Rolls-Royce RB211-524B402
Service difficulty reports · 102
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 = 'RB211524B402' 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 = 'RB211524B402' 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 CA011211026Drain Line · leaking(CAN) -HYDRAULIC SYSTEM LEVEL LOW, FOUND HYDRAULIC DRIPPING AT AFT BELLY DRAIN NEAR OUTFLOW VALVE (FS 1363) . -THE TUBE ASSY. SYSTEM C HYDRAULIC PUMP DRAIN LINE WAS LEAKING BETWEEN LINE AND FITTING .SDR ARWA0011012Compressor · vibrationAIRFRAME VIBRATION FELT FOLLOWED BY INCREASED VIBRATION ON NR 3 ENGINE. ENGINE SHUTDOWN PER CHECKLIST, REPORTED TIME 16:50Z. REMOVED AND REPLACED LP FAN BLADES IAW MM 72-31-05, REMOVED 3 HOLE BALANCE WEIGHT FROM THRUST RING. RAN ENGINE NR 3, PERFORMED TEST SDR ARWA0011010Engine · vibrationEXPERIENCED SUDDEN INCREASE IN VIBRATION ON NR 3 ENGINE FROM 1.2 TO 2.4. RETURNED TO MIAMI FOR AN UNEVENTFUL LANDING. LUBED CLAPPERS, CHECKED CHIP DETECTORS ACCOMPLISHED TEST NR 11 VIBRATION SURVEY IAW L1011 FORM 7102B VIBRATION WITHIN LIMITS.SDR ARWA0011011Engine · vibrationON TAKEOFF ROLL C&W PANEL ENGINE VIBRATION FILTER PRESS LIGHT ON NR 3 ENGINE INDICATING 2.6 UNITS FAN POSITION. ABORTED TAKEOFF AT 80 KNOTS POWER SETTING .427 EPR. CHECKED CHIP DETECTORS AND MAIN OIL SCREEN, ALL OK. LUBED BLADES IAW MM 72-31-05, PERFORMED TSDR ARWA0011006Engine · vibrationENGINE NR 3 SHUTDOWN AT 0535Z DUE TO VIBRATION A & B LOW POSITION 2.5 WARNING LIGHT ON OTHER PARAMETERS NORMAL.SDR ARWA0011001EngineLOG PAGE 21133. DISCREPANCY: IN CRUISE FL 330 #1 ENGINE VIBRATION SPIKED TO 4.5 BOTH CHANNELS ON VIBRATION MONITOR WITH NOTICEABLE INCREASE IN AIRFRAME VIBRATION. AS PER EMERGENCY CHECKLIST ENGINE WAS SHUT DOWN AT 12:40Z ALL OTHER ENGINE INDICATIONS APPEARED NSDR CA010831008Indicator · failed(CAN) THE AIRCRAFT RETURNED TO THE STATION AFTER 2 HOURS OF FLIGHT DUE TO FLIGHT CREW EXPERIENCED DIFFICULTY TO USE FUEL FROM TANK NR 2 RT. DURING INITIAL INVESTIGATION AN ACTUAL UNBALANCE WAS FOUND BETWEEN TANK NR 2R AND TANK NR 2 LT. ENGINES GROUND RUN CONFISDR ARWA0010809Engine · vibrationNR 2 ENGINE VIBRATION SPIKED AT 2.8 SHUT DOWN ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT.SDR ARWA0010806Fan Blade · bindingDuring cruise # 2 engine shut down due to vibration enroute to CLO. Continue Flt., landing CLO.Corrective Action: Inspected # 2 engine IAW MM fault isolation 71-91-00, configuration 2, figure 103, and no damage found. Blades # 11 and # 12 found to be lockedSDR