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 96ZZZX3167Crosstube · failedAFTER LANDING AND ROLLING THROTTLES BACK TO GROUND IDLE WITH CREW AND 10 PASSENGERS ON BOARD, AIRCRAFT'S CROSSTUBE FRACTURED IN TWO RESULTING IN AIRCRAFT ROLLING TO THE LEFT. BROKEN SECTION OF TUBE CONTACTED HELIPORT PREVENTING AIRCRAFT FROM ROLLING OVER. FOSDR HAI00000075Fitting · wornFWD CROSS TUBE STRAP ASSY WORN INTO RIGHT FWD CROSS TUBE FITTING. REPLACED FITTING PER PRODUCT SUPPORT WEAR LIMITS.SDR GJQR9675Fitting · wornFWD CROSS TUBE STRAP ASSY. WORN INTO RIGHT FW.CROSS TUBE FITTING. REPLACED FITTING PER PRODUCT SUPPORT WEAR LIMITS.SDR 96ZZZX3035Gland Nut · crackedFSD/OMA - FLT 252 - UPON LANDING IN OMA AS THE AIRCRAFT TOUCHED DOWN, THE PILOT FELT THE RT MAIN GEAR START TO SINK MORE THAN NORMAL, PILOT ELECTED TO MAKE A GO-AROUND. CONTROL TOWER ADVISED THE RT GEAR DID NOT APPEAR TO BE ALL THE WAY DOWN. PILOT USED THE ESDR CA960527011Torque Linkshaft · broken(CAN)ON ROLL OUT ON LANDING, THE AIRCRAFT'S R/H TIRE BLEW. FURTHER INSPECTION REVEALED THAT THE TORQUE LINK SHAFT WAS ALSO BROKEN.SDR AU960897Cylinder · cracked(AUS) RH MAIN LANDING GEAR OUTER CYLINDER AFT TRUNNION CRACKED AND CORRODED IN AREA OF FILLET SEALSDR 96ZZZX2561Fitting · crackedFOUND 2 CRACKS IN FITTING THAT HOLDS AXLE STUB TO LANDING GEAR DURING A 100-HOUR INSPECTION.SDR HEEA967117Crosstube · corrodedCROSSTUBE CORRODED BEYOND LIMITS IN AREA B-4 .006. SCRAPPED CROSSTUBE.SDR HEEA967116Crosstube · corrodedCROSS TUBE CORRODED BEYOND LIMITS IN AREA A-4 .014. SCRAPPED CROSSTUBE.SDR AALA960751Piston · crackedTUL - LEFT MLG PISTON, LEFT LUG CRACKED. NDT PROCEDURE MD-80/PT/002. REPLACED WITH SERVICEABLE MLG PISTON. TST: 16,454.22 HRS. CYCLES, 9,103. (X)SDR CA960924032Crosstube · cracked(CAN) DURING ANNUAL INSPECTION AFT CROSSTUBE SUPPORT STRUCTURE FOUND CRACKED AND CORRODED.SDR 96ZZZX4801Fork · failedLOWER LEFT LANDING GEAR FORK FAILED APPARENTLY DUE TO 'INTERNAL' CORROSION. DURING TAKEOFF ROLL (TIME OF FAILURE), THE LEFT TIRE WAS CAUSED TO WEDGE AGAINST UPPER STRUT. THIS EFFECTED SEVERE LEFT BRAKING AND CAUSING ACFT TO DEPART RUNWAY TO LEFT.SDR 96ZZZX3006Saddle · crackedDUE TO THE RELATIVELY LOW TOTAL TIME ON THIS AIRCRAFT (1,399 HRS) AND THE FACT THE LANDING GEAR SADDLES HAD BEEN REPLACED AT 739 HOURS, AD 76-14-07 R2 DID NOT APPLY AT THIS TIME, HOWEVER, THE PART IN QUESTION HAD A CRACK THAT WAS EVIDENT WITHOUT DYE PENETRANT SDR CA970311029Support · cracked(CAN) CRACKS AROUND LANDING GEAR ATTACHMENTS.SDR 96ZZZX3412Fitting · crackedDURING