JASC 3213
Service difficulty reports · 2,210
Reports filed under 3213 · Main Landing Gear Strut/Axle/Truck, newest first.
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 = '3213' 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 = '3213' 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 HEEA078339Crosstube · damagedMLG CROSSTUBE SPREAD BEYOND LIMITS.SDR CA020322015Strut · cracked(CAN) DURING INSPECTION, MAINTENANCE FOUND LT MAIN LANDING GEAR CRACKED. MAIN LANDING GEAR REMOVED AND REPLACED.SDR GLBA2002034Motor · inoperativeLANDING GEAR RELAY C/B POPPED, REPLACED HYDRAULIC MOTOR OPS CHECKED SYSTEM SATISFACTORYSDR 2002FA0000545Strut · brokenFOUND LANDING STRUT BROKEN AT THE DRAG BRACE BOLT HOLE. REMOVED AND REPLACED STRUT.SDR 2002FA0000430Cylinder · corrodedWHILE PERFORMING 6 YEAR LANDING GEAR INSPECTION IAW MFG SPECIAL INSPECTION, FOUND CYLINDER ASSEMBLY IN NOSE GEAR HAD SEVERE CORROSION ON INTERNAL BORE.SDR GLBA2002033Torque Link · damagedLEFT MAIN TORQUE KNEE SEPARATED DURING TAXI. REPLACED, OPS CHECKED SATISFACTORY.SDR CA020312001Fitting · cracked(CAN) RIGHT FLOAT WAS REMOVED FROM AIRCRAFT FOR REPAIRS TO BOTTOM SKIN. UPON REMOVAL, THE FRONT STRUT ATTACH FITTING WAS FOUND CRACKED AT HOLE FOR TAPER PIN. PART IS BEING REPLACED WITH NEW.SDR CA020408006Axle · sheared(CAN) DURING THE TAKEOFF RUN ON ICE THE AIRCRAFT CROSSED OVER SOME SMALL SNOWMOBILE TRACKS. WHEN THE AIRCRAFT BECAME AIRBORNE THE RIGHT SKI SEPARATED. THE SKI, STILL ATTACHED BY THE SAFETY WIRE, FLAILED AROUND CAUSING SUBSTANTIAL DAMAGE TO THE BELLY AND RT STRSDR 2002FA0000465Strut · failedDURING A MAINTENANCE RUN-UP OF THE ENGINES, THE RIGHT STRUT OUTER HOUSING FAILED CAUSING THE STRUT TO COLLAPSE. DAMAGE WAS CAUSED TO THE PROPELLER, ENGINE, NACELLE, WING, AND FUSELAGE.SDR ALG2002F00023Crosstube · corrodedDAILY SERVICE CHECK, FOUND HEAVY PITTING CORROSION UNDER WEAR PADS. SCRAPPED CROSSTUBE. PROBABLE CAUSE IS WATER ENTRAPMENT. EXTENT OF CORROSION ALMOST UNDETECTABLE WITH ALL PARTS INSTALLED. RECOMMEND INSPECTION BE DONE WITH CROSSTUBE REMOVED FROM AIRCRAFT SDR CA020215013Strut · cracked(CAN) ON INSPECTION PISTON LOWER SHOCK TUBE WAS FOUND WITH CHROME BLISTERED. NDT SHOWED A CRACK IN TUBE.CHROME WAS REMOVED TO EXPOSE THE CRACK WHICH WAS 8 1/4 INCH DOWN FROM THE TOP OF THE TUBE. THE CRACK RAN HORIZONTAL FOR 1 1/2 INCH THROUGH THE TUBE.SDR CA020220007Crossover Tube · cracked(CAN) DURING A POST FLIGHT INSPECTION THE AME FOUND A CRACK ON THE MAIN LANDING GEAR CROSS TUBE WHEN REMOVED. THE CRACK WAS FOUND TO BE 360 DEGREES AROUND THE TUBE, ALLOWING SEPARATION OF THE ROD END. THE TUBE WAS REPLACED.SDR IXXA0200004OStrut · crackedEN ROUTE FROM TOL TO BDL, THE LANDING GEAR AND DOOR UNSAFE WARNING LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE FLIGHT CREW CYCLED THE LANDING GEAR BUT THE UNSAFE WARNING INDICATION REMAINED THE SAME. THE FLIGHT RETURNED TO TOL FOR AND UNEVENTFUL LSDR ALG2002F00022Crosstube · corrodedDAILY SERVICE CHECK, FOUND PITTING CORROSION ON CROSSTUBE AT STRAP ATTACH POINT. PROBABLE CAUSE IS WATER ENTRAPMENT. SCRAP CROSSTUBE.SDR ALG2002F00021Crosstube · corrodedDURING DAILY