CA010823003Duct · split(CAN) AIRCRAFT REJECTED TAKE OFF AT 80 KTS DUE A LOUD NOISE IN COCKPIT. FOUND THE #2 ZONE TRIP MANIFOLD DUCT HOSE COUPLING SPLIT. THE COUPLING WAS REPAIRED AS PER MAINTENANCE MANUAL AND SUBSEQUENTELY THE HOSE COUPLING WAS REPLACED AT THE NIGHT LAYOVER.SDR CA010723041Engine · damaged(CAN) NR 1 ENGINE STALLED ON TOP OF DESCENT INTO YYZ DURING DECELERATION, ENGINE WAS SHUT DOWN. STALL INSPECTION, ENGINE BOROSCOPE DISCOVERED THAT 1 HP COMPRESSOR BLADE BROKEN OFF AND DAMAGED REMAINING HP COMPRESSOR.SDR ARWA0010604Engine · vibrationENGINE NR 1 SUDDEN INCREASE IN VIBRATION FROM 1.8 TO 3.0 UNITS WITH A OR B SELECTED ON NORMAL OR LOW. WARNING LIGHT WAS ON. AIRCRAFT LANDED WITHOUT INCIDENT. ACCOMPLISHED BORESCOPE INSPECTION, NO DEFECTS NOTED. INSPECTED CHIPS AND REMOVED AND REPLACED OIL SDR CA010626016Wire · arced(CAN) REMOVING THE TCAS CONTROL PANEL ON THE CAPT SIDE FOR PART NUMBER VERIFICATION, SPARKES AND ARCING WHERE OBSERVED COMING OUT OF THE BUNDLE BEHIND THE PANEL. CB PULLED AND SOURCE INVESTIGATED FOUND SEVERVAL WIRES WITH THE INSULATION MISSING DUE TO WIRE CHASDR CA010626017Access Panel · missing(CAN) AFTER ARRIVAL FROM CUN DURING THE ACCOMPLISMENT OF THE TRIP CHECK, MAINTENANCE DISCOVERED THE C2 CARGO DOOR MANUAL LOCK ACCESS PANEL LOWER HALF MISSING, BELIEVED THAT IT OPENED IN CUN BY GROUND HANDLERS AND NOT PROPERLY LATCHED. AIRCRAFT RELEASED AS PER SDR CA010531006Terminal Block · overheated(CAN) ON ARRIVAL CREW REPORTE SMOKE AT ROW 23 LT CEILING. FOUND LUMINARE TERMINAL BLOCK OVERHEATED. LUMINARE ASSY REPLACED AND TERMINAL BLOCK REPLACED AIRCRAFT RETURNED TO SERVICE.SDR CA010531008Terminal Block · failed(CAN) FOLLOWING APU WARNING HORN RCCB TRIPPED OFF FOUND 5 WIRES WHERE THE INSULATION WAS BROKEN AND RELATED TERMINAL BUS CHEMICALLY DESTROYED BY SKYDROLL. APU FIRE-EX BOTTLE SQUIB WS INTERMITTENT DUE TO DAMAGE. REPLACED TERMINAL BLOCK AND REPAIRED WIRING AND ASDR CA010706006Terminal Block · destroyed(CAN) FOLLOWING APU WARNING HORN RCCB TRIPPED OFF FOUND 5 WIRES WHEE THE INSOLATION WAS BROKEN AND RELATED TERMINAL BUS CHEMICALLY DESTROYED BY SKYDROLL. APU FIRE-EX BOTTLE SQUIB WAS INTERMITTENT DUE TO DAMAGE. REPLACED TB AND REPAIRED WIRING AND AREA CLEAN FRSDR CA010706007Terminal Block · overheated(CAN) ON ARRIVAL CREW REPORTED SMOKE AT ROW 23 L/H CEILING. FOUND LUMINARE TERMINAL BLOCK OVERHEATED. LUMINARE ASSEMBLY REPLACED AND TERMINAL BLOCK REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR CA010706003Actuator · worn(CAN) DURING