Rolls-Royce RB211-524B402
Service difficulty reports · 102
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 = 'RB211524B402' 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 = 'RB211524B402' 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 1LSM2010LVS01Actuator · stickingSHORTLY AFTER ROTATION ON TAKEOFF, NR 1 ENGINE COMPRESSOR STALLED & SURGED, TOWER REPORTED SEEING FLAMES FROM TAIL PIPE. ENGINE SHUTDOWN, SECURED & FIRE BOTTLE DISCHARGED AS A PRECAUTION. ACFT RETURNED TO FIELD & LANDED WITHOUT INCIDENT. ENGINE INSPECTED FOSDR ARWA20040103Liner · damagedENGINE NR 3 EXPERIENCED A SLOW INCREASE IN VIBRATION FROM 105 TO 218 UNITS IN 3 MINUTES WITH A OR B SELECTED. ALL OTHER PARAMETERS NORMAL. INSPECT MASTER AND INTERNAL GEARBOX CHIP DETECTORS AND OIL FILTERS, NO EVIDENCE OF ENGINE FAILURE NOTED. ACOMPLISHED BORSDR ARWA20030706Compressor · damagedLOG PAGE 23902 NR 3 ENGINE VIBRATION 4 UNITS BOTH A & B CHANNELS IN NORMAL POSITION NR 3 ENGINE SHUTDOWN AT 1340 Z. INSPECTED NR 3 ENGINE; FOUND METAL ON EXHAUST TAIL PIPE; BOROSCOPED ENGINE, FOUND DISCREPANCIES ON HIGH PRESSURE COMPRESSOR OUT OF LIMITS AND SDR CA030704001Line · ruptured(CAN) DURING CLIMB-OUT, A COMPLETE (RAPID) LOSS OFB HYD SYS OCCUR. THE AIRCRAFT RETURNED TO THE STATION WITH NO FURTHER PROBLEM. DURING INVESTIGATION THE (B PRESSURE LINE) TO THE FILTER MODULE, LOCATED IN THE HYDRAULIC SERVICE CENTER WAS FOUND RUPTURED. TSDR ARWA20030601Engine · vibrationABORTED TAKE OFF AT 130 KTS 470,000 LBS DUE TO NR 3 ENGINE VIBRATION WARNING AT 2.8 UNITS. BRAKES OK, TIRES OK. RETURNED TO RAMP. LUBED FAN BLADES, PERFORMED INSPECTION IAW L1011 MM 71-91-00. ALL PARAMETTERS WITHIN LIMITS ON RUN UP NR 3 ENGINE.SDR CA030428003Oil Cap · leaking(CAN) DURING ENGINE START NR 3 ENGINE OIL CAP WAS LEAKING FROM THE CENTER. OIL CAP WAS REPLACED AND SYSTEM CHECKED SERVICEABLE.SDR CA030317003Electrical Box · burned(CAN) FLIGHT CREW REPORTED BURNING ODOR IN CABIN BETWEEN ROW 22 AND 28.MAINTENANCE FOUND THE SEAT ELECTRONIC BOX (SEB) AT FAULT. UNIT WAS REPLACED AND SYSTEM TESTED RERVICEABLE.SDR CA030304001Landing Gear · malfunctioned(CAN) AFTER GEAR SELECTED DOWN , THE INTRANSIT LIGHT WAS ON, ALL OTHER GEARS AND DOORS LIGHT WERE OFF. GEARS DID NOT EXTEND. ALTERNATE GEAR EXTENSION PROCEDURE PERFORMED AND GEARS EXTENDED NORMALY. TROUBLE SHOOTING UNDERWAY.SDR CA030228005Fan · seized(CAN) TROUBLE SHOOTING WAS CARRIED OUT BY MAINTENANCE ON ALL CABIN INTERIOR ELECTRICAL SYSTEMS. UNABLE TO DUPLICATE. ALL CABIN SYSTEMS CHECKED SERVICEABLE AS IAW MAINTENANCE MANUAL. DURING ROUTINE INSPECTION,FOUND MID GALLEY EXHAUST FAN INOPERATIVE (SEIZED)SDR ARWA20030104Engine · vibrationNR 3 ENGINE VIBRATION DURING CRUISE AT 350 FT LOW POSITION A-B 2.8 CAUTION LIGHT ON. SHUTDOWN