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 IPXA09655459Cylinder · damagedINSPECTION TYPE:6C OUTER CYLINDER INNER WALL FOUND SEVERAL AREA CHIPPED. RT MLG OUTER CYLINDER INNER WALL NICK MARKS REPAIR CUTOUT AS PER HX RS R32-11-36300 AND IPXA EO C-3210-33050-A.SDR CA090406004Torque Link · cracked(CAN) DURING PHASE INSP, THE RT UPPER TORQUE LINK WAS FOUND TO BE CRACKED AT THE CENTER JOINT. THE CRACK STARTED FROM THE GREASE HOLE AND SPREAD ABOUT 70 PERCENT ACROSS THE END.SDR CA090407005Axle · broken(CAN) GEAR USED PA 18 SUPER CUB INSTALLED AT TIME ACFT WAS BUILT. 1,284.00 ON HOMEBUILT 1.2500 AXLE IS FITTED INSIDE 1.5 GEAR TUBE AILED AT WHAT APPEARS LIKE ROSETTE WELDS OPERATING ON WHEEL SKIS GEAR WHEEL APPEARED MISALIGNED INSPECTED (JAKED UP) FOUND BROKENSDR CA090403011Tie Bolt · failed(CAN) IT WAS THE USUAL ON TOUCHDOWN, BUT WE HAD A 15-20 KNOT WIND TO HELP SLOW THINGS DOWN AND FOUND THE LANDING NOT REMARKABLE IN ANY WAY. SAME WITH TAKEOFF, THEN 3 MORE HOURS OF FLYING AND CARIBOU SURVEY, AND BACK. AS THE WEIGHT CAME OFF THE WINGS ONTO THE SDR CA090305010Strut · low(CAN) RT MLG OLEO FAILED TO EXTEND FULLY WHEN THE CREW RETRACTED THE GEAR. THE RT MAIN TIRE STRUCK THE AFT OTBD EDGE OF THE WHEEL CAUSING DAMAGE TO THE STRUCTURE WITHIN THE RT WHEEL WELL. CREW DID NOT HAVE ANY INDICATION OF A PROBLEM OR FEEL THE WHEEL STRIKE TSDR 2009FA0000159Pivot · crackedLEFT MAIN LANDING PIVOT FOUND CRACKED WHEN INSPECTED IAW SEB90-1 REV 3.SDR 2009FA0000156Pivot · shearedDURING SLOW FLIGHT MANEUVERS THE INSTRUCTOR NOTICED THE GREEN GEAR SAFE LIGHT WAS OUT. THE STUDENT OBSERVED THE LEFT GEAR WAS HANGING OUT AND SWINGING. THE GEAR WAS CYCLED BUT THE GEAR REMAINED HANGING. AFTER CONTACTING DISPATCH THE INSTRUCTOR ELECTED TO RESDR MASA2009022600079Strut · lowASH FLT 7193 IAD-LGA. CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD DUE TO A LOUD BANG DURING LANDING GEAR RETRACTION. MX SERVICED ALL GEAR STRUTS.SDR 2009FA0000177Strut · wornPREVIOUSLY REPORTED DURING SUPPLEMENTAL INSPECTION FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING DIASSEMBLY AND INSPECTION IAW SUPPLENTAL INSPECTION NR 32-10-06 FOUND PROTECTIVE COATING WORN OFF PISTON BARREL PN 5941132-8. REPAIRED PISTON BARREL WITH PSDR 2009FA0000172Strut · wornPREVIOUSLY REPORTED DURING SUPPLEMENTAL INSPECTION FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. LT MLG PISTON BARREL HAS BARE METAL SPOTS FOUND DURING SUPPLEMENTAL INSP NR 32-10-06. REPAIRED PISTON BARREL WITH PROTECTIVE COATING.SDR SWIA200921866Axle · corrodedC-CHECK, LEFT AND RIGHT AXLE RADIUS CORRODED. REPAIRED PER REO.SDR CA090206007Casting · crackedDURING 72 MONTH INSPECTION IT WAS FOUND THAT THE LOWER CASTING WAS CRACKED AT THE LOWER TORQUE KNEE CONTACT POINT.SDR SWIA200921617Axle · corrodedC-CHECK, AXLE CORRODED. REWORKED PER REO.SDR CHQA200900025Strut · underservicedFLIGHT 