TAKEOFF LEADING EDGE SLAT TRANSIT LIGHT CAME ILLUMINATED ON FLAP/SLAT INDICTOR WHEN A/C REACHED 80 KTS, REJECTED TAKEOFF OCCURRED. AFTER INVESTIGATION BY MAINTENANCE, NR 1 SLAT ACTUATOR FOUND WITH EXCESSIVE RADIAL PLAY AT JACKSCREW. ACTUATOR REPLASDR CA010430017Proximity Switch · out of adj(CAN) DURING CLIMB C1A CARGO DOOR OPEN LIGHT CAME ON AT 6.5 DIFF PRESSURE, AIRCRAFT RETURNED TO BASE. DURING DESCENT THE LITE EXTINGUISHED AT 4.5 DIFF PRESSURE.MAINTENANCE INSPECTED DOOR CLOSING AND LOOKING MECHANISM NO FAULT FOUND. DOOR RIGGING CHECKED FOUND SDR CA010430018Handle · out of adj(CAN) AT 9,000 FEET, DURING CLIMB, ON F/E ANNUNICATOR PANEL CARGO DOOR LIGHTS ILLUMINATE, AIRCRAFT RETURNED TO MAIN BASE. FOUND T HANDLE ADJUSTMENT OUT OF RIG, ADJUSTED IN ACCORDANCE WITH MAINTENANCE MANUAL 52-35-01 AND PROXIMITY SENSOR IN ACCORDANCE WITH 52-7SDR CA010103020Panel · missing(CAN) ACFT ARRIVED TO WITH L/H LE SLAT ACCESS PANEL MISSING. AREA INSPECTED, NEW PANEL INSTALLED.FEW SCREWS FOUND LOOSE ON THIS PANEL, WHICH MADE THE PANEL TO DROP ENOUGH FOR THE PIN TO COME OUT. DUE TO VIBRATION THE LE PANEL CAME LOOSE DURING FLIGHT AND DETACSDR CA001107002Blade · damaged(CAN) DURING CRUISE NR 3 ENGINE VIBRATION INCREASED TO 5.0 UNITS AND FELT INSIDE THE AIRCRAFT. NR 3 ENGINE SHUT DOWN AS PER EMERGENCY PROCEDURES.FAN BLADES SUSPECTED.SDR CA011211006Transformer · failed(CAN) FLIGHT CREW REPORTED, DURING FLIGHT, EXCESSIVE HEAT GENERATED BY BOTH FWD LAVATORY CEILLING LIGHTS FLUORESCENT AND INCADESCENT BULB VERY HOT, WHEN MASTER LAVATORY SWITCHON, BOTH LIGHTS ON FULL BRIGHT IN BOTH LAVATORIES, SMELL OF BURNED RUBBER VERY PRSDR CA000919016Fan Blade · damaged(CAN) - FAN BLADES (33) REPLACED (REF: DEFECT NR 00492). - A/C RETURNED TO SERVICE.SDR CA000714012Control Unit · failed(CAN) DURING CRUISE AT 35000 FEET, NR 1 ENGINE STALLED. EPR WENT DOWN TO 0.1 AND RECOVERED IN 2 SECONDS, REPLACEMENT OF VIGV AIRFLOW CONTROL UNIT CURED THE SNAG. AIRCRAFT RETURNED TO SERVICE.SDR CA000724009Pump · failed(CAN) DURING CLIMB OUT OF YYZ, NR 1 ENGINE EXPERIENCE A MOMENTARY LOST OF THRUST. ALL ENGINE PARAMETERS DROPPED AND THEN COME BACK. FUEL AMPLIFIER N1 AND N2 DATUM ADJUSTED, WIRING CHECKED FROM AMPLIFIER TO FUEL PUMP, FUEL PUMP REPLACED. AIRCRAFT RELEASE FOR FLSDR CA000714014Computer · failed(CAN) BOTH DLC AUTO SPOILER FAILED AFTER LANDING WITH SPOILER DEPLOYED. BOTH YAW / SAS FAIL LIGHTS ON AND AUTO PILOT B HANDLE LOCKED OFF.MAINTENANCE RESET THE FLIGHT CONTROL COMPUTER AS PER MM 22-00-01 