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 UIEA2021092302090Fitting · leakingDURING FLIGHT HYD QTY 1 MSG, FOLLOWED BY HYD SYS 1 MSG AND LIGHT(<P ><SPAN>FOUND FITTINGS ON FUSE ASSY FOR RH BODY GEAR LEAKING. REPLACED RH BODY GEAR TRUCK POSITIONING FUSE IAW AMM 32-13-24/401. LEAK CHECK GOOD.</SPAN></P>)SDR 2021F00285Axle · chippedRH MLG AXLE MISSING PLATING. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER 31045M1 DATED AUGUST 12, 2021; 680A-0112 (N562QS) RIGHT MAIN LANDING GEAR AXLE PLATING DAMAGE (CHIPPED).SDR 2021F00222Axle · chippedLEFT MAIN LANDING GEAR TRAILING LINK AXLE HAS AN AREA OF CHROME PLATING CHIPPED OFF.SDR FDEA202107151791Truck · damagedANTISKID MSG AFTER TAKEOFF, SUSPECT DUE TO DAMAGE #3 TIRE. R/R L/H MAIN TRUCK IAW AMM 32-11-17-004-0001.SDR YV3R2021072200470Strut · leakingCUSTOMER REPORTED CYLINDER ASSEMBLY P/N: D679-3 WAS LEAKING. UPON TROUBLESHOOTING, GAUGE P/N: D769-1 WAS FOUND LEAKING.SDR DALA2021061503269Strut · faultedSHIP 3247 - DIV - TO MSY DUE TO LANDING GEAR SHOCK ABSORBER FAULT AND OTHER ASSOCIATED AIR/GROUND SHIFT FAILURE MESSAGES. CORRECTIVE ACTION: FOUND NLG PROXIMITY SENSOR 24/25GA TARGET ARM WITH EXCESSIVE PLAY. INSTALLED NEW BUSHINGS AND RIGGED PROX SENSORS.SDR DALA2021060102998Strut · dischargedSHIP 3242 -ATB- DUE TO A L/G SHOCK ABSORBER FAULT AFTER ROTATION. CORRECTIVE ACTION: T/S FOUND R/H MLG H DIMENSION WAS 3 INCHES. TOP CHARGE VALVE PRESS. AT 1197 PSI AND BOTTOM AT 1200 PSI AT 52F. PER A320 AMM SERVICED R/H MLG FLUID AND NITROGEN, SERVICED L/H MSDR QXEA2021051100229Axle · corroded#1 MLG AXLE REQUIRES REPLACEMENT DUE TO CORROSION FINDINGS ON THE PISTON PLUG BORE. REMOVED #1 MLG AXEL IAW AMM TASK 32-11-04-000-801. BEGAN INSTALL OF #1 MLG AXEL IAW AMM 32-10-04-400-801 PARA 1-4A (1)-(9). CONTINUED INSTALLATION OF #1 MLG AXEL IAW AMM 32-11-SDR JJBA20210510011Strut · inoperativeLH MLG SIDE STRUT LOWER BEARING FLANGE HAS MISSING ARROWS. REMOVED AND REPLACED LH MLG LOWER SIDE BRACE. OPS CHECK GOOD.SDR DALA2021050702594Bushing · worn(LOG 1799887) DURING INSPECTION FOUND UPPER HANGAR LINK ATTACH BUSHINGS WORN ON A/C. REPLACED UPPER ATTACH BUSHINGS PER BOEING DWG 144A1650.SDR DALA2021050702593Bushing · wornDURING INSPECTION FOUND LOWER HANGAR LINK ATTACH BUSHINGS WORN ON A/C. REPLACED R/S LOWER ATTACH BUSHINGS PER CMM 57-15-01.SDR DALA2021050702592Bushing · worn(LOG 1799852) DURING INSPECTION FOUND LOWER HANGAR LINK ATTACH BUSHINGS WORN ON A/C. REPLACED R/S LOWER ATTACH BUSHINGS PER CMM 57-15-01.SDR DALA2021050702591Bushing · worn(LOG 1799849) DURING INSPECTION FOUND UPPER HANGER LINK ATTACH BUSHINGS WORN ON A/C. REPLACED UPPER ATTACH BUSHINGS PER BOEING DWG 144A1650. R/S UPPER ATTACH BUSHING PER BOEING DWG 144A1650.SDR DALA2021041202129Not Reported · corroded(LOG 1776213) DURING INSPECTION FOUND LH PIN BORE HOLE B HAS SIGNS OF CORROSION ON THE OUTBD FACE AND