Rolls-Royce SPEY-555-15
Service difficulty reports · 261
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 = 'SPEY55515' 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 = 'SPEY55515' 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 AU001315Altimeter · out of adj(AUS) FIRST OFFICERS ALTIMETER OUT OF CALIBRATION. FOUND DURING COMPLIANCE WITH AD/RAD/68 AMDT2.SDR AU001316Actuator · faulty(AUS) RUDDER ACTUATOR ASSEMBLY FAULTY.SDR AU000900Transceiver · faulty(AUS) WEATHER RADAR TRANSCEIVER FAULTY.SDR AU001317Transceiver · faulty(AUS) WEATHER RADAR TRANSCEIVER FAULTY.SDR AU000901Duct · leaking(AUS) TAIL DUCT ASSEMBLY LEAKING.SDR AU000902Motor · leaking(AUS) FLAP HYDRAULIC MOTOR LEAKING. LOSS OF HYDRAULIC FLUID FROMUTILITY SYSTEM.SDR AU001318Actuator · leaking(AUS) FLAP HYDRAULIC MOTOR LEAKING. LOSS OF SYSTEM 1 HYDRAULIC FLUID.SDR AU001319Duct · leaking(AUS) TAIL DUCT ASSEMBLY LOCATED AFT OF THE REAR PRESSURE BULKHEADLEAKING.SDR AU000899Motor · leaking(AUS) FLAP HYDRAULIC MOTOR LEAKING. LOSS OF UTILITY HYDRAULIC SYSTEMFLUID.SDR AU001320Actuator · leaking(AUS) FLAP HYDRAULIC MOTOR LEAKING. LOSS OF UTILITY HYDRAULIC SYSTEM FLUID (SYSTEM 1).SDR AU000808Tire · separated(AUS) LT MAIN LANDING GEAR NR 2 TIRE TREAD SEPARATED. DAMAGE TO LT INBOARD FLAP LEADING EDGE AND FLAP VANE.SDR CA000926005Switch · malfunctioned(CAN) PILOTS RPTED OUTBOUND THAT CARGO DOOR WARNING LIGHT CAME ON AT 4.4 PSI DIFFERENTIAL. A/C RETURNED & LANDED W/O INCID..MAINT INSP FOUND WIRING ON REAR CARGO DOOR HANDLE SWITCH CHAFED & GROUNDING OUT ON WARNING CCT. WIRING REPD IN ACCORD WITH APPLICABLE STSDR AU000898Wire Rope · failed(AUS) NOSE WHEEL STEERING CABLE FAILED.SDR AU001321Control Cable · broken(AUS) NOSE WHEEL STEERING CABLE BROKEN.SDR AU001322Generator · failed(AUS) NR 2 GENERATOR DROPPED OFF LINE.SDR AU001295Fuel Control · faulty(AUS) NR 1 ENGINE THRUST AND N2 FLUCTUATING. TGT WARNING ILLUMINATED.SDR AU001292Radio · contaminated(AUS) FIRST OFFICERS RADIO SYSTEM CONTAMINATED WITH WATER. WINDOW HAD BEEN LEFT OPEN THE PREVIOUS NIGHT AND RAIN ENTERED THE COCKPIT.SDR CA000801004Harness · chafed(CAN) AFTER TAKEOFF CREW NOTED THAT LDG GEAR SELECTOR REMAINED RESTRICTED BY ANTI-RETRACTION PLUNGER,&LIFT- DUMPER SYS MAGNETIC INDS REMAINED BARBER POLED. CREW USED MANUAL OVERRIDE TO RETRACT LDG GEAR, HOWEVER, SINCE COMBINED DISCREPANCIES INDICATED GROUND/FSDR CA000905005Stop · loose(CAN) SHORTLY AFTER TAKEOFF AIRCRAFT REPORTED THE LEFT MAIN GEAR DOOR WOULD NOT CLOSE AFTER GEAR RETRACTION. THE GEAR WAS CYCLED SEVERAL TIMES WITH THE SAME RESULT. THE CREW ELECTED TO RETURN TO WITH THE GEAR DOWN SELECTION NORMAL - 5 GREEN LIGHTS AND BOTH