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 UVVR2020020300049Strut · overservicedDURING LANDING ROLLOUT THE AIRCRAFT DEPARTED THE RIGHT SIDE OF THE RUNWAY AND STOPPED IN THE GRASS. THE FLIGHT CREW REPORTED LOSS OF NOSE STEERING AND BRAKES. AIRCRAFT WAS TOWED TO HANGAR. SUBSEQUENT TESTING IN HANGAR WAS ABLE TO DUPLICATE THE LOSS OF STEERINGSDR YENA2019122400713Strut · corrodedDURING HEAVY MAINTENANCE, CORROSION SHOCK STRUT FWD PINTLE PIN ON RH MLG (1 EA), CORROSION SHOCK STRUT FWD PINTLE PIN ON LH MLG (1 EA); REF WO# 2019-240/1 AEROMAN WCC 2019-370284 & WCC 2019-370283 FOR WORK PERFORMED. REMOVED AND REPLACED SHOCK STRUT FWD PINTLSDR DALA2019102406144Axle · damagedDURING INSPECTION, LEFT MAIN GEAR BOGIE AXLE SLEEVE NBR 2 CHROME PLATING MISSING AND PEELING. REPLACED AXLE SLEEVE PER AMM 32-41-14. LP 1328862SDR DALA2019102406143Axle · damagedDURING INSPECTION, LEFT MAIN GEAR BOGIE AXLE SLEEVE NBR 5 CHROME PLATING MISSING AND PEELING. REPLACED AXLE SLEEVE PER AMM 32-41-14. LP 1328860SDR 2019FA0000311Cylinder · brokenLEFT MAIN LANDING GEAR STRUT CYLINDER TORQUE LUGS SHEARED AFTER CENTER TORQUE LINK BOLT AN310-8 NUT HAD LOOSEN UP, CAUSING EXCESSIVE SIDE MOVEMENT. LOWER STRUT/AXLE WHEEL ASSEMBLY DEPARTED UPPER CYLINDER.SDR QXEA2019091800359Axle · corrodedLEFT MAIN LANDING GEAR AXLE CORRODED BETWEEN INNER AND OUTER BEARING RACES, AND HAS A GOUGE IN SAME AREA. REPLACED AXLE IAW AMM 32-11-04-000-801.SDR QXEA2019091800358Axle · corrodedRIGHT MAIN LANDING GEAR AXLE CORRODED BETWEEN INNER AND OUTER BEARING RACES OF BOTH WHEELS. REPLACED AXLE IAW AMM 32-11-04-000-801.SDR IPXA2019092047017Bushing · gougedINSPECTION TYPE:12YR RT MLG SHOCK ABSORBER P/N D22485020 S/N B483 ON O/B LEG AT BOGIE ALIGNMENT PIN I/B BUSHING IS GOUGED. REPAIRED GOUGED RT MLG SHOCK ABSORBER O/B LEG AT BOGIE ALIGNMENT PIN I/B BUSHING IAW EO A300-3210-73966-A SECTION 6A. (MINOR)SDR I5EA2019091001Scissor Link · brokenDISCREPANCY: UPON LANDING AFTER NOSE WHEEL TOUCHDOWN A VIOLENT SHIMMY OCCURED. FOUND RT MAIN UPPER SCISSOR LINK BROKEN. SUPPLEMENTAL INFORMATION: REMOVED AND REPLACED RT MAIN GEAR UPPER AND LOWER TORSION LINKS, TORSION LINK PIN, SHIMMY DAMPER, WOW CABLE, RT MASDR QXEA2019080600305Axle · corrodedLEFT MAIN LANDING GEAR #1 OUTBOARD AXLE HAS EXCESSIVE PITTING AND CORROSION AT THE OUTBOARD SIDE NEXT TO THE INBOARD BEARING JOURNAL. REPLACED #1 AXLE IAW AMM Q400 32-11-04-400-801.SDR UIEA2019080294895Strut · corrodedL/H WLG SHOCK STRUT CYLINDER LOWER INNER SURFACE RUSTY.