Rolls-Royce RB211-22B-02
Service difficulty reports · 211
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 = 'RB21122B02' 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 = 'RB21122B02' 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 CA000830014Seal · leaking(CAN)- FLIGHT CREW REPORTED THAT COULD NOT MAINTAIN CABIN PRESSURE ABOVE 31,000 FEET. PRESSURIZATION CHECK CARRIED OUT FOUND C2 CARGO DOOR SEAL ASSEMBLY LEAKING. SEAL ASSEMBLY REPLACED.SDR CA000810012Fire Loop · failed(CAN) A/C DEPARTED WITH NR 2 ENGINE LOOP DEFERRED AS PER MEL. AIRCRAFT TO OPERATE WITH B LOOP SELECTED. 4 HRS AFTER DEPARTURE FLT CREW RECEIVED NR 2 ENGINE FIRE WARNING (LIGHT & AUDIO), FLT CREW ACCOMPLISHED FIRE DRILL & DISCHARGED BOTH FIRE-EX BOTTLES & SHUTSDR CA000802009Line · leaking(CAN) HYDRAULIC FLUID QUANTITY ON SYSTEM A DECREASING, CREW SWITCHED THE PUMP OFF AND STOPPED THE LEAK. MAINTENANCE FOUND PRESSURE LINE FITTING LEAKING AT ENGINE DRIVEN PUMP. O-RING REPLACED AND A/C RETURNED TO SERVICE.SDR CA000802008Wire · broken(CAN) WHILE TROUBLE SHOOTING HF PROBLEM, FOUND COAX CABLE BEHIND TRANSCEIVER DAMAGE AT CONNECTOR (SHIELD BROKEN). CABLE REPLACED AND AIRCRAFT RETURNED TO SERVICE. SPECIAL INSPECTION WILL BE IN PLACE SHORTLY TO INSPECT THESE CABLE ON ALL L-1011.SDR CA000714016Oil Filter · clogged(CAN) DURING TAKEOFF, CREW OBSERVED NR 1 ENGINE OIL FILTER PRESSURE LIGHT ON CW PANEL. ALL OTHER PARAMETERS NORMAL. LIGHT WENT OFF DURING INITIAL CLIMB. AFTER INVESTIGATION, MAINTENANCE FOUND NO METAL IN MCD AND PRESSURE OIL FILTER BUT SCAVENGE OIL FILTER WAS SDR CA000714015Pump · failed(CAN) CREW REPORTED THAT INBOARD FUEL BOOST PUMP CIRCUIT BREAKER POPPED. INSPECTION OF THE PUMP REVEALED ARCING THROUGH CASING BUT NO SIGN OF BURN ON HOUSING. BOOST PUMP REPLACED. THIS WAS A 4 YEARS OLD PUMP. AWAITING FOR SHOP REPORT ABOUT REASON OF ARCING.SDR CA000714011Engine · overheated(CAN) DURING TAKE OFF OUT OF LAS VEGAS, TGT ON NR 1 ENGINE WENT UP TO 740 DEG FOR 2 SEC. E.P.R. BROUGHT BACK IMMEDIATELY TO MAINTAIN 728 DEG. WHEN SAFELY AIRBORNE, E.P.R. REDUCED TO .462 MAINTAIN 725 DEG. BECAUSE OF PREVIOUS PROBLEM WITH THIS ENGINE, YYZ MAINSDR CA000621033Cable · bent(CAN) DURING APPROACH, UNABLE TO MOVE NR 3 ENGINE THRUST LEVER. INFLIGHT SHUTDOWN CARRIED OUT AS PER PROCEDURE. AFTER INSPECTION, MAINTENANCE FOUND TELEFLEX CABLE BENT