AND ALL RETURNED TO NORMAL.. FLIGHT CONTROL COMPUTER REPLASDR CA000621034Apu · fire(CAN) DURING TAXI , CREW WAS ADVISED OF FIRE AND SMOKE ON RT SIDE OF THE AIRCRAFT, NR 3 ENGINE SHUT DOWN , BUT REALIZED THAT THE FIRE WAS COMING FROM THE APU TAIL PIPE. APU SHUT DOWN. CREW REPORTED THAT THEY HAD NO PROBLEM WHEN THEY STARTED THE APU FEW MINUTESSDR CA000614056Duct · failed(CAN) VERY LOUD BANG WAS HEARD AFTER LANDING AT YYZ WITH AREA C OVERHEAT INDICATION AFTER INVESTIGATION, MAINTENANCE FOUND NR 3 PACK COMPRESSOR OUTLET DUCT BLOWN, DUCT REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR CA000317013Engine · vibrates(CAN) FAN BALANCED AND VIBRATIONS AT TAKEOFF. RETUNED WITHIN PARAMETERS.SDR CA000307017Fan · overheated(CAN) VIDEO PROJECTOR OVERHEATING. APPEARS TO BE DUE TO FAN NOT PROVIDING ENOUGH COOLING AIRFLOW. MODIFICATION BY MANUFACTURER TO CHANGE OUT FAN FOR A LARGER UNIT.SDR CA991231057Sensor · out of adj(CAN) AFT CARGO DOOR UNSAFE WARN ILLUMINATED ON TAXI. DOOR WARN SWITCH TARGET ADJUSTED.SDR CA990927074Seal · leaking(CAN) IN-FLIGHT SHUTDOWN DUE TO DECREASING OIL QUANTITY. ENGINE OIL CAP O-RING FOUND TO BE UNSERVICEABLE.SDR CA990927075Connector · loose(CAN) AIRCRAFT LANDED DUE TO LOW HYDRAULIC QUANTITY SYS A. INVESTIGATION REVEALED A LOOSE CONNECTOR AT THE SENDING UNIT.SDR CA990707066Gearbox · making metal(CAN) ENGINE FLAME-OUT AT 35,000 FEET. NO FUEL FLOW WAS OBSERVED. GEARBOX MCD FERROUS CONTAMINATION OBSERVED. THE PRELIMINARY CONCLUSION WAS DUE TO THE GEARBOX FAILURE, THE FUEL FLOW REGULATOR STOPPED TURNING CAUSING THE FUEL FLOW TO DROP TO ZERO CAUSING THSDR CA990311071Harness · melted(CAN) ON DEPARTURE, CREW REPORTED THE STROBE LIGHT CIRCUIT BREAKER KEPT TRIPPING. INVESTIGATION REVEALED WIRE CHAFING ON CLAMP CLOSE TO WING LANDING LIGHT. REPAIRED.SDR CA980622024Flow Reg · failed(CAN) DURING TAKEOFF THERE WAS FLUCTUATION OF NR 3 ENGINE PARAMETERS, WHEN THRUST POWER WAS RETARDED PARAMETERS STABILIZED. DURING CRUISE THE ENGINE PARAMETERS WERE NORMAL. POST-FLIGHT TROUBLESHOOTING LED TO REPLACEMENT OF THE NR 3 ENGINE FUEL FLOW REGULATORSDR DLL14981023Oil Tube · crackedEN ROUTE TO HNL CONT DROP NR-3 OIL QTY DIVERTED TO SFO. QTY, DROPPED TO 3.1 QTS SHORTLY AFTER DROPPED TO ZERO NML TEMP/PRESS AT 2055Z OIL PRESS FLUCT 10 PSI FROM 35 TO 55 PSI, ENG SHUT DN AT THAT TIME AND FOLLOW UP PROC ACCOMP. FOUND OIL TUBE CRACKED AT OIL SDR CA980430033O-Ring · damaged(CAN) DURING SERVICING CHECK, NR 2 ENGINE FUEL TUBES WERE FOUND LEAKING. BOTH O-RING SEALS WERE