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 CA990311081Actuator · cracked(CAN) PRIOR TO DEPARTURE, HYDRAULIC LEAK FROM RT MLG DOOR ACTUATOR. ACTUATOR CASING CRACKED. REPLACED.SDR CA981214022Angle · cracked(CAN) NOSE GEAR DOOR PAN ANGLE CRACKED AT OUTBOARD END OF DOOR BETWEEN DOOR ROD FITTING AND AFT HINGE ASSY. CRACK SEVEN INCHES LONG, REPAIRED.SDR CA981216014Rod · worn(CAN) IN PYLON, ON NR 3 ENGINE, AT ROD END BETWEEN THE THROTTLE TORQUE SHAFT AND THE TENSION REGULATOR LEVER, THE ROD END WAS WORN (BEARING DESTROYED) AT REGULATOR LEVER ASSEMBLY.SDR DLL10982447Hose · chafedLOSS OF C HYDRAULIC QTY DURING DESCENT, QUARTER TANK REMAINING. ENG PUMP AND C2 ATM WOULD NOT PROVIDE PRESS. C3 ELEC PUMP PROVIDED PRESS ONCE ON GROUND. FOUND C-SYS EDP PRESS FLEX LINE AND RIGID LINE CHAFED. REPLACED FLEX LINE, STILL NEEDS RIGID LINE REPLASDR CA981125091Bulb · failed(CAN) AFTER LANDING GEAR EXTENSION, NOSE LANDING GEAR GREEN LIGHT DID NOT COME ON AND DID NOT TEST. AFTER LANDING, FOUND BOTH BULBS BURNT, REPLACED.SDR CA981125090Link · cracked(CAN) ON INSPECTION, FOUND GREASE COMING OUT OF CRACK IN NR 2 OUTBOARD AFT FLAP SWING JOINT. REPLACED.SDR CA981125089Duct · cracked(CAN) BAD NOISE COMING FROM E BAY, FOUND AVIONIC EXHAUST DUCT BADLY CRACKED CAUSING PARTIAL LOSS OF PRESSURIZATION. DUCT AND HOLDING CLAMP REPLACED.SDR CA981125087Tube · damaged(CAN) IN CRUISE, NR 3 ENGINE APPROACHING VIBRATION LIMITS, THRUST WAS REDUCED AS PRECAUTION. FOUND SPINNER AND ANTI-ICING TUBE DAMAGED, REPLACED.SDR CA981125086Window · cracked(CAN) ON WALKAROUND, FOUND PASSENGER WINDOW AT 38K CRACKED, REPLACED.SDR CA980916062Sensor · loose(CAN) AFTER TAKEOFF AND GEAR SELECTED UP, DOOR INTRANSIT LIGHT REMAINED ON. FUEL DUMPED AND AIRCRAFT LANDED. RIGHT DOOR PROXIMITY SWITCH LOOSE, ADJUSTED AND TESTED SERVICEABLE.SDR CA980915024Control Cable · frayed(CAN) UNABLE TO RELEASE PARKING BRAKE, CREW HAD TO CYCLE BRAKES TO RELEASE PARKING BRAKE. DUAL POWER BRAKE VALVE CONTROL CABLE FRAYED AT PULLEY UNDER PILOT'S SEAT. REPLACED.SDR CA980908038Pump · failed(CAN) NR 1 ENGINE COULD NOT OBTAIN TAKEOFF E.P.R. FUEL FLOW REGULATOR REPLACED AND CHECKED SERVICEABLE. THE FOLLOWING DAY THE SAME SNAG RECURRED. THE FUEL PUMP WAS REPLACED AND THE PROBLEM WAS FIXED. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR CA980908041Gearbox · failed(CAN) WHEN CLOSING REAR LEFT PASSENGER DOOR, LOUD NOISE WAS HEARD AND DOOR STOPPED MOVING. GEARBOX BROKEN, COUNTER-BALANCE CASING UNRIVETED, AND FLEX DRIVE BOTH ENDS UNSWAGED. REPAIRED, PARTS REPLACED.SDR CA980909023Duct · loose(CAN) AFTER TAKEOFF, AIR CONDITIONING LEAK IN F.E.S.C. HEAVY LANDING CARRIED OUT. FOUND MOISTURE CONTROL MODULATING VALVE DUCT ADRIFT. CLAMP INSTALLED.SDR DLL10981741Engine · failedNR 3 ENG SHUT DOWN, LOW OIL PRESS. FOUND METAL ON CHIP DETECTORS. REPLACED ENGINE.SDR CA980908037Skin · cracked(CAN) 3 INCH CRACK FOUND IN FUSELAGE OUTER SKIN TRIPLER AT R2 DOOR CUT-OUT LOWER CORNER. FS901 WL 206 REPAIRED PER SB 093-53-237 REV 4.SDR CA980908040Fitting · cracked(CAN) DURING INSPECTION, FOUND SIDE FRAME FITTING AT FS 1163 LEFT SIDE CRACKED. FITTING TO BE REPLACED.SDR CA980916064Valve · overheated(CAN) ON FINAL APPROACH, NR 3 PACK FLOW CONTROL VALVE OVERHEAT LIGHT CAME ON. ON TOUCHDOWN, CABIN FILLED WITH SMOKE, PACK WAS IN AUTOMODE. IN-FLIGHT FLOW BAR WAS CYCLING CONSTANTLY, BUT NO OVERHEAT OBSERVED. PACK FLOW CONTROL VALVE AND TURBINE BYPASS REPLACSDR CA980908035Engine · making metal(CAN) AFTER PUSH BACK DURING START OF NR 2 ENGINE, THE OIL FILTER PRESSURE LIGHT CAME ON. INSPECTION FOUND METAL IN THE MAIN OIL FILTER. THE ENGINE WAS REMOVED FOR INVESTIGATION.SDR CA980908034Line · fractured(CAN) DURING CLIMBOUT, NR 2 ENGINE HAD A LOSS OF POWER. THE FUEL FLOW REGULATOR WAS REPLACED, BUT THE SNAG WAS NOT FIXED. FURTHER INSPECTION FOUND THE P1 LINE BROKEN AT THE PROBE. THE LINE WAS REPAIRED AND THE AIRCRAFT RETURNED TO SERVICE.SDR DLL10981430Chip Detector · not installedNR 1 ENG OIL LOSS IN EXCESS OF 4 QTS HR. DIVERTED SLC. ENG WAS NOT SHUTDOWN AND NO LOSS OF OIL PRESS. FOUND NR 1 ENG FINE SCAVAGE CHIP DET NOT IN HOUSING AND LAYING ON TOP OF OIL TANK. DET VISUALLY CKD OK BUT ONE O-RING FELL OFF WHEN HANDLED. REPLACED BOTSDR CA980908039Fairing · missing(CAN) ON TURNAROUND INSPECTION, FOUND HALF OF C-2 CARGO DOOR FAIRING MISSING. RIGHT STABILIZER LEADING EDGE BENT, POSSIBLY HIT BY FAIRING. LEADING EDGE REPLACED AND FAIRING INSTALLED.SDR DLL10981315O-Ring · leakingENG NR 1 SHUTDOWN IN FLT DUE TO HIGH FUEL FLOW AND FUEL USED INDICATIONS WITH ENG AT IDLE F/F IND. 9,500 TO 10,000 LBS. POM COMPLIED WITH FOR HIGH FUEL USE AND ENG SHUTDOWN. FOUND O-RING SEAL LEAKING AT FUEL FILTER FUEL LINE. REPLACED SEAL PER MM AND ENG RUSDR CA980629025Generator · cracked(CAN) IDG LOW PRESSURE LIGHT ILLUMINATED IN-FLGHT, IDG DISCONNECTED. POST-FLIGHT INSPECTION FOUND THE CHARGE FILTER PRESSURE HOUSING CRACKED. NR 3 ENGINE IDG AND OIL COOLER WERE REPLACED.SDR CA980608013Skin · corroded(CAN) DURING INSPECTION, CORROSION FOUND AROUND OUTFLOW VALVE CUT OUT SKIN, FS 609-629 AND STR 42-35. REPAIRED PER SRM.SDR DLL14980943Turbine Blabe · damagedNR 3 ENGINE HIGH VIBRATION ON CLIMB. ENGINE SHUTDOWN AND RTN TO TPA. BORESCOPED ENGINE FOUND HPT BLADE DAMAGE. REPLACED ENGINE.SDR CA980430031Spinner · loose(CAN) NR 2 ENGINE WAS SHUTDOWN ON CLIMB-OUT DUE TO HIGH VIBRATION AND THE AIRCRAFT RETURNED TO ITS POINT OF DEPARTURE. POST-FLIGHT INSPECTION FOUND OIL IN THE ENGINE SPINNER AND TWO BOLTS OF THE SPINNER CAP WERE FOUND LOOSE. THE SPINNER CAP AND ANTI-ICE TUBES SDR DLL10980740Gearbox · failedBEGINNING DESCENT, -A- SYSTEM PRESSURE 0, QUANTITY REMAINED. IDG LOW OIL PRESSURE LIGHT ON, GEN DISCONNECTED. DISCONNECTED IDG. ON APPROACH NR 1 OIL QTY DROPPED, QTY BELOW 10. NR 1 ENG SHUTDOWN. AT GATE NR 1 ENG OIL QTY 0. REPLACED NR 1 ENG MAIN GEARBOX SDR CA980325044Stop · damaged(CAN) DAMAGED BLOCKER DOOR FOUND ON RAMP INSPECTION, REPLACED.SDR CA980325042Duct · detached(CAN) DURING CRUISE, NR 2 ENG NACELLE PYLON OVERHEAT LIGHTS CAME ON BOTH A AND B CHANNELS. PLUS CAWP AND THRUST REVERSER LIGHT ON. ENG USED UNDER REDUCED POWER. AFT DUCTING CONNECTING TO PRESSURE REGULATING AND SHUT OFF FOUND COMPLETELY DETACHED. RECONNECTEDSDR CA980311024Duct Assy · cracked(CAN) CRACK FOUND AT CONNECTION OF OVER PRESSURE VALVE FLANGE ON DUCT. REPLACED.SDR CA980311025Fuel Flow Reg · faulty(CAN) DURING TOP OF DESCENT, NR 2 ENGINE WOULD NOT THROTTLE BACK BELOW 83 PERCENT N1. ALL ENGINE PARAMETERS WERE NORMAL. NR 2 ENGINE WAS SHUTDOWN. POST-FLIGHT INSPECTION FOUND THE NR 2 ENGINE FUEL FLOW REGULATOR (FFR) INTERNAL DAMAGED. FFR REPLACED. AIRCRASDR DLM11980313Projector · smokingSMOKE AND ELECTRIC SMELL FROM B/C PROJECTOR DURING TAXI OUT. DISABLED B/C PROJECTOR. INSPECTED AREA, NO TROUBLE FOUND.SDR DLL10980103Fuel/Oil Cooler · failedPAX REPORTED VAPOR TRAIL FROM NR 3 ENG, S/O AND CAPT CONFIRMED. FLT SERV REPORTED FUEL ODOR. DUMPED 37,000 LBS FUEL. RETURNED TO LAX AFTER DISCUSSION WITH ATL MTC. NO ABNORMAL INDICATIONS IN COCKPIT LANDING GROSS WT 358,000 LBS. REPLACED FUEL/OIL COOLER ANSDR DLL10972330Fire Wire · chafedON T/O, GOT FIRE WARNING ON NR 1 ENGINE. REPAIRED CHAFED WIRES IN ENGINE SPLITTER AREA.SDR CA971104011Thrust Reverser · malfunction(CAN) THRUST REVERSER LIGHT ON DURING CRUISE. AIRCRAFT DIVERTED. THRUST REVERSER HAS BEEN LOCKED AND AIRCRAFT HAS BEEN DISPATCHED AS PER MEL 78-31-33.SDR CA971031010Duct · failedDUCT FAILED IN FUSELAGE.SDR DLL13971811Plug · looseA AND B LOOP FIRE WARNING ON NR 3 ENG. FOUND BOROSCOPE PLUG LOOSE AT THE NUMBER TWO FUEL NOZZLE.SDR CA970909015Brace · failed(CAN) NLG JURY BRACE FOUND BROKEN AT LOWER ATTACH POINT. REPLACED.SDR DLL13971713Coalescer Bag · dirtyAFTER T/O, SMOKE AND OIL SMELL WAS REPORTED BY CABIN ATTENDANTS. THE CREW