Rolls-Royce RB211-535E437

Service difficulty reports · 236

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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 = 'RB211535E437'
  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.

SDR CA000714009Duct · cracked(CAN) IN FLIGHT, LOUD WISHING NOISE FROM CEILING AT ROW 12 AND PASSENGER WERE COMPLAINING ABOUT VERY COLD TEMPERATURE. AFTER INVESTIGATION, MAINTENANCE FOUND A LEAK AT AIR PLENUM AROUND R2/L2 DOOR AREA. LEAK WAS COMING FROM A PREVIOUS REPAIR. PLENUM REPAIRED AJun 20, 2000 · Boeing 75723A · Air Distribution SystemSDR USAABB00079Transmitter · faultyCLT-JAX - FLT 257 - ON DESCENT INTO JAX AT FL150, RECEIVED A LOW PRESSURE PUMP STATUS MESSAGE IMMEDIATELY FOLLOWED BY LEFT ENGINE SHUTDOWN. PILOT DECLARED AN EMERGENCY AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENGINE TIME WAS 15 MINUTES. MAINJun 9, 2000 · N622AU · Boeing 7572B7 · Compressor Bleed ControlSDR CA000621030Bolt · sheared(CAN) WHILE MECHANIC WAS CARRYING OUT HIS INSPECTION HE OBSERVED THAT NR 7 MAIN WHEEL ASSEMBLY TIE BOLTS WERE SHEARED OFF (X3). MAIN WHEEL ASSEMBLY WAS REMOVED & SERVICEABLE ASSEMBLY WAS INSTALLEDI.A.W. M.M. 32-45-01. NO FUTHER PROBLEMS ON SUBSEQUENT FLIGHTS.Jun 8, 2000 · Boeing 757236 · Wheel/Ski/FloatSDR CA000621031Fan Blade · damaged(CAN) NOT AN SDR - DEPARTING FROM YYZ DURING CLIMB AND CRUISE LEFT ENGINE VIBRATION WENT TO 2.4 UNITS. AIRCRAFT DIVERT TO YMX.MAINTENANCE REPLACED ALL THE ANNULUS FILLER AND CLEANED ALL THE BLADE ROOT. VIBRATION SURVEY CARRIED OUT AND VIBRATION WITHIN LIMITS. Jun 5, 2000 · Boeing 75728A · Turbine Engine Compressor SectionSDR CA000110077Panel · separated(CAN) DURING SERVICE CHECK NR 2 ENGINE COLD STREAM PANEL RIPPED OFF. OPERATOR REPORTED TO ROLLS ROYCE FOR INVESTIGATION. PANELS AND BOLT TORQUE ARE TO BE INSPECTED AT D.I. ITEM CLOSED BY OPERATOR. AMO INFORMED AND WILL COMLPLY WITH THE DI CHECK ALSO.Jan 4, 2000 · Boeing 75723A · Turbine Engine Compressor SectionSDR CA991210025Line · loose(CAN) DURING CRUISE LH HYD QTY DECREASED TO ZERO QTY PRESSURE LIGHT ON AND SYS DEACTIVATED. FOUND PRESSURE LINE JUST BEFORE FILTER MODULE AND BRACKET BROKEN. LINE TIGHTENED. PUMP SEIZED AND REPLACED. UNDER INVESTIGATION. PMUP WENT DRY AND THEN FAILED, UNIT FRODec 3, 1999 · Boeing 75728A · Hydraulic System, MainSDR CA991210024Connector · corroded(CAN) DURING ROUTINE INSPECTION, HARNESS BRACKET ALD393 AND CONNECTOR D40488P FOUND CONTAMINATED WITH WATER ON 25 PERCENT OF THE CONNECTOR AREA. CAUSED WIRES TO BECOME BRITTLE AT CRIMPED AREA. ALSO, THE BACKSHELL OF THE CONNECTOR WAS SEIZED DUE TO CORROSIONov 22, 1999 · Boeing 75723A · Landing Gear Retraction/Extension SystemSDR CA991231054Pump · failed(CAN) PRECAUTIONARY REPLACEMENT MEASURE TAKEN OF HP FUEL PUMP AS PER MMNov 16, 1999 · Boeing 757236 · Engine Fuel PumpSDR CA991116013Flow Valve · failed(CAN) AIRCRAFT RETURNED DUE UNABLE TO PRESSURIZE. AFT CABIN DOOR SEAL FOUND ADRIFT. LEFT PACK UNDER MEL UNABLE TO PRESSURZIZE. REPLACED RIGHT PACK FLOW CONTROL VALVE.Nov 12, 1999 · Boeing 75728A · Air Distribution SystemSDR CA991103097Bolt · broken(CAN) DURING INSP FOUND MW WITH WITH PORTION OF LUG BOLT MISSING. BOLTS REPLACED .Nov 2, 1999 · Boeing 757236 · Wheel/Ski/FloatSDR CA990203007Window · cracked(CAN) ON FINAL APPROACH, EXPLOSION, SMOKE AND THEN FIRE FROM BOTTOM OF PILOT'S NR 1 WINDOW, SHORTLY AFTER WINDOW CRACKED. TOTAL INCIDENT TIME APPROXIMATELY 15 TO 20 SECONDS. FIRE WAS EVIDENT FOR ABOUT 2 SECONDS. LEFT NR 1 WINDOW AND WINDOW HEAT, COMPUTER REJan 25, 1999 · Boeing 75728A · Flight Compartment WindowsSDR CA990125012Sensor Line · loose(CAN) RIGHT ENGINE BLEED OFF - EICAS MESSAGE WHEN TAKEOFF POWER APPLIED. MESSAGE WENT OUT WHEN POWER REDUCED. SECOND ATTEMPT NORMAL. RT ENGINE PRESSURE RELIEF SHUT OFF VALVE SENSOR LINE INSPECTED AND TIGHTENED.Jan 16, 1999 · Boeing 75723A · Bleed Air Indicating SystemSDR CA990318069Seal · debonded(CAN) PILOT ATTEMPTED THREE STARTS, BUT ENGINE OVERTEMPTED AND WITH NO N2 INDICATION. DURING EACH ATTEMPT, THE EGT WENT TO 576 DEGREES CELSIUS FOR LESS THAN ONE MINUTE. WALK-AROUND FOUND NO ABNORMALITIES OR LOOSE MATERIALS IN THE EXHAUST. IP COMPRESSOR WOULJan 14, 1999 · Boeing 757200 · Turbine SectionSDR CA990111023Valve · failed(CAN) RIGHT ENGINE CONTINUES TO RUN 45 SECONDS AFTER RT FUEL CONTROL POSITIONED TO CUT OFF. REPLACED B & D VALVE.Dec 30, 1998 · Boeing 757200 · Engine Fuel PumpSDR CA990111022Sensor · failed(CAN) FORWARD CARGO DOOR INDICATION JUST AFTER TAKEOFF. AIRCRAFT RETURNED TO GATE. MEL ACTION CARRIED OUT. AIRCRAFT RETURNED TO SERVICE.Dec 23, 1998 · Boeing 757200 · Door Warning SystemSDR CA990111020Pump · failed(CAN) WHILE PARKED ECAIS MESSAGES: RT GENERATOR; RT DRIVE DISK, AND RT OIL PRESSURE RED WARNING. NR 2 ENGINE WAS SHUT DOWN. TROUBLESHOOTING CARRIED OUT AND HP FUEL PUMP AND FUEL FLOW GAUGE WERE REPLACED. ENGINE CHECKED SERVICEABLE. A SECOND SPOOL DOWN OCCDec 19, 1998 · Boeing 757200 · Engine Fuel PumpSDR CA981216010Valve · failed(CAN) AS SOON AS EPR WAS SELECTED ON TAKEOFF ROLL AND TAKEOFF THRUST WAS ATTAINED, A LEFT HAND HIGH STAGE EICAS MESSAGE WAS RECEIVED. TAKEOFF WAS ABORTED. QRH ACTION AND AIRCRAFT RETURNED TO THE GATE. ITEM WAS DEFERRED PER MEL AND FLIGHT CONTINUED WITHOUT FNov 13, 1998 · Boeing 75728A · Compressor Bleed ValveSDR CA981216009Valve · failed(CAN) AS SOON AS EPR WAS SELECTED ON TAKEOFF ROLL AND TAKEOFF THRUST WAS ATTAINED, A LEFT HAND HIGH STAGE EICAS MESSAGE WAS RECEIVED. TAKEOFF WAS ABORTED. QRH ACTION AND AIRCRAFT RETURNED TO THE GATE. ITEM WAS DEFERRED PER MEL AND FLIGHT CONTINUED WITHOUT