ENGINE AT 06:35 Z. REMOVE AND REPLACE ALL NR 3 ENGINE C-1 BLADES IAW MM 72-31-01. REMOVED AND REPLACED VIBRATION MONITOR IAW MM 77-31-00. COMPLETED TRIM BALANCE CHSDR ARWA20030103Blade · damagedNR 3 ENGINE AT 370 FEET, BOTH CHANNEL A AND B 2.7 CAUTION LIGHT ON. SHUTDOWN ENGINE 1200Z. FEELING THE VIBRATION ON THE FLOOR. REMOVED AND INSPECTED MASTER AND INTERNAL GEAR-BOX MAGNETIC CHIP DETECTOR AND OIL FILTERS IAW MM. NO EVIDENCE OF INTERNAL FAILUSDR CA030130005Engine · vibration(CAN) DURING TAKE OFF, CREW REPORTED NR 1 ENG HIGH VIBRATION, VIBRATION REACHED 5 UNITS ON BOTH CHANNELS. THE ENGINE WAS SHUTDOWN AS PER QRH. ESN 14858 HAD SHOWN AN INCREASE IN N1 VIBRATION TREND IN THE 2 WEEKS PREVIOUS TO THE EVENT AND A FAN CLEAN AND RELUBRISDR CA030113004Tube · cracked(CAN) HYDRAULIC LEAK RT SIDE FLAP WELL NEAR NR 1 SPOILER ACTUATOR. SPOILER NR 1 PRESSURE HYDRAULIC TUBE, SYSTEM B REPAIRED PER AMM 20-29-02, P801.SDR CA030113013Engine · vibration(CAN) UPON DEPARTURE OF FLIGHT 703 FROM VRA-YMX, TAKE OFF WAS REJECTED DUE TO NR 3 ENGINE VIBRATION LIGHT CAME ON. DURING TAKE OFF, VIBRATION WAS CONFIRMED ON BOTH CHANNELS. CHECK LIST CARRIED OUT AT 60 KNOTS. TEST 11 CARRIED OUT IAW AMM 71-00-00. VIBRATION LSDR CA021227003Rod End · sheared(CAN) DURING FLIGHT FROM, FLIGHT CREW REPORTED THAT, RUDDER HYD LIMITER ANNUNCIATOR AND RUDDER LIMITER HYDRAULIC PUSH LIGHTS ON, FLAPS 4 DEGREES, AIRSPEED 190 KNOTS.PUSH LIGHT GOES OUT WITH FLAPS SELECTED UP AND AIR SPEED 210 KTS (WHICH IS NORMAL).UPON TROUBLESDR CA030113012Fuel Tank · contaminatedTANK 2R INBD, QTY HIGHER THAN NORMAL WITH QTY SWITCH LIGHT LATCHED IN. FUEL QTY GAUGES OK. INBD QTY READS 4000 LBS, WITH TOTAL BELOW 7000LBS. PER FAULT ISOLATION AMM 28-27-00 P 107, REPLACED BOOST PUMP CHECK VALVES PER AMM 28-24-03 (NIL FIX). FUEL WAS STILSDR CA021223006Proximity Sensor · failed(CAN) A/C ABORTED TAKE OFF AND RETURNED TO THE GATE DUE TO UNSAFE TAKE OFF WARNING RT SLAT NR 3 GREEN LIGHT 'OFF', ON THE FLIGHT ENGINEER PANEL AND LEADING EDGE SLAT GREEN LIGHT 'ON'. MTCE REPLACED THE SLAT POSITION PROXIMITY SWITCH SENSOR FOR THE RT SLAT NR SDR CA030112010Sensor · failed(CAN) AT 5:45 HRS LOCAL , FLIGHT 044, REJECTED T/O AT 90 KNOTS, DUE TO UNSAFE T/O WARNING HORN RELATED TO SLAT MALFUNCTION. THE PROXIMITY CARD A12 (P/N 805006, S/N 53) WAS REPLACED PER AMM 31-22-02 AND UNSAFE T/O WARNING TEST PARA. CITEM 1,2,3 C/OUT PER AMM 3SDR CA030112003Skin · damaged(CAN) DURING WALK AROUND IN YYZ, MTCE FOUND THE LT STABILIZER TRAILING EDGE TIP SKIN DAMAGED. A REPAIR WAS CARRIED OUT IAW SRM 55-22-00. LOOSE RIVITS REPLACED IAW 51-40-01.SDR CA030112007Duct · separated(CAN) A DEPRESSURIZATION OCCURRED AT 21000 , ABNORMAL PROCEDURE CARRIED PER QRH. LOUD NOISE HEARD IN FLIGHT DECK DURING APPROACH. FOUND