WITH GROOVE SPLINE BROKEN. TELEFLEX CABLE AND FUEL FLOW REGULATOR LOWER BOX REPLACED AND AIRSDR CA000714010Actuator · failed(CAN) ON LIFT OFF, A SUDDEN AND UNCOMMAND INCREASE OF POWER OBSERVED. TGT WENT UP TO 728 DEG ON ROTATION. AFTER TAKE OFF, THROTTLE RETARDED. AFTER INVESTIGATION, MAINTENANCE REPLACED MASTER AND SLAVE ACTUATOR, TEST NR 4 CARRIED OUT AND AIRCRAFT CHECKED SERVISDR DLL10001119Connector · failedNR 2 ENG FUEL FLOW 4000 LBS HIGHER THAN NR 1 AND NR 3. HIGH FLOW CONFIRMED BY FUEL BURN ACTUAL.AFTER LANDING NR 2 ENG. SHUTDOWN IMMEDIATELY AND FUEL LEAK CONFIRMED BY EMERGENCY PERSONNEL AND MAINTENANCE. LOWER OIL TEMP AND FUEL TEMP VERIFIED HIGH FLOW. FOUSDR CA000614055Check Valve · clogged(CAN) DURING FUEL TRANSFER, UNABLE TO TRANSFER FUEL OUT OF TANK NR 1 BELOW 1450 POUNDS WITH BOTH BOOST PUMP ON. ON F/E PANEL, LOW PRESSURE LIGHT CAME ON. AFTER INVESTIGATION, MAINTENANCE FOUND AT FUEL TANK NR 1, CHECK VALVE AT BOOST PUMP HOUSING CLOGGED BY FORSDR DLL10001027Engine · fireNR 2 ENG ROLLED BACK AFTER START. MAINT INSP TAILPIPE AND MADE NORMAL RESTART. REPORT BY TWR THAT A/C HAD FLAME FROM NR 2 ENG ON PUSHBACK. CREW REPORTED ENG DID NOT EXCEED 500 EGT. A/C WAS TAILED INTO WIND. ENGINE SPUN TO EXTINGUISH FIRE.SDR CA000530053Check Valve · missing(CAN) NO FLOW WAS COMING OUT OF NR 3 PACK. WHEN REMOVING NR 3 PACK CONTROL VALVE, FOUND PART OF A CHECK VALVE STUCKED INSIDE THE PACK VALVE. AFTER INVESTIGATION, FOUND 2 PIE SHAPE SEGMENTS MISSING OF THE APU DISCHARGED CHECK VALVE. PNEUMATIC SYSTEM DUCTS INSPSDR CA000621032Bulb · burned out(CAN) DURING APPROACH , NO INDICATION DOWN AND LOCK FOR NOSE LANDING GEAR. AIRCRAFT MADE GO AROUND TO VISUALLY VERIFY GEAR DOWN AND LOCK AND FINALLY LAND WITH NO PROBLEM. THE PROBLEM RESULT AT 2 LIGHT BULB BURNT OUT. BULB REPLACED AND AIRCRAFT RETURNED TO SERVSDR CA000530052Bolt · sheared(CAN) DURING C CHECK FOUND RUDDER HINGE RT OTBD BOLT SHEARED.SDR DLL10000930Engine · damagedENGINE VIB ON NR 2 ENGINE 2.6 ON CLIMBOUT. SHUT ENG DOWN, ENG WINDMILLED APPROX 20 - 25 MIN. REPLACED DIFF PRESS SWITCH SCAVANGE OIL FILTER, BORO IPC AND HPC, CKS NORMAL. BORO 1ST STAGE FOUND DAMAGED. ENG CHANGE IN PROGRESS.SDR DLL10000757Elbow · crackedSYSTEM B HYDRAULIC RESEVIOR LEVEL DECREASED TO .25. TANK SHUT DOWN SYSTEM. REPLACED ELBOW ON PRESSURE LINE ON NR 2 ENGINE, HYD PUMP AND REPLACED