INTER FACE. REPAIRED PER B737 SRM 57-20-90 REP 2.SDR 2021FA0000105Bolt · shearedDURING THE LANDING PORTION OF OUR FLIGHT ON THE ROLL OUT THE RIGHT GEAR COLLAPSE UNDERNEATH THE AIRPLANE. UPON FURTHER INSPECTION IT WAS DETERMINED THAT THE BOLT HOLDING THE FOLLOWING SIDE BRACE AND DOWN LOCK SHEARD CAUSING THE RIGHT SIDE BRACE LOCK LINK ASSESDR 8HBR20210327025Strut · crackedFOUND CRACKS IN RH LANDING GEAR STRUT TUBE WHILE PERFORMING INSPECTION PER PIPER SL-1263.SDR 8HBR20210219024Strut · crackedRIGHT HAND LANDING GEAR STRUT CRACKED AND SEPARATED FROM THE AIRCRAFT AFTER LANDING.SDR IPXA2021020565352Strut · misinstalledINSPECTION TYPE:N/A**ATB - NO EMERG DECL'D-LANDED W/NO INCIDENT-AC TAKEN OOS** AFTER GEAR HANDLE RAISED EICAS MSGS GEAR TILT & GEAR DOOR SYNOPTIC SHOWED LH INBD BODY GEAR AMBER TILT & DOOR NOT CLOSED, GEAR DOOR MSG INTERMITTENT FOR 5 MIN, THEN SHOWED CLOSED SPSDR UIEA2021012600130Drag Brace · chafedRIGHT MLG AFT DRAG BRACE ATTACH FITTING IS CHAFED. COMPLIED WITH BLENDING DENT/AREA, AS PER REPAIR PLAN MESSAGE NUMBER TLS-21-0055-06B(R1). REF NDT W/O TOL81602. NO DEFECTS NOTED. TREATED, PRIMED, AND PAINTED AREA, IAW B767 AMM 51-21-10-377-003. REPAIR COSDR 2020FA0000559Landing Gear · out of limitsA LT & RT BOEING 737 MAIN LANDING GEAR (MLG) ARRIVED AT AEROTEK AVIATION ENGINEERING LIMITED (AAEL) WITH A FAA 8130-3 CERTIFICATE OF RELEASE TO SERVICE (CRS) SHOWING THAT BOTH MLGS HAD BEEN OVERHAULED ON 31 OCT 2019. FAA 8130-3 FORM TRACKING NUMBER FRC15947 & SDR LF1R202012030001Link · corrodedCOMPLIED WITH ADVENT AIRCRAFT SYSTEMS SB AAS-SB-32-016 BY INSPECTION OF THE WHEEL AXLES ON BOTH MAIN GEAR. FOUND INTERNAL SURFACES OF BOTH AXLES CORRODED BEYOND SURFACE CORROSION. NO ALLOWABLE LIMITS PUBLISHED IN PILATUS MANUALS. CORROSION CAUSED BY WATER BSDR 2020FA0000518Strut · corrodedTHIS AIRCRAFT IS USED IN A PART 147 TRAINING FACILITY AND HAS NOT FLOWN SINCE 2012. CORROSION FOUND IN RT MLG STRUT TUBE BEHIND FELT WIPER. THE SAME IS SUSPECTED IN THE LT CYLINDER.SDR R39R202012020001Strut · corrodedDURING THE 6 YEAR/8,000 CYCLE INSPECTION OF THE MAIN LANDING GEAR ASSEMBLY (101-810082-3), THE INTERNAL DIAMETER OF THE PISTON (101-810213-0001) FROM THE PISTON/AXLE ASSEMBLY (101-810045-0009) HAD MAJOR CORROSION BELOW THE LOWER SEALING PLUG. THIS CORROSION WSDR HYIA20201124002Axle · crackedTHE PILOT REPORTED THAT AFTER LANDING, THE AXLE BROKE WHILE EXITING THE RUNWAY. MAINTENANCE INSPECTED AND FOUND THE RIGHT AXLE TO BE CRACKED. REMOVED AND REPLACED THE RIGHT LOWER BARREL AND AXLE ASSEMBLY. NO FURTHER DEFECTS NOTED.SDR HYIA20201106002Axle · crackedTHE PILOT REPORTED THAT DURING A TURN ONTO THE RUNWAY THE AIRCRAFT THE WING DROPPED AND THE AIRCRAFT WOULD NOT ROLL. THE RIGHT TIRE WAS FOUND TO BE LEANING AGAINST THE STRUT. MAINTENANCE INSPECTED AND FOUND THE RIGHT AXLE TO BE CRACKED. REMOVED AND REPLACEDSDR B4VR2020966WWStrut · damagedTHIS AIRCRAFT HAS RETRACTABLE LANDING GEAR. THE ACTUATOR ROD END FITS BETWEEN TWO TABS ON THE STRUT ASSEMBLY. ON INSPECTION WE FOUND AN ISSUE ON THE STRUT ASSEMBLY WHERE THE LANDING GEAR ACTUATOR ATTACHES TO THE STRUT. WE FOUND ONE OF THOSE TABS COMPLETELY SDR RU3A2020100500032Landing Gear · collapsedRIGHT MAIN LANDING GEAR COLLAPSED ON LANDING ROLLOUT.SDR SIMA20200927001Shock Absorber · failedLAND GEAR AIR/GROUND FAIL. AIRCRAFT REQS EXTENSION/RETRACTION CHECK DUE TO REPLACEMENT OF SHOCK ABSORBER & CARDAN JOINT. C/A LANDING GEAR EXTENSION/RETRACTION CHECKS GOOD, IAW EMB 145 AMM 32-30-00 AND 32-34-00.SDR RJ3R20200908001Tube · crackedIDENTIFIED A CRACK NEAR THE JACKING DOME BORE DURING THE SECOND OVERHAUL OF AN A320 MLG SLIDING TUBE OFF.. THE FIRST OVERHAUL OF THIS SLIDING TUBE WAS PERFORMED IN JULY 2010. ON 22 APRIL 2020, INFORMED OPERATOR ABOUT THE DAMAGED SLIDING TUBE. ON 20 MAY 2020SDR T17A202008108030Strut · malfunctionedDURING LANDING, LEFT STRUT REMAINED EXTENDED AND THRUST REVERSER, SPEED BRAKE AND BRAKES DID NOT WORK. USED EMERGENCY BRAKES TO SLOW AIRCRAFT AND AS WE SLOWLY TURNED CORNER TO EXIT RUNWAY. LEFT MAIN COMPRESSED AND EVERYTHING WAS NORMAL. JACKED AIRCRAFT, LETSDR JJBA202008041001Strut · misrepairedLH MLG MAIN SIDE STRUT LOWER BEARING INSTALLED BACKWARD. REMOVED AND REPLACED LH MLG LOWER MAIN SIDE STRUT.SDR JJBA202008041002Bushing · dislodgedFOUND RH ML SIDE STRUT LOWER JOINT BUSHING COMING OUT. R*R RH SIDE LOWER AND JACKED AIRCRAFT. GEAR SWUNG 3 TIMES, ALL WERE SUCCESSFUL. NO OTHER DEFECTS NOTED.SDR ASOA202007224018Strut · separatedFLIGHT 3990, DURING CLIMB THE CREW REPORTED A LANDING GEAR DISAGREE MESSAGE. AIRCRAFT RETURNED DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RT MLG SIDE STRUT LOWER STRUT ASSEMBLY TO BE SEPARATED FORM THE LOWER ATSDR 2020FA0000326Tube · crackedSHIP SET OF LANDING GEAR WAS SENT FOR SCHEDULED MAINTENANCE. DURING STRIP DOWN INSPECTION THE RIGHT-HAND MAIN LANDING GEAR SLIDING TUBE WAS FOUND TO BE DAMAGED. CRACK AT THE JACKING DOME AREA. CRACK WAS DISCOVERED IN THE SLIDING TUBE ASSY ON THE FWD FACING SDR AALA2020070979010Leg Assy · corrodedAIRCRAFT IN BASE MAINTENANCE:RIGHT HAND MAIN LANDING GEAR SHOCK ABSORBER HAD AN INTERNAL LEAK. THE MAIN LANDING GEAR WAS REMOVED AND CORROSION WAS FOUND IN THE INTERNAL SURFACE OF THE MAIN FITTING LEG ASSEMBLY. REPLACED MAIN LANDING GEAR ASSEMBLY PER TASK CSDR MGTY2020062900004Bearing · crackedDURING SCHEDULED REMOVAL OF LT MLG SHOCK ABSORBER IT WAS NOTED THAT THE UPPER BEARING WAS CRACKED AND SPLIT COMPLETELY IN HALF. PARTIAL PENETRATION ON THE RT UPPER SHOCK ABSORBER BEARING WAS ALSO NOTED. ITEM TO BE REPLACED.SDR 2020FA0000284Axle · failedAFTER TOUCHDOWN A WIND GUST CAUSED THE AIRCRAFT TO BECOME AIRBORNE AGAIN. RETURNED TO THE GROUND AT A SLIGHT ANGLE AND AS THE PILOT STRAIGHTENED THE AIRCRAFT DOWN THE RUNWAY THE LT WHEEL AXLE BROKE & TIRE ASSEMBLY ROLLED DOWN RUNWAY. VEERED RT OF RUNWAY. ASDR SIMA2020061005003Strut · low pressure"LG AIR/GND FAIL" EICAS MSG WHEN RAISING GEAR ON TAKEOFF. ON LANDING AIRCRAFT DIPPED RT WING LOW. INSPECTED AND FOUND RIGHT MLG STRUT TO HAVE LOW NITROGEN PRESSURE AND HIGH HYD FLUID, SERVICED IAW AMM 32-10-02 PERFORMED GEAR SWING IAW AMM 32-30-00 ALL CLEARANCSDR 2020FA0000282Strut · crackedLEFT MAIN STRUT CRACKED AT THE AFT WEB AT THE HOLE DRILLED FOR THE SQUAT SWITCH BRACKETRY ATTACHMENT TO THE STRUT. THERE WAS FLUID AND NITROGEN (AIR) LEAKAGE THROUGH THE CRACK.SDR MASA2020050910061Shimmy Dampener · damagedTHE LT MLG SHIMMY DAMPER CAME APART ON LANDING CAUSING THE MLG TO TURN SLIGHTLY AND UPPER TORQUE LINK CAME IN CONTACT WITH THE NUMBER 2 MLG TIRE CAUSING TIRE TO BURST. A/C IN PROCCESS OF LH MLG REPLACEMENT.SDR 2020FA0000238Axle · corrodedCORROSION OBSERVED IN BOTH LEFT AND RIGHT MLG AXLE BORE INBOARD OF ANTI-SKID WHEEL SPEED TRANSDUCER. AIRCRAFT HAS ANTI-SKID BRAKES INSTALLED UNDER STCSA03275CH. BOTH TRAILING LINK/AXLE ASSEMBLIES REPLACED.SDR P6UR20200417001Cotter Pin · missingDURING INSPECTION, FOUND LH MLG SHOCK ABSORBER UPPER AND LOWER ATTACH NUTS WERE MISSING COTTER PINS.SDR HALA2020042700096Axle · corrodedFOUND #5 AXLE SLEEVE WITH CORROSION ON SHOULDER. // #5 AXLE SLEEVE REPLACED AS PER AMM 32-41-14 REV 75.02SDR 2020FA0000219Bolt · brokenAFTER LANDING, THE AIRCRAFT WAS ON ROLLOUT AND SLOWING WHEN THE AIRCRAFT LOST DIRECTIONAL CONTROL DUE TO THE RH MLG TURNING AFTER TORQUE LINK BOLT HAD BROKEN.SDR 2020FA0000210Crosstube · corrodedDURING A SCHEDULED LANDING GEAR ASSEMBLY ATTACH POINT INSPECTION, CORROSION (GREATER THAN SURFACE) WAS DISCOVERED ON THE REAR CROSS-TUBE SINGLE ATTACH POINT.SDR QXEA2020031300135Axle · corroded#1 MAIN GEAR AXLE HAS PITTING CORROSION UNDER THE BRAKE ASSEMBLY. REPLACED AXLE ASSEMBLY.SDR AALA202003109001Strut · damagedAIRCRAFT WAS GROUNDED: LEFT HAND MAIN LANDING GEAR STRUT HAS APROXIMATELY 1.5 IN WIDE BY OVER 2 IN LONG AREA OF CHROME MISSING FROM AFT SIDE. REPLACED MAIN LANDING GEAR STRUT AND AXLE ASSEMBLY PER TASK CARD 32-94-08.SDR FQAR20200430001Strut · crackedDURING THE TAKEOFF ROLL AFTER A SIMULATED ENGINE FAILURE ON TAKEOFF, THE LEFT GEAR FAILED WHERE THE STRUT TUBE IS ATTACHED TO THE LOWER STRUT CASTING,CAUSING THE LOWER GEAR ASSEMBLY TO BREAK AWAY, BREAKING THE TORQUE LINK AT THE MIDDLE BOLT, CAUSING THE PLANE SDR JGVR2020012017004Axle · corrodedFOUND CORROSION ON THE LT MAIN LANDING GEAR AXLE. REPLACED CORRODED AXLE WITH NEW P/N 6641646-1.SDR AALA2020011319007Tube · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT MAIN GEAR SLAVE LINK BRACKET LOWER LUG ATTACH POINT APPEARS CRACKED AT BOTH LOWER BOLT HOLES. REPLACED RIGHT HAND MAIN LANDING GEAR SLIDING TUBE ASSEMBLY PER AMM 32-11-13.
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