ISOLATED THE PROBLEM TO NR 2 PACK WITH AN ASSOCIATED NOTICABLE OIL QTY DROP ON NR 2 ENG. REPLACED COALESCER BAGS, RAN ENGINES ALL CHECK NORMAL.SDR CA970811009Vib Monitor Box · faulty(CAN) TAKEOFF WAS REJECTED FOLLOWING NR1 ENGINE VIBRATION INDICATION. "A" CHANNEL FOUND IN FAULT AND AIRCRAFT DISPATCHED AS PER MEL 77-31-00. VIBRATION MONITOR BOX REPLACED.SDR DLL10971521Fan Blades · lack of lubeHIGH ENGINE VIBRATIONS IN A AND B CHANNELS, SHUT ENGINE NR 3 DOWN IN FLIGHT. ENG VIB FLTR PRESS LIGHT ON PILOTS PANEL, YELLOW LIGHT IN NR 3 VIB GAUGE ON S/O PANEL. DID NOT HAVE FILTER PRESS LIGHT UNDER OIL PRESS GAUGE. REMOVED FOR BORO INSP-3LP TURBINE, 1HPSDR CA970811010Switch · out of adj(CAN) DURING CLIMB AT 13000 FEET, C-1 CARGO DOOR LIGHT CAME ON ON F/E PANEL. AIRCRAFT RETURNED TO BLOCKS. PROXIMITY SWITCH ADJUSTED.SDR CA970728019Idg · faulty(CAN) ON APPROACH ALL GENERATORS TRIPPED OFF LINE. LOSS OF ALL GENERATORS CHECK LIST CARRIED OUT, UNABLE TO RESTORE GENERATORS ON LINE. APU GENERATOR ESTABLISHED ON LINE. POST FLIGHT INSPECTION FOUND #1 AND #3 IDG GENERATORS FAULTY AND THEY WERE REPLACED. SYSTSDR DLL14971376Decoder · malfunctionedDURING TAXI OUT, PASSENGERS REPORTED ELECTRICAL ODOR IN THE VICINITY OF SEATS 28HJ. AIRCRAFT RETURNED TO GATE. AFTER BRIEF TROUBLE SHOOTING FOUND PASSENGER SVC SYS DECODER AT 27HJ TO BE EXCESSIVELY WARM AND SMELLING OF THE SAME ELECTRICAL ODOR. REMOVED THSDR DLL10971337Chip Detector · defectiveNR 2 ENG OIL QTY DROPPED TO ZERO, OIL PRESS LOW LIGHT ILLUMINATED. ENG SHUTDOWN, PERFORMED VISUAL INSP, FOUND MASTER CHIP DETECTOR HOUSING DEFECTIVE AND PACKINGS ON CHIP DETECTOR ONE CUT AND ONE MISSING. REPLACED CHIP DETECTOR HOUSING AND PACKINGS, RAN ENSDR DL72S971304Hydraulic Line · leakingCLIMBING THROUGH FL310, TOTAL HYD LOSS DETECTED BEFORE A-SYS LOST PRESSURE. PUMPS OFF IMMEDIATELY NO CAVITATION QTY WENT TO ZERO. REPLACED A-SYSTEM RETURN LINE IN RT WHEEL WELL CHECKS GOOD.SDR DLL10971303Engine · failedNR 2 ENG ROLLED BACK, RAMP REPORTS TAIL PIPE FIRE. REPLACED ENGINE.SDR CA970715029Turbine · damaged(CAN) AFTER TAKEOFF DURING CLIMB AT 1000 FEET THERE WAS A LOUD BANG FROM #1 ENGINE FOLLOWED BY HIGH VIBRATION AND LOSS OF POWER. #1 ENGINE WAS SHUTDOWN AND THE AIRCRAFT RETURNED TO ITS POINT OF DEPARTURE.VISUAL INSPECTION SHOWED TURBINE STAGES DAMAGED. ENGINE SDR DLL13971290Controller · intermittentNR 2 ENGINE A LOOP FIRE DETECTION CAME ON DURING CLIMB-OUT. LIGHT WENT OUT WHEN POWER WAS REDUCED. FOUND CONTROLLER INTERMITTENT, REPLACED CONTROLLER AND SYS CHECKS NORMAL.
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