(<P>REPAIRED CORROSION ON INNER SURFACE AREA OF L/H WLG OUTER CYLINDER IAW RI-32-00-13681 REV.A</P>)SDR CA190730008Axle · sheared(CAN) DURING REPLACEMENT OF #6 M/W FOUND MLG AXLE SLEEVE RETAINER PIN SHEARED AND SLEEVE MIGRATION OF APPROX 0.400` AFT AND 0.300` INBD. RESOLUTION L/H MAIN LANDING GEAR CENTER AXLE REPLACED AS PER AMM 32-11-26. (TC# 20190730008)SDR CA190729014Axle · damaged(CAN) WHEN WE WERE REPLACING THE TIRE ASSEMBLY ON THE R/H MLG, WE NOTICED THAT THE AXLE P/N 0541199-1 HAS SOME PLAY (BOTH UP AND DOWN AND ROTATIONAL) ON THE MAIN LANDING GEAR. THE BOLT THAT HOLDS THE AXLE ON WAS WAS TIGHT. WE TRIED A NEW AXLE AND IT WENT ON VESDR CA190711017Bolt · sheared(CAN) UPON ARRIVAL INSPECTION, FOUND THE R/H MLG SHOCK STRUT GEAR DOOR MOUNT BOLT SHEARED. THE DOOR WAS REMOVED UNDER CDL THE AIRCRAFT WAS RETURNED TO SERVICE. SB 320194R2 HAS NOT BEEN CARRIED OUT ON THIS DOOR MOUNT HARDWARE. (TC# 20190711017)SDR CA190801010Strut · cracked(CAN) LEFT HAND MAIN LANDING GEAR STRUT COLLAPSED ON LANDING. FOLLOWING INSPECTION BY AN AME THE LANDING GEAR HOUSING WAS FOUND TO HAVE AN 8 INCH LONG CRACK THAT ALLOWED THE HYDRAULIC FLUID AND NITROGEN TO LEAK OUT ON LANDING. THE LANDING GEAR HOUSING WAS REPLSDR CA190613008Axle · damaged(CAN) DURING TOWING OF AIRCRAFT, THE #4 MAIN WHEEL WAS WOBBLING AND MAKING A NOISE. UPON INVESTIGATION, THE #4 MAIN WHEEL HUB, WHEEL BEARING AND AXLE WAS FOUND WITH SEVERE DAMAGE. AIRCRAFT WAS REMOVED FROM SERVICE AND RH MLG TO BE REPLACED AS WELL AS WHEELS, WSDR HAEA20190614001Axle · missingON DEPARTURE FROM KGVT THE CREW HEARD A NOISE FROM THE RH WING AREA, NOT SURE WHAT IT WAS THEY LEFT THE GEAR DOWN AND LOCKED AND PERFORMED A FLY BY THE TOWER AND DETERMINUED THE RH M/L/G PISTON/AXLE ASSEMBLY WAS MISSING. THE AIRCRAFT WAS FLOWN TO KAFW WHERE THSDR CA190517007Strut · malfunctioned(CAN) THE LANDING GEAR OLEOS IN THE S92A UTILIZE A FLOATING PISTON DESIGN AND IT IS VERY SUSCEPTIBLE TO IMBALANCE OF NITROGEN AND HYDRAULIC FLUID. THE INCORRECT GEAR INDICATION WAS DRIVEN BY A LOW LEFT HAND (L/H) SHOCK STRUT SERVICING, CAUSING A LACK OF WOW SISDR SWAA2019040931515Strut · corrodedR/H MAIN LANDING GEAR SHOCK STRUT OUTER CYLINDER CORRODED AT AFT SIDE OF UPPER TORSION LINK OUTBOARD ATTACH LUG. / REPAIRED GEAR PER EA.SDR SWAA2019040931514Strut · corrodedR/H MAIN LANDING GEAR SHOCK STRUT OUTER CYLINDER CORRODED AT FORWARD SIDE STRUT PIN LUG, AFT SIDE. / REPAIRED GEAR PER EA.SDR SWAA2019040931451Strut · corrodedR/H MAIN LANDING GEAR SHOCK STRUT OUTER CYLINDER CORRODED AT R/H AFT TRUNNION WEB. / REPAIRED GEAR PER EA.SDR JGVR20190329002Axle · corrodedRT MLG TRAILING LINK AXLE IS HEAVILY CORRODED. VISUALLY INSPECTED TRAILING LINK ASSEMBLY AND FOUND AXLE CORRODED. REMOVED AXLE AND INSTALLED NEW CUSTOMER SUPPLIED AXLE. REASSEMBLED AND APPLIED SEALANT. REPAIRED IN ACCORDANCE WITH MM REVISION 28 DATED DEC 10, 2SDR CA190327013Arm · damaged(CAN) DURING TAXI WITH NO BRAKES APPLIED, CREW FELT THE AIRCRAFT MOMENTARILY PULL TO THE RIGHT FOLLOWED BY A R OUTBD BRAKE FAIL MESSAGE POSTED ON EICAS. POST TAXI INSPECTION REVEALED SEVERE DISCOLORATION OF THE #4 WHEEL HUB CAP AS WELL AS A PIECE OF MATERIAL PSDR FDEA201903240703Landing Gear · failedRT MAIN GEAR NEEDS TO BE REPLACED DUE TO FAILED BOROSCOPE INSPECTION OF OUTER CYLINDER FILL VALVE BORE. REMOVED RT MAIN GEAR IAW AMM 32-11-01-4, DETAILS UNDER