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 CA040503011Governor · inoperative(CAN) LT ENG VALVE LIGHT ILLUMINATED AND EICAS MSG L ENG FUEL VAL DISPLAYED WITH FUEL CONDITION SWITCH IN RUN. NO FUEL FLOW INDICATED. LT ENG FFG REPLACED C/O IAW AMM 73-21-01. TEST 1, 2, 9 AND 10 CARRIED OUT SATIFACTORY.SDR CA040316006Wire · chafed(CAN) RT SPAR FUEL SHUTOFF VALVE CB C1062 ACTIVATED DURING SHUTDOWN AFTER FLIGHT. CB WOULD NOT RESET, AND SPAR VALVE DISAGREEMENT LIGHT ALSO ILLUMINATED. TROUBLESHOOTING REVEALED WIRE HAD CHAFING DAMAGE AT BULKHEAD LOCATED AT STATION PP STN 208.40 VISIBLE BEHSDR CA040303005Brake · contaminated(CAN) NR 5 BRAKE SMOKING ON ARRIVAL. A/C HAS JUST RETURNED FROM PAINT, IT IS SUSPECTED THAT EXCESS FLUID HAD COLLECTED ON THE SURROUNDING AREA OF NR 5 BRAKE. BRAKE AND WHEEL AREA THOROUGHLY CLEANED.SDR P9RA20040003Light · inoperativeTWO EMERGENCY LIGHTS OUT AT AFT LAVATORY LOCATION. REMOVED AND REPLACED FLOOR LIGHT ASSY'S AT AFT LAV LOCATION IAW MM 33-10-01.SDR P9RA20040004Drive Assy · bindingON APPROACH IN TO POS; AS FLAPS WERE SELECTED DOWN, EICAS MESSAGE L/E SLAT ASSY APPEARED. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED SLAT PDU IAW BMM 27-81-00.SDR CALA0400021Engine · making metalSMOKE WITH OILY ODOR REPORTED IN CABIN & NR 1 ENG AUTO SHUTDOWN. A/C DIVERTED & LANDED WITHOUT INCIDENT. INSP OF NR 1 ENG FOUND CHIP DETECTORS COVERED IN METAL, ENG OIL QTY ZERO, & DAMAGE TO NR 1 ENG FAN & COWL. A/C OUT OF SERVICE FOR REMOVAL OF NR 1 ENG. SDR CA040114005Pin · mismanufactured(CAN) UPON ROTATION, TAT PROBE EICAS MESSAGE FOLLOWED BY AUTO THROTTLE DISCONNECT, AND ASSOCIATED WARNINGS. AIR TURN BACK. TAT PROBE REPLACED. GROUND TEST GOOD. DEFECT RECURRED ON NEXT TAKEOFF.K143 AND K203 AIR/GND RELAYS REPLACED. TESTED GOOD IAW MM 30-33-0SDR CA031006009Control Unit · will not test(CAN) LT ENGINE FLAMED OUT ON WHILE TAXIING IN. EICAS MSG 'LT ENG LP PUMP'. TROUBLESHOOT PER FIM 75-32-00 BITE CODE 90 ON THE TRANSIENT PRESSURE UNIT LED TO ITS REPLACEMENT. DURING ENGINE RUN N3 WAS NOTED TO BE ON LOWER END OF LIMIT PER MM71-00-00 FIG.517A.SDR CA030113011Compressor · malfunctioned(CAN) STRONG BURNING ODOR AND LIGHT SMOKE IN AFT CABIN. FAULT TRACED TO POTABLE WATER COMPRESSOR. CB FOUND POPPED. DEFERRED FOR REPLACEMENT. ELECTRICAL CONNECTOR REMOVED FROM COMPRESSOR.SDR CA030107019Bolt · broken(CAN) DURING WALK AROUND IN YMX, MTCE FOUND NR 8 MAIN WHEEL ASSY WITH ONE BOLT BROKEN (NUT WITH PORTION OF BOLT MISSING). THE MLG WHEEL ASSY WAS REPLACED I.A.W. AMM 32-45-01 (REF., DEF. 58871).SDR CA030112001Bolt · sheared(CAN) UPON ARRIVAL OF A/C IN YYZ, FLT 421, DURING WALK AROUND, MTCE DISCOVERED 2 TIE BOLTS MISSING FROM NR 7 MLG WHEEL ASSY. THE NR 7 MLG WHEEL WAS REPLACED IAW AMM 32-45-01.SDR AALA20021627Engine · making metalLAX - FLT 192 - EN ROUTE LAX-BOS, AT CLIMB POWER, RIGHT ENGINE COMPRESSOR STALLED AND OVERTEMPED. RETURNED AND LANDED AT LAX WITHOUT FURTHER INCIDENT. FOUND METAL IN TAIL PIPE. REPLACED RIGHT ENGINE. GROUND CHECKED NORMAL OPERATION. (M)SDR CA021110002Bolt · sheared(CAN) DURING WALK AROUND INSPECTION, A MAIN WHEEL WAS FOUND WITH ONE TIE BOLT MISSING AND TWO OTHERS NOT SAFE (TORQUE WISE). THEY COULD BE ROTATED USING HAND FORCE. ALL THE BOLTS AFFECTED WERE SIDE BY SIDE. UPON FURTHER INVESTIGATION THE FINAL FINDINGS WERE: 1SDR 751PA0003Engine · flamed outON DESCENT INTO POS, NR 2 ENGINE FLAMED OUT. WENT TO FLT AND GOT A RELIGHT. INSPECTED NR 2 ENGINE FOR INTAKE & EXHAUST FOD DAMAGE, CHECKED N3 ROTATION, INSPECTED LP FUEL PUMP FOR DAMAGE, INSPECTED LP & HP FUEL FILTERS, NO DEFECTS NOTED IAW 757 FIM 71-05-00 FSDR CA020816004Bearing · seized(CAN) CREW REPORTING RUDDER PEDAL HARD TO MOVE ON GROUND. AFTER INVESTIGATION, MAINT FOUND A ROLLER BEARING SEIZED IN THE CAM ROLLER ARM ASSY. OF THE RUDDER FEEL CENTERING MECHANISM MAINTENANCE REPLACED THE ROLLER AND TESTED THE RUDDER PEDAL FORCES IAW AMM 2SDR CA020426006Smoke · detected(CAN) CROSSING TOP THURDERSTORM, APPLIED MAX CONTINUOUS FOR 30 SEC. SPEED DROP TO M.72 AT FL 360. SMELL OF OIL BURNED FOR 3 MINS ALL PARAMETERS NORMAL ACTION TAKEN LMWS 51130 ITEM 1,2 BVCU BITE CHECK, MCD'S INSPECTED ON BOTH ENGINE. BOTH ENGINE TEST C/O AS PSDR CA020328009Tie Bolt · sheared(CAN) DURING A "RAMP 1 CHECK" ONE TIE BOLT WAS FOUND BROKEN ON NR 6 MAIN WHEEL ASSY. MAINTENANCE REPLACED THE MAIN WHEEL ASSY.I.A.W. MM 33-45-01.SDR CA020222001Access Panel · missing(CAN) WHEN AIRCRAFT LANDED CREW SELECTED REVERSERS, THE NR 2 ENGINE, RT THRUST REVERSER WOULD NOT STOW. DURING THE WALK AROUND, THE CREW FOUND THE NR 2 ENGINE THRUST REVERSER DUCT ACCESS PANEL (P/N LJ76673) RIPPED OFF AND DAMAGE TO THE THE RT TRANSLATING SDR CA020221009Clamp · loose(CAN) WHEN REACHING FL330 , THE CABIN ALTITUDE LIGHT CAME NI AND THE RT PACK INOP LIGHT CAME N. WE STARTED DESCENT, THE CABIN STABILIZED AT FL 250. THE RT PACK WAS RESETTED AND FOUND OK. THE CREW STAYED AT THAT LEVEL FOR THE REMAINDER OF THE FLIGHT . MAINTENASDR CA020201016Clamp · loose(CAN) DURING DEFECT INVESTIGATION, FOUND ON NR 1 ENGINE IN THE STRUT AREA, JUST BELOW THE REVERSE FLOW CHECK CONTROLLER, A CLAMP WITH BURNED RUBBER ON IT. PROCEEDED WITH AN AIR LEAK INVESTIGATION AND FOUND A LEAKING CLAMP. THE CLAMP WAS REPLACED.SDR CA011211007Fitting · cracked(CAN) ELBOW HYDRAULIC FITTING CRACKED AT OUTLET PORT OF LT ELECTRICAL HYDRAULIC PUMP.SDR CA011211021Torque Tube · cracked(CAN) DURING INTER 1 CHECK, THE INSPECTION CARRIED OUT ON THE CAPTAIN SEAT REVEALED THAT THE SEAT TORQUE TUBE WHICH HAS THE ELECTRICAL WIRING FOR THE VERTICAL ADJUSTMENT GOING THROUGH ,HAD 4 CRACKS ON THE TUBE.SDR CA011211020Wire Harness · damaged(CAN) 1-) DURING INTER 1 CHECK INSPECTION , THE NR 1 ENGINE EEC PATCH MODULE LOOM INTO CONNECTOR D1380 REVEALED DAMMAGED TO THE WIRING AT CLIPPING POINT CP2281. PROBLEM FOUND WAS CAUSED BY WIRING CHAFFING INTO CLIP CP2281 THAT HAD ITS RUBBER INSULATOR TORNAND SDR CA011211012Wire Harness · damaged(CAN) DURING INSPECTION , FOUND DAMAGE OF THE WIRING HARNESS THAT GOES TO THE P1 PROBE HEATER NOSE COWL INTERFACE CONNECTOR. TYPE OF DAMAGES ON THE TWISTED SHIELDED PAIR WIRES CABLE FOUND OUTER JACKET AND SCREEN DAMAGE BY ABRASION.SDR AALA20011859Engine · flamed outLAX - FLT 2469 - EN ROUTE DFW-LAX - ON LANDING, LEFT ENGINE FLAMED OUT. DISCHARGED FIRE BOTTLE. LANDED LAX WITHOUT FURTHER INCIDENT. REPLACED LEFT ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR CA011211022Rod · broken(CAN) AIRCRAFT ARRIVED WITH NR 1 BRAKE TORQUE ROD ASSEMBLY BROKEN IN HALF AND HYDRAULIC LINE TO BRAKE WAS BROKEN.SDR CA011211023Duct · cracked(CAN) NR 2 ENGINE STARTER DUCT CRACKED JUST BELOW THE UPPER FLANGE.SDR CA010808032Door · missing(CAN) AIRCRAFT ARRIVED ON STATION WITH NR 2 ENGINE OIL SERVICING DOOR MISSING. ROLLS ROYCE SERVICE BULLETIN RB 211-71-B592 WAS INCORPORATED ON THE DOOR. A NEW ACCESS DOOR WAS INSTALLED. NEW SPRING CLIP FROM GOODRICH WILL BE INSTALL WHEN MODIFICATION BECOME AVASDR CA010727020Hydraulic Line · leaking(CAN) AIRCRAAFT RETURNED TO THE GATE, AFTER PUSH BACK, DUE TO A HYDRAULIC LEAK AT THE L/H MAIN LANDING GEAR DOWNLOCK ACTUATOR SUPPLY FLEX LINE. LINE WAS FOUND RUPTURED AT MID POINT. LINE WAS REPLACED AND AIRCRAFT WAS RETURNED TO SERVICE.SDR CA010704016Shaft · failed(CAN) DURING CRUISE PILOT REPORTED ENGINE OIL PRESSURE DROP AND QTY DROP, VIBS STARTED TO INCREASE AND THE FLIGHT CREW ELECTED TO SHUT DOWN THE ENGINE IN ACCORDANCE WITH QRH PROCEDURES. AIRCRAFT DIVERTED AND RETURNED TO GANDER. MAINTENANCE INSPECTED THE LP COUSDR CA010626008Tube · cracked(CAN) TORQUE TUBE CRACKED WHERE THE CUTOUT HAS BEEN MADE FOR THE WIRING TO GO THROUGHT. THIS IS THE SECOND SEAT WE FIND WITH THE SAME PROBLEM.SDR CA010704023Spring · broken(CAN) RUDDER PEDAL HAS A LACK OF NORMAL RESISTANCE WHEN DISPLACED. INSPECTION FOUND THAT ONE OF THE FEED BACK SPRINGS WAS BROKEN, SPRING WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR ANCF200100011Harness · chafedLEFT ENGINE FIRE WARNING WITH EICAS MESSAGE “LT ENGINE FIRE”, FIRE INDICATION STOPPED WHEN FIRE SWITCH PULLED. CORRECTIVE ACTION:THE FIRE DETECTOR HARNESS WERE CHECKED AND FOUND CHAFING, IT WAS ISOLATED, THE TURBINE OVERHEAT SWITCH S10140 WAS FOUND GROUNDED ASDR CA010626024Duct · leaking(CAN) #1 ENG THRUST REVERSER DEACTIVATED AS PER MEL. INVESTIGATION FOUND THE PYLON MOUNTED FAN THRUSR REVERSER ELECTRICAL HARNESS PN LJ6579 AND LJ 76580 MELTED AND HEAVELY DAMAGED. HOT AIR LEAK FROM HP2 ANDHP7 BLEED AIR DUCT PN 312N5321-7 AND 312N5306-1 ALSO CSDR CA010531009Shaft · sheared(CAN) DURING CRUISE FLIGHT CREW REPORTED R/H ENGINE HYDRAULIC PRESSURE LOW LIGHT CAME ON WITH ECIAS MESSAGE "R/H ENG EDP". AIRCRAFT DIVERTED AND LANDED. R/H EDP FOUND SHAFT SHEARED, PUMP REPLACED, FILTERS REPLACED AND SYSTEM FLUSHED AS PER AMM 29-11-00 AND 29-SDR CA010402013Valve · cracked(CAN) R/H HYDRAULIC QUANTITY DECREASING DURING LAST MINUTE OF FLIGHT. FOUND DURING WALKAROUND, RT ANTI-SKID MODULE VALVE V35 IN WHEEL WELL CRACKED, VALVE REPLACED, LEAK CHECK CUT OUT AND ACFT BACK TO SERVICE.SDR CA010307014Bolt · sheared(CAN) DURING ROUTINE CHECK FOUND NR 1 ENGINE RT C DUCT AFT FORWARD BOLT SHEARED. AIRCRAFT WAS FERRIED ON A FERRY FLIGHT PERMIT WITH BOEING SUPPORT AND BOLT REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR AALA20002008Sensor · defectiveMIA - FLT 9509 - EN ROUTE RBR-MIA, DETECTED ELECTRICAL SMELL IN LEFT SIDE COCKPIT. SMELL DISSIPATED AFTER SIXTY SECONDS. LANDED MIA WITHOUT FURTHER INCIDENT. REPLACED NR 1 SIDE TRANSIENT PRESSURE UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA20002036Engine · vibrationTPA - FLT 1818 - EN ROUTE MIA-LAX, FIFTEEN MINUTES INTO FLIGHT DETECTED NR 1 SIDE ENGINE VIBRATION. RETURNED THROTTLE TO IDLE. ACCOMPLISHED ENGINE VIBRATION CHECKLIST. ENGINE CONTINUED TO VIBRATE. PROCEEDED TO SHUT NR 1 ENGINE DOWN PER THE CHECKLIST. DIVESDR CA010103021Expansion Ring · leaking(CAN) HP 6 EXPANSION DUCT LEAK CAUSING BURNS TO DIFFERENT COMPONENTS IN THE AREA (NR 1 PYLON). THE MAJOR COMPONENT THAT WAS AFFECED IS THE C DUCT RT SIDE THE FWD UPPER CORNER IS DELAMINATED AND REQUIRED REPAIR MANY OTHER PARTS HAD DAMAGES AND NEEDED REPLACEMENSDR CA010103018Control Valve · stuck(CAN) AFTER LANDING, PILOT REPORTED THAT NR 1 ENGINE THROTTLE WAS JAMMED AT IDLE. FOUND NR 1 DCV (DIRECTIONAL CONTROL VALVE) STUCKED IN EXTEND POSITION. DCV WAS REPLACED AND THROTTLE WAS SERVICE.SDR CA001219009Tube · failed(CAN) THIS UNIT WAS SENT FOR OVERHAUL AND FAILED HYDROSTATIC TEST, AND THE INFLATABLE FAILED THE PROOF TEST, ALSO NOTICE THAT THE LOWER TUBE FAILED THE TEST AT 4 PSI AND SEPARATED ALONG THE MAIN SEAM ADJACENT TO THE PRESSURE RELEASE VALVE.SDR CA001212007Structure · missing(CAN) AIRCRAFT IN CLIMB PHASE OF TAKEOFF. CREW REPORTED THAT WHEN THEY MOVED THE FLAP/SLAT HANDLE FROM POSITION 1 TO FULLY RETRACTED THAT A NOISE WAS HEARD. UPON CARRYING OUT A VISUAL INSPECTION, IT WAS OBSERVED THAT A PORTION APPROXIMATELY 800 SQUARE INCHES SDR CA001123009Selector Knob · failed(CAN) THRU 10,000 FEET CABIN ALTITUDE EICAS WARNING. QRH ACTIONED. AIRCRAFT RETURNED TO YYZ WITHOUT INCIDENT. CABIN PRESSURE SELECTOR REPLACED.SDR CA001107005Tube · worn(CAN) DURING C-CHECK INSPECTION, FOUND CARGO FIRE EXTINGUISHING TUBE RUBBED THROUGH BY CONTACTING APU BLEED AIR DUCT. CAUSE OF PROBLEM IS THE APU DUCT VIBRATION WITH CLOSE TOLERANCE. FIX IS INCORPORATION OF SB 57-26A0040.SDR CA001004009Fan · seized(CAN) AIRCRAFT WAS DIVERTED DUE TO BURNING ODOR IN COCKPIT AND FWD CABIN, CREW STATED THAT ODOR STOPPED AS SOON AS ALTERNATE FAN SELECTION WAS CARRIED OUT. UPON ARRIVALMAINTENANCE FOUND NR 1 EQUIPMENT COOLING FAN BREAKER POPPED, FAN FOUND SEIZED. AIRCRAFT WAS SDR CA000830016Door Seal · obstructed(CAN) AIRCRAFT RETURNED TO BASE AFTER NOT BEING ABLE TO MAINTAIN CABIN PRESSURIZATION ABOVE 23,000 FEET,. DURING GRD PRESSURIZATION CHECK FOUND HEAVY AIR LEAK FROM L/H PRSOV AND C1 CARGO. C1 CARGO FOUND NET OVER CARGO DOOR SEAL, NET REPOSITIONED. PRSOV LOCKED SDR CA000830017Cable · damaged(CAN) LOG BOOK DEFECT REPORTED BY FLIGHT CREW ON ARRIVAL . NR2 ENGINE THROTTLE BINDING. FOUND THRUST REVERSER FEEDBACK PUSH PULL CABLE DAMAGED CAUSING THE T/R FEEDBACK CAM TO BEND. FORWARD THRUST FEED AND SENSE C/O, NO FAULT FOUND, T/R LOCKED OUT AS PER MEL.SDR CA000802010Coupling · contaminated(CAN) UNABLE TO ACHIEVE TAKEOFF POWER, WITHOUT RETURNING AT THE DATE, CREW DID A SUCCESSFUL POWER RUN AND A/C DEPARTED. SAME THING HAPPENED ON THE NEXT LEG. AFTER INVESTIGATION, MAINTENANCE FOUND COUPLING BETWEEN ENGINE AND FRAME FFG CABLE CONNECTOR CONTAMINATSDR CA000714013Retainer · corroded(CAN) DURING SLIDE/RAFT REPLACEMENT, THE GIRT BAR RETAINER PLATE FOUND SPLIT IN HALF DUE TO EXCESSIVE CORROSION. PLATE REPLACED AND FLEET CAMPAIGN WILL BE DONE TO VERIFIED THE CONDITION OF THE PLATE AS PER SPECIAL INSPECTION 3-25-30 REV-0.
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