MAISDR CA000905004Tire · failed(CAN) THE PILOT RPTED LT INBOARD MAIN WHEEL TIRE ASSY BLEW ON ROTATION & GEAR SAFE IND. LIGHT WENT OUT. MAINT CNTL TROUBLESHOT PROBLEM WITH FLT CREW BUT WERE UNABLE TO GET LEFT MAIN GEAR TO INDICATE DOWN AND LOCKED. DECISION MADE TO DIVERT WHERE EMERG LDG CARSDR CA000606011Switch · intermittent(CAN) PILOTS REPORTED THAT ON HEAD START DEPARTURE OUT OF YVR, THE NR 1 ENGINE FIRE DETECT SYSTEM WOULD NOT TEST. MAINTENANCE WAS CALLED OUT TO THE AIRCRAFT AND FOUND THAT THE PROBLEM TO BE THE TEST SWITCH. THEY SPRAY CLEANED THE SWITCH & IT TESTED SERVICEABLESDR CA000614014Actuator · contaminated(CAN) ON JUN 6/2000 MASTER FLT CAUTION LIGHT ILLUMINATED ALONG WITH BOTH UTILITY & FLT CNTL CHANNEL LIGHTS ON FLT CNTL PANEL AS REORTED BY CREW INBOUND ALT ELECTRIC SYS POPPED CCT BREAKER TWICE UPON ACTIVATION. CREW THEN PROCEEDED AS PER CHECK LIST WITH JAMMESDR AU001297Computer · faulty(AUS) GROUND PROXIMITY WARNING SYSTEM (GPWS) COMPUTER FAULTY.SDR CA000427007Blade · damaged(CAN) LPT 2 BLADE MISSING RR AND CAA AWARE OF THIS ON GOING ISSUE. AD 002-02-97 AND 008-08-97 APPLY. PROJECT THROUGH CORRECTIVE ACTION GROUP ON GOING.SDR CA000317003Gcu · failed(CAN) 3 MINS AFTER TAKEOFF PILOT REPORTED NAVIGATIONAL PROBLEMS AND RETURNED TO BLOCKS. NR 2 GEN FELL OFF LINE, THIS IS A RECURRING PROBLEM, NO 1 ADI TOPPLED. NR 1 VG REPLACED AND SERVICEABLE. NO 2 GEN PUT ON MEL THEM REPLACED, HED BEEN REPLACED TWO OTHER TIMESDR AU000189Duct · leaking(AUS) PRESSURISATION SYSTEM DUCT LEAKING.SDR CA000306007Gcu · burned out(CAN) PASSENGERS DEPLANED DUE TO HEAVY SMOKE SMELL EMANATING THROUGHOUT THE CIOCKPIT. FOUND COCKPIT GCU BURNED OUT, REPLACED. GCU CHECKED AND NOT AT FAULT AND REINSTALLED THREE DAYS LATER SAME PROBLEM. UNIT SENT TO MANUFACTURER FOR INVESTIGATION.SDR CA000110030Gcu · failed(CAN) PILOTS REPORTED DURING BOARDING PROCESS A HEAVY SMOKE SMELL FROM THE MAIN CB PANEL EMANATING THROUGHOUT THE COCKPIT. CREW UNABLE TO PINPOINT SOURCE. A/C SHUT DOWN AND PASSENGERS DEPLANED. REPLACED COCKPIT GCU AND AC BUS CONTACTOR.SDR CA991229053Gcu · failed(CAN) PILOT REPORTED THAT DURING THE BOARDING PROCESS. A HEAVY SMOKE SMELL FROM THE MAIN CABIN CB PANEL WAS EMANATING THROUGH THE COCKPIT. THE CREW WRE UNABLE TO PINPOINT THE SOURCE. THE AIRCARAFT WAS SHUTDOWN AND THE PASSENGERS WERE DEPLANED WITHOUT INCIDENTSDR CA000110029Turbine Wheel · failed(CAN) NR 2 LP TURBINE BLADE FAILURE. SEE PROJECT-CORRECTIVE ACTION 1999. CAA AWARE OF PROBLEMS AND R.R ESTABLISHED DIMENSIONAL MEASUREMENTS AS INDICATOR FORSUSPECT BLADE IRREGULARITIES THE EFFECTIVENESS OF THE TOOL IS UNDERSDR CA991229063Blade · failed(CAN) NR 2 LP TURBINE BLADE