W/O 00074057 NR 0047.SDR FDEA2019032200697Strut · crackedQC DETECTED A CRACK WHILE INSPECTING THE LEFT MAIN GEAR AND THE WORK CARD IS CALLING FOR A GEAR CHANGE. REPLACED LH MLG STRUTSDR DALA2019032001835Cover · missingPDA PART DEPARTING AIRCRAFT. LOG PAGE 5290092 CLOSED. A/C 3125 FLT/CHK 0842 PILOT REPORT SDR: N POSITION: LT TASK HRS: 000009.2 TASK ELAPSE TIME HRS: 000009.2 01 18MAR19 W LEFT LANDING GEAR STRUT DUST COVER MISSING LOG-PAGE UPDATED @ 18MAR19 1846 UTC 02 18MAR1SDR CA190830006Saddle · damaged(CAN) MAR 15 2019 :UPON 36HRS FOUND #1 MAIN WHEEL TIRE ASSY BELOW 2MM MINIMUM REQUIREMENT AND NEED TO BE REPLACED. AS PER AMM 32-41-01 UPON REPLACEMENT WE NEED TO ENSURE ALL AXLE SADDLE IS INTACT AND NOT DAMAGE, HOWEVER, AS OF FEB 25, 2019 MAINTENANCE ENTRY HASDR FQAR20190213001Mount · crackedDURING A SCHEDULED INSPECTION, BOTH THE LT AND RT LOWER MAIN GEAR LEGS WERE FOUND TO BE CRACKED ON THE EARS FOR THE TORQUE LINKS MOUNTING, CRACKS WERE LOCATED ON THE UPPER SIDE OF THE EAR IN THE RADIUS FROM THE MAIN BODY TO THE EAR.SDR DALA2019020400772Plug · missingLEFT GEAR UPPER BEARING BLANKING PLUG MISSING ON ARRIVAL. REMOVED SPEED TAPE ERA 575079 AS A TEMPORARY REPAIR AND REPLACED WITH LEFT GEAR UPPER BEARING BLANKING PLUG STK NR 00-3200-3-0198 PER ERA 575079 PERMANENT REPAIR.SDR DALA2019012900615Strut · collapsedON WALK AROUND FOUND RT MAIN STRUT COLLAPSED. REPLACED RT MLG PER WORK CARD 3200-4346. PERFORMED EXTENSION & RETRACTION TEST PER CARD 3230-7202. CHECKS GOOD. CHECKED ANTI-SKID PER AMM 32-45-00-720-801. JACKED A/C AND DOWN JACKED PER 0711-8197. ALL RII'S FOR THSDR DALA2019010200006Deflector · missingRT MLG DEBRIS DEFLECTOR O/B MISSING. FWD TO MCO PER CDL 32-12-03. PLACARDS INSTALLED. REMOVED AND REPLACED RT MLG O/B SPRAY DEFLECTOR PER AMM 32-12. CDL AND PLACARD REMOVED. (LP # 4451198)SDR SWIA2018112745272Landing Gear · icedGEAR DISAGREE WARNING MESSAGE AFTER TAKE OFF. (FLT#5015) CLOSED LT MLG NOT UP AND LOCKED. CLEARED ALL ICE FROM GEAR AND INSPECTED ALL LANDING GEAR EXTENSION AND RETRACTION COMPONENTS, NO FAULT NOTED IAW FIM. PERFORMED LANDING GEAR RETRACTION AND EXTENSION CHECSDR V6NA2019012402Axle · corrodedAT SCHEDULED INSPECTION, DETERMINED RIGHT MAIN LANDING GEAR AXLE CORRODED. REPLACED AXLE WITH NEW.SDR QMLA2018111118120Crosstube · failedAFTER RETURNING FROM FLIGHT ON LANDING AIRCRAFT TILTED TO THE LEFT, FORWARD LANDING GEAR CROSSTUBE FAILED.SDR JJBA2018111601006Bearing · corrodedNLG L/H AND R/H LOWER HALF BEARING CAPS HAVE CORROSION. REMOVED AND REPLACED NLG L/H AND R/H LOWER HALF BEARING CAPS.SDR 2018FA0000485Bolt · crackedDURING ACCIDENT INVESTIGATION OF N3267S, THE FORWARD OUTBOARD ATTACH BOLT P/N NAS147-34 HAD A PREEXISTING CRACK AT THE BEGINNING OF THE THREADS FROM THE SHAFT WITH THE PRESENCE OF CORROSION. THIS LEAD TO AN INSTANTANEOUS FAIL OF THE BOLT UPON LANDING AND SPRINSDR ANCF2018FA0000372Shock Absorber · faultedPILOT REPORT UNABLE TO RAISE