Rolls-Royce RB211-535E437
Service difficulty reports · 236
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 = '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.
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
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 CA110215002O-Ring · damagedON FLIGHT THE ACFT EXPERIENCED A LARGE FUEL IMBALANCE IN CRUISE FLIGHT DUE TO A RT ENGINE FUEL LEAK. THE ACFT DECLARED AN EMERGENCY AND DIVERTED. WHEN THEY ARRIVED THE RT FUEL QUANTITY WAS 1500 KG LESS THAN THE LT. AN O-RING WAS FOUND LEAKING AT THE RT HP FSDR CA110211002Light · brokenFLIGHT CREW CONDUCTED A MISSED APPROACH AFTER THE RT MAIN GEAR DOWN AND LOCK GREEN LIGHT FAILED TO ILLUMINATE AFTER GEAR DOWN SELECTION. AN EMERGENCY WAS DECLARED AND ACFT LANDED WITHOUT FURTHER INCIDENT. MX FOUND THAT THE LIGHT WAS NOT TESTING AND CONCLUDED SDR CA101206015Panel · missingON ARRIVAL AFTER A FLIGHT, IT WAS NOTICED THAT INSP PANEL 443BR ON THE OTBD SIDE OF THE NR 2 ENGINE PYLON WAS MISSING. PANEL PN 311N5049-139, IPC 54-53-01-05, ITEM 175. THE PANEL WAS REPLACED. ACFT TSN 46089, CSN 14630. THIS IS THE SECOND PANEL TO GO MISSINGSDR CA101202003Panel · missingON ARRIVAL AFTER A POSITIONING FLIGHT FROM MANCHESTER, UK, IT WAS NOTICED THAT INSPECTION PANEL 443HL ON THE INBOARD SIDE OF THE NR 2 ENGINE PYLON WAS MISSING. PANEL P/N 311N5049-155, IPC 54-53-01-05, ITEM 208. THE PANEL WAS REPLACED. AIRCRAFT TSN 46050, CSSDR ANCF2010060800062Governor · malfunctionedPILOT REPORT: RTO DUE TO LEFT ENGINE EPR WAS 1.27 WITH THE THRUST LEVER AT FULL FWD POSITION, EPR TARGET WAS 1.61 WITH 50C FLEX TEMP. IAW B757 MM 73-21-01 PG 401-420 REMOVED AND REPLACED LEFT ENGINE FUEL FLOW GOVERNOR. IAW B757 AMM 71-00-00/501 PERFORMED LTSDR XE5RTAES086Compressor · damagedTHE OPERATOR REMOVED THE ENGINE FROM SERVICE DUE TO A SURGE AND REJECTED TAKEOFF. BORESCOPE INSPECTION FOUND EXTENSIVE HPC STAGE SIX BLADE DAMAGE. TAESL CONFIRMED THIS DAMAGE DURING TEARDOWN OF THE ENGINE AFTER 5616 HOURS SINCE LAST FULL REFURBISHMENT AT ANOSDR AALA20091029LAX01Heat Exchanger · leakingCLIMBING THROUGH 20,000 FEET, SMOKE WAS NOTED IN THE CABIN FOLLOWED BY COMPLETE LOSS OF OIL PRESSURE AND QUANTITY IN RIGHT ENGINE. RETURNED TO LAX AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE FOR EVALUATION. REPLACED ENGINE NUMBER TWO AND REPLSDR 22AA20090402Mast · missingLOG PAGE NR 130694: RAFT REMOVED FROM AIRCRAFT FOR DEMOSTRATION PURPOSE. DURING DEMOSTRATION THE RAFT DEPLOYED PROPERLY AND IT WAS DISCOVERED THAT THE CANOPY ROD (MAST) WAS MISSING FROM THE RAFT.SDR ANCF2009031600036Governor · malfunctionedDURING TAKEOFF RT ENGINE