Rolls-Royce RB-211 series
Service difficulty reports · 353
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 = 'RB211' 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 = 'RB211' 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 AALA20090818LAX01Sensor · faultyLAX - DURING TAKEOFF ROLL LEFT ENGINE BLEED OFF LIGHT AND ASSOCIATED EICAS MESSAGE ILLUMINATED. CREW ABORTED TAKEOFF AND PULLED BACK ON THROTTLES CAUSING LIGHT AND MESSAGE TO EXTINGUISH. RETURNED TO LAX WITHOUT INCIDENT. REPLACED REVERSE FLOW SENSOR. SYSTESDR FDEA200906102014Restrictor Valve · malfunctionedREJECTED TAKE OFF AT 75KT FOR LT REVERSER ISOLATION VALVE EICAS MSG. COMPLIED WITH QRH PROCEDURES, RETURNED TO GATE. ( STATUS MSG "L REV ISLN VAL") FAULT CODE: 78-34-XC. ACFT RELEASED FOR SERVICE IAW MEL/CDL: 78-31-01-01. FOUND BOTH TRANS COWL GAPS OUT OF LSDR DL777090897Igniter · failedATTEMPTED 5X APU STARTS IN CRUISE AS REQUESTED BY MX. APU WOULD NOT START. PEAK RPM 29 PERCENT. CA-NO LATCHED FAULTS APU OPERATES NORM. REMOVED AND REPLACED APU IGNITORS IAW MM FIM 49-40-00-810-814. OPS CK GOOD ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS SDR CA090423004Wire Harness · damaged(CAN) AMCU NR1 J1 PORT SHORTED OUT. DURING POWER UP OF SEATS 1-9 IN SEQUENCE, ONCE ARRIVING AT SEAT 5A THE J1 PORT IN THE AMCU TRIPPED OFF DUE TO A POWER OVERLOAD. CAUSE OF THE POWER OVERLOAD WAS DUE TO A MISWIRED HARNESS BETWEEN SEAT 4A AND 5A. THE HARNESS SDR CA090420003Electrical Box · damagedDURING THE COURSE OF AN RADIO MODIFICATION, SPECIFIC SNAGS APPEARED DURING THE POST-INSTALLATION AND TESTING PHASE OF THE CHECK WITH THE FOLLOWING DISCREPANCY NOTED: "DURING THE CONTOUR SEAT POWER UPS, MCU NR 1, J2 PORT SHORTED OUT MAKING MCU UNSERVICABLE" MSDR AALA2009030200001Engine · inoperativeMIA - NUMBER ONE ENGINE OIL QUATITY AND PRESSURE WENT TO ZERO AND THE CREW SHUTDOWN THE ENGINE. SINGLE ENGINE TIME 10 MINUTES. EMERGENCY DECLARED, RETURNED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER 1 ENGINE ON MARCH 3,2009 AT MIASDR CA090504005Wire Harness · misinstalled(CAN) DURING REMOVAL OF TRIM TANK TRANSFER PUMP , ELECTRICAL CONNECTOR PIN FOUND BENT AND ASSOCIATED CONNECTOR PLUG INSULATOR FOUND DAMAGED WITH SIGNS OF ARCING. IT WAS DETERMINED THAT PIN 2, ON THE PUMP HSG (MALE) CONNECTION POINT, BENT UPON A PREVIOUS INSTASDR CA090216006Video Unit · smoke(CAN) APPROX 30 MINUTES AFTER DEPARTURE, THE CREW REPORTED THAT THE VIDEO MONITOR AT SEAT 29F WAS SMOKING. POWER