FOUND LEAKING. THE SEALS WERE REPLACED, A LEAK CHECK WAS CARRIED OUT SERVICEABLE AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CA980325043Controller · failed(CAN) A/C RETURNED DUE TO PRESSURIZATION PROBLEMS IN CRUISE. RAPID DESCENT INITIATED, AND PRESSURIZATION RECOVERED AT FL280, DESCENT STOPPED AT FL250 LANDED SAFELY. CABIN PRESSURE CONTROLLER REPLACED.SDR CA980311023Connector · disconnected(CAN) AFTER TAKEOFF AND DURING CLIMB, AFT OUTFLOW VALVE STUCK IN THE OPEN POSITION, MANUAL MODE SELECTED AND STILL COULD NOT BRING THE AFT OUTFLOW VALVE IN THE GREEN BAND. AIRCRAFT RETURNED TO BLOCKS. AFT OUTFLOW VALVE CANNON PLUGS FOUND DISCONNECTED FROM SDR CA980309014Line · cracked(CAN) NR 3 ALTERNATE FUEL QUANTITY INCREASING DURING REFUELING WITH NR 3 ALTERNATE FUEL SHUT-OFF VALVE CLOSED. CONNECTOR ASSY FUEL LINE CENTER TANK CRACKED. REPAIRED.SDR CA971024012Drain · leaking oil(CAN) OIL WAS LEAKING FROM THE NR3 ENGINE TURBINE CASE DRAIN. NO OIL LEAKAGE IS PERMITTED FROM THAT DRAIN. THE NR3 ENGINE IS BEING REPLACEDSDR DLL12961981Gearbox · seizedENG NR 1 FLAME-OUT ON CLIMBOUT. NO INDICATION OF FIRE. COMPLIED WITH POM, NO RELIGHT ATTEMPTED. ENG INDICATED WIND MILL ON N1, N2, N3, NO OIL PRESS INDICATED. QTY AND TEMP WAS GOOD. REPLACED 06 GEARBOX, LEAK AND OPS CHECK NORMAL.SDR DLL17960296Fuel Pump · failedDURING CLIMBOUT, NR 2 ENG FUEL PRESS LIGHT BLINKED AND CAME ON STEADY. AT 25,000 FT COULD NOT ADVANCE ENG PAST 5,000 PPH F/F. ALSO, DECREASE IN N1 FROM 90 PERCENT TO 80. REPLACED NR 2 FUEL PUMP, OPERATION NORMAL.SDR DLL16952120Oil Cap · leakingDURING CRUISE HAD EXCESSIVE OIL LOSS ON NR 2 ENGINE, 6 QTS IN IN ABOUT 3 HOURS, LANDED LGW. FOUND OIL TANK OIL CAP LEAKING THROUGH LOCK ASSEMBLY. REPLACED OIL CAP RETURNED TO SERVICE.SDR DLL14952011Access Gearbox · failedDURING CRUISE, NR 3 ENGINE FLAMED-OUT, UNABLE TO RESTART, LANDED ATL. FOUND ACCESSORY GEARBOX WITH INTERNAL FAILURE. REPLACED GEARBOX, OPERATION NORMAL.SDR DLL16951932Fuel Pump · failedDURING CRUISE, HAD NR 1 ENGINE FUEL PRESSURE LIGHT ILLUMINATED, THEN ENGINE FLAMED-OUT, ALL AIR STARTS WERE UNSUCCESSFUL, DIVERTED TO KEF. REPLACED HP FUEL PUMP, OPERATION NORMAL.SDR DLL17951604Sense Line · brokenON CLIMBOUT, GOT NR 2 ENG REVERSER LIGHT ON S/O PANEL, ACCOMPANIED BY A VIBRATION LIGHT AND NOTICABLE VIBRATION. SHUT NR 2 DOWN, RETURNED FRA. FOUND TWO SENSE LINES TO PRSOV BROKEN. ALSO, ACOUSTIC PANELS AT TOP HALF COLLAPSED. REPLACED PANELS AND SENSE LINE
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