LEFT FRONT WINDSHIELD HEAT CONTROL RELAY AND SOCKET OVERHEATED. THE WIRES CONNECTED TO CONTACTS A1, A2, B1 AND B2 WERE BROWN FROM OVERHEATING. THE PLASTIC ON THE SOCKET HAD STARTESDR LD22001F00003Rotor · crackedNR 1 BRAKE ASSEMBLY - TO SMALL CRACKS WERE FOUND IN NR 1 ROTOR DURING PREFLIGHT. BRAKE WAS REMOVED AND OVERHAULED UNIT INSTALLED.SDR LD22001F00004Rotor · crackedBRAKE ASSEMBLY NR 2 - SMALL CRACKS WERE FOUND IN THE NR 1 ROTOR DURING PREFLIGHT INSPECTION. BRAKE WAS REPLACED WITH AN OVERHAULED UNIT.SDR LD22001F00005Rotor · crackedNR 1 BRAKE ASSEMBLY - SMALL CRACKS WERE FOUND IN THE NR 1 ROTOR DURING PREFLIGHT INSPECTION. BRAKE WAS REPLACED WITH AN OVERHAULED UNIT.SDR LD22001F00006Rotor · crackedNR 2 BRAKE ASSEMBLY - SMALL CRACKS WERE FOUND IN THE NR 1 ROTOR DURING PREFLIGHT INSPECTION. BRAKE WAS REPLACED WITH AN OVERHAULED UNIT.SDR LD22001F00007Rotor · crackedBRAKE ASSEMBLY NR 3 - SMALL CRACKS WERE FOUND IN THE NR 1 ROTOR DURING PREFLIGHT INSPECTION. BRAKE WAS REPLACED WITH AN OVERHAULED UNIT.SDR LD22001F00008Rotor · crackedBRAKE ASSEMBLY NR 4 - SMALL CRACKS WERE FOUND IN THE NR 1 ROTOR DURING PREFLIGHT INSPECTION. BRAKE WAS REPLACED WITH AN OVERHAULED UNIT.SDR BTV2001F00002Rotor · failedDURING A ROUTINE SCHEDULED BRAKE INSPECTION IT WAS NOTED THAT NR 3 BRAKE, OUTBOARD DRIVE ROTOR KEYS WERE FRACTURED. AFTER REMOVING THE WHEEL IT WAS NOTED THAT ALL EIGHT FORWARD SIDE DRIVE CLIPS WERE FAILED. MFG IS INVESTIGATING. A SERVICEABLE BRAKE WAS INSTSDR 20010427CW006O-Ring · splitAFTER DEPLANING PASSENGERS , CREW NOTICED A FUEL LEAK AT THE RIGHT HAND ENGINE. IT WAS REPORTED AS DRAINING FROM THE COWLING. AN INSPECTOR AND MECHANIC WERE DISPATCHED AND FOUND A FAULTY ORING AT THE LOW PRESSURE FUEL FILTER BOWL. THE ORING WAS REPLACED ANDSDR 20010427CW005Computer · incorrectAFTER DEPLOYING AND STOWING THE THRUST REVERSERS THE THRUST REVERSER MISCOMPARE ANNUNCIATOR ILLUMINATED MOMENTARILY. APPARENT CAUSE WAS DCU DATA LATCH UP. CONFIRMED BOTH T/RS TO BE STOWED PROPERLY AND RESET DCU, NR 1 AND NR 2 WITH NO FURTHER OCCURRENCE.SDR 20010427CW009Pump · unserviceableHYDRAULIC PUMP CASE DRAIN FILTER SAMPLES FOR LEFT ENGINE DID NOT PASS THE PATCH TEST. REPLACED PUMP WITH SERVICEABLE UNIT, BLED AIRCRAFT SYSTEMS AND RETURNED AIRCRAFT TO SERVICE. WE WILL CONTINUE SAMPLE SYSTEM FLUID AS REQUIRED.SDR 20010503CW002Pump · defectiveFLUID CONTAMINATION IN RIGHT ENGINE PUMP WAS THE LATEST MODEL AND WAS NEW AT INSTALLATION AND HAS ONLY BEEN OPERATED FOR 48.4 HOURS. WE ARE GETTING BETTER TIME OUT OF THE OLD STYLE PUMPS.SDR 20010514CW002Support Bracket · crackedCRAWLWAY SUPPORT BRACKET IS CRACKING AT BEND RADIUS ON 3 EA FLANGES THAT SUPPORT THE A FLOORBOARD. PART CANNOT BE REPAIRD, MUST BE REPLACED.SDR LD22001F00000Rotor · crackedSMALL CRACKS WERE FOUND IN THE NR 1 ROTOR DURING PREFLIGHT INSPECTION. BRAKE WAS REPLACED WITH NEW UNIT. WHILE REPLACING UNIT WE NOTICED THAT THE BOLT HOLES APPEAR LARGER THAN NEEDED, MEASURED HOLES, ALL ARE WITHIN SPECS.SDR 20001218SH024Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 850.3 HOURS. TOTAL CYCLES 567. (X)SDR 20001218SH025Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THAT THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP. WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 850.3 HOURS. TOTAL CYCLES 567. (X)SDR 20001218SH027Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP, WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 812.0 HOURS. TOTAL CYCLES 546. (X)SDR 20001218SH028Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDS TO BE REPLACED. REPLACED PUMP WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 812.0 HOURS. TOTAL CYCLES 546. (X)SDR 20001219SH001Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDED TO BE REPLACED. REPLACED PUMP, WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 640.8 HOURS. TOTAL CYCLES 347.SDR 20001219SH002Pump · wornFLUID SAMPLE TAKEN AT 100-HOUR INTERVAL SHOWS THE PUMP NEEDED TO BE REPLACED. REPLACED PUMP, WILL CONTINUE TO TAKE FLUID SAMPLES AT 100-HOUR INTERVALS AND CHANGE PUMPS AS REQUIRED. AIRCRAFT TOTAL TIME 640.8 HOURS. TOTAL CYCLES 347. (X)
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