5298, STL TO PHL - THE FLIGHT CREW RECEIVED A LANDING GEAR AIR/GROUND FAIL MESSAGE AFTER GEAR RETRACTION ALONG WITH AN E1 AND E2 REVERSE DISAGREE. THE FLIGHT RETURNED TO STL AND LANDED WITHOUT INCIDENT. DURING TROUBLESHOOTING THE RIGHT MAIN LANDING GESDR USAA EMB09006Strut · lowFLIGHT 1553, PHL-DEN - AFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT. THE CREW RECEIVED A "LG WOW" EICAS MESSAGE. MAINTENANCE - ACCOMPLISHED A FULL STRUT SERVICE ON ALL THREE LANDING GEAR STRUTS AND CYCLED SEVERAL TIMES WITH NO FAULTS.SDR DXTA2009010603469Seal · wornLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. GEAR HANDLE WAS LOCKED IN THE DOWN POSITION AND WOULD NOT MOVE. TROUBLESHOT TO NLG STRUT LEAKING AND UNDERSERVICE NOT PROVIDING FULL EXTENSION OF STRUT. DISASSEMBLED, INSPECTED STRUT. INSTALLED NEW SEALS AND SESDR 2009F00011Strut · peelingWHEN PERFORMING SCHEDULED TASK AMP 32-999-30 "TRUCK BEAM PIVOT PIN" AIRCRAFT, REGISTER NR B18251, IT WAS FOUND THAT RT BLG INNER CYLINDER CHROME PEELING OFF. IAW AMM 32-00-03, L/G WAS REPLACED. SENT THE REMOVED GEAR, ADVISED THAT THERE WAS EXTENSIVE DAMAGE DSDR UALA2008122406987Cylinder · corrodedLT MLG OUTER CYLINDER IS CORRODED. OUTER CYLINDER CORROSION REPAIRED. REPLACED STRUT SEALS. PRESSURE CHECKED OK.SDR AALA200803167Strut · dischargedCOS - INFLIGHT, CREW REPORTED NOSE LANDING GEAR GRINDING OR SPINNING NOISE ON RETRACTION WITH BURNING RUBBER ODOR NOTED. RETURNED TO COS AND LANDED WITHOUT INCIDENT. REPLACED LEFT AND RIGHT NOSE TIRES AND ACCOMPLISHED STRUT SERVICE. SYSTEM GROUND CHECKED NOSDR DXTA2008122003419Strut · inoperativeAFTER TAKE-OFF, GEAR WOULD NOT RERACT. 3 GREEN GEAR DOWN + LOCKED LIGHT, NO RED LIGHTS , RETURN TO DEPARTURE FOR LANDING UNDER LANDING WEIGHT TO APROX 30660 POUNDS. REMOVED AND REPLACED THE NOSE GEAR UPPER AND LOWER BARREL ASSY. PERFORMED OPS CHECK SATISFACTOSDR DXTA2008122003415Strut · leakingLANDING GEAR WOULD NOT RETRACT AFTER T/O. ASSOCIATED ITEMS INCLUDED TRANSPONDER NOT REPORTING, LARGE PRESSURIZATION BUMP WHEN LEVELED OFF. AOA TAPE & INDEXER DID NOT WORK ON LANDING RETURN. INSTALLED OVERHAULED LT MLG OLEO STRUT DUE TO BLOWN SEAL. IAW MFG COMPSDR CA081217012Bearing · worn(CAN) RIGHT MAIN LANDING GEAR SHOCK ABSORBER STRUT LOWER BEARING WORN AND LOOSE INTERNALLY. REPLACED WITH NEW.SDR CA081210005Cylinder · worn(CAN) RT MLG LOST FLUID. DURING ATTEMPTED SEAL CHANGE, THE INNER CYLINDER OF THE GEAR HAD A 6" BY 2" PIECE OF CHROME MISSING FROM THE INNER CYLINDER.SDR DL76S081692Strut · unknownMLG SHOCK STRUT CYLINDER REPAIR IAW ERA 01-471561-14 REV A C/W ERA 01-471561-14.SDR WRLA2008091Strut · chafedCHAFING - DURING BRIDGE CHECK+4C CHECK, EGAT MECHANIC FOUND RT MAIN GEAR SHOCK STRUT UPPERSIDE HAD CHAFED L=3" AT STA Y=1240 (REFER TO EGAT NRC NO. U05124) IAW EGAT EI NR W2008A32B-1088 REV OO, EGAT EI NR W2008A32B-1088 