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 jasc_code = '3252' 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 jasc_code = '3252' 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 AALA201907199010Shimmy Dampener · brokenAIRCRAFT WAS GROUNDED: CREW DECLARED AN EMERGENCY INTO IAH ON ACCOUNT OF HYDRAULIC ISSUE. ENG 1 HYD LOW PRESSURE LIGHT ILLUMINATED. MAINTENANCE FOUND BROKEN CONNECTION LINE ON THE LT MLG SHIMMY DAMPER. REMOVED AND REPLACED LT MLG SHIMMY DAMPER AND ALSO PERFORMSDR AALA201907149014Shimmy Dampener · excess playAIRCRAFT WAS GROUNDED: PILOT REPORTS BRAKES CHATTERING STRONGLY AT LOW SPEED DIFFICULT TO STOP WITHOUT VIOLENT SHAKING. TWO FLIGHTS IN A ROW. MAINTENANCE REMOVED AND REPLACED THE #3 BRAKE ASSEMBLY. REMOVED AND REPLACED THE RH SHIMMY DAMPER IAW AMM 32-11-81. RSDR 2019FA0000079Shimmy Dampener · failedDURING LANDING ROLL AFTER NOSE GEAR CONTACT WITH THE RUNWAY HIGH VIBRATION STARTED. (NOTE: LEFT MLG SHIMMY DAMPER EVENT CAUSED TORSION LINK FRACTURE). CORRECTIVE ACTION: REMOVED AND REPLACED SHIMMY DAMOER, TORSION LINK, TIRES 1 AND 2, BRAKE 1 AND 2.SDR 2017FA0000192Barrel · brokenNOSE WHEEL SHIMMY DAMPENER BARREL ASSEMBLY. ATTACHMENT BOSS BROKE CAUSING SHIMMY DAMPENER TO LOSE ITS FLUID CAUSING LOSS OF STEERING CONTROL.SDR ZP8R20160318002Shimmy Dampener · jammedSHIMMY DAMPER WOULD NOT TEST PER CMM, INTERNALS JAMMED. UPON TEARDOWN INSPECTION SEVERAL DISCREPANCIES WERE DISCOVERED: MISSING PARTS WITHIN UNIT. DUE TO MISSING PARTS, ORFICE WAS JAMMED SIDEWAYS. INCORRECT RETAINER PIN INSTALLED. PREVIOUS REPAIR STATION USESDR CALA2015042300321Shimmy Dampener · unserviceableUPON LANDING WITH MAIN WHEELS ON THE GND & PRIOR TO NOSE WHEEL TOUCHING GND, EXPERIENCED EXCESSIVE SHIMMY. SEVERAL CEILING PANEL CAME DOWN, 2 PSU FELL DOWN & LATCHES BROKE & TWO VIDEO MONITOR FELL DOWN & LATCHES BROKE. COMPLIED WITH AMM 05-51-08-210-802, INSSDR GLBA2014110400463Shimmy Dampener · faultyDURING TAXI OUT, THE CREW NOTED THAT THE ACFT WOULD NOT STEER TO THE RT WITH MAX DIFFERENTIAL BRAKING POWER & NOSE WHEEL STEERING. TOWED THE ACFT BACK TO THE GATE & REPLACED THE NOSE SHIMMY DAMPER IAW BMM 32-50-00. AFTER RELEASE, THE ACFT FLEW & WHILE TAXIINSDR CA140903010Damper · misoverhauled(CAN) THE DAMPER WAS REPAIRED AT A VENDOR IN 2011, AND WAS REASSEMBLED INCORRECTLY. IT WAS THEN INSTALLED BACKWARDS TO MAKE UP FOR THE IMPROPER ASSEMBLY. IN 2013 VENDOR DID A PHASE 2 AND PHASE B ON THE AIRCRAFT AND DID NOT NOTE ANY DEFECTS. WE WERE CONDUCTING SDR CA131125002Nut · loose(CAN) LT AND RT MLG SHIMMY DAMPERS BOTH FOUND WITH LOOSE JAM AND FLANGED NUTS. MPN 2225-0070 AND 2225-0069, RESPECTIVELY. REF IPC 32-11-03, FIG 01 ITEMS 60 AND 70. BOTH SHIMMY DAMPERS RETORQUED IAW AMM 32-11-03, SUBTASK 212-005-A.SDR USAA2012051400030Shimmy Dampener · faultyCREW REPORTED THE RIGHT BRAKE ON BOTH CAPT'S AND F/O PEDALS PULSE WITH LITTLE TO NO BRAKING AVAILABLE. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR SHIMMY DAMPER PER AMM 32-11-81. CHECKED WIRING TO ALL WHEEL SPEED TRANSDUCERS AND ANTI SKID VALVES FOR SHOSDR K5SR2012050123536Shimmy Dampener · leakingAFT WAS LANDING WHEN A VIOLENT SHIMMY AND VIBRATION OCCURRED BETWEEN 40 TO 50 KTS, EMANATING FROM THE NOSE LANDING GEAR. THE AIRCRAFT WAS BROUGHT INTO MAINTENANCE. FOUND SHIMMY DAMPER LEAKING FLUID. NOSE LANDING GEAR SHIMMY DAMPENER, PN 5543001-11, S/N 684,SDR CA111107006Piston · cracked(CAN) DURING A ROUTINE OVERHAUL OF THE SHIMMY DAMPER ASSY, PISTON WAS NOTED AS REQUIRED AND SEVERAL SMALL CRACKS WERE FOUND, BOTH INSIDE AND ON THE OUTER EDGE OF THE PISTON O-RING GROOVE, AND THEY DIDN`T APPEAR TO BE IN AN AREA THAT IS SUBJECT TO EXCESSIVE SSDR BSYA2010035Shimmy Dampener · brokenAFTER TAKEOFF WHEN RETRACTING THE GEAR NOSE GEAR DID NOT GO UP ALL THE WAY, THE CAUSE WAS THE SHIMMY DAMPER ROD END BROKE CAUSING NOSE GEAR TO JAM IN WHEEL WELL. CYCLED GEAR BACK DOWN AND RETURNED TO EWN. REMOVED AND REPLACED SHIMMY DAMPER AND NOSE GEAR ASSYSDR CA090331005Shimmy Dampener · malfunctioned(CAN) BENT SHIMMY DAMPER ROD CAUSED NOSE WHEEL TO JAM TO MAX. RT DEFLECTION AND WHEN GEAR WAS RETRACTED CAUSED MISALIGNMENT OF THE ALIGNER ASSY AND THE GUIDE BRACKET. GEAR SELECTION UP OR DOWN WAS AFFECTED AND RESULTED IN AN EMERGENCY LANDING WITH A UNLOCKED NSDR 2009FA0000096Roll Pin · brokenPILOT REPORT: ON LANDING SEVERE NOSE WHEEL SHIMMY. FOUND ROLL PIN THAT SECURES PISTON TO DAMPER ROD BROKEN AT PISTON THE DAMPER ROD. REPLACED ROLL PIN AND ALL O-RINGS. OPS NORMAL ON NEXT LANDING. (K)SDR CA080812002Clevis · broken(CAN) DAMPER SHAFT CLEVIS BROKE AT NOSE STRUT ATTACHMENT ALLOWING UNRESTRAINED MOTION OF SHIMMY DAMPER.SDR COMA0770040Shimmy Dampener · wornMLG SHIMMY ON TAKEOFF AND GEAR RETRACTION. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED RIGHT MLG SHIMMY DAMPENER.SDR COMA0770039Shimmy Dampener · wornFLIGHT 5058 - MLG SHIMMY ON TAKEOFF AND GEAR RETRACTION. AIRCRAFT RETURNED BACK TO CVG AND LANDED SAFELY. REMOVED AND REPLACED LEFT MLG SHIMMY DAMPENER.SDR GLBA20060914Shimmy Dampener · missingUPON PRE-FLIGHT INSPECTION, PILOT REPORT OF SHIMMY DAMPENER DAMAGE/MISSING AND SUSPECTED DAMAGE TO STRUCTURE IN SURROUNDING AREA WAS ALSO REPORTED. MAINTENANCE REMOVED AND REPLACED THE SHIMMY DAMPER IAW B1900D MM 32-20. MAINENANCE REMOVED AND REPLACED STEERINSDR KBM2006F00185Bearing · wornDAMPERS, BEARINGS ARE WORN, REMOVED AND REPLACED. (K)SDR SAI030603Roll Pin · shearedDURING TAKE-OFF PILOT NOTED VIBRATION AND ABORTED TAKE-OFF. AIRCRAFT RETURNED TO RAMP. AIRCRAFT WAS INSPECTED AND FOUND FAULTY SHIMMY DAMPNER. ROLL PIN, P/N NAS561P5-18, SHEARED.SDR SWAA060316Damper · shearedSEVERE VIBRATION FELT FROM RIGHT MLG. FOUND RIGHT MLG SHIMMY DAMPER BOLT SHEARED