NR 2 WATER SEPARATOR DUCT SEPARATED FROM WATER SEPARATOR. FURTHER INSPECTION REVEALED A LARGE CRACK ON THE INLET FLANGE OF TSDR CA021117001Duct · chafed(CAN) IN HANGAR, AT ENGINE INSTALLATION DURING RE CONNECTION OF THE INTERMEDIATE PRESSURE, (IP) DUCT INSIDE THE PYLON NR 3 AREA IT WAS NOTICED THAT THE FLEXIBLE SECTION OF THE PIPE SECTION FOR THE ANTI-ICE TAP-OFF OF THE IP DUCT WAS CHAFED THROUGH. DAMAGE OCCSDR CA021001013Hose · cracked(CAN) THE 'MEDIUM PRESSURE OXYGEN HOSE ASSY AT THE OXYGEN CYLINDER HOOKUP PANEL, WAS FOUND TO DAMAGED. THIS FLEXIBLE BRAID LINE WAS FRAYED AT THE PANEL CONNECTION AND THE FLEXIBLE LINE INSIDE WAS CRACKED.9 OF THOSE LINES WERE ORDERED AOG. ALSO, FOR PRECAUTIOSDR CA020912004Blocker Door · bent(CAN) ENGINE NR 3, BLOCKER DOOR AT 5 O`CLOCK POSITION BENT ACROSS ITS WIDTH. MAINTENANCE REPLACED THE BLOCKER DOOR PER AMM 78-31-16SDR CA020912001Wire Harness · chafed(CAN) NR 2 PACK RAM AIR LOUVER WILL NOT POSITION PROPERLY ON GROUND, IN FLIGHT IT STAYS AT ONE O`CLOCK POSITION. C/B TRIPPED WHEN PACK NR 2 IS OPERATED IN MANUAL. NR 2 PACK CONTROLLER INOP IN AUTO AND MANUAL. FOUND NO CONTINUITY BETWEEN RAM AIR ACTUATOR LSDR CA020829015Engine · vibration(CAN) AFTER TAKE OFF, THE NR 3 THROTTLE WAS RETARDED, THE ENGINE WAS SHUT DOWN DUE TO HIGH VIBRATIONS (2.5 2.7 UNITS) , CHANNEL A&B FROM LOW CHANNEL. THE AIRCRAFT RETURNED TO BASE (YYZ). MAINTENANCE C/OUT A BOROSCOPE AND THE FINDINGS WERE, HP COMPRESSOR STAGSDR CA020829016Blocker Door · bent(CAN) FOUND NR 1 ENGINE THRUST REVERSER BLOCKER DOOR AT THE 8 O`CLOCK POSITION, DAMAGED AND THE TRANSLATING SLEEVE NOT CLOSED PROPERLY (GAP TO LARGE). MAINTENANCE REPLACED THE BLOCKER DOOR I.A.W. AMM 78-31-16 AND THE TRANSLATING COWL RIGGED I.A.W. 78-30-00 SDR CA020912002Wire Harness · damaged(CAN) APU FAILS TO START, NO ROTATION. AIRCRAFT RELEASED PER MEL 49-00-01. BLEED AIR VALVE CONFIRMED CLOSED. CHECKED CURRENT LIMITER AND FOUND SERVICEABLE. RERACKED ECU, NO FIX. AIRCRAFT REQUIRED TO HAVE A JET START AND GPU AT ALL STATIONS. FURTHER TROUBLE SDR CA020820009Tube · cracked(CAN) CREW REPORTED AFT CABIN BURNING ODOR WITH WHITE SMOKE NEAR AFT GALLEY LT CABIN DOOR AREA. THE AFT GALLEY POWER WAS TURNED OFF IN FLIGHT BY CREW AND THE SITUATION WAS BACK TO NORMAL. UPON ARRIVAL, AFT GALLEY CHILLER WAS REPLACED. THE EVAPORATOR WAS RSDR CA020820010Manifold · cracked(CAN) DURING NORMAL MAINTENANCE OPERATION, THE MAIN LANDING GEAR CONTROL MODULE IN THE HYDRAULIC SERVICE CENTER, WAS FOUND LEAKING BECAUSE THE MAIN LANDING GEAR CONTROL MODULE MANIFOLD WAS CRACKED. MAINTENANCE REPLACED THE MLGCM IAW THE AMM 32-31-01SDR CA020829017Controller · failed(CAN) THE AIRCRAFT WAS FLYING AND DIVERTED DUE TO NR 2 PACK UNABLE TO CONTROL IN MANUAL MODE WHILE THE AUTO