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 55YR202610130001Strut · damagedCAME IN FOR PHASE MAINTENANCE, AND THE OPERATOR REQUESTED AN EARLY LANDING GEAR REPLACEMENT. THE LANDING GEAR WAS DUE SOON FOR REPLACEMENT, AND REPRESENTATIVES FROM BERING AIR DECIDED TO HAVE IT CHANGED AHEAD OF SCHEDULE. AFTER INSTALLING NEW MLG ASSEMBLIESSDR DXTA2026092509835Strut · dischargedDURING GEAR RETRACTION AFTER TAKEOFF, THE NOSE GEAR INDICATED IN TRANSIT AND NEVER FULLY RETRACTED. LG LEVER DISAG CAS MESSAGE DISPLAYED. HYDRAULIC PRESSURE WAS NORMAL. ALL GEAR EXTENDED NORMALLY WHEN SELECTED DN. SERVICED NLG STRUT. OPS CHECK GOOD. IAW PHENOSDR 2026F00210Spacer · missingAFTER GEAR RETRACTION LOW FREQUECY VIBRATION. WHEN READY TO TOWING OUR TECH NOTED TOO MANY THREADS VISIBLE ON LH NLG WHEEL AXLE. FURTER INSPECTION REVEALED MISSING SPACER UNDER WHEEL NUSDR NI6R202608260068Strut · wornRIGHT MLG SHOCK STRUT HAS DAMAGE FROM UPLOCK SWITCH, CHROME CHIPPED OFF TO BARE METAL. CHROME ON MLG STRUT ASSEMBLY HAS A DIVOT AT THE LOCATION WHERE UPLOCK PUSH BUTTON APPLIES FORCE TO PLUNGE THE BUTTON FOR GEAR UPLOCK NOTIFICATION. DIVOT BEYOND LIMITS PER CSDR DXTA2026071508807Axle · wornDURING TAKEOFF AND LANDING ROLL AT HIGHER SPEEDS THERE IS A LOUD GRINDING/SQUEAKING NOISE COMING FROM THE NOSEWHEEL ACCOMPANIED BY A STRONG NOSEWHEEL SHIMMY. REPEAT WRITE UP. REMOVED AXEL P/N: 2310-1165-001 S/N: 3128269 ALONG WITH ALL TORQUE LINK HARDWARE. RESDR DALA2026070904018Sleeve · damagedNR 3 AND 4 MLG AXLE SLEEVE DAMAGED. R & R NR 3 & 4 MLG AXLE ADAPTER SLEEVES PER AMM 32-42. OK FOR SVC. (LP: 8924695, AIRCRAFTT WAS GROUNDED)SDR 2026FA0000574Strut · brokenDURING TAXI, FAILURE OF THE LEFT MAIN LANDING GEAR OCCURRED AROUND THE OLEO STRUT PISTON TUBE BOLT HOLE. PIPER AIRCRAFT SERVICE LETTER 1263 RECOMMENDS ROUTINE INSPECTION OF THIS FAILURE POINT EVERY 700 HOURS TIS ON AIRCRAFT WITH OVER 6,500 TOTAL HOURS IN SERVSDR IPXA2026062555305Swivel Fitting · corrodedAFTER REMOVAL RT MLG STRUT SWIVEL FITTING FOUND OUTER SHAFT OF INBOARD CRANK AND DRIVE ARMS WITH CORROSION IN THE TEETH, FLL-023, ATA 57. NEW SHAFT ASSEMBLY PROCURED AND ACCOMPLISHED INSTALLATION ON TASK CARD "T3F18E008YJ8T" LINE # 50. NO FURHTER ACTION IS RSDR CALA2026052516512Strut · dischargedLEFT MAIN SHOCK STRUTAPPEARS TO BE ALMOSTFULLY COMPRESSED FOUND H DIMENTION WITHIN LIMIT REF AMM 12-14-32-200-001-A, BUT DIFFERENCE BETWEEN LEFT AND RIGHT MLG H DIMENTIONS IS MORE THAN 1.7 IN. REQUEST DIP OF FUNCTIONAL CHECK OF MLG SHOCK ABSORBER FLUID LEVEL BSDR AALA202604299403Strut · collapsedAIRCRAFT WAS GROUNDED: DURING LANDING ROLLOUT MANUAL BRAKING DECELERATION THE AIRCRAFT FELT AS THOUGH THE BRAKES STOPPED WORKING