SERVICE CHECK, NOTED FORWARD CROSSTUBE FITTING WAS CRACKED. FITTING WAS FOUND CRACKED IN THE SAME AREA AS REPORTED ON MDR SUBMITTED ON 2-7-94. THE FITTING WAS MANUFACTURED IN OCTOBER, 1992, WHICH IS DIFFERENT FROM THE PREVIOUSLY REPORTED CRACKED FITTISDR 96ZZZX2970Gear Leg · crackedLOWER GEAR LEG CRACKED AT BOLT HOLE AT ATTACHMENT TO UPPER ARM ASSEMBLY. CRACK CAUSED GEAR LEG TO FAIL ON LANDING. CRACK WAS NOT DETECTED BECAUSE OF SKI ATTACHMENT BRACKET COVERING GEAR LEG AT THIS AREA. SUBMITTER SUGGESTS FOR MECHANIC TO INSPECT BOLT HOLE SDR 96ZZZX2643Trunnion Pin · corrodedRT MLG TRUNNION WOULD NOT TAKE GREASE. TRIED UNSUCCESSFULLY TO REMOVE TRUNNION PIN. PIN HAD TO BE CUT TO FACILITATE REMOVAL. REPLACED UPPER BODY OF MLG, PIN, AND BUSHINGS DUE TO CORROSION. SUBMITTER STATED 2ND AIRCRAFT THIS YEAR WITH SAME PROBLEM. REF: OSDR 96ZZZX2642Strut · corrodedRT MLG TRUNNION WOULD NOT TAKE GREASE. TRIED UNSUCCESSFULLY TO REMOVE TRUNNION PIN. PIN HAD TO BE CUT TO FACILITATE REMOVAL. REPLACED UPPER BODY OF MLG, PIN, AND BUSHINGS DUE TO CORROSION. SUBMITTER STATED 2ND AIRCRAFT THIS YEAR WITH SAME PROBLEM. REF: OSDR CA970513007Saddle · cracked(CAN) SKID GEAR SHIFTED LATERALLY ALLOWING SADDLE TO WEAR ON LUG ON SKID CROSS TUBE.SDR 96ZZZX3019Fitting · chafedFORWARD CROSS TUBE STRAP ASSY WORN INTO RIGHT FORWARD CROSS TUBE FITTING. REPLACED FITTING PER PRODUCT SUPPORT WEAR LIMITS.SDR CA960513027Bolt · missing(CAN) ON LANDING, LT TORQUE LINK CENTER BOLT (AN 175-20) BUSHING (5041013) AND WASHERS (AN 960-7L) AND WASHERS (5045018-2) DEPARTED FROM AIRCRAFT CAUSING WHEEL TO CAMBER TO A CROSSWISE CONDITION AFFECTING LANDING ROLLOUT. DYE PENETRANT INSPECTION CARRIED OUT SDR 96ZZZX2520Trunnion · scoredAFTER LANDING, STRUT WAS FOUND WITH SNAP-RING, WASHER AND BEARING ASSY HAVING FALLEN FROM WITHIN TRUNNION HOUSING. STRUT WAS COCKED TO THE OUTSIDE. NO FLUID OR AIR PRESSURE PRESENT. REMOVED STRUT ASSY AND FOUND SCORE MARK INSIDE TRUNNION. RESEARCHED LOG BOSDR AALA960622Bushings · rotatedAFW - FOUND LEFT AND RIGHT MAIN GEAR INNER SHOCK STRUT BUSHINGS AT TRACK ATTACH POINT HAS CRACKED SEALANT, POSSIBLE BUSHING ROTATION. REQUEST TO CLEAN SEALANT CHECK FOR CORROSION, RESEAL AND APPLY TORQUE STRIPE FOR FURTHER INSPECTION. PER MRB 757-789. (M)SDR AALA960621Bushing · rotatedAFW - NOSE GEAR SHOCK STRUT BUSHINGS AT DRAG STRUT ATTACH POINT HAS CRACKED SEALANT, POSSIBLE BUSHING ROTATION, REQUEST TO CLEAN SEALANT CHECK FOR CORROSION, RESEAL AND APPLY TORQUE STRIPE FOR FURTHER INSPECTION. PER MRB 757-790. (M)SDR 96ZZZX2452Fitting · crackedDURING SERVICE CHECK, NOTED MLG FITTING WAS CRACKED. FITTING WAS FOUND CRACKED IN THE SAME AREA AS REPORTED ON MDR SUBMITTED ON 2-7-94. THE FITTING WAS MANUFACTURED IN OCTOBER, 1992, WHICH IS DIFFERENT FROM THE PREVIOUSY REPORTED CRACKED FITTINGS.SDR 96ZZZX2447Fitting · crackedDURING SERVICE CHECK, NOTED MLG FITTING WAS CRACKED. FITTING WAS FOUND CRACKED IN THE SAME AREA AS REPORTED ON MDR SUBMITTED ON 2-7-94. THE FITTING WAS MANUFACTURED IN OCTOBER, 1992, WHICH IS DIFFERENT FROM THE PREVIOUSLY REPORTED CRACKED FITTINGS.SDR 96ZZZX2608Strut · failedAFTER LANDING, PILOT LOWERED COLLECTIVE, AIRCRAFT SETTLED AND SHORTLY AFTER, AFT LEFT LANDING GEAR STRUT FAILED SLOWLY SETTLING UNTIL STRINGER CONTACTED THE GROUND. UPON FURTHER INVESTIGATION A CRACK WAS FOUND EMANATING FROM THE BRACE TO STRUT ATTACHING BOLT SDR 96ZZZX3627Piston · brokenWHILE DISASSEMBLYING THE LEFT MAIN LANDING GEAR FOR AN AXLE CHANGE, FOUND ISOLATION PISTON STEM THAT THE DAMPENING SPRING SURROUNDS WAS BROKEN FLUSH AT THE PISTON HOUSING. SEE CITATION 500 COMPONENT MM, PAGE 32-10-00, FIGURE 1002, SHEET 2, ITEMS 110, 113, 114SDR 96ZZZX3549Torque Knee · crackedINITIALLY IDENTIFIED A CRACK IN THE UPPER MAIN LANDING GEAR TORQUE KNEE OF ONE BEECHCRAFT C90A TRAINING AIRCRAFT WHILE LOOKING FOR CRACKS IN THE LOWER KNEE FOLLOWING A LOWER KNEE FAILURE. ALTHOUGH NO CRACKS OR IRREGULARITIES ON OTHER LOWER KNEES WERE FOUND, DSDR AU960898Cylinder · cracked(AUS) RH MAIN LANDING GEAR OUTER CYLINDER AFT TRUNNION CRACKED AND CORRODED IN AREA OF FILLET SEALSDR AU960873Axle · failed(AUS) LH AXLE FAILED - LH WHEEL AND AXLES SEPARATED FROM LANDING GEAR LEG HELD ONLY BY BRAKE CABLE - AIRCRAFT HAD HEAVY LANDING TWO DAYS PREVIOUS - THIS DEFECT WAS RECEIVED FROM THE AUF AND IS FOR INFORMATION ONLYSDR CA960507014Gear Leg · broke(CAN) ON SLOWING DOWN AFTER LANDING ON SKIS, LEFT GEAR BROKE AT THE UPPER AXLE ATTACHMENT BOLT HOLES. THIS AIRCRAFT HAS HAD PREVIOUS REPAIRS DUE TO A HARD LANDING ON SKIS.SDR CA960429008Torque Links · cracked(CAN) TORQUE LINKS INSPECTED AS PER AWD AND FOUND CRACKED IN THE LOCATION SHOWN IN THE SERVICE MANUAL. CRACKS WERE DYE PENETRANT CHECKED BUT SUBMITTER STATES THAT THE CRACKS WERE VISIBLE WITH A 10X MAGNIFYING GLASS.SDR 96ZZZX2377Axle Bolt · failedUPON LANDING, THE AXLE BOLT NUTS STRIPPED OFF OF THE BOLTS CAUSING THE AXLE AND WHEEL TO DEPART THE AIRCRAFT. THIS CAUSED THE GEAR TO DIG INTO THE GROUND AND FLIP THE AIRCRAFT ON ITS BACK.SDR HEEA966887Crosstube · brokenCROSSTUBE BROKEN AT R/H SIDE OF THE CENTER SUPPORT