MODE WAS UNDER MEL 21-21-01 CATC. MAINTENANCE REPLACED THE PACK CONTROLLER IAW AMM 21-62-01SDR CA020816003Fairing · missing(CAN) UPON ARRIVAL, THE CREW NOTICED THAT THE C2 CARGO DOOR FAIRING ASSY. WAS MISSING. FURTHER INVESTIGATION REVEALED THAT C2 CARGO PANEL ASSY DOOR FAIRING , TOP AFT FAIRING CUT OUT PANEL CRACKED 1 INCH LONG AND PART OF AFT LIP IS MISSING. MAINTENANCE REPLASDR CA020816001Sensor · missing(CAN) LEFT ALPHA AIR DATA SENSOR HEAT OFF LEGEND CAME ON IN FLIGHT. ON ARRIVAL IT WAS FOUND THAT THE AOA VANE WAS MISSING. AN INSPECTION OF THE WING AND STABILIZERS WAS C/O, NO DAMAGED WAS FOUND. THE AOA SENSOR WAS REPLACED, AND TESTED SERVICEABLE. AIRCRAFT WASDR CA020708003Module · cracked(CAN) AIRCRAFT(IN MANCHESTER) RETURNED TO RAMP DUE TO B HYD SYSTEM LEAK FROM LT BRAKE MODULE. MAINTENANCE DISCOVERED THAT THE UNIT WAS CRACKED 2.5 INCHES JUST OVER SYSTEM B BRAKE RETURN PORT LT AND REPLACED THE UNIT IAW AMM 32-44-01.SDR CA020705005Signal Cond Unit · malfunctioned(CAN) IN CLIMB, EPR 1.515, ENG NR 2 , VIBRATION CONFIRMED ON BOTH CHANNELS, 4.2 INDICATED, CAUSED IN-FLT SHUTDOWN. -ALL MCD INSP & NO CONTAMINATION FOUND PER AMM 72-01-00- VISUAL INSP OF AIR INTAKE , LP COMPRESSOR & EXHAUST COLLECTOR C/OUT & NO FOD OR DEBRIS FSDR CA020705004Decoder · failed(CAN) WHILE PERFORMING READING LIGHT TEST, BURNING ODOR COMING FROM AREA AROUND SEAT ROWS 26 ABC TO 30 ABC NOTICED. ALL READING LIGHTS WERE WORKING AT TIME & SMELL VERY WEAK. AFTER MOMENT LIGHTS FROM ROW 27 ABC TO END WENT OUT. IN THAT AREA TECHNICIAN HEARD STSDR CA020527004Access Panel · departed(CAN) ON ARRIVAL AT DESTINATION, FOUND INBOARD OF NR 1 ENGINE, INSPECTION PANEL (BLOW OUT), MISSING ( BROKEN AT HINGE LEVEL, REFERENCE IPC 57-33-10,ITEM 272). MAINTENANCE INSPECTED THE LT LOWER WING LEADING EDGE ACCESS AND NO DAMAGE FOUND. A LEAK CHECK WAS CASDR CA020429004Actuator · failed(CAN) WHEN LOWERING THE LANDING GEAR CONTROL LEVER A LOUD BAG WAS HEARD, LT GEAR CONFIRMED DOWN AND LOCK WITH THE OVERWING GEAR POP-UP INDICATOR AND AIRCRAFT LANDED SAFELY. UPON INVESTIGATION ON THE GROUND, THE F/E REPORTED A COMPLETE FRACTURE OF THE LT MLG RSDR CA020501009Windshield · failed(CAN) CAPTAIN WINDSHIELD HAD MAJOR DELAMINATION IN FLIGHT . THE CREW PROCEDURES WERE CARRIED OUT BY PULLING THE CIRCUIT BREAKER TO DEACTIVATE THE WINDSHIELD HEAT SYSTEM. MAINTENANCE REPLACED THE WINDSHIELD AND ALSO REPLACED THEWINDSHIELD HEAT CONTROL UNIT.SDR CA020408013Control Box · failed(CAN) SEAT ELECTRONIC BOX POSITIONED AT ROW 25 DE , STARTED SMOKING. THE SEB WAS DICONNECTED BY THE CREW. MAINTENANCE REPLACED THE UNIT.SDR CA020405027Tube · broken(CAN) WHILE CLIMBING THROUGH FLT LEVEL 290 , NR 2 ENGINE POWER WENT DOWN TO IDLE POWER ONLY. ABNORMAL CHECK LIST CARRIED OUT WITH NO