MOMENTARILY. DURING POST FLIGHT INSPECTION, LEFT MAIN STRUT IS COLLAPSED. COMPLETED FULL STRUT SERVICE. PER AMM 12-15-31. NO DEFECSDR CALA2026042815790Axle · failedBRAKES APPEAR TO BE TO BE LOCKING UPON TOUCHDOWN & EXIT FROM R WY GRABING...UPON TAXI INTO RAMP, ACFT EXPERIENCED NR 4 MAIN TIRE DEFLATION. NR 4 BRAKE FOUND DISINTEGRATED. HUB CAP WAS FOUND ON A TAXIWAY PARTIALLY SHAVED OFF & ALSO DISINTEGRATED. ACFT TOWED TO SDR VNAA202606120060Axle · corrodedLEFT RUSTED AND MISSING TOPCOAT ON ROOT RADIUS INBD AND OTBD SECTIONS PISTON, PISTON AXLE LT MLG. ROOT RADIUS INBD AND OTBD SECTIONS PISTON, PISTON AXLE LT MLG. WERE REPAIRED AND ATTENDED PER REO 670-32-11-361 REV. A.SDR VNAA202606120059Axle · corrodedEXPOSED MATERIAL ON ROOT SETTLEMENT AREA AT RH MLG PISTON AXLE. EXPOSED MATERIAL ON ROOT SETTLEMENT AREA AT RH MLG PISTON AXLE WAS ATTENDED PER REO 670-32-11-361 REV A.SDR 2026FA0000264Axle · out of toleranceDURING THE 1ST TIRE CHANGE ON THIS AIRCRAFT SINCE PRODUCTION, IT WAS FOUND THAT BOTH MLG AXLE NUTS HAD JUST FINGER TIGHT TORQUE. THE MAINTENANCE MANUAL CALLS OUT 550 IN LBS INTIAL TORQUE, BACK TO ZERO, THEN 265 -275 IN LBS FINAL TORQUE. IT WAS FOUND AFTER INSPSDR AALA202604081377Shock Absorber · collapsedAIRCRAFT WAS GROUNDED: UPON LANDING GEAR RETRACTION RECEIVED A NOSE LANDING GEAR SHOCK ABSORBER FAULT. FAULT CLEARED WHILE READING ECAM ACTIONS. THEN LANDING GEAR DOOR NOT CLOSED. FOLLOWED ECAM RECYCLED GEAR HANDLE, GEAR RETRACTED NORMALLY. THE FAULT REOCCURESDR 2026FA0000476Strut · fracturedPIPER PA-18 EXPERIENCED RIGHT HAND LANDING GEAR COLLAPSE AFTER LANDING ROLLOUT CAUSING DAMAGE TO MAIN LANDING GEAR AND RIGHT WING ASSEMBLY. DETAIL INSPECTION FOUND 2 EACH FRACTURES ON RIGHT HAND LANDING GEAR ASSEMBLY. RIGHT SHOCK STRUT HYDRASORB (PN 487 558) FSDR 2026FA0000149Bushing · missingDURING A RECENT LANDING GEAR INSPECTION AT STANDARD AERO VNY IT WAS NOTED THAT BOTH LH AND RH AXLES WERE MISSING BUSHINGS FOR STRUT ATTACH PINS TO AXLES, RESULTING IN DAMAGE REQUIRING REPLACEMENT OF BOTH AXLES AND THE RH STRUT PISTON SPHERICAL BEARING. BOTHSDR CVGA20260216002Strut · overservicedON LANDING, REVERSERS WOULD NOT DEPLOY. BELOW 60 K LOST BRAKES. USED EMERGENCY BRAKES TO STOP ACFT. AFTER TAXIING OFF RUNWAY, PLACED BRAKES IN ANTI SKID OFF POSITION. BRAKES WERE RESTORED. AIRSPEED INDICATOR SPEED LOW BAR WAS VISUAL. AFTER ACFT PARKED MAIN WHSDR SIMA20260123001Strut · underservicedLG WOW SYS FAIL AFTER TAKEOFF RETURN TO ORD. EMERGENCY DECLARED. PERFORMED LT MAIN LANDING GEAR SHOCK STRUT SERVICNG IAW AMM 12-12-07. LEAK CHECK PASSED NO FAULT DETECTED OPS CHECK GOOD.SDR VNAA2026041500002Sleeve · chafedLH MLG IB PISTON AXLE HAS CHIPPED METAL AT EDGE OF BRAKE UNIT ASSEMBLY BEARING SURFACE.SDR VNAA2026041500003Strut · scratchedRH MLG STRUT HAS 3 SCRATCHES ON REAR SIDE, ONE SCRATCH SHOWING BARE METAL.SDR SIMA20260119001Strut · dischargedAFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT POSITIVE RATE CALL ATTEMPTED TO RETRACT GEAR. LEVER WOULD NOT MOVE, APPROX. 