Rolls-Royce RB211-524D419
Service difficulty reports · 92
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 = 'RB211524D419' 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 = 'RB211524D419' 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 AUS20010761Squib · wrong part(AUS) NR 1 MAIN CARGO FIRE EXTINGUISHER BOTTLE FORWARD AND AFT SQUIBSCROSS CONNECTED.SDR AUS20010738Governor · faulty(AUS) NR 2 ENGINE RPM DECREASED AND EGT INCREASED. VIGV AIR FLOW CONTROL UNIT PNO 754-1-32148-019A AND PUMP AND GOVERNOR UNIT (PAG) PNOPAC102MK4S CHANGED.SDR AUS20010718Regulator · faulty(AUS) NO2 ENGINE FUEL FLOW REGULATOR FAULTY.SDR AUS20010676Apu · fire(AUS) FOLLOWING APU BATTERY FITMENT AND WHILE INSTALLATION CHECKS WERE CARRIED OUT ON THE THERMAL SWITCH, A FLASH FIRE OCCURRED WHICH SET FIRE TO THE THERMAL BLANKET LOCATED UNDER THE APU BATTERY TRAY AND ALSO CAUSED FLASH BURNS TO MAINTENANCE PERSONNEL. THEFISDR AUS20010668Engine · vibrates(AUS) NR 2 ENGINE EXCESSIVE VIBRATION. ENGINE INSPECTED IAW MAINTENANCEMANUALS WITH NO FAULTS FOUND. HPC STAGES 5/6 BOROSCOPED AND FOUND OK. AIRCRAFT RETURNED TO SERVICE.SDR AUS20010671Compensator · corroded(AUS) NO6 PASSENGER OXYGEN BOTTLE THERMAL COMPENSATOR SWAGED FITTINGCORRODED. AIRCRAFT IS REGISTERED DQ-FJE.SDR AUS20010681Cable · worn(AUS) ENGINE THRUST CONTROL CABLE GUARDS AND COVERS CRACKED/DAMAGED.GUARDS ARE FOR CABLES T1, T2, T3, T4A, T4B, STN940 TO STN960 LT AND RT. CABLE PULLEY FOR CABLE T3A CRACKED AND CABLE T3A WORN AT RT WING INBOARD LOCATION 352.00. FOUND DURING INSPECTION IAW EISDR AUS20010644Controller · faulty(AUS) PRESSURISATION SYSTEM OUTFLOW VALVES SLIGHTLY OPEN. INVESTIGATION COULD FIND NO CAUSE OF THE DEFECT. THE CABIN PRESSURE CONTROLLERWAS REPLACED BUT FOUND TO SERVICEABLE WHEN WORKSHOP TESTED.SDR AUS20010631Module · leaking(AUS) RUDDER CONTROL MODULE LEAKING.SDR AUS20010573Cable · worn(AUS) DURING INSPECTION OF ENGINE THRUST CONTROL CABLES, FITTINGS AND PULLEYS IAW EI 743-076-0002 REV01 FIVE SEPARATE AREAS OF CABLEWEAR WERE FOUND. FOUND DURING INSPECTION IAW AD/B747/229 AND FAAAD 2000-05-30 AMDT 39-11640.SDR AUS20010565Brake · faulty(AUS) PARKING BRAKES WOULD NOT RELEASE.SDR AUS20010550Cable · out of adj(AUS) NO1 RH DOOR SLIDE FAILED TO DEPLOY DURING TEST. INVESTIGATION FOUND THE DOOR EMERGENCY POWER RESERVOIR FIRING CABLE OUT OFADJUSTMENT AND FAILING TO RUPTURE THE DISC OF THE EPS BOTTLE. THE EPS CABLE WAS ADJUSTED AND THE SLIDE DEPLOYED NORMALLY.SDR AUS20010526Regulator · faulty(AUS) NR 