PACKING ON TRANSFER LINE ON LEFT ELEVATOR FEEL UNIT. PERFORMED LEAK CHECK, NO DISCREPANCIES ENCOUNTERED.SDR DLL10000735Engine · vibrationNR 2 ENGINE HIGH VIBES EGT EXCEEDED WITH LOUD BANG. REPLACED ENGINE.SDR DLL10000643Control Cable · brokenFROM ABOUT 13000 FT TO GROUND, NR 2 ENGINE WAS NOT RESPONSIVE TO THROTTLE MOVEMENT. ENGINE SHUT DOWN AT TOUCH DOWN WITH FUEL SWITCH. FOUND TELEFLEX CABLE END BROKEN AT FFR END. REPLACED CABLE, NOW CKS OK.SDR CA000323007Cable · frayed(CAN) NR 3 THROTTLE REPORTED TO BE JAMMED BETWEEN UNIT 4 AND 4. CABLE CASING ASSY INNER TEFLON SHEATHING FOUND FRAYED. LOWER THROTTLE BOX, CABLE ASSY, AND CABLE CASING REPLACED.SDR CA000323026Pump · contaminated(CAN) NR 2 INBOARD QUANTITY LOW LIGHT ON WITH MORE THAN 700 POUNDS. AFTER SEVERAL BOOST PUMP REPLACEMENTS A BOLT WAS DISCOVERED IN BOOST PUMP CHECK VALVE. THE BOLT HAD DAMAGED THE CHECK VALVE. ORIGIN OF BOLT WAS UNKNOWN.SDR CA000307016Turbine · vibration(CAN) DAMAGE WAS FOUND ON POWER TURBINE. TEARDOWN REPORT REQUESTED. ENGINE IN UK FOR OVERHAUL AS OF JUNE 23, 2000. CONTACTED OPERATOR QA, AND WILL AWAIT TEARDOWN REPORT. (X)SDR CA000224043Gearbox · making metal(CAN) HIGH TGT AND COMPRESSOR STALL OBSERVED AT STARTER CUTOUT DURING START ATTEMPT. METAL FOUND ON GEARBOX MAGNETIC CHIP DETECTOR. REPORT TO FOLLOW.SDR CA000215033Wire · contaminated(CAN) OVEN REPORTED NOT WORKING. PHASE 1 WIRE DAMAGED DUE TO WATER CONTACT. WIRE REPAIRED AND COUNTER RESEALED. INSPECTION EVERY A-CHECK IMPLEMENTED.SDR CA000118051Tube · broken(CAN) EPR FLUCTUATIONS REPORTED ON NR 2 ENGINE. P1 PROBE LINE FOUND CRACKED.SDR CA000128058Compressor · damaged(CAN) HP COMPRESOR FOUND DAMAGED OVER LIMITS. TC: FOLLOW-UP/TEARDOWN REPORT EXPECTED FROM OPERATOR.SDR CA000110072Wire · shorted(CAN) SPARKS FROM WIRING SHORTING IN AFT GALLEY POWER DISTRIBUTION PANEL. INVESTIGATION REVEALED SEVERAL WIRES SATURATED WITH WATER APPARENTLY FROM BOTTLES BEING STORED ABOVE PANEL IN CUPBOARD. COMPANY FLEET CAMPAIGN UNDERWAY.MODI FICATION IMPLEMENTED ON ALL CSDR CA000110073Blade · failed(CAN) REMOVED AND REPLACED ONE BLADE OF HP 04 COMPRESSOR WAS BROKEN CAUSING HIGH VIBS AND IFSD. NO REASON SPECIFIED FOR BROKEN BLADE ISSUER INDICATES INCIDENT CLOSED.SDR CA991231058Connector · arced(CAN) DURING C CHECK MAINT FOUND ONE WIRE FROM HARNESS OF CONNECTOR 9811-P571 ENGINE START CONTROLPANEL ARCING