BEAM ASSEMBLY CLAMP.SDR AU960372Housing · cracked(AUS) RH MAIN LANDING GEAR STRUT HOUSING CRACKED AT AFT END OF RH AND LH SIDE DRAG BRACESSDR 96ZZZX3190Skid Plate · wornWORN SKID PLATE. REMOVED AND REPLACED 2 EACH.SDR 96ZZZX2277Skid Tube · corrodedINSPECTION FOUND 2 EACH SKID TUBES CORRODED THROUGH BETWEEN SKID SHOE AND TUBE. SUSPECT DUE TO TRAPPED SPRAY CHEMICALS AND WATER FROM WASHING THE AIRCRAFT.SDR 96ZZZX1593Cross Tube · failedAIRCRAFT PARKED ON RAMP WHEN AFT CROSS TUBE FAILED ON RT SIDE OF CENTER SUPPORT BEAM ASSEMBLY CLAMP. THE AIRCRAFT IMPACTED THE GROUND RUPTURING RIGHT EXTERNAL STC FUEL CELL.SDR AU960570Trunnion · corroded(AUS) LH AND RH MAIN LANDING GEAR OUTER CYLINDER AFT TRUNNIONS CONTAINED UNACCEPTABLE CORROSION DURING ULTRASONIC AND EDDY CURRENT INSPECTIONS IAW ER B76-32-10-24 - RH OUTER CYLINDER CORRODED IN AREA OF JOURNAL CHAMFER AT THE 2 O'CLOCK POSITION -LH TRUNNION CSDR AU960334Mlg · cracked(AUS) MAIN LANDING GEAR LEG ASSEMBLY PNO 540004-501 CRACKED ADJACENT TO BOTTOM WELD ATTACHING LOWER PIVOT SUPPORT PLATE TO CROSS TUBE -TRUSS ASSEMBLY PNO 540001-503 DIAGONAL TUBES CRACKED ADJACENT TO WELDSSDR CA960325003Cap End · cracked(CAN)SHOCK STRUT UPPER AND LOWER ATTACHMENT LUGS PIN PISTON CAP ENDS CRACKED AND EARS TORN OFF. ON DISASSEMBLY LOWER PIN PISTON WAS FOUND CRACKED.SDR HEEA966837Shoe Assy · mis mfgSHOE ASSY BOLT HOLES DO NOT LINE UP DURING INSTALLATION.SDR COMA9630059Strut · failedRIGHT MLG STRUT IS LEAKING. ATTEMPTED RESEAL OF STRUT AND FOUND IT TO BE DAMAGED INTERNALLY. REPLACED SHOCK STRUT. PART TOTAL CYLES, 2,360.SDR AU960375Mlg · distorted(AUS) LANDING GEAR LEG BENT IN AREA ABOVE OVERCENTRE LINKSDR 96UAL900158Gland Nut · fracturedON GEAR RETRACTION LEFT MAIN GEAR RED LIGHT STAYED ON WITH GEAR HANDLE IN THE UP POSITION. RECYCLED GEAR AND GOT 3 GREEN LIGHTS IN DOWN POSITION. RED LIGHT REMAINED ON WITH GEAR HANDLE IN THE UP POSITION, HAD HEAVY DRAG IN CRUISE. *S/D* LEFT MAIN GEAR GLANSDR AU960474Shock Absorber · faulty(AUS) RH MAIN LANDING GEAR STRUT STAGE 1 AND 2 PRESSURES BOTH FOUND TO BE 1000 PSI - UNABLE TO SERVICE SHOCK ABSORBER - SUSPECT ANINTERNAL FAILURESDR AALA960286Strut Bushing · rotatedAFW - RIGHT MLG LOWER SIDE STRUT SWIVEL UPPER BUSHING HAS ROTATED SLIGHTLY. TST: 13,691. CYCLES: 4,900. (X)SDR CA960227012Clamp · cracked(CAN)CRACKED CLAMP ON FORWARD CROSSTUBE. AIRCRAFT USED AS A TRAINER.SDR HEEA966614Crosstube · crackedBOLT HOLE CRACKED AT L/H AFT MOUNTING HOLE TO SKIDTUBE AT AFT CROSSTUBE.
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