3 ENGINE FUEL FLOW REGULATOR (FFR) FAULTY.SDR AUS20010501Elbow · cracked(AUS) HYDRAULIC SYSTEM LEAKING FROM CRACKED PRESSURE LINE ELBOW LOCATED UNDER NO3 STRUT REAR SAILBOAT. LOSS OF HYDRAULIC FLUID.SDR AUS20010510Panel · loose(AUS) NO1 MAIN FUEL TANK INTERNAL RIB ACCESS/BAFFLE PANEL LOOSE. THEPANEL WAS FOUND UNSECURED ON THE FLOOR WITH THE MOUNTING SCREWS CONTAINED IN A CANVAS SCREW BAG ATTACHED TO THE PANEL. THE AREA HAD RECENTLY BEEN ACCESSED DURING D4 INSPECTION.PERSONNEL/MAINTESDR AUS20010503Liner · missing(AUS) NR 1 ENGINE LOW POWER. INVESTIGATION FOUND ONE SECTION OF FRONTFAN ACOUSTIC LINING BETWEEN 2 O'CLOCK AND 4 O'CLOCK AREAS MISSING AND ONE AREA OF ICE IMPACT PANEL BETWEEN 1 O'CLOCK AND 5 O'CLOCKAREAS MISSING WITH LOOSE MATERIAL STILL TRAPPED BY THEENGINE.SDR AUS20010463Bolt · wrong part(AUS) NR 2 ENGINE FUEL FLOW TRANSMITTER INLET GASKET LEAKING. LOOSEBOLTS RETIGHTENED BUT THE LEAK CONTINUED. FURTHER INVESTIGATION FOUND THAT THE MOUNTING BOLTS WERE PNO AS21515 INSTEAD OF THE CORRECT PNO AS21514. FITMENT OF THE INCORRECT BOLTS HAD DAMAGED THESDR AUS20010406Panel · separated(AUS) NO4 ENGINE VIGV CONTROLLER ACCESS PANEL SEPARATED. DAMAGE CAUSEDTO THE REAR FAN CASE ACOUSTIC LINER.SDR AU010341Actuator · failed(AUS) RT WING LANDING GEAR DOWNLOCK ACTUATOR SUFFERED A CATASTROPHIC FAILURE. THE FAILURE OCCURRED DURING THE FIRST OPERATION OF THE ACTUATOR WHICH HAD JUST BEEN FITTED FOLLOWING MAINTENANCE.SDR AU010329Drain Valve · clogged(AUS) DRAINS LOCATED IN WING CENTRE SECTION AFT CAVITY AT BS 1241 WERE BLOCKED BY FOREIGN MATERIALS WITH EIGHT TO TEN LITRES OF WATER PRESENT. TIDE MARKS ALSO PRESENT ON SURROUNDING STRUCTURE INDICATING EVIDENCE OF GREATER QUANTITIES OF WATER RETENTION.SDR AU010335Hose · leaking(AUS) LT WING MAIN LANDING GEAR DOOR ACTUATOR FLEXIBLE HOSE LEAKING.LOSS OF HYDRAULIC FLUID. NR 4 ENGINE DRIVEN HYDRAULIC PUMP CHANGED DUE TO OPERATION WITH LOW HYDRAULIC QUANTITY.SDR AU010202Nut · unlocked(AUS) LT AND RT NOSE GEAR STEERING CABLES DID NOT HAVE SPLIT PINS FITTED THROUGH CASTELLATED NUTS. BOTH NUTS WERE ONLY FINGER TIGHT AND THE LT NUT WAS HELD BY ONLY TWO THREADS.PERSONNEL/MAINTENANCE ERROR.SDR AU010205Socket · burned(AUS) SIDEWALL WASH LIGHT SOCKET LOCATED AT SEAT 25 HJK BURNED OUT AND ARCING DUE TO WATER CONTAMINATION. AREA AROUND SEATS FOUND TO BE SOAKING WET DUE TO BLOCKAGE OF RT SIDE UPPER DECK DOOR DRAINBLOCKAGE ALLOWING WATER LEAKAGE. AIRCRAFT HAD BEEN ON THE GROUNDSDR AUS20011165Regulator · faulty(AUS) NR 4 ENGINE