BETWEEN TORSION LINKS. REMOVED AND REPLACED RIGHT MLG SHIMMY DAMPER ASSY, NR 3 & NR 4 BRAKE LINES, NR 3 & NR 4 MAIN BRAKE ASSY, NR 3 & NR 4 MAIN TIRE/WHEEL ASSY AND RT MLG UPPERSDR CA051020002Nut · loose(CAN) CREW REPORTED MAINWHEEL SHIMMY ON LANDING. MAINTENANCE FOUND BOLT (ITEM 45)FROM THE RT MLG TORQUE LINK TO THE SHIMMY DAMPER HAD BACKED OUT AND THE TORQUE LINKS SEPARATED 1.2500 INCHES. THE SAFTEY BOLT (ITEM 35) AND LOCKING PLATE (ITEM 60) WERE FOUND LAYISDR DJFA2005147Shimmy Dampener · wornUPON ARRIVAL AFTER APPROACH AND NORMAL LANDING WITH NORMAL DECELERATION USING THRUST REVERSERS, AND AFTER ACHIEVING TAXI SPEED OF A FAST PACED WALK, THE AIRCRAFT EXPERIENCED A SEVERE NOSEWHEEL VIBRATION. NORMAL BRAKING APPEARED TO BE LOST, AND EMERGENCY BRAKISDR 2005FA0000913Cap · crackedCAP IS CRACKED ON PORT SIDE. CATASTROPHIC FAILURE. MANFACTURE CAP FROM SOLID BLOCK OF MATERIAL INSTAD OF CASTING PART. (K) (REF: 195920/JMG)SDR 2005FA0000912Cylinder · delaminatedCHROME HAS DELAMINATED IN CYLINDER BORE. IMPROPER PLATING. IMPROVE CHROME PLATING METHOD TO IMPROVE ADHESION TO CYLINDER. (K) (REF: 195920/JMG)SDR CA050405003Shimmy Dampener · failed(CAN) SHIMMY DAMPNER FAILED AT TAKEOFF CAUSING A VIBRATION. AIRCRAFT CAME TO REST WITH ONLY MINIMAL DAMAGE. SHIMMY DAMPNER REPLACED.SDR 2005FA0000143Bolt · misinstalledDURING RAMP INSPECTION, INSPECTOR NOTICED BOLT ATTACHING NOSE GEAR CENTERING DEVICE WAS INSTALLED INCORRECTLY, HEAD OF BOLT AT TOP OF HARDWARE STACK. AD 92-13-05 AND SB 893 REQUIRE BOLT TO BE INSTALLED WITH HEAD DOWN AND A CAUTIONARY PLACARD TO BE AFFIXED. PSDR CA040810005Shimmy Dampener · broken(CAN) SHIMMY DAMPENER BARREL END ENTIRELY BROKE OFF AT CIRCLIP GROOVE. ALL FLUID LOST,CIRCLIP MISSING, BROKEN PIECE MISSING. NO EVIDENCE OF PRIOR OVERSTEER.SDR AUS20040056Damper · faulty(AUS) NOSE WHEEL SHIMMY DAMPER END CAP RETAINING CIRCLIP MISSING.SDR 1BShimmy Dampener · misinstalledSHIMMY DAMPENER SLIDING SHAFT INSTALLED 180 DEGREES OUT. UNIT WAS OVERHAULED.SDR 2002FA0001300Bolt · misinstalledBOLT WAS INSTALLED BACKWARDS ON SHIMMY DAMPNER. GEAR WAS LOWERED IN FLIGHT AND HUNG UP ON COWL LT V CHANNEL. SUBSEQUENT DAMAGE WAS CAUSE TO CHANNEL AND REAR SUPPORT. TIME SINCE LAST WORK TO SHIMMY DAMPENER MOUNT CLAMP UNKNOWN.SDR 2002FA0001181Computer · malfunctionedNOSE WHEEL STEERING WILL NOT ARM. FOUND NO OUTPUT VOLTAGE ON P224 PIN A. 1.0 VAC REQUIRED FROM THIS PIN.SDR AUS20020788Barrel · broken(AUS) NOSE LANDING GEAR SHIMMY DAMPER BODY BROKEN AWAY FROM ATTACHMENTLUG.SDR CA020619002Shaft · sheared(CAN) INVESTIGATION OF A SEVERE NOSEWHEEL SHIMMY REPORT REVEALED THAT THE SHIMMY DAMPENER SHAFT HAD SHEARED. BOTH HALVES OF THE ASSEMBLY REMAINED ATTACHED BUT THE UNIT COULD NO LONGER FUNCTION AS DESIGNED. THE FAULTY UNIT WAS REMOVED FROM SERVICE AND REPLACED SDR CA020619003Shaft · sheared(CAN) SEVERE NOSEWHEEL