FNov 12, 1998 · Boeing 75728A · Compressor Bleed ValveSDR CA981216008Connector · damaged(CAN) F/O WAS ABLE TO VISUALLY CONFIRM SMOKE RISING FROM BULKHEAD VIDEO MONITOR, SB G-25 HAD POPPED. MONITOR WIRE BUNDLE CAPPED AND STOWED BY MAINTENANCE. CONDENSATION DRIPPING DOWN WIRE BUNDLE INTO BACK SHELL OF MONITOR CONNECTOR AND MONITOR. PIN 2 (28VDC)Nov 5, 1998 · Boeing 75728A · Instrument PanelSDR CA981216007Module · damaged(CAN) NR 2 ENGINE DID NOT ATTAIN TAKEOFF THRUST (MAX OBTAINED 1.63 EPR) WITH POWER LEVER FULL FORWARD. AUTO THROTTLE AND RIGHT EEC DISCONNECTED AUTOMATICALLY. AIRCRAFT RETURNED TO THE GATE AND WAS RELEASED PER MEL 73-21-1.Oct 2, 1998 · Boeing 75728A · Fuel Control/Turbine EnginesSDR 98ZZZX4088Valve · leakingMDW - DURING P/F, FOUND NR 2 ENGINE TRANSLATING COWL (11 O'CLOCK) WITH EVIDENCE OF HEAT DAMAGE. FURTHER INSPECTION REVEALED THE HIGH PRESSURE (PNEUMATIC) SHUT-OFF VALVE WAS LEAKING. TRANSLATING COWL AND PNEUMATIC VALVE WERE REPLACED, OPERATIONS CHECKED SYSTEJul 21, 1998 · N521AT · Boeing 75728A · Compressor Bleed ValveSDR UPS98526604Engine · vibrationNR 2 ENG VIB INDICATOR WENT TO 5.0 YELLOW RANGE ON CLIMB-OUT LEVELED OFF POWER TO IDLE, VIB WENT TO 2.8 - 4.3 FLUCTUATING. ENG SHUT DOWN. RETURN TO PIE. AWAITING PARTS, USED A/C 707 TO PICK UP LOAD. VISUAL CK OF INLET AND EXHAUST AND CHIP DETECTORS OK. MOMay 13, 1998 · N457UP · Boeing 75724APF · Engine (Turbine/Turboprop)SDR CA990318067Annulus Filler · failed(CAN) DURING TAKEOFF, FAN ANNULUS FILLER RELEASED. LOUD BANK WAS HEARD WITH REPORTED TAIL PIPE FLAME. TAKEOFF ABORTED AND FIRE BOTTLES DISCHARGED. AIRCRAFT TOWED BACK TO GATE. PRELIMINARY REPORT INDICATES FILLER BETWEEN 4 AND 5 FAN BLADES FAILED PENETRATINMay 8, 1998 · Boeing 757* · Turbine Engine Compressor SectionSDR CA980504024Windscreen · cracked(CAN) FOLLOWING INITIAL LEVEL OFF AT 37,000 FEET, FIRST OFFICER'S WINDSHIELD CRACKED. WINDSHIELD HEAT DEACTIVATED. WINDSHIELD AND CONTROLLER REPLACED.Apr 23, 1998 · Boeing 75723A · Flight Compartment WindowsSDR CA980424005Valve · failed(CAN) ENGINE HIGH STAGE EICAS MESSAGE CAUSED FLIGHT CREW COMPLETE QRH CHECKLIST AND SELECT NR 1 ENGINE BLEED TO OFF. APPROXIMATELY ONE HOUR LATER, CREW NOTICED CABIN ALTITUDE AT 10,000 FEET RISING SLOWLY. DESCENT INITIATED AND NORMAL PRESSURIZATION RECOVEREApr 11, 1998 · Boeing 75728A · Compressor Bleed ValveSDR CA980424022Valve · failed(CAN) ENGINE HIGH STAGE EICAS MESSAGE CAUSED THE FLIGHT CREW TO COMPLETE QRH CHECKLIST AND SELECT NR 1 ENGINE BLEED TO OFF. APPROXIMATELY ONE HOUR LATER, CREW NOTICED CABIN ALTITUDE AT 10,000 FEET RISING SLOWLY. DESCENT INITIATED AND NORMAL PRESSURIZATION REApr 11, 1998 · Boeing 75728A · Compressor Bleed ValveSDR 98ZZZX1036Fuel Valve · disbondedWOODWARD RB211-535 CONTROL SN WYG 2328482 RETURNED DUE TO IN-FLIGHT SHUT DOWN (IFSD). INVEST CONFIRMED AN FFG MALFUNCTION WAS THE CAUSE OF THE IFSD AND MALFUNCTION CAUSED BY DISBONDMENT OF A REPAIR BUSHING WHICH HAD BEEN PERFORMED ON THE FUEL VALVE HOUSING WFeb 13, 1998 · Boeing 757* · Engine Fuel DistributionSDR CA980225015Stator · delaminated(CAN) TWO STATORS FOUND DELAMINATED AND BROKEN. BRAKE DISC WAS IMPROPERLY ASSEMBLED INTO THE HEAT PACK. THE ANTIVIBRATION GROOVES AROUND THE DRIVE TENIONS SHOULD FACE THE ROTOR, ON THIS ASSY THEY WERE ASSEMBLED FACING THE THRUST PLATE. REPAIRED.Feb 10, 1998 · Boeing 75723A · BrakeSDR CA971104010Cadc · sticking(CAN) CAPTAINS AIR SPEED INDICATOR STICKING AT 100 KNOTS. REPLACED.Oct 24, 1997 · Boeing 75723A · Air Data ComputerSDR AWXA9700592Fuel Line · blownAIR TURNBACK, AFTER TAKEOFF SMOKE WAS REPORTED BY TOWER FROM NR 1 ENGINE. NO COCKPIT INDICATIONS FIRE OR OVERHEAT. IMMEDIATE RETURN ACCOMPLISHED. NR 1 ENGINE SHUTDOWN ON SHORT FINAL 200 FT. REMOVED AND INSTALLED FUEL LINE FROM THE LOW PRESSURE FUEL FILTER Sep 29, 1997 · N915AW · Boeing 757225 · Engine Fuel DistributionSDR CALA9701384Bleed Controler · inoperativeTHE NR 2 ENGINE FLAMED OUT WHILE ON FINAL APPROACH. ALL APPROPRIATE CHECKLISTS WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT BLEED VALVE CONTROLLER TO BE AT FAULT. THE CONTROLLER WAS REMOVED AND REPLACED IAW MM 75-32-Sep 23, 1997 · N58101 · Boeing 757224 · Compressor Bleed ControlSDR CA970106011Cdu · failed(CAN) #1 CDU WENT OFF DURING CLIMB. RETURNED TO BLOCKS. CDU REPLACED.Dec 20, 1996 · Boeing 75723A · Central DisplaySDR USAA950902Oil Sleeves · leakingMCI - FLT NR 0675 - CAPTAIN DIVERTED TO MCI DUE TO HIGH OIL CONSUMPTION ON THE LEFT ENGINE. THE ENGINE WAS NOT SHUT DOWN. FLIGHT LANDED SAFELY. MAINTENANCE FOUND A CUT SEAL ON THE LEFT ENGINE HIGH SPEED GEAR BOX RADIAL DRIVE SHAFT. THE ASSEMBLY WAS RESEALEAug 13, 1995 · N618AU · Boeing 757225 · Turbine Engine Accessory DriveSDR USAA9509901Fan Blades · damagedLAX - FLT NR 1898 - AT 131 KNOTS, A BIRD WAS INGESTED INTO THE NR 1 ENGINE CAUSING A LOSS OF POWER AND NOTICEABLE ENGINE VIBRATION. IT WAS DECIDED TO DIVERT TO LAX. NO EMERGENCY WAS DECLARED. MAINTENANCE REPLACED THE NR 19 AND NR 20 FAN BLADES. OPERATIONS Aug 11, 1995 · N618AU · Boeing 757225 · Turbine Engine Compressor SectionSDR 95ZZZX3072Fuel Pump · leakingDTW - ON A CHECK, FOUND FUEL LEAK FROM NR 1 ENGINE FUEL PUMP PAD SEAL DRAIN. REMOVED AND REPLACED NR 1 FUEL PUMP IAW MM73-11-01. OPS CHECK GOOD. NO LEAKS NOTED.May 20, 1995 · N751AT · Boeing 757212 · Engine Fuel PumpSDR 95ZZZX3069Fuel Control · failedLAX - IN-FLIGHT ENGINE FAILURE (LT ENGINE). REMOVED AND REPLACED LT ENGINE FUEL CONTROL UNIT. ENGINE RUN-UP CHECK OKAY.Apr 18, 1995 · N751AT · Boeing 757212 · Fuel Control/Turbine Engines
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