INSPECTION, FOUND PITTING CORROSION ON CROSSTUBE .2500 INCH DEEP .5000 INCH ROUND. SCRAPPED CROSSTUBE. PROBABLE CAUSE IS WATER ENTRAPMENT. ALMOST UNDETECTABLE WITH ALL PARTS INSTALLED.SDR DL76L020111Axle · shearedRIGHT MLG OUTBOARD AFT REAR AXLE SHEARED DURING GROUND MOVEMENT TO WING OUT OF HANGAR. FAILURE WAS NOTICED BY TIRE TILT. REMOVAL OF TIRE AND BRAKE ASSY SHOWED COMPLETE SHEAR FAILURE OF AXLE UNDER BRAKE. REPLACED AXLE.SDR CA020205002Cylinder · failed(CAN) A/C C-2 SKIMMERS, BOTH UTILIZE COLONIAL STYLE MAIN UNDER CARRIAGE OLEOS. ONE OLEO PER A/C CAME APART.THE MAIN GEAR OLEOS ARE CRACKING AT LOWER END CAP TO CYLINDER (CASING) ATTACH BOLTS. WHEN THIS OCCURS, BEFORE LONG END CAP DISLODGES FROM OLEO CAUSING GESDR QXEA0200134Strut · chafedPDX - RT MAIN LANDING GEAR SHOCK STRUT HAS CHAFE MARK ON INBOARD RADIUS OF OUTBOARD LUG TOP END WHERE THE DRAG STRUT ATTACHES. REPAIRED IAW CMM 32-10-01.SDR NSVA0204Bearing · seizedALB - NOSE TIRES FLAT JUST AFTER LANDING, TURNING ONTO TAXIWAY. MAINTENANCE FOUND LEFT INNER BEARING SEIZED ONTO AXLE. BEARING AND AXLE DESTROYED. (M)SDR C7WA200202001Strut · fracturedFLIGHT CREW REPORTED (RIGHT GEAR DOWN LIGHT ON IN FLIGHT) POST FLIGHT INSPECTION BY MAINTENANCE FOUND RT MLG SIDE STRUT UPPER SEGMENT FRACTURED AT WALKING BEAM ATTACH POINT. THE CAUSE OF THE FAILURE OF THIS PART REMAINS UNDER INVESTIGATION.SDR 2002FA0000120Axle · crackedDURING FLOURESCENT PENETRANT INSPECTION, FOUND CRACK IN AXLE SHAFT RADIUS.SDR 2002FA0000119Axle · crackedDURING FLOURESCENT PENETRANT INSPECTION, FOUND CRACK IN RADIUS OF AXLE SHAFT (AREA 1A )SDR 2002FA0000118Axle · crackedDURING FLOURESCENT PENETRANT INSPECTION, FOUND CRACK IN AREA 1A (AXLE SHAFT RADIUS)SDR CA020104006Collar · cracked(CAN) PILOT LANDED NORMAL: WHILE ROLLING ON RUNWAY AIRCRAF WENT RIGHT AND PILOT HAS A HARD TIME CONTROLLING AIRCRAFT BUT MANAGED TO GET AIRCRAFT STOPPED. SHUT DOWN ENGINES AND GOT OUT TO INVESTIGATE; NOTICED RIGHT MAIN GEAR TIRE 90 DEGREES FROM NORMAL WITH HELSDR AUS20011375Nut · missing(AUS) LH MAIN LANDING GEAR TORQUE LINK CONNECTING BOLT NUT MISSING.SDR CA011220002Hinge · cracked(CAN) AFTER T/O SELECTED GEAR UP, THE HANDLE RETURNED WITH A RED LIGHT. THE GEAR WAS RECYCLED, WITH NO CHANGE.GEAR SELECTED DOWN AND AIRCAFT LANDED WITHOUT INCIDENT. PART TIMES AND CYCLES FROM AIRCRAFT TIME.SDR AUS20011378Cylinder · broken(AUS) AFTER A HEAVY LANDING THE LH LANDING GEAR WAS FOUND TO BE LOWER THAN THE RH GEAR AND SITTING AT AN ODD ANGLE. INVESTIGATION FOUND THAT THE LH MAIN LANDING GEAR CYLINDER TORQUE LINK ATTACHMENT LUGS BROKEN OFF.SDR 2002FA0000095Fork · brokenDURING LANDING THE AIRCRAFT VEERED OFF TO THE RIGHT SIDE OF THE RUNWAY. AN INSPECTION REVELED A RIGHT HALF FORK WAS BROKEN. THE WHEEL ATTACHES TO THIS HALF FORK WHICH ATTACHES TO THE MAIN STRUT. PER A GLASAIR REPRESENATIVE, MFG. OF THE GLASAIR KITS FOR AMATUERSDR AUS20011446Block · failed(AUS) RH MAIN LANDING GEAR COMPRESSION BLOCKS FAILED. DAMAGE CAUSED TOTHE FUSELAGE LOCATED INBOARD OF THE RH MLG.SDR CA011217017Strut · broken(CAN) 1/4 INCH RETAINER PIN BROKE AT COTTER PIN HOLE ON RT SHOCK STRUT ASSY. WHEN THE RETAINER