REV 01 AND APPROVED RDR DATED 11/11/08.SDR UPS08M53974Cylinder · contaminatedINSPECTION TYPE:N/A GEAR HANDLE WOULD NOT MOVE TO THE UP POSITION. ALTERNATE PROCEDURE DID NOT BRING THE GEAR HANDLE UP. AIR TURNBACK. PERFORMED FIM 32-30-23-00 STEP GEAR HANDLE WOULD NOT RETRACT. BLEED TRUCK BEAM CYLINDER PER MM 32-37-01. AFTER BLEEDING SDR QXEA2008111401174Pin · backed outSEA - ON DEPARTURE WOW CAUTION ILLUMINATED AND AURAL TONE HEARD AT HIGH POWER SETTINGS. RETURNED TO THE FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. FOUND THE SHOCK STRUT PIVOT ARM PIN BACKED OUT 1.5 INCH APPROX. INSPECTED PIN WITH NO DAMAGE FOUND, REINSTALSDR F3LA2008102800699Bearing · corrodedDURING C4/S1 C-CHECK, INSPECTION NOTED CORROSION ON LEFT MAIN LANDING GEAR LOWER BEARING. MAINTENANCE REMOVED AND REPLACED LOWER BEARING ASSEMBLY IN ACCORDANCE WITH ENGINEERING AUTHORIZATION A9-32R-30744 AND A9-32R-30742.SDR SWIA200820193Axle · corrodedREMOVED RIGHT MLG AXLE DUE TO CORRSION. C-CHECK, REPLACED RIGHT MLG AXLE.
SDR SWIA200820191Axle · corrodedLEFT MLG AXLE REQUIRES REPLACEMENT DUE TO CORROSION. C-CHECK, INSTALLED LEFT MLG AXLE.
SDR SWIA200820547Axle · corrodedC-CHECK, LEFT MLG PISTON AXLE ROOT CORRODED. REPAIRED PER SCR.SDR SWIA200820545Axle · corrodedC-CHECK, RIGHT MLG PISTON AXLE ROOT CORRODED. REPAIRED PER SCR.SDR CA081020002Torque Link · cracked(CAN) DURING REGULAR MX, A MECHANIC NOTICED A CRACK ON THE UPPER TORQUE LINK OF THE LT MLG. THE TORQUE LINK WAS REPLACED AND ACFT RETURNED TO SERVICE. THE RT MLG TORQUE LINKS WERE INSPECTED WITH NO FAULTS FOUND.SDR SWIA200820528Piston · corrodedDURING C-CHECK, RIGHT MLG PISTON BLISTERED BETWEEN AXLES. REPAIRED PER CMM.SDR DLM88081311Cylinder · corrodedCORROSION PITTING WAS FOUND IN THE LOWER LEFT QUADRANT OF THE RT MLG OUTER CYLINDER. AN ER/A WAS ISSUED TO REWORK THE CYLINDER TO REMOVE THE DAMAGE. SAFE-LIFE LIMIT REDUCED TO 26000 CYCLES FROM FAA APPROVAL DATE OF 9-05-2006.SDR CALA0800947Lug · corrodedEA3210-01986 REV B LEFT MAIN LANDING GEAR INNER CYLINDER PIVOT BORE OF INBOARD LUG FOUND CORROSION AFTER BUSHING REMOVED. MAIN LANDING GEAR INNER CYLINDER INBOARD LUG PIVOT BORE REPAIRED IAW ECRA 3210-02114. GEAR RETRACTION TEST COMPLETED IAW AMM 32-32-00.SDR USAA920081929Pin · corrodedSAL C7 MAJOR REPAIR NR 6109431 CORROSION ON REAR PINTLE PIN OF RT MLG. REPLACED REAR PINTLE PIN OF RT MLG IAW AMERICA WEST AIRLINES TASK CARD R4M32304.SDR SWIA200820499Torque Link · corrodedDURING C-CHECK, RIGHT MLG OUTER CYLINDER UPPER TORQUE LINK CORRODED. REPAIRED PER CMM.SDR CA080917002Support · cracked(CAN) WHEEL ASSEMBLIES AND BRAKES REMOVED FOR INSPECTION AND REBUILD. IT WAS DISCOVERED THAT THE AXLE SUPPORT BODIES ON BOTH MAIN GEAR ASSEMBLIES HAD CRACKS AND REQUIRED REPLACEMENT. THIS WAS FOUND ON A 200 HR. INSPECTION.SDR SWIA200820483Torque Link · corrodedDURING C-CHECK, RIGHT MLG