SHIMMY REPORTED AFTER LANDING. INSPECTION OF THE DEFECT BY MAINTENANCE REVEALED THAT THE SHAFT WAS SHEARED. THE DAMPENER UNIT REMAINED ATTACHED BUT IN TWO SEPARATE PARTS PREVENTING IT FROM FUNCTIONING AS DESIGNED. NO FURTHER DAMAGE WAS FSDR CA020513001Rod End · separated(CAN) ROD END SEPARATED FROM PISTON.UNIT RETURNED TO VENDOR AND WAS OVERHAULED. SERVICE BULLETIN NR 169B EMBODIED TO PRECLUDE FURTHER EVENTS.SDR HEEA073107Damper · leakingLEAKING AROUND SHAFT SEAL.SDR 2002FA0000045Shimmy Dampener · damagedPILOT MADE A HARD LEFT TURN CAUSEING DAMAGE TO THE NOSE GEAR AREA. BENT ROD ON THE SHIMMY DAMPER CAUSING INTERNAL DAMAGE TO THE COMPONENT.SDR CA010426003Strap · broken(CAN) NOSE GEAR BONDING STRAP P/N 532.20.12.262 WAS WRAPPED AROUND SHOCK STRUT P/N 571.10.12.353 AND HAD BENT THE STRUT SOME 70 DEGREES UP FROM ITS NORMAL POSITION. THE STRUT COULD NO LONGER OPEN AND CLOSE THE OIL COOLER DOOR UPON GEAR RETRACTION. BONDING STRASDR 20010323CW004Shimmy Dampener · defectiveFOUND MULITUDE OF (AIR) POCKETS AND AIRCRAFT SHIMMIED EXCESSIVELY ON LANDING AND TAXI.SDR 20010328CW009Transponder · meltedIN CRUSE FLIGHT, SMOKE IN COCKPIT, ACRID SMELL IN COCKPIT. PHOTOCELL AND ADJACENT AREA OF CONTROL HEAD MELTED.SDR AU000796Damper · faulty(AUS) SHIMMY DAMPER LOW ON FLUID. ON FURTHER INVESTIGATION THE FOLLOWING COMPONENTS WERE FOUND TO BE DAMAGED: 1. HEAD BEARING P/N 0542102-3. 2. ROLL PIN P/N NAS 561P4-143. RING RETAINER P/N MS16625-1118. DAMPER WAS ATTACHED BY TWO FULLY THREADED METRIC SDR 20000609SH028Shimmy Dampener · failedAFTER LANDING, THE PIC WAS TAXIING TO THE RAMP WHEN THE NOSE WHEEL STARTED TO SHIMMY. HE APPLIED BRAKES AND THE AIRCRAFT MADE A HARD RIGHT TURN CAUSING THE AIRCRAFT TO TOP OVER TO THE LEFT/FRONT SIDE AND THE LEFT WING TIP AND PROPELLER MADE CONTACT WITH THE GSDR 2000ZZZX614Shimmy Dampener · brokenAFTER REPLACING AN OLD SHIMMY DAMPENER WITH A NEW ONE AT APPROXIMATELY 100 HOURS IN SERVICE, THE NEW PART BROKE AT THE OUTER C-CLAMP RING SPLITTING THE OUTER CYLINDER CASE. THIS HAPPENED AS THE AIRCRAFT STOPPED SHIMMING. THE END PLUG, C-CLAMP AND ALL FLUID WSDR AGQA065695Damper · dischargedMAIN LANDING GEAR DAMPER IS LOW.SDR AGQA065694Damper · dischargedMAIN LANDING DAMPER IS LOW.SDR AU990795Pin · wrong part(AUS) INCORRECT SHIMMY DAMPER PISTON ROLL PIN FITTED. A BRASS SCREW WAS USED INSTEAD OF THE CORRECT STEEL ROLL PIN. THE BRASS SCREW SHEARED CAUSING COMPLETE FAILURE OF THE DAMPER WITH ASSOCIATED NOSE WHEEL SHIMMY. UNAPPROVED PART.SDR 20000508SH002Shimmy Dampener · failedRETRIEVED SUBJECT SHIMMY DAMPENER FROM STOCK ROOM. ON FUNCTIONAL CHECK, DETERMINED MUCH WORSE THAN THE REMOVED UNIT.SDR 20000508SH001Shimmy Dampener · leakingSHIMMY DAMPENER HAS NUMEROUS DEAD SPOTS (AIR INSIDE) WHEN ACTUATED. CAUSES NOSE WHEEL TO SHIMMY READ BAD. (X)
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