FUEL FLOW REGULATOR (FFR) FAULTY. INVESTIGATION FOUND THE CAUSE TO BE FAILURE OF THE VMO QUILLSHAFT CUP WASHER DUE TO HIGH CYCLE FATIGUE.SDR AU010127Cable · damaged(AUS) ENGINE THRUST CONTROL SYSTEM CABLES, PULLEYS AND FITTINGS DAMAGED. FOUND DURING INSPECTION IAW AD/B747/229 AND FAAAD/2000-05-30 AMDT39-11640.SDR AU010129Fire Loop · malfunctioned(AUS) APU LOWER DOOR FIRE DETECTOR LOOP HAD HIGH RESISTANCE. FALSE WARNING INDICATION RESULTED IN DISCHARGE OF FIRE BOTTLE.SDR AU010080Panel · missing(AUS) NR 1 ENGINE NR 1 AND NR 3 & 4 ACOUSTIC PANELS MISSING.SDR AU010049Brake · failed(AUS) LT FORWARD WING LANDING GEAR NR 2 POSITION BRAKE FAILED.SDR AU010033Door · damaged(AUS) NR 1 ENGINE BLOCKER PARTIALLY MISSING. DAMAGE TO CORONA AND COLD STREAM DUCT AT 10 OCLOCK POSITION.SDR AU001252Control Box · damaged(AUS) NR 1 ENGINE FFR THROTTLE CONTROL BOX RACK DAMAGED.SDR AU001220Bolt · broken(AUS) REAR SPAR LOWER LT SPLICE PLATE / CENTER WING TANK BOLT BROKEN. THE BOLT SHANK WAS COMPLETELY SEVERED AND THE BOLT HEAD WAS PROTRUDING APPROXIMATELY 19.05MM (0.75IN) INTO THE CENTER WING TANK WITH SURROUNDING SEALANT DAMAGE EVIDENT. FOUND DURING INSPECTISDR AU000695Seal · failed(AUS) BLEED AIR DUCT SEAL DETERIORATED AND BROKEN INTO PIECES. HOTBLEED AIR LEAKING ONTO CENTRE WING AND FUEL TANK.SDR AU981515Regulator · faulty(AUS) NR 1 ENGINE FUEL FLOW REGULATOR (FFR) FAULTY.SDR AU981514Regulator · faulty(AUS) NR 4 ENGINE FUEL FLOW REGULATOR (FFR) FAULTY.SDR AU981513Tailpipe · fire(AUS) NR 3 ENGINE TAILPIPE FIRE.SDR AU981402Engine · overheated(AUS) NR 4 ENGINE EXPERIENCED HIGH EGT DURING TAKEOFF. LIMITED INFORMATION PROVIDED.SDR AU980814Pipe · leaking(AUS) ENGINE HIGH PRESSURE FUEL LINE LOCATED BETWEEN THE FFR AND THE HP SHUTOFF VALVE LEAKING AT THE SHUTOFF VALVE END.SDR AU971376Bolt · rubbing(AUS) NO2 ENGINE THRUST LEVER PLA TRANSDUCER ROD END EYE BOLT BINDING WITH FFR POWER LEVER INPUT ROD.SDR AU970328Liner · burnt(AUS) NO3 ENGINE COMBUSTION CHAMBER OUTER LINER BURNT AND HOLED IN TWO PLACES ADJACENT TO THE AFT FLANGE IN THE 3 O'CLOCK POSITIONSDR AU970327Liner · burnt(AUS) NO3 ENGINE COMBUSTION CHAMBER OUTER LINER BURNT THROUGH IN TWO PLACESSDR AU961074Regulator · faulty(AUS) NO1 ENGINE FUEL FLOW REGULATOR FAULTY - ENGINE OVERSPED TO 107% FOR APPROXIMATELY 10 SECONDS - EGT 710 DEGREES CSDR AU960350Fan Blade · incorrect fit(AUS) NO4 ENGINE FAN BLADES (4OFF) FITTED TO INCORRECT POSITION CAUSING VIBRATIONS - PERSONNEL/MAINTENANCE ERROR
Back to Rolls-Royce RB211-524D419