3 SECONDS LATER LG WOW SYS FAIL EICAS MESSAGE APPEARED. RAN QRH CHECKLIST. MESSAGE CLEARED UPON TOUCHDOWN. EMERGENCY DECLARED NOT OVER WT. SDR DALA2026083104905Sleeve · corrodedCORROSION ALONG THE BEVELED PART OF THE BEARING SLEEVE. FITTING REPLACED ON NR 18. (1393346)(AIRCRAFT GROUNDED)SDR 2026FA0000010Strut · misoverhauledLANDING GEAR WOULD NOT RETRACT, CYCLED GEAR, ONCE GEAR WAS UP AND LOCKED, LEFT HYDRAULIC SYSTEM COMPLETE LOSS OF FLUID AND PRESSURE. UPON LANDING HAD TO SELECT THE LANDING GEAR DOWN, EMERGENCY BLEW LANDING GEAR DOWN FOLLOW EMERGENCY PRODUCERS. CONTACTED GULFSTSDR SCNA20260120038Strut · leakingDUE TO HISTORY OF LEFT MAIN LANDING GEAR STRUT LEAK- PERFORM REPLACEMENT OF THE ACTIVE AND SPARE SEALS IAW AMM 32-11-21-960-802. REMOVED AND REPLACED LT MAIN MANDING GEAR IAW CC 320400100.SDR SIMA202512310001Strut · dischargedLANDING GEAR WOW SYS FAIL CAUTION MESSAGE, RETURNED TO THE FIELD, DECLARED EMERGENCY, NO INJURIES. SERVICED NITROGEN TO LT MLG SHOCK STRUT TO CORRECT HEIGHT IAW AMM 12-12-07. NO MLG WOW OR NO DISPATCH MESSAGE NOTED ON THE EICAS.SDR AALA202512192290Strut · low pressureAIRCRAFT WAS NOT GROUNDED: AFTER TOUCHDOWN DURING MAX BRAKING CHECK AIRCRAFT PULLS SLIGHTLY LEFT. LEFT MAIN GEAR STRUT APPEARS LOW. SERVICED LEFT HAND MAIN LANDING GEAR SHOCK STRUT WITH NITROGEN. PER AMM12-15-31.SDR REXA2026052700738Strut · corrodedPITTING WAS FOUND ON MLG SHOCK STRUT LH SIDE BELOW IDENTIFICATION PLACARD. MLG SHOCK STRUT WILL BE REPLACED BY CARD 900-32-730-705SDR UIEA2025121101339Flex Line · crackedAFTER ROTATION, RECEIVED GEAR TILT EICAS MSG. GEAR SYNOPTIC PAGE SHOWED LEFT BODY GEAR TILT MSG. FOUND LT BODY GEAR POSITIONING ACTUATOR HYD LINE CRACKED. REPLACED THE LINE WITH TEMPORARY FLEX LINE IAW GMM 3.25.1 AND AMM 20-11-18.SDR DXTA2025112605816Packing · faultedWHILE LEVEL AT FL410, HEARD A LOUD THUMP IN THE NOSE FOLLOWED BY GEAR DISAGREE N AMBER CAS MESSAGE. NOSE GEAR INDICATOR WAS ALSO SHOWING YELLOW HASH INDICATION. QRH PROCEDURES WERE ACCOMPLISHED. INDICATIONS REMAINED UNTIL DESCENDING THROUGH FL230, HEARD ANOTHSDR 2025FA0000769Bushing Sleeve · debondedDURING ANNUAL INSPECTION IT WAS NOTED THAT THE LT MLG HAD A DISBONDED BUSHING LINER.SDR AALA202512022587Axle · failedAIRCRAFT WAS GROUNDED: DURING TAXI IN AIRCRAFT BEHIND US ADVISED THE TOWER WE HAD SMOKE COMING FROM LEFT MAIN NUMBER 1 