TO THE ENTERTAINMENT SYS WAS TURNED OFF AND THE MONITOR STOPPED SMOKING. ACFT TIMES WERE: 33815 FH, 5420 FC. XM RELEASE DATE FOR THE ACFT: FEB 13 SDR AALA2009021301039Control Unit · inoperativeORD - CREW REPORTED ON CLIMBOUT IN FLIGHT SHUTDOWN OF RIGHT ENGINE, SINGLE ENGINE TIME 9 MINUTES. EMERGENCY DECLARED, RETURNED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED BLEED VALVE CONTROL UNIT AND TRANSIT PRESSURE UNIT. SYSTEM GROUND CSDR UPS08554083Engine · faultyINSPECTION TYPE:N/A RT PACK EXTREME ODOR/FUMES WHEN OPERATING SHUT DOWN RT PACK & FUMES EXTINGUISHED. ACCOMPLISHED NR 2 ENG PWR RUN PER MM 71-00-00-5. OIL FUMES EMITTED FROM NR 2 ENG WITH EITHER PACK L OR R SELECTED AND ENG ABOVE GRD IDLE. FUMES DISSIPATED SDR USAABB08125Connector · damagedPHL FLT 1209 PHL TO SXM - DURING TAKEOFF ROLL, TNE NR 2 ENG WOULD NOT DEVELOP TAKEOFF POWER. THE CREW ABORTED THE TAKEOFF AT 60 KNOTS AND RETURNED TO THE GATE. MAINTENANCE REPAIRED THE CONNECTOR ON THE FUEL FLOW GOVERNOR SOLENOID. OPERATIONALLY CHECKS OK. SDR RYN2008F00000Computer · malfunctionedAIR TURN BACK, DUE TO LOSS OF ALL 3 AUTO PILOTS AND THE CAPTAIN`S FLIGHT DIRECTOR, COULD NOT ENTER RVSM AIRSPACE. RESET LT FCC AND ACCOMPLISHED TEST 2 AND 10 IAW AMM 22-30-00. ALL CHECKED NORMAL. (K)SDR ANCF200800006Duct · damagedENG OVHT DISPLAYED WITH ENG OVHT LIGHT ILLUM. LIGHT EXTING AFTER THRUST REDUCTION AND CAUTION LIGHT ON. 4AW AMM 36-11-01 P.401 / 36-11-07 P.401. REMOVED AND REPLACED BOTH HP2 AND HP6 DUCT ASSY IAW AMM 71-00-00 ENG RUN PERFORMED SATISFACTORY. P/N 312N5306-1 SDR CA080314005Tire · failed(CAN)THE AC BLEW THE NR (4) MAIN TIRE ON DEPARTURE. THE FLIGHT CREW ELECTEDTO DIVERT, AND ULTIMATELY LANDED APPROXIMATELY 15000 KGS OVER THE MAXIMUM STRUCTURAL LANDING WEIGHT OF 185000KGS. DURING TAXI, THE NR (3), RT FWD IB MAIN TIRE DEFLATED AND THE AC WAS SSDR AMTA200800015Transceiver · malfunctionedHF 2 RADIO INOPERATIVE. (K) PERFORMED HF COMM SYSTEM BITE IAW FIM 23-11-00-810-810 TEST PASSED NO FAULTS. SWAPPED HF TRANSCEIVER IAW AMM 23-11-21-4. HF NR 2 TRANSCEIVER IS NOW SN 0386. HF NR 1 TRANSCEIVER IS NOW SN 0025.SDR AMTA200800014Apu · unserviceableAPU ON START OIL QTY FLLUXUATION, CHIP DETECTOR HAS DEBRIS AND OIL DRAINS FROM CHECK VALVE TO ZERO QTY. REPLACED APU IAW M57-49-02. APU OPS AND LEAK CHECKED GOOD. (K)SDR AMTA200800012Display · malfunctionedF/O MCDU BLANK. REMOVED AND REPLACED FO`S MCDU, IAW AMM 34-60-00, OPS CHECKS GOOD. (K)SDR AMTA200700556Warning Message · false activationSTATUS MSG (R TURB OH DET2) DISPLAYED. TROUBLESHOOT IAW FIM 26-13-00, FIG 103 AND 104, OPS CHECK NORMAL. (K)SDR CA070905009Fan · melted(CAN) AFTER T/O, SMOKE AND UNUSUAL SOUND COMING FROM L2 AREA. HAZE REPORTED IN THE CABIN. FLT RETURNED TO AIRPORT. ELECTRICAL ODOR WAS COMING FROM THE L2/R2 AREA WITH HAZE VISIBLE AT 5 DIFFERENT TIMES. IT WOULD APPEAR AND THEN DISAPPEAR. AREA INSPECTED AND FOSDR ANCF200700019Fire Loop · malfunctionedPILOT REPORT: RT ENGINE FIRE AT MDE THE FAULT WAS PRESENTED AFTER 5 MIN OF DEPARTURE. BOTTLE NR 1 WAS DISCHARGED AND RETURNED TO MDE WITH NORMAL LANDING FLIGHT TIME WITH SINGLE ENG +/- 13 MTS. INSPECTED RT ENGINE IAW AMM 71-00-00 PAGE 604. NO FIRE EVIDENCE FOSDR UPS07550215Fuel Filter · unknownRECEIVED NR 2 ENGINE FUEL FILTER MESSAGE. A/C IS OOS FOR TROUBLESHOOTING. [08-01-07] REMOVED & REPLACED EPR TRANSMITTER RT ENGINE PER MM 77-11-01-4. PERFORMED EPR HIGH POWER ENG RUN PER MM 71-00-00-5 TEST 13. ALL ENG PARAMETERS CHECK OK. ITEM CLEARED.SDR CA070531004Unknown · odor(CAN) DURING FLIGHT, A PAPER BURNING SMELL AT SEAT 26DE WAS REPORTED TO THE CABIN CREW. THE AUDIO SYSTEM WAS SHUTOFF IAW PRECAUTION AND SMELL DISAPPEARED AFTER 20 MINUTES. THE AUDIO SYSTEM WAS TESTED ON ARRIVAL AND THE AREA INSPECTED FOR BURNING MARKS. AUDIO SSDR AMTA200700186Coupler · damagedLT HF TRANSMISSION AND RECEPTION WEAK AND INTERMITTENT. REMOVED AND REPLACED LEFT HF COUPLER IAW MM 23-11-01-4, OPS CHECKS GOOD AT THIS TIME, TRANS AND RECEPTION LOUD AND CLEAR. (K)SDR AMTA200700185Wire · disconnectedEMERGENCY FLOOR TRACK LIGHTING 3 DEF THRU 10 DEF INOPERATIVE. INSPECTED FLOOR TRACK WIRING FOUND WIRES DISCONNECTED RESECURED TRACK COVERS, OPS CHECK GOOD. (K)SDR AMTA200700176Control Panel · malfunctionedRT AFT FUEL BOOST PUMP LOW PRESS LIGHT INOPERATIVE, RELAMP NO HELP. REMOVED AND REPLACED FUEL MANAGEMENT CONTROL PANEL IAW AMM 28-22-14-4, TEST OK. (K)SDR AMTA200700175Printed Ckt Board · faultyEICAS STATUS MSG RT ENG OH LP2 DISPLAYED. REMOVED AND REPLACED FIRE DETECTION PRINTED CIRCUIT CARD M684 IAW FIM 26-11-00 AND AMM 26-10-01-4, PERFORMED FIRE/OVHT TEST, NO FAULTS NOTED. (K)SDR AMTA200700177Warning System · malfunctionedGIRT BAR ENGAGEMENT LIGHT EXT WITH EVACUATION SLIDE ARMING LEVER IN ARMED POS AT ENTRY DOOR 2L. INSPECTED DOOR SLIDE LIGHT. LIGHT OPS CHECK NORMAL.(K)SDR AMTA200700178Warning System · malfunctionedGIRT BAR ENGAGMENT LIGHT EXTN WITH DOOR IN THE ARMED POSITION R-2. INSPECTED DOOR SLIDE LIGHT. LIGHT OPS CHECK NORMAL.SDR AMTA200700046Generator · unserviceableLT GEN DRIVE LGT DID NOT ILLUMINATE WITH ENGINE SHUTDOWN. REMOVED AND REPLACED LT ENG. IDG IAW M57-24-01. OPS CHECK AND LEAK CHECK GOOD. (K)SDR USAA061433Floorbeam · corrodedLOCATION: BETWEEN FR 16 AND 17 AND -Y50 REMOVED AND REPLACED FLOORBEAM AND BRACE IAW SRM 51-72-00; CORR TASK JA-220-53500; LEVEL 1 DEFECT SIZE: 5 SQ. IN.SDR AMTA200600693Seat Track · corrodedCABIN SEAT TRACK FOUND WITH CORROSION AND SCRATCHES. REPLACED SEAT TRACK CROWN IAW SRM. (PART OF REPLACEMENT OF CROWN TRACK ON NRC 4193). (K)SDR AMTA200600695Seat Track · brokenCABIN FLOOR SUPPORT SEAT TRACK CROWN FOUND BROKEN. REPLACED SEAT TRACK IAW SRM.SDR AMTA200600690Light · inoperativeEMERGENCY FLOOR TRACK LIGHTS INOPERATIVE AT FWD GALLEY. REMOVED AND REPLACED FWD GALLEY LIGHT STRIP, OPS CHECK NORMAL IAW MM. (K)SDR AMTA200600691Seat Track · corrodedCABIN FLOOR SUPPORT SEAT TRACK FOUND WITH CORROSION AND SCRATCHES. REPLACED SEAT TRACK CROWN IAW SRM. (PART OF REPLACEMENT OF CROWN TRACK OF NRC 4193). (K)SDR USAABB06079Charger · inoperativeDURING MAINTENANCE, 4R EMERGENCY EXIT LIGHT FOUND INOPERATIVE. MAINTENANCE REPLACED THE BATTERY AND CHARGER.SDR CA061011004Oven · smoke(CAN) BURNING SMELL WAS NOTICED IN THE FWD GALLEY BY THE FLIGHT ATTENDANT WITH AN ASSOCIATE ECAM SMOKE WARNING OF THE FWD LAVATORY. F/A NOTICED SMELL COMING FROM NR 3 OVEN TIMER. OVEN WAS SWITCHED OFF FOR THE REMAINING OF THE FLIGHT WITH NO FURTHER PROBLEM. AISDR NOCA13906Frame · missingAFTER TAKEOFF RIGHT ENGINE EGT CLIMBED O 863 DEGREES CELCIUS. UPDATED (10/04/06) PERFORMED FIM TASK 71-03-00 FIG 116 AND NO FAULTS FOUND IN INSP, PERFORMED TEST NR 3 IP/HP COMPRESSOR AIRFLOW TEST. ACCOMPLISHED TEST NR 13 TAKEOFF POWER TEST AND NO ABNORMALITISDR DL777060661Start Valve · failedENGINE START VALVE L EICAS MSG DURING START, RTB. REPLACED NR 1 ENG START VALVE. OPS CHECK OK.SDR CA060801007Wire · burned(CAN) (FWD CARGO VENT FAULT) DISPLAYED ON ECAM. TROUBLESHOOTING IDENTIFIED BURNED WIRING UNDER FWD CARGO FLOOR, APPROX 2 IN FROM ELECTRICAL CONNECTOR 285HN-A ON FWD CARGO EXTRACTION FAN. BURNED WIRES WERE LOCATED BETWEEN SUPPORT STANDOFFS WITH NO EVIDENCE OF CSDR AALA20060288Engine · shutdownGRU - AT 8000 FEET LEFT ENGINE HAD AN UNCOMMANDED SHUTDOWN AFTER A STRONG BANG. RETURNED TO GRU AND LANDED WITHOUT INCIDENT. INSPECTED LEFT ENGINE INLET AND EXHAUST AND NO DAMAGE FOUND. DURING INSPECITONS FOUND SEVERAL METALIC DEBRIS ON EXHAUST. REPLACED NSDR CA060410005Limiter · malfunctioned(CAN) AT BEGINNING OF APPROACH, WHEN SELECTING SLATS/FLAPS DOWN, THE FLIGHT CONTROL FLAPS FAULT ECAM CAME ON. UNABLE TO EXTEND FLAPS FROM 0 POSITION. (REPEAT SNAG) DURING INVESTIGATION, FOUND THE LT TORQUE LIMITER AND THE LT ROTARY ACTUATOR TRIPPED. RESET CARRSDR CA060410002Limiter · tripped(CAN) AIRCRAFT ARRIVED WITH THE FLIGHT CONTROL FLAPS FAULT ECAM MESSAGE ON FINAL WHEN SELECTING FLAPS 2IN. UNABLE TO EXTEND FLAPS FROM THE 0 POSITION. DURING TROUBLE SHOOTING, FOUND THE LT FLAP TORQUE LIMITER TRIPPED. TORQUE LIMITER REPLACED AND SYSTEM CHECKEDSDR AALA20060201Engine · bird ingestionORD - LEFT HAND ENGINE EXPERIENCED BIRD STRIKE AND SURGED INFLIGHT. SHUT ENGINE DOWN PER CHECKLIST. LANDED ORD WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE. FOUND EVIDENCE OF BIRD STRIKE IN COMPRESSOR. ACCOMPLISHED BIRD STRIKE BOROSCOPE INSPECTION. NOSDR DL777060214Blade · damagedNR 2 ENG FAILED BOROSCOPE, INTERNAL BLADE DAMAGE. REPLACED ENGINE.SDR CA060405005Canister · brokenFOB 5100 KG WING CROSSFEED SELECTED ON AS PER ATB 376. FUEL IS 2500KG IN EACH TANK. NO FUEL IN OUTERS AND TRIM. ON SHORT FINAL "L TANK LOW FUEL" ON ECAMLTANK INDICATED 1200 KG AND RIGHT TANK 3500 KG REF SNAG 4205167. FOUND RT WING NR 1 MAIN BOOST PUMP CANNSDR DL777060120Valve · leakingAFTER T/O, LEFT ENG BLEED OFF EICAS MESSAGE. A/C RETURN TO ATL. MTC REPLACED HPSOV AND PNEU PRESSURE LINE FROM BRACKET DISCO, HPSOV NEED LEAK CHECK AND OP CHECK. PERFORMED LEAK CHECK, ENGINE AIR SUPPLY OP TEST PER MM 36-10-00-700-801. FOUND PNEUMATIC LINE SDR AMTA200600130Charger · unserviceableEMERGENCY POWER PACK AMBER CHARGE LIGHT DID NOT ILLUMINATE AFTER PERFORMING OPERATIONAL CHECK. REPLACED EMERGENCY POWER PACK IAW MM. OPS CHECK NORMAL. (K)SDR AMTA200600127Powerpack · out of adjustL1 DOOR OUTSIDE EMERGENCY EGRESS FLOODLIGHT COMES ON BUT EXTINGUISHES AFTER 30 SECONDS. PERFORMED EMERGENCY POWER PACK ADJUSTMENT AND TEST REF MM. OPS CHECK GOOD. (K)SDR AMTA200600128Light · malfunctionedL3 DOOR OUTSIDE EMERGENCY EGRESS FLOODLIGHT COMES ON MOMENTARILY THEN EXTINGUISHES. PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYSTEM IAW MM. OPS CHECK NORMAL. (K)SDR AMTA200600129Light · intermittentLT P4A DOOR OUTSIDE EMERGENCY EGRESS FLOODLIGHT COMES ON MOMENTARILY THEN EXTINGUISHES. PERFORMED OPS CHECK OF EMERGENCY LIGHTING SYSTEM IAW MM. OPS CHECK NORMAL. (K)
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