PIN FALLS OUT THE LANDING GEAR FALLS DOWN.SDR BTV2001F00004Bearing · crackedDURING A ROUTINE, SCHEDULED LANDING GEAR INSPECTION, THE MECHANIC NOTED WHAT APPEARED TO BE A CRACK ON THE LOWER MOUNT BALL OF THE RIGHT HAND SHOCK ABSORBER. UPON REMOVAL OF THE SHOCK ABSORBER, VISUAL INSPECTION CONFIRMED THAT THE SPHERICAL BALL PORTION OF THSDR HEEA077432Crosstube · corrodedCROSSTUBE HAS CORROSION.SDR HEEA077431Crosstube · corrodedCROSSTUBE HAS CORROSION.SDR AUS20011251Damper · loose(AUS) LH REAR LANDING GEAR DAMPER UPPER CAP UNSCREWED AND SEPARATED FROM PISTON. SUSPECT CAUSED BY VIBRATION.SDR CA020405002Strut · cracked(CAN) AS A PRECAUTION DUE TO NOT KNOWING THE HISTORY. THE MAIN LANDING GEAR LEGS WERE SENT FOR MAGNAFLUXING. TWO LONGITUDINAL CRACKS OF ABOUT ONE AND ONE QUARTER INCH LONG WERE DETECTED ON THE LOWER THIRD OF THE LEFT HAND GEAR LEG. NOTE: PART CYCLES, PART TSSDR AUS20011219Fitting · cracked(AUS) RH MAIN LANDING GEAR FITTING CRACKED AND RUBBING ON BRAKE DISC.SDR LCQPad · crackedCRACK INDICATIONS AROUND JACK PAD ON BOTTOM OF LOWER SEGMENT OF RT MAIN LANDING GEAR.SDR RMM2001F00000Strut · crackedDURING A SCHEDULED INSPECTION A CRACK WAS FOUND IN ONE LEFT GEAR LOWER TORQUE LINK ATTACHMENT EAR. THIS CONDITION HAS BEEN FOUND PREVIOUSLY OVERHAULED MID TO HIGH TIME AIRCRAFT USED IN TRAINING. TIME ON PART COULD NOT BE DETERMINED. AIRCRAFT TOTAL HOURS 11SDR AC2A077049Crosstube · corrodedTHE MANUFACTURED DATE IS JAN. 2001 WITH 619 HOURS. TWO SPOTS OF CORROSION WERE FOUND UNDER THE SUPPORT CLAMPS. THE CROSSTUBE WAS REPLACED.SDR ERAA076675Crosstube · corrodedFORWARD CROSSTUBE HAS CORROSION. ACTION TAKEN: CROSSTUBE IS SCRAPPED.SDR AWXA200100517Valve · leakingPHX - AIR TURNBACK - FLT 27 - AFTER T/O THE LANDING GEAR WOULD NOT RETRACT. CREW RESET LGCIU 1 & 2 PER MAINTENANCE CONTROL, NO HELP. THE AIRCRAFT APPEARED TO REMAIN IN GROUND MODE. THE AIRCRAFT RETURNED TO PHX, MAKING AN UNEVENTFUL LANDING. MAINTENANCE TROUBLESDR CA011031013Link · cracked(CAN) UPON INSPECTION, A CRACK WAS FOUND AT NOSE GEAR LINK ATTACH POINT.SDR HEEA076484Skid Shoe · wornWORN. REPLACED WITH SERVICEABLE SKID SHOE.SDR HEEA076483Skid Shoe · wornWORN. REPLACED WITH SERVICEABLE SKID SHOE.SDR HEEA076473Crosstube · corrodedCORRODED IN SEVERAL AREAS BEYOND LIMITS. THE CORRODED AREAS ARE NEAR THE SKID MOUNTS TO 18" TOWARD THE CENTER. RETURNING FOR CREDIT.SDR SWIA200110218Strut · overservicedAT 80 KTS AIRCRAFT VEERED HARD LEFT. ABORTED TAKEOFF.FOUND RIGHT MAIN LANDING GEAR OVERSERVICED. RETURNED RIGHT MAIN LANDING GEAR TO PROPER POSITION.SDR HEEA076441Crosstube · corrodedCORRODED BEYOND LIMITS AT SUPPORT MOUNT AREA, MEASURED .010 INCHES IN ZONE 1. REPLACED WITH SERVICEABLE CROSSTUBE.SDR HEEA076440Crosstube · corrodedCORRODED BEYOND LIMITS AT SUPPORT MOUNT AREA, MEASURED .010 INCHES IN ZONE 1. REPLACED WITH SERVICEABLE CROSSTUBE.SDR HEEA076405Crosstube · corrodedAFT CROSSTUBE HAS CORROSION. SCRAPPED AND REPLACED WITH SERVICEABLE CROSSTUBE.SDR HEEA076404Crosstube · corrodedFORWARD CROSSTUBE HAS CORROSION. SCRAPPED AND REPLACED WITH SERVICEABLE CROSSTUBE.
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