FAILURE. R/RSDR CA991209012Line · leaking(CAN) ON CLIMB, CREW NOTICED THAT THE FLIGHT CONTROL MASTER CAUTION LIGHT CAME ON AND THE NR 2 HYDRAULIC SYSTEM QUANTITY AND PRESSURE HAD DROPPED TO ZERO. ALL ASSOCIATED NR 2 SYSTEM CAUTION LIGHTS WERE NOW ON. AIRCRAFT RETURNED AND LANDED OK. PRESSURE LINESDR AU991087Blade · damaged(AUS) LEFT ENGINE SECOND STAGE LP TURBINE BLADES CONTAIN IMPACT MARKS ON THE TRAILING EDGES. FINE SLIVERS OF METAL IN THE TAILPIPE. THE ENGINE WAS ALSO USING EXCESSIVE OIL.SDR AU991076Fitting · broken(AU) LEFT MAIN LANDING GEAR UPPER TORQUE LINK FITTING PIVOT PIN BOSS FAILED. THE FAILURE WAS DIAGONAL FROM THE REAR OF THE INBOARD SIDE OF THE BOSS TO THE FRONT OF THE OUTBOARD SIDE. THE BREAK TRAVERSED THROUGH THE PIVOT PIN LOCATING HOLE.SDR CA991008004Blade · bent(CAN) LP1 AND LP2 TURBINE BLADE FAILED.SDR AU990889Shaft · corroded(AUS) RUDDER POST CORRODED IN AREA OF LOWER BUSHING.SDR CA990915044Actuator · failed(CAN) AIRCRAFT HAD TURNBACK DUE TO LOSS OF HYDRAULIC FLUID. LANDING GEAR DOOR ACTUATOR REPLACED.SDR CA990927037Pump · leaking(CAN) FUEL LINE FROM HP FUEL PUMP TO FFR BLEW 0FF.SDR AU990830Turbine Blade · separated(AUS) LEFT ENGINE LOW PRESSURE TURBINE BLADE SEPARATED. REMAINING BLADES AND GUIDE VANES DAMAGED.SDR CA990817023Blade · failed(CAN) LP TURBINE BLADE FAILURE (1). TEAR-DOWN REPORT TO FOLLOW AS SPECIFIED.SDR CA990804011Nlg · sheared(CAN) AIRCRAFT SLID 200 FEET PAST END OF RUNWAY SHEARING OFF NLG AND DAMAGING LT WING LEADING EDGE WHEN IN CONTACT WITH LIGHT STANDARD. MORE TO FOLLOW.SDR AU990916Stringer · corroded(AUS) STRINGER 58 DIMPLED LAP JOINT LOCATED IN THE RIGHT REAR FUSELAGE SKIN BETWEEN FS 16495 AND FS 17845 CORRODED.SDR CA990728037Blade · broken(CAN) FAILURE OF FIRST STAGE COMPRESSOR BLADE, TEAR DOWN REPORT TO FOLLOW.SDR CA990728036Compressor · failed(CAN) LP 2 COMPRESSOR FAILURE, TEAR-DOWN REPORT TO FOLLOW.SDR AU990915Angle · corroded(AUS) LEFT COCKPIT WINDOW LOWER ATTACHMENT ANGLE CORRODED.SDR AU990917Beam · corroded(AUS) FUSELAGE MAIN KEEL BEAM CORRODED AT LEFT FUSELAGE FRAME 13345.SDR AU990918Bracket · corroded(AUS) HORIZONTAL STABILIZER ACTUATOR MOUNT BRACKETS CORRODED.SDR AU990919Bracket · corroded(AUS) RIGHT AILERON CONTROL UNIT LOWER MOUNT BRACKET CORRODED.SDR CA990505004Duct · failed(CAN) IN CLIMB, NR 2 ENG REQD 5 PERCENT HIGHER RPM TO MAINTAIN SAME THRUST AS NR 1 ENG. ON LEVELING OFF, CREW DECIDED TO TREND BOTH ENGS TO ASSIST MAINT IN T/S OF LOWER POWER PROBLEM. 100 MILES OUT, A THUD FOLLOWED BY A CONTINUOUS SHUDDER FELT ACCOMPANIED BYSDR AU990693Bleed Valve · faulty(AUS) MAIN AIR BLEED VALVES FAULTY.
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