LANDING GEAR AFTER LIFTOFF, LT SHOCK ABSORBER FAULT ON ECAM.SDR DALA2018091705629Strut · corrodedDUE TO THE REMOVAL OF RT MLG. CORROSION ON RT MLG LOWER SIDE STRUT LOWER/FWD SPOT FACE. R&R LOWER SIDE STRUT AT RT MLG PER AMM 32-11-61.SDR I5EA2018090600000Torque Link · brokenDURING LANDING WHEN REVERSE WAS APPLIED THE AIRCRAFT STARTED SHAKING HARD. REMOVED AND REPLACED LT MLG UPPER TORSION LINK PIN, 69-72023-1, AND LOWER, P/N 65-67693-3, TORQUE LINK PER AMM 32-11-51.SDR FDEA2018082982271Truck · failedON TAXI OUT PVD FELT UNUSUAL VIBRATION WHILE TAXIING. WE SUSPECTED A FLAT TIRE ON THE RIGHT MAIN TRUCK. REMOVED AND REPLACED LT MLG TRUCK ASSEMBLY PER AMM 32-12-20-4.SDR IPXA2018072732121O-Ring · damagedDIVERSION, HYD PRESS SYS 1 & EICAS. FOUND LT BLG TRUCK TILT SHUTTLE VLV O-RING DAMAGED. REPLACED O-RING IAW AMM, LEAK TEST SATIS.SDR DXTA2018070901157Strut · lowLEFT MLG LANDING GEAR RETRACTION DID NOT RETRACT. AT GEAR RETRACTION ON TAKEOFF MAIN LANDING GEAR LIGHTS REMAINED GREEN AND MAIN LANDING GEAR REMAINED DOWN. NOSE GEAR RETRACTED NORMALLY. RAN ABNORMAL CHECKLIST H2 "UNLOCK", "IF LANDING GEAR WILL NOT RETRACT". PSDR 2018FA0000187Link · corrodedRIGHT MLG TRAILING LINK WAS CORRODED. REPAIRED.SDR JGVR20180613002Axle · corrodedFOUND THE LEFT MAIN LANDING GEAR AXLE CORRODED OUT OF LIMITS, REPLACED THE AXLE.SDR QXEA2018052900203Axle · corrodedNR 2 MLG AXLE HAS CORROSION AND PITTING DAMAGE EXCEED 0.005 INCHES ON NON-WEAR SURFACES. REPLACED THE AXLE IAW AMM 32-11-04-400-801.SDR HYIA20180525001Axle · crackedDURING TAXI FOR DEPARTURE, THE CREW REPORTED THE AIRCRAFT PULLED TO THE RIGHT AS IF THE TIRE HAD GONE FLAT. THE AIRCRAFT BECAME DISABLED ON THE TAXIWAY. THE RT AXLE ASSEMBLY HAD FAILED CAUSING THE WHEEL ASSEMBLY TO RUB AGAINST THE RT LANDING GEAR STRUT. UPSDR R61A2018005020555Tube · scoredMAINTENANCE FOUND THE RT MLG WHEEL AXLE OUTBOARD BORE SHOWING EVIDENCE OF SCORING AND MINOR CORROSION. MAINTENANCE REMOVED THE SCORING AND CORROSION IAW CMM 32-11-01, AND ETD2018-170-045594.SDR SIMA20180314007Strut · lowRTF LDG GEAR DISAGREE. AFTER ROTATION DURING GEAR RETRACTION, LG/LVR DISAGREE MESSAGE ON EICAS FOLLOWED SHORTLY BY ENG 1-2 REV DISAGREE. GEAR SHOWED 3 WHITE UP INDICATIONS AND SEEMED TO OPERATE NORMALLY. MESSAGES EXTINGUISHED ONCE THE GEAR WAS EXTENDED. SERVICSDR 2018FA0000074Axle · brokenWHEN PERFORMING ANNUAL INSPECTION WE FOUND RT AXLE COMPLETELY BROKEN IN HALF. ALL THAT WAS HOLDING THE WHEEL ON WAS THE BRAKE ASSEMBLY. THERE WERE NO REPORTS GIVEN OF HARD LANDING. NO HISTORY IN LOGBOOKS OF TIRE/WHEEL CHANGES SINCE FACTORY NEW.SDR 2018FA0000110Cylinder · brokenFAILURE OF THE UPPER PART OF THE RIGHT MAIN GEAR, THE CYLINDER. THIS FAILURE APPEAR TO BE A MECHANICAL FAILURE OF BOTH THE UPPER ATTACHMENT EARS FOR THE TORQUE LINK ASSEMBLY, BOTH SECTIONS WERE SHEARED OFF. THE SEPARATED SECTIONS SHOWS WHAT APPEARS TO BE E
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