PISTON ASSEMBLY LOWER INBOARD TORQUE LINK CORRODED. REPAIRED PER CMM.SDR SWIA200820482Piston · corrodedDURING C-CHECK, LEFT MLG PISTON ASSEMBLY LOWER AFT TOP OF AXLE SUPPORT CORRODED. REPAIRED PER REO.SDR CA080902005Housing · broken(CAN) WHEN LANDING AT THE AIRPORT ON A TRAINING FLIGHT THE NLG PARTIALLY RETRACTED TOWARDS THE REAR OF THE ACFT. THE ACFT PITCHED RT AND FULL LT BRAKE WAS USED TO KEEP THE ACFT ON THE RUNWAY. THE ACFT MOMENTARILY LT THE RT SIDE OF THE RUNWAY AND STRUCK A RUNWASDR CA080826004Strut · contaminated(CAN) AFTER TAKEOFF CHECKS COMPLETED AND CONDITION LEVER RETARDED, RESULTING IN CONFIG WARNING AND OAT LIGHT ILLUMINATING. THIRD OCCURANCE. UNSCHEDULED LANDING MADE. (FUEL BURNED OFF TO ACCOMODATE LANDING WEIGHT) THE LT MLG WAS NOT FULLY EXTENDED DUE TO AIR RESDR 08FDEA03432Cylinder · damagedDURING GEAR RETRACTION RED GEAR INDICATION REMAINED ILLUMINATED FOR RIGHT MAIN GEAR APPROXIMATELY FIVE SECONDS LONGER THAN THE OTHER GEAR. REMOVED AND REPLACED RETRACT CYLINDER IAW MM 32-33-20-4. REMOVED AND REPLACED RT MLG BUNGEE (UNLOCK) CYLINDER REF MM 32SDR EHS2008F00001O-Ring · leakingWHILE FLYING A FIRE MISSION IN SUPPORT OF USFS, THE PILOT NOTICED THE RT GEAR START TO EXTEND FOLLOWED BY A LOSS OF HYDRAULIC PRESSURE. PILOT RETURNED TO THE AIRPORT AND LANDED. THE PROBLEM WAS TRACED TO THE RT MAIN GEAR RETRACT CYLINDER. UPON DISASSEMBLY OSDR 2009FA0000176Piston · corrodedPREVIOUSLY REPORTED DURING SUPPLEMENTAL INSPECTION FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING DIASSEMBLY AND INSPECTION IAW SUPPLENTAL INSPECTION NR 32-10-06 FOUND DEEP SCRATCHES AND CORROSION ON THE ISOLATION PISTON PN 5941136-1. REPLACED ISOLATIONSDR 2009FA0000175Piston · corrodedPREVIOUSLY REPORTED TO MFG DURING SUPPLEMENTAL INSPECTION FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. DURING DISASSEMBLY AND INSPECTION IAW SUPPLENTAL INSPECTION NR 32-10-06 FOUND DEEP SCRATCHES AND CORROSION ON THE ISOLATION PISTON PN 5941136-1. REPLACED ISDR 2009FA0000171Strut · scratchedPREVIOUSLY REPORTED DURING SUPPLEMENTAL INSPECTION FOR CONTINUED AIRWORTHINESS OF THE AIRPLANE. LT MLG PISTON BARREL HAS DEEP SCRATCHES IAW SUPPLEMENTAL INSPECTION NR 32-10-06. REPLACE PISTON BARREL WITH PN 5941132-8.SDR PNS2008F00006Sleeve · crackedPILOT WROTE UP A DISCREPANCY FOR HYDRAULIC OIL AROUND 31 GEAR LEG. MAINT FOUND THE NR 1 BRAKE ASSY LEAKING, PART WAS REMOVED AND SENT OUT FOR O/H AND FIND THE CAUSE OF LEAK. VENDOR O/H UNIT FOUND THAT ONE OF THE CYLINDER SLEEVES PN 2012648 WAS CRACKED AROUNDSDR C2XA08RI105Bolt · shearedDURING INSTALLATION OF MAIN LANDING GEAR OLEO STRUT ASSEMBLY, LOWER ATTACHMENT BOLT SHEARED AT TORQUE BELOW 1200 IN LBS. RIC MX REMOVED AND REPLACED LOWER ATTACHMENT BOLT, APPLIED TORQUE AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. (S)
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