DIDN´T ACELERATE NORMALLY IAW LIST. REJETED TAKE OFF WAS PERFOMED AT 85KTS. IAW FIM 73-21-00/109 FAULT CODE 34 IT WAS NESSESARY REPLACE FUEL FLOW GOVERNOR. IAW AMM73-21-01 PAG 401 IT WAS REPLACED FUEL FLOW GOVERNOR .THE TEST 1,2,9,10 SDR CA090225005Fairing · departed(CAN) AFTER A HIGH POWER ENGINE RUN, MX FOUND DAMAGED AND MISSING FAIRINGS (COMPRESSOR), WHEN FAIRINGS DEPARTED ACFT, THEY CAUSED DAMAGE TO THE THRUST REVERSER BLOCKER DOOR ARMS. IT IS POSSIBLE THAT ONE FAIRING WAS NOT CORRECTLY SECURED WHICH RESULTED IN OTHESDR CA081212001Switch · malfunctioned(CAN) COCKPIT MAIN CARGO DOOR WARNING LIGHT ILLUMINATED AT FL340 AND THE AMBER CAUTION LIGHT ON THE CARGO DOOR CONTROL PANEL ALSO ILLUMINATED. AIRCRAFT BEGAN TO RETURN TO BASE AND WHILE DESCENDING THROUGH 13,000 FEET THE LIGHTS EXTINGUISHED. THE AIRCRAFT RETSDR CA081125001Wire Harness · chafed(CAN) IN FLIGHT CREW NOTICED SMOKE AND FLASHES ABOVE ROW 4DEF. MX FOUND WIRING HARNESS CHAFED BY CEILING PANEL RESULTING IN EXPOSED WIRES ARCHING.SDR CA080618001Hose · leaking(CAN) LT TRUCK TILT ACTUATOR RETURN LINE FOUND LEAKING.SDR CA080408003Cabin Pressure · malfunctionedAIRCRAFT C-GTDX DEPARTING FROM YYZ ON APRIL 4TH 2008, AROUND 7000 FT AN EICAS MSG AUTO PRESSURIZATION SYS 1 AND 2, AIRCRAFT RETURNED BACK TO YYZ AND REQUESTED FIRE TRUCKS ON ARRIVAL DUE TO OVERWEIGHT LANDING. TROUBLESHOOTING CARRIED OUT, BOTH PRESSURIZATION CSDR CA080225007Monitor · malfunctioned(CAN) CREW REPORTED A BURNING SMELL IN THE CABIN JUST BEFORE LANDING. IN-FLIGHT ENTERTAINMENT WAS SELECTED OFF AND SMELL DISSIPATED. MAINTENANCE DETERMINED THAT THE SMELL WAS COMING FROM THE NR 7 MONITOR. (TC NR 20080225007)SDR BB08002O-Ring · brokenCUN FLT 816 EN ROUTE CLT TO CUN: FMC FUEL DISAGREE MESSAGE. RIGHT TANK QTY DECREASED AT A HIGHER RATE. AIRCRAFT USED 4000 LBS MORE THAN FLIGHT PLAN. AFTER ARRIVAL CAPT OBSERVED FUEL LEAKING FROM RT ENGINE ON GROUND. MAINTENANCE FOUND LEAK ON RT ENGINE AT SDR ANCF200700029Blades · damagedN1 ENGINE VIBRATION HIGH, READS 3.0. ENGINE INDICATIONS NORMAL. VIBRATION RETUNED BELOW 2.5 WITH THRUST LEVER RETARDED. ENGINE WAS NOT SHUTDOWN. ON THE LT ENGINE FAN BLADE NR 17 WAS REPLACED CHOCKING PAD IAW AMM 72-31-73 PAGE 401, IAW AMM 71-00-00 PAGE 548, SDR CA071108005Line · chafed(CAN) DURING CLIMB, THE CREW NOTICED THAT NR1 ENGINE PARAMETERS WERE NOT AS SCHEDULED. AIRCRAFT RETURNED TO THE AIRPORT. WITH DECREASING ALTITUDE THE NR1 ENGINE PARAMETERS IMPROVED AND A NORMAL LANDING WAS PERFORMED. FOUND P1 LINE CHAFED THROUGH. LINE REPLACEDSDR NOCA15207Control Unit · malfunctionedEGT N2 N3 EXCEEDED LIMITS REJECTED T/O RIGHT ENGINE EGT 889 N2 105 N3 100. PERFORMED FIM 71-05-00 CHECK INLET AND EXHAUST INSPECTED CHIPS REPLACED BVCU AS PER MM 75-32-01.SDR NOCA10107Control Unit · malfunctionedLEFT ENG EXCEEDANCE EGT AND N2 ON TAKEOFF ROLL FOR LESS THAN ONE SECOND. REMOVED AND REPLACED NR 1 ENG BVCU IAW MM 75-32-01. IDLE RUN DONE. BVCU BITE CKS OK IAW 71-00-00 & 75-32-00. HIGH POWER RUN ACCOMPLISHED TEST 3. PERFORMED OF 71-00-00. ENG CHECKS OKSDR CA070504001Line · leaking(CAN) FORWARD PYLON PRESSURE LINE FOUND CHAFED THROUGH CAUSING LEAK. DAMAGE CAUSED BY A DEFECTIVE HOSE CLAMP. (TC NR 20070504001)SDR NOCA08507Switch · malfunctionedLEFT ENGINE SURGE COMPRESSOR STALL AT FL.360 DURING CLB AT 1.38 EPR LEFT ENG SURGE AGAIN BEFORE INITIAL DESCENT AND DURING DESCENT TOTAL OF 3 TIMES ALL ENGINE INDICATIONS NORMAL AFTER ENGINE SURGE. ACP INSPECTION OF LEFT ENG INLET, EXHAUST CHIP DETECTORS NO FSDR ANCF200600046Engine · failedLT ENGIINE SURGED DURING CONSTANT POWER DURING CLIMB AT 6.000 FT. ENGINE OPS NORMAL AFTER SURGE AT LOW THRUST. BOROSCOPE INSPECTION ACCOMPLISHED TO INTERMEDIATE PRESSURE COMPRESOR, HIGH PRESSURE COMPRESOR, COMBUSTION CHAMBER, HIGH PRESSURE TURBINE BLADES, LOSDR CA070226001Connector · burned(CAN) CREW REPORTED EICAS STATUS MESSAGE, WXR SYSTEM. ON REPLACEMENT OF WXR DRIVE UNIT, FOUND BURNED ELECTRICAL CONNECTORS. (TC NR 20070226001)SDR CA061220008Pump · failed(CAN) LT ACMP LEAKING FLUID CAUSING LOSS OF HYDRAULIC QUANTITY AND SYSTEM PRESSURE. AIRCRAFT LANDED AND WAS TOWED OFF THE RUNWAY DUE TO NO NOSE WHEEL STEERING. (TC NR 20061220008)SDR ANCF200600013Control Unit · malfunctionedLEFT ENGINE N2 RPM WENT TO OVERSPEED. IAW AMM 75-32-01 PAGE 401, REPLACED BLEED VALVE CONTROL UNIT. OPS CHECK OK FOR SERVICE.SDR CA060315005Monitor · odorELECTRICAL BURNING SMELL FROM MONITOR. MONITOR SWITCHED 'OFF'. SMELL DISSIPATED. MONITOR ELECTRICALLY DISCONNECTED.SDR BB06015Controller · failedFLIGHT 979, BDL-CLT: ON APPROACH, THE NUMBER ONE ENGINE EXPERIENCED MULTIPLE COMPRESSOR STALLS AND SHUT DOWN. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLEED VALVE CONTROL UNIT AND BOTH DGCU'S.SDR CA060214007Bearing · seized(CAN) REPORTED THAT ELEVATOR FELT HEAVY FOR BOTH CAPT AND F/O. AILERON NORMAL. TROUBLESHOOTING SHOWED THAT THE ROLLER BEARING THAT RIDES IN THE ELEVATOR INPUT CAM WAS SEIZED, CAUSING HIGHER THAN NORMAL FORCE REQUIED TO MOVE FLIGHT CONTROL OUT OF (DETENT). BESDR CA051229002Governor · unserviceableDURING FLIGHT FROM YYC TO PVR, NR 2 ENGINE LOST PARTIAL POWER. FLIGHT CONTINUED WITHOUT INCIDENT. MAINTENANCE INVESTIGATION DETERMINED THE FUEL FLOW GOVERNOR TO BE AT FAULT. THE GOVERNOR WAS REPLACED, POWER PERFORMANCE RUNS CARRIED OUT SATISFACTORY AND THE SDR CA051024005Hydraulic System · warning lightAIRCRAFT EN ROUTE HNL - YVR, LOST LT HYDRAULIC SYSTEM APPROX 2 HOURS FROM YVR. ORIGINALLY PLANNED NORMAL LANDING UTILIZING ALTERNATE SYSTEM BUT DURING LANDING PHASE, FLIGHT ENCOUNTERED FURTHER INDICATION OF HYDRAULIC LOSS AND DECLARED AN EMERGENCY AND WAS METSDR CA051021003Terminal · damagedDURING VISUAL INSPECTION, NOTICED DISCOLORATION ON FASTON TERMINAL AND INSULATION ON WIRE NR W1272-2001R-12 AT CIRCUIT BREAKER C-0392, TERMINAL B2. R1 WINDOW HEAT CIRCUIT BREAKER, NO FAULTS WERE REPORTED ON THE FUNCTIONING OF WINDOW HEAT. TERMINAL REPLACED ISDR CA050822004Strap · cracked(CAN) DURING DAILY INSPECTION, FOUND LOW PRESSURE CASE UPPER ACCESSORY MOUNTING STRAP BROKEN.SDR CA050816001Windshield · cracked(CAN) WHILE IN FLIGHT, THE FLIGHT CREW NOTICED ARCING INSIDE THE FIRST OFFICER WINDSHIELD WHICH RESULTED IN A SEVERELY CRACKED OUTER PANE.SDR CA050727005Wire · damaged(CAN) DURING T/S OF INBOUND DEFECTS (PA INOP, NSSB INTERMITTENT) FOUND C/B`S POPPED. RESET SAME (ONE WOULD RESET, OTHER NOT). FOUND WIRE LOOM (W3702) FOR UNINSTALLED PSU (9ABC) PINCHED BETWEEN AFT WALL SURFACE OF MID GALLEY AND STRUCTURE OF A/C. GALLEY INSTSDR CA050721001Battery · overheated(CAN) EICAS MSG 'MAIN BATT DISCH' OBSERVED DURING DAILY ROUTINE CHECK. BATTERY FOUND EXTREMELY HOT TO TOUCH. LIFE TIME REMAINING OF THIS COMPONENT UNTIL NEXT SCHEDULED REPLACEMENT WAS 142:47 HOURS.SDR CA050708001Nose Cowl · crackedDURING ROUTINE C-CHECK INSPECTION OF AIRCRAFT, SEVERAL CRACKS WERE FOUND ON THE NR 1 ENGINE INTAKE COWL. THE FORWARD DIAPHRAGM HAD MULTIPLE CRACKS ALL AROUND THE CIRCUMFERENCE, INCLUDING A 27 INCH CRACK AT THE LOWER SIDE. THE REAR DIAPHRAGM HAD 2 CRACKS. THSDR CA050706010Attach Fitting · corrodedDURING ROUTINE C2 INSPECTION OF AIRCRAFT, BOTH LOWER FLAP MECHANISM ATTACH FITTINGS WERE FOUND TO BE CORRODED. DATA WAS PASSED TO COMPANY ENGINEERING DEPARTMENT WHO CONTACTED BOEING ENGINEERING. BOEING SENT AN APPROVED TIME LIMITED REPAIR WHICH WAS CARRIED OSDR CA050531003Engine · making metal(CAN) DURING ENGINE START, ENGINE FAILED TO ACHIEVE APPROPRIATE RPM. START ABORTED. TROUBLESHOOTING FOUND DEBRIS IN THREE CHIP DETECTORS. ENGINE WILL BE CHANGED AND SHIPPED BACK TO OVERHAUL FACILITY FOR INVESTIGATION.SDR CA050517006Bolt · missing(CAN) DURING C CHECK, IT WAS FOUND THAT THE FRONT MOUNT ASSEMBLY HAD A KEEPER BOLT MISSING FROM THE AFT PICKUP BEARING BUSHING. THE BEARING BUSHING HAD SHIFTED TRANSFERING ALL WEIGHT TO ONE LUG OF THE BRACKET. COMPLETE MOUNT WAS REPLACED AS A PRECAUTION. APPRSDR CA060502007Heat Shield · delaminated(CAN) NR 1 ENG RT THRUST REVERSER COWL AFT HEAT SHIELD DAMAGED (DISBONDED). REPAIR FOR HEATSHIELD IN OEM MANUAL. (TC NR 20060502007)SDR CA050217004Idg · inoperative(CAN) DURING INITIAL CLIMB, DEPARTING OGG, R (GEN DRIVE) MESSAGE DISPLAYED, GEN DRIVE LIGHT ILLUMINATED. RT IDG DISCONNECTED. AIRCRAFT DIVERTED. RT IDG REPLACED WITH LOANER UNIT, A/C DEPARTED, NO FAULTS REPORTED. REPLACEMENT UNIT FITTED. IDG SENT TO OEM FSDR CA050128005Cooling Fan · binding(CAN) CREW NOTICED A BURNING SMELL THROUGHOUT AIRCRAFT AND THEN HAD AN EICAS MESSAGE (EQUIPMENT OVERHEAT) . MAINTENANCE CONFIRMED FWD EQUIPMENT COOLING FAN BINDING AND A BURNT SMELL COMING FROM UNIT.SDR CA050114003Motor · leaking(CAN) A/C DEPARTED AND TURNED AROUND AFTER NOTICING SLOW STEADY DECLINE IN CENTER SYSTEM QUANTITY. MAINTENANCE FOUND FLUID LEAKING FROM FUSELAGE DRAIN HOLES IN THS COMPARTMENT. UPON INVESTIGATION MAINTENANCE FOUND CENTER SYSTEM HYD MOTOR ON THIS GEARBOX LEAKINSDR CA041022002Control Panel · failed(CAN) AFTER DEPARTURE YVR ENROUTE LAX, CREW NOTICED NUMBEROUS FAILURES IN AUTOFLIGHT MODE CONTROL PANEL.NOT ABLE TO SELECT SPECIFIC HEADING. HEADING INDICATIONS ON CAPT/FO EHSI DIFFERENT. UNABLE TO SELECT ALTITUDE, ALSO AUTOPILOT WOULD NOT CONTROL AIRCRAFT TOSDR CA041021008Fixture · burned(CAN) BURNING SMELL NOTICED IN FORWARD CABIN AFTER DEPARTURE. CREW ELECTED TO RETURN TO AIRPORT. ON ARRIVAL, MTX NOTICED CEILING LIGHTING NOT WORKING AT ROW 2DEF FOUND CONNECTOR ON LIGHTING FIXTURE HAD ARCED/BURNED AND EMITTED STRONG ODOUR. FIXTURE REMOVED, ISDR 513NA0010Gearbox · vibrationON TAXI OUT, HAD EICAS MESSAGE: LT OIL FILTER. FOUND METAL ON CHIP DETECTOR FOR HIGH SPEED GEAR BOX. REPLACED MAIN OIL FILTER AND SCAVENGE FILTER AND RAN ENGINE. LT ENGINE HAD VIBRATION DURING POWER RUN. SENT MECHANICS. 10/10/2004: REPLACED HIGH SPEED GSDR AALA20040794Sensor · malfunctionedORD - INFLIGHT T2252/01 ON FINAL RIGHT ENGINE FIRE INDICATION SHUT ENGINE DOWN AND FIRED BOTH BOTTLES. REPLACED BOTH ENGINE FIRE BOTTLES AND SQUIBS PER MM 26 21 01 4 FOR RIGHT HAND ENGINE AND REPLACED NR 1 TS5031 FIRE LOOP AND REPLACED NUMBER TWO CARD M684. SDR CA040629006Idg · failed(CAN) RT GEN FAILED ON CLIMBOUT. COULD NOT RESET, QRH CARRIED OUT. AIRCRAFT RETURNED TO DEPARTURE. ETOPS DOWNGRADED TO 120MIN. OPERATE IAW MEL 24-00-1.SDR CA040513004Slide · misinstalledADDITIONAL PARTS P/N D30854 S/N 0278 AND P/N 61571 S/N 0175, DURING OVERHAUL INSPECTION BY AIR CRUISERS ALL 3 SLIDES WERE FOUND IMPROPERLY PACKED WITH IMPROPER RESTAINTS. THIS COULD HAVE A SERIOUS PROBLEM IF UNITS WERE DEPLOYED.
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