SUCCESS. A/C RETURNED TO YMX. NO THROTTLE RESPONSE AT ALL. MAINT REPLACED THE FUEL FLOW REGULATOR IN ACCORDANCE WITH MM. FOUNSDR CA020221017Engine · overheated(CAN) 2 MINUTES AFTER LANDING , AFTER THRUST REVERSER STOWING , THE FIRST OFFICER CALLED OUT HIGH TGT RAISING RAPIDALY AND ENGINE RUN DOWN , TEMPERATURE ROSE TO 850 DEGREES ON NR 1 ENGINE. THE TAIL PIPE FIRE DRILL WAS CARRIED OUT. MAINTENANCE CARRIED OUT ANSDR CA020201011Engine · failed(CAN) DURING FINAL APPROACH , FLAPS 33 DEGREES , 160KNOTS ON FLIGHT TSC 372 FROM YMX TO MCO THERE WAS A HIGH VIBRATION ON NR 1 ENGINE AT 3.8 UNITS ON CHANNELS A & B. THE AIRCRAFT LANDED SAFELY AND THE ENGINE VIBRATION DRILL WAS CARRIED OUT. THE BOROSCOPE CARRSDR CA020117015Gearbox · sheared(CAN) C1A CARGO DOOR, AFT LIFT GEARBOX SHEARED FROM ATTACHMENT DURING OPENING.SDR CA020110016Uplock Sensor · out of adjust(CAN) GEAR DOWN APPROACH YYZ, HAD THREE GREEN & RED DOOR LIGHT, FLIGHT ENGINEER LT GEAR OR DOOR LIGHT. FOLLOWED ABNORMAL PROCEDURE 03:18:03 (ALL LIGHTS WENT NORMAL ON SHORT FINAL). LT MAIN GEAR INBOARD UPLOCK SENSOR ADJUSTED I.A.W. M.M.32-61-07.SDR CA020117014Gyro · failed(CAN) ON DEPARTURE FROM AUA - YYZ, A MODERATELY STEADY LATERAL AIRFRAME OSCILLATION ( AT APPROXIMATE RATE OF TWO PER SECOND) STARTED AT 180 KNOTS / 2100 FT ABOVE SEA LEVEL / FLAPS 4 DEGREES. IT STOPPED ONLY WHEN POWER WAS REDUCED TO 1.4 EPR AT 5100 FT ABOVE SSDR CA020117018Control Valve · malfunctioned(CAN) ON FERRY FLIGHT TSC 2257 FROM CUN-YMX , DURING TAKE OFF , SLAT SYSTEM LOCKED IN EXTEND POSITION , BUT FLAPS RAISED FULL UP. FLAP RED LIGHT WAS ILLUMINATED ON THE FLAP POSITION INDICATOR (PILOTS CENTER INSTRUMENTS PANEL) AND SLAT MONITOR INDICATED SLATSSDR ARWA20011117Engine · making metalAT CRUISE 33,000; NR 3 ENGINE OIL PRESSURE DROPPED TO 30 PSI - MOVED THROTTLE TO IDLE, OIL PRESSURE REDUCED TO 20 PSI; COMPLETED ENGINE SHUTDOWN PROCEDURE AT 23:45 ZULU. OIL QUANTITY IS OK. INSPECTION REVEALED METAL IN OIL SYSTEM. ACCOMPLISHED NR 3 ENGINE CSDR CA020709002Engine · vibration(CAN) VIBRATION INDICATION ON NR 1 ENGINE, 3.0 UNITS ON CHANNEL A AND B. THE ENGINE WAS SHUT DOWN IAW THE SOP. MAINTENANCE REMOVED THE LP FAN BLADES , CLEANED AND REINSTALLED THEM IAW AMM 72-31-05. THE TEST NR 11, VIBRATION SURVEY WAS C/OUT AND FOUND TO BE WITSDR ARWA20011103Engine · vibrationSHUTDOWN NR 2 ENGINE AFTER EXPERIENCING VIPS SPIKE 3.0 BOTH CHANNELS AT APPOX 2325Z.SDR ARWA20020505Engine · vibration(SUPPLEMENT TO: ARWA20011103) LOG PAGE # 22235. DISCREPANCY: SHUTDOWN NR # 2 ENGINE, AFTER EXPERIENCING VIPS SPIKE 3.0 BOTH CHANNELS AT APPOXIMATELY 2325 ZULU. CORRECTIVE ACTION: REMOVED AND REPLACED # 2 ENGINE IAW ARROW AIR RB211-L1011 MAINTENANCE FORM L-101
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