ON THE BACKSHELL OF THE CVR CONNECTOR 23-71-P1. INSULATION IN AREA FOUND BURNT AND MELTED. FLEET CAMPAIGN INITIATED. INVESTIGATION REVEALED POSITIONISDR DLL10992620Pneu Duct · failedWHILE ADVANCING PWR FOR A NO PACK T/O, A LOUD BANG WAS HEARD FOLLOWED BY A CABIN PRESSURE SURGE. J-AREA OVERHEAT, POM PROCEDURES COMPLETED. RETURNED TO GATE. MTC FOUND NR 2 DUCT BLOWN BEHIND AFT B/B WALL ON LEFT SIDE OF LAV TANK.SDR CA991116014Nr 1 Bearing · leaking(CAN) ENGINE EXPERIENCED HIGH VIBRATIONS ON TAKEOFF. OIL FOUND IN SPINNER. OPERATOR SPECIFIED THAT THIS IS A KNOWN PROBLEM BUT HAPPENS VERY INFREQUENTLY. OIL IS PROPAGATING FROM NR 1 BEARING UNDER CERTAIN CONDITIONS.SDR DLL10992431Throttle · wornWHILE IN CRUISE NR 2 ENGINE POWER DECREASED AS THROTTLE WAS IN STATIONARY POSITION DURING APPROACH AT FL 100 THROTTLE WAS RETURNED TO IDLE STOP, BUT FUEL FLOW REMAINED AT 5000 LBS AND N2 WAS AT 79 PERCENT ENGINE WAS SHUT DOWN. FOUND THROTTLE RACK AND TELEX DSDR DLL10992231Engine · malfunctionedSHUT DOWN NR 2 ENGINE IN CRUISE DUE TO FILTER PRESSURE LIGHT ON S/O PANEL AS WELL AS LOW OIL QUANTITY, QUANTITY DECREASING. REPLACED NR 2 ENG GEARBOX HIGHSPEED EXTERNAL PER OPN NR 62304, 72312, REF ITEM 4,14 THIS LOG ITEM 4. CHIP DETECTORS REMOVED AND ISDR CA991028038Torque Tube · cracked(CAN) DURING INSPECTION LIFT TORQUE TUBES, FOUND CRACKED NEAR ENDS. FLEET CAMPAIGN INITIATED.SDR CA990916001Fire Loop · failed(CAN) FIRE DETECT LOOP B HAD INTERMITTENT FAILURE.SDR CA990817043Outlet Elbow · cracked(CAN) NR 1 ENGINE HP OUTLET ELBOW FOUND CRACKED, POSSIBLY DUE TO HEAT STRESS. OPERATOR AWAITING COMMENTS FROM ROLLS ROYCE.SDR DLL13991707Sensor · shortedON DESCENT, NR 3 ENG 'A' LOOP FIRE LIGHT AND 'B' LOOP ON MCO. ENGINE SHUTDOWN, FIRED BOTH EXT BOTTLES, STILL HAD A LOOP LIGHT. REPLACED UPPER AND LOWER FAN CASE LOOPS AND GEARBOX LOOP.SDR CA990728086Gasket · misinstalled(CAN) NR 2 ENGINE OIL QUANTITY DECREASED DURING FLIGHT. AIRCRAFT LANDED. INVESTIGATION REVEALED THAT THE GASKET WAS NOT INSTALLED PROPERLY ON THE GEARBOX.SDR CA990728085Actuator · cracked(CAN) AFTER LOSS OF C-SYSTEM HYDRAULIC FLUID, CREW INITIATED A MANUAL GEAR EXTENSION RESULTING IN A LARGE AUDIBLE BANG FROM THE RIGHT MLG. AIRCRAFT LANDED WITHOUT INCIDENT. INVESTIGATION REVEALED THAT THE RIGHT LANDING GEAR ACTUATOR SHEARED, JURY DRAG BRACE SDR CA990728084Switch · malfunctioned(CAN) SPARKS AND FOUL SMELL SEEN COMING FROM THE COAT RACK (L3) ADJACENT TO THE MICROSWITCH. WIRES FOUND BROKEN AND ARCING. WIRES REPAIRED.SDR DLL10991100Fire Loop · inoperativeNR 1 ENG LOOP A ON MCO, LOOP B FLICKERED THEN CAME ON STEADY. CREW SHUTDOWN NR 1 ENG PER POM. REPLACED UPPER GEARBOX LOOP.SDR CA990521061Oven · faulty(CAN) NR 2 AFT GALLEY OVEN STARTED SMOKING, OVEN TURNED OFF AND LATER FOUND TO BE AT FAULT.SDR CA990521060Brake · broken(CAN) NR 1 AFT MAIN WHEEL HARD TO REMOVE. INVESTIGATION REVEALED ONE BRAKE DISK RUBBING AGAINST HEATSHIELD ON WHEEL. EXCESSIVE EXPANSION OF THE DISK CAUSED IT TO CONTACT THE HEATSHIELD. BRAKES WILL BE MODIFIED TO BF GOODRICH SL 142 9.SDR CA990430049Engine · malfunctioned(CAN) ON CLIMB-OUT, THE NR 1 ENGINE VIBRATION WENT FROM 2 TO 5 UNITS ON BOTH CHANNELS. THE THROTTLE WAS RETARDED AND THE VIBS STILL REMAINED AT 3 UNITS. THE NR 1 ENGINE WAS SHUTDOWN. THE OIL LEVEL WAS 18 LITRES ON SHUTDOWN AND WENT DOWN TO 3 LITRES AT LANDISDR DLL13990665Panel · damagedFOUND ON WALKAROUND, NR 1 ENG PYLON PANEL 451FT DAMAGED. FABRICATED NEW PANEL PER ERA 367054-14.SDR DLL10990426Engine · failedENG FLAME-OUT OCCURED 5 MINUTES AFTER T/O ON CLIMBOUT. APPARENTLY RESULTED FROM FAILURE OF NR 1 ENG FUEL HP SOV. REPLACED ENGINE.SDR DLL10990404Pump · bypassingEXCESSIVE OIL CONSUMPTION, NR 1 ENGINE BEGAN FLT WITH FULL OIL QTY. AT TOP OF CLIMB, NR 1 ENG QTY WAS 15 QTS. CONSUMED 2.5 QTS IN THE NEXT 1 HR 15 MIN, INDICATED AS LOW AS 9 QTS AFTER 3.5 HRS OF FLT. REPLACED SCAVENGE/LUBE PUMP ASSEMBLY. RAN ENGINE, OPS ANSDR CA990614076Axle · leaking(CAN) AFTER HARD LANDING, FOUND AFT DRAIN MAST SEPARATED FROM FUSE ENG 2. APU FUEL SHROUD BENT, AFT BODY SHROUD AND VHF 3 BENT TAIL SKID AT 150 PSI, FLAT SPOT ON SHOE AND LOCKWIRE BROKEN. ALSO FOUND LT REAR AXLE OF MAIN LANDING GEAR WITH GREASE OUT AND A FUSDR CA990311083Windshield · cracked(CAN) CAPTAIN'S WINDSHIELD DELAMINATED AND FAULT LIGHT ALWAYS ON, WINDSHIELD DELAMINATED AT MANY PLACES AROUND CONTOUR OF WINDOW. REPLACED.SDR CA990311067Torque Link · cracked(CAN) ON WALKAROUND AT NLG UPPER TORQUE LINK, RT SIDE INNER SLEEVE CRACKED. CRACK STARTED FROM SMALL RADIUS NOTCH AND GOES TO THE OPPOSITE SIDE CAUSING SEPARATION OF PART. WHEN NLG DISCONNECTED, OUTER SLEEVE FOUND CRACKED AND NO GREASE PRESENT, ZEUS FITTING
Back to Rolls-Royce RB211-22B-02