TIRE. STOPPED THE AIRCRAFT AND CALLED FOR ARFF, WAS ADVISED TIRE WAS FLAT. WHILST PARKED AFTER 15 MINS ANTI-SKID INOPERATIVE LIGHT CAME ON. SDR DALA2025111208280Strut · dischargedDECLARED EMERGENCY FOR THE FLIGHT DUE TO WEIGHT ON WHEELS FAULT WITH POSSIBLE LOSS OF NOSE WHEEL STEERING. JACKED A/C. FOUND RT STRUT NOT FULLY EXTENDED. SERVICED RT STRUT, OPS CHECK GOOD. (LP# 8002764)SDR DALA2025102007647Strut · out of limitsSHIP 171 RT MLG UPPER PISTON TORSION LINK ATTACHMENT POINT FOUND OUT OF LIMITS. CORRECTIVE ACTION: REPAIRED DIA II A+B PER LGCMM 32-00-00 (1259603)SDR CALA2025100709749Spring · missingPDA 2 REFRENCE LOG 6494784 FOUND LEFT HAND GEAR SIDE BRACE SPRING MISSING ON ARRIVAL . .LANDING GEAR LEFT STRUT DOWNLINK SPRING MISSING FWD DRAG BRACE AFT SPRING INSTALLED NEW LEFT MLG DRAG BRACE AFT LOCK SPRING AND SPOOLHALF, REF AMM 32-32-07-400-802.SDR 2025FA0000563Bushing · debondedDURING ANNUAL INSPECTION IT WAS NOTED THAT LEFT MLG HAS DISBONDED BUSHING LINER.SDR 2025FA0000562Bushing · debondedDURING ANNUAL INSPECTION IT WAS NOTED THAT LEFT MLG HAS DISBONDED BUSHING LINER. IT WAS ALSO NOTED THE RIGHT BUSHING BEGINNING TO DISBOND.SDR 2025FA0000618Spring Strut · shearedAIRCRAFT LH MAIN SPRING STRUT SHEARED AT THE FUSELAGE ATTACH POINT. THE SERIAL NUMBER OF THE FAILED STRUT IS 6L85, RETURNED TO SERVICE IN 2017. VISUAL INSPECTION OF THE SPRING STRUT SHOWS THAT THE CRACK HAD BEEN THERE FOR A LONG TIME, EVIDENCED BY IRON OXIDE ASDR IPXA2028080700149Strut · corrodedSUSPECTED CORROSION RH MLG UPPER STRUT BODY - APPROX 14€? X 0.75€? TOTAL AREA BLENDED CORROSION AREAS IAW CMM 20-10-01 STEP 2.F AND 2.H. PITTING STILL REMAINS. MAPPED AND SENT DAMAGE PHOTOS TO ENGINEERING OF PITTED AREAS AND ATTACHED TO FAULT. PITTED AREAS SDR UIEA2025073001067Bushing · gougedLH BODY GEAR SIDE STRUT BUSHING (AIRCRAFT SIDE) IS GOUGED ON INSIDE.(<P>FABRICATED A NEW BUSHING PER BOEING SOPM 20-43-04 & EA 747-53-40-28-130537. NO FURTHER DEFECTS NOTED.</P>)SDR DALA2025061004419Bearing · gougedR/H MLG ASSEMBLY, AFT SPHERICAL BEARING GOUGED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 211-0002:3210-4001-RH/001 00496 REMOVED AND REPLACED SPHERICAL BEARING REF A220 AMP 32-11-03. RH MLG ASSEMBLY INSTALLATION ANDSDR 4DPA2025041300001Strut · underservicedPILOT REPORTED- AFTER NORMAL TAKEOFF LG AIR/GND FAIL CAUTION MESSAGE PRESENTED MOMENTS AFTER GEAR FINISHED ITS RETRACT CYCLE. CYCLED GEAR IN AIR TO NO AVAIL. MX, OPS AND CREW ELECTED TO PERFORM AN AIR RETURN. LANDING WAS NORMAL AND SPOILERS, T/R'S DEPLOYED ANDSDR FXTA20250411001Strut · low pressureRH MLG STRUT LOW AND NEEDS SERVICED.SDR ANCF20250331006Shock Absorber · corrodedON MARCH 31, 2025, DURING THE EXECