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 CA970620018Cap · corrosion(CAN) HEAVY CORROSION ON LOWER CAP BULKHEAD 983 BETWEEN STR 30-34. REPAIRED.SDR CA970602009Vibration Monito · faulty(CAN) #2 ENGINE WAS SHUTDOWN DURING CLIMB DUE TO HIGH VIBRATION INDICATION. POST FLIGHT INSPECTIONS AS PER THE MAINTENANCE MANUAL FOUND NO FAULT. FOLLOWING GROUND RUNUP AND FURTHER INVESTIGATION THE VIBRATION MONITOR WAS FOUND FAULTY. THE VIBRATION MONITOR WASSDR CA970513020Duct · broken(CAN) DURING TAKEOFF THE HIGH PRESSURE AIR DUCT BLEW. DUCT COMPENSATOR BLEW CAUSING DAMAGE TO SEVERAL OTHER DUCTS. AIRCRAFT RETURNED TO MAINTENANCE BASE FOR REPAIR. COMPENSATOR AND OTHER DUCTS AND BRACKETS REPAIRED OR REPLACED.SDR CA970526007Engine · making metal(CAN) #1 ENGINE SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE AND FALLING OIL QUANTITY. POST FLIGHT INSPECTION FOUND METAL DEBRIS ON CHIP DETECTORS IN THE SCAVENGE SYSTEM AND THE GEARBOX, ALSO METAL FOUND IN THE SCAVENGE FILTER. THE ENGINE WAS REPLACED AS PER THESDR CA970409010Pin · broken(CAN) RH MAIN LANDING GEAR TRUCK BEAM LIGHT CAME ON AFTER TAKEOFF. AFTER LANDING RH MLG TRUCK POSITION PIN FOUND BROKEN, REPLACED.SDR CA970319009Skin · cracked(CAN) LOWER FUSELAGE SKIN CRACKED APPROXIMATELY 5 INCHES LONG AT R/H SIDE STRINGER 31 FUSELAGE STATION 1368, PRESSURIZED AREA. OPPOSITE SIDE ALSO CRACKED. SKIN CORROSION DUE TO WASTE WATER TRAPPED IS PROBABLE CAUSE. REPAIRED.SDR CA970319010Spoiler · damaged(CAN) L/H SPOILER #2 DAMAGED AT ACTUATOR ATTACHMENT AND THE SPOILER PANEL WAS ALSO DAMAGED BY CONTACT WITH SUROUNDING STRUCTURE.SDR CA970314007Actuator · req adjustment(CAN) ON TAKEOFF SLAT AMBER LIGHT CAME ON AND #1 RH GREEN LOCK LIGHT WENT OUT FOLLOWED BY THE UNSAFE TAKEOFF WARNING HORN. TAKEOFF REJECTED. #1 SLAT ACTUATOR ADJUSTED.SDR CA970314006Pdu · malfunction(CAN) APPROACH SLATS DID NOT EXTEND WHEN SELECTED. NO SLAT LANDING CARRIED OUT. AFTER SEVERAL ATTEMPTS ON GROUND SLATS CAME OUT WHEN SELECTED BUT LOCKED IN THE EXTENDED POSITION. REPLACED PDU, TORQUE LIMITER AND #6 AND #7 RH ACTUATORS.SDR CA970306009Actuator · tripped(CAN) ON APPROACH NO SLATS ON SELECTION, NO SLAT LANDING. 'A' AND 'C' SYSTEM FILTERS CLEANED. FOUND #3 AND #7 ACTUATORS TRIPPED, REPLACED.SDR TWAA9710001Gearbox · failedSTL - FLT 442 - DURING CRUISE, THE NR 2 ENGINE SHUTDOWN DUE TO GEARBOX FAILURE. GEARBOX MFG P/N A01026, MANUFACTURED BY ROLLS ROYCE, LTD. REMOVED AND REPLACED THE GEARBOX. OPERATIONAL CHECKS NORMAL. (M)SDR CA970310007Jury Brace · cracked(CAN) RIGHT HAND MAIN LANDING GEAR UPPER JURY BRACE CRACKED. REPLACED.SDR CA970219017Gearbox · making metalACESSORY GEAR BOX MAKING METALSDR CA970306010Actuator · tripped(CAN) SLATS DID NOT EXTEND WHEN SELECTED. FOUND #6 ACTUATOR TRIPPED. REPLACED #6 SLAT ACTUATOR.SDR CA970306011Switch · intermittent(CAN) ON APPROACH WHEN FLAPS SELECTED SLATS DID NOT EXTEND. REPLACED SLAT POSITION INDICATION SWITCH.SDR CA970206019Fan · seized(CAN) NO N1 ROTATION DURING START OF #3 ENGINE. LP FAN FOUND SEIZED. ENGINE REPLACED.SDR CA970203014Thermal Strips · fused(CAN) IN CRUISE CREW REPORTED SMOKE FROM COFFEE MAKERS GALLEY L3 POSITION FOUND OUTBOARD COFFEE MAKER CIRCUIT BREAKER POPPED AND PULLED INBOARD CIRCUIT BREAKER NO FURTHER SMOKE AN OVERHEAT CONDITION OF THE OUTBOARD COFFEE MAKER THERMAL STRIPS DE FUSED AND A WSDR CA970117005Line Assembly · chafed(CAN) 'A' SYSTEM HYDRAULIC FLUID DEPLETED TO LOW QUANTITY LIGHT. PUMPS OFF AT HALF TANK. FLUID CONTINUED TO DECREASE. LINE AT HORIZONTAL STABILIZER AREA FOR TAIL SKID ACTUATOR LEAKING. CHAFED AT LIGHTENING HOLE. REPAIRED.SDR DLL10962727Engine · fireNR 1 ENG TAILPIPE FIRE ON START. GROUND CREW FIRED HALON INTO TAILPIPE. TAILPIPE FIRE/ENGINE RUNDOWN CHECKLIST COMPLIED WITH. ENGINE WAS INSPECTED PER M/M AND RETURNED TO SERVICE.SDR CA961126006Regulator Valve · failed(CAN) AFTER SELECTING GEAR DOWN LOST ALL 'C' SYSTEM HYDRAULIC FLUID. LANDING GEAR CONTROL MODULE CARTRIDGE REPLACED.SDR CA961120005Amplifier · faulty(CAN) TAKEOFF REJECTED DUE TO LOW EPR ON #3 ENGINE. THE FUEL CONTROL AMPLIFIER SWITCH OVERRODE TO RESTORE POWER. THE FUEL CONTROL AMPLIFIER WAS REPLACED WHEN THE AIRCRAFT RETURNED TO BASE.SDR CA961113007Engine · failed(CAN) ON APPROACH AT 700 FEET THE #2 ENGINE FAILED. AIRCRAFT LANDED AND PASSENGERS DEPLANED SAFELY. ENGINE FIRE BOTTLES FIRED AS A PRECAUTIONARY MEASURE. INVESTIGATION REVEALED METAL IN THE TAILPIPE. MAGNETIC CHIP DETECTOR VERIFIED NO METAL FLAKES.SDR CA961021015Hinges · cracked(CAN) FLIGHT DECK ESCAPE HATCH HINGES CRACKED, REPLACED.SDR CA961007021Clamp · broken(CAN) ON WALKAROUND FOUND 2 GAS GENERATOR FAIRINGS MISSING FROM #3 ENGINE. HP SHUT-OFF VALVE LOWER CLAMP BROKEN IN TWO PIECES AND HP PNEUMATIC PRESSURE FORCED TWO FAIRINGS TO SEPARATE. REPLACED.SDR CA960909040Fitting · broken(CAN) #2 LH SPOILER ATTACH FITTING BROKEN IN HALF, REPLACED.SDR DLL13961973Oil Pump · leakingSMOKE IN CABIN, ISOLATED PACKS, FOUND PROBLM TO BE IN NR 3 ISO VLV. ALL PACK TEMPS NORMAL, CONTINUED WITH ALL PACKS AND NR 3 ISO VLV UNLATCHED. REPLACED NR 3 ENGINE OIL PUMP, OPS CHECK GOOD.SDR CA960909036Fuel Line · punctured(CAN) FUEL LEAK AT #2 ENGINE. RIGID FUEL TUBE PUNCTURED BEHIND CLAMP AT REAR SECTION BETWEEN FS 1975 AND 1860 OVER WL200. LINE REPLACED.SDR CA960808010Duct · blown open(CAN) TAKEOFF REJECTED DUE TO AFT FUSELAGE SECTION OVERHEAT AND UNSAFE TAKEOFF WARNING ON FLIGHT ENGINEER ANNUNCIATOR PANEL. CONTROL TOWER ADVISED OF SMOKE/FUMES COMING FROM AIRCRAFT AFT SECTION. BOTH #2 ENGINE FIRE BOTTLES DISCHARGED AND TAKEOFF REJECTED. FOUSDR CA960715007Generator · faulty(CAN) TWO HOURS AFTER TAKEOFF #1 ENGINE IDG LOW PRESSURE LIGHT CAME ON. GENERATOR VOLTAGE AND FREQUENCY WENT TO ZERO. POST FLIGHT MAINTENANCE CHECK FOUND IDG OVERHEATED. IDG AND OIL COOLER REPLACED.SDR DLL10961512Oil Pump Packing · failedFLT ATTENDENTS REPORTED SMOKE AND HAZE IN CABIN ON APPROACH. AFT LAV SMOKE DET WENT OFF. REPLACED OIL PUMP PACKING, CKS GOOD.SDR CA960703023Pitot Tube · cracked(CAN) REJECT TAKEOFF AT 80 KNOTS DUE TO NO AIRSPEED INDICATION ON CAPTAIN'S SIDE. PITOT TUBE REPLACED.SDR CA960703026Video Control · shorted(CAN) WHILE ENROUTE VIDEO CONTROL UNIT IN AFT STORAGE COMPARTMENT SMOKING BADLY. ALL CBS PULLED AND SYSTEM DEACTIVATED. FLIGHT CONTINUED. UNIT REPLACED.SDR CA960614009Actuator · out of adjust(CAN)REJECTED TAKEOFF DUE TO #3 ENGINE N2 OVERSPEED. IP COMPRESSOR MASTER RAM OUT OF ADJUSTMENT, ADJUSTED IN ACCORDANCE WITH MAINTENANCE MANUAL.SDR CA960610012Motor Assy · leaking(CAN) HYDRAULIC SHUTOFF VALVE AND MOTOR ASSEMBLY IS USED AS A FUSE FOR "A" SYSTEM RUDDER SYSTEM. FOR UNKNOWN REASON MOTOR HAS BEEN SPLIT FROM THE VALVE, CAUSING HYDRAULIC LEAK AND LOSS OF "A" SYSTEM FLUID. HAPPENED ON LANDING. REPLACED.SDR CA960502058Engine · vibration(CAN)#3 ENGINE SHUTDOWN DUE TO VIBRATION ON BOTH CHANNELS DURING CRUISE. NO FAULT FOUND BY MAINTENANCE, LP COMPRESSOR CLEANED, SURVEY TEST 11 FOUND WITHIN LIMITS.SDR CA960415013Air Motor · seized(CAN)DURING LANDING AFTER THRUST REVERSER OPERATION, #1 THRUST REVERSER JAMMED IN THE DEPLOY POSITION. UPPER RH COWL TRANSLATING ROD BENT AND CRACKED. #1 SCREW JACK BENT. BOTH DRIVE CABLES SHEARED AT AIR MOTOR AND MOTOR SEIZED. PARTS REPLACED.SDR DLL10960497Chip Detector · leakingNR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED - GAUGE SHOWED LOW OIL QUANTITY. ENGINE NR 1 SHUT DOWN IAW POM AND EMERG PROCEDURES ON FINAL APPROACH. N3 WENT TO ZERO. FOUND EVIDENCE OF LEAKING AT MASTER CHIP DETECTOR HOUSING. REPLACED FINE SCAVANGE FILTER.SDR DLL10960495Scavenge Pump · failedDURING CRUISE HAD STRONG ENGINE EXHAUST TYPE ODOR. PERFORMED INSPECTION OF ENGINES, FOUND NR 2 ENGINE OIL SCAVENGE PUMP FAULTY. REPLACED PUMP AND PERFORMED DUCT BURNOUT.SDR CA960311035Engine · making metal(CAN) DURING CLIMB, VIBRATION INCREASED STEADILY. ENGINE SHUT DOWN AND AIRCRAFT RETURNED TO AIRPORT. FOUND HEAVY METAL CONTAMINATION FROM LOCATION BEARINGS (MAGNETIC CHIP DETECTOR). #2 ENGINE REPLACED AND CHECKED SERVICEABLE.SDR 96ZZZX1752Engine · vibrationON RIA FERRY FLT 7104 - KMKE/DTW - A/C RETURNED TO KMKE AFTER EXPERIENCING VIBRATION (4.0 A AND B) ON NR 2 ENGINE AT ABOUT 4,000 FEET. REDUCING POWER REDUCED VIBRATION TO 1.0. UPON LANDING, INSPECTED CHIP DETECTORS AND OIL FILTERS, FAN BLADES, NO DAMAGE FOUNSDR CA960202020Hose · ruptured(CAN)'C' SYSTEM LOST DURING FLIGHT. 'C' SYSTEM PUMP PRESSURE HOSE CAME APART AT ELBOW AT THE PRESSURE MODULE. REPLACED.SDR 96ZZZX925Engine · failedSFO/HNL - FLT 1113 - DURING CRUISE, NR 1 ENGINE WAS SHUT DOWN AT 1726, AIRCRAFT DUMPED FUEL, AND RETURNED TO SFO DUE TO HIGH VIB'S, BOTH CHANNELS. UPON LANDING AT SFO, FOUND METAL ON ALL 3 CHIP DETECTORS. AIRCRAFT FERRIED TO MIA ON TWO ENGINES ON 1-20-96 FORSDR CA960123020Liner · delaminated(CAN) ON DEPARTURE, NR 1 ENGINE SUFFERED A COMPRESSOR STALL, TAKEOFF WAS REJECTED. POST INSPECTION FOUND NR 1 ENGINE LP COMPRESSOR CASE ACOUSTIC LINER DELAMINATED AND STUCK ON BYPASS DUCT VANE. DEBRIS REMOVED ON THE GROUND. ENGINE GROUND RUN, NO VIBRATIONS,SDR CA960205013Controller · failed(CAN)DURING CRUISE #1 & #3 GENERATORS DROPPED OFF LINE. #2 GENERATOR INDICATED LOW FREQUENCY. #1 LOAD FREQUENCY CONTROLLER AND GENERATOR CONTROL UNIT REPLACED. #3 GENERATOR CONTROL UNIT REPLACED.SDR CA960115016Actuator · faulty(CAN)WHEN #3 THROTTLE WAS ADVANCED THE ENGINE SPOOLED DOWN AND THE ENGINE WAS SHUTDOWN. THE AIRCRAFT RETURNED TO THE RAMP AND MAINTENANCE FOUND THE MASTER AND SLAVE RAM ACTUATORS NOT WORKING PROPERLY. BOTH ACTUATORS WERE REPLACED AND THE AIRCRAFT RETURNED TO SSDR CA960122024Actuator · faulty(CAN)WHEN #3 ENGINE THROTTLE WAS ADVANCED THE ENGINE SPOOLED DOWN AND THE ENGINE WAS SHUTDOWN. THE AIRCRAFT RETURNED TO THE RAMP AND MAINTENANCE FOUND THE MASTER AND SLAVE RAM ACTUATORS NOT WORKING PROPERLY. BOTH ACTUATORS WERE REPLACED AN D THE AIRCRAFT RETSDR CA960126037Fairing Panel · damaged(CAN)ON ARRIVAL #3 ENGINE GAS GENERATOR PANEL (FAIRING) WAS FOUND DAMAGED DURING REVERSE. DAMAGE WAS EVALUATED AND PANEL WAS REPLACED. #3 ENGINE REVERSER LOCKED-OUT & AIRCRAFT DISPATCHED AS PER MM 78-03 & MEL 79-31-00.SDR CA951122030Fan Blades · fod ice damage(CAN)TAKEOFF REJECTED DUE TO ENGINE PARAMETERS BELOW REQUIREMENTS. HIGH N1 AND LOW EPR. DURING RUN-UP PARAMETERS WERE FOUND NORMAL AT LOW POWER SETTINGS. CREW DID NOT BRING TO HIGHER POWER DUE TO HEAVY ENG INE RUMBLE HEARD IN THE COCKPIT. DURING VISUAL INSPECTSDR DLL10954341Engine · oil leakSMOKE IN CABIN, ALL SMOKE ALARMS WENT OFF. THE NR 3 ISOL VLV UNLATCHED SEEMED TO HELP SOME, BUT NOT COMPLETELY. FWD TO MCO PER MEL 36-11-18. SUBSEQUENTLY NR 3 ENGINE WAS REMOVED AND ROUTED TO SHOP FOR OIL LEAK IN COMPRESSOR.SDR CA951102008Pin · migrated(CAN)ON ROUTINE INSPECTION OF #3 ENGINE LOW PRESSURE COMPRESSOR SUPPORT STRUCTURE, THE LEFT HAND LOWER ROD END LUG PIN WAS FOUND MIGRATED BY 2.0" AND THE RETAINING BOLT MISSING. THE RETAINING BOLT HAD BEEN FITTED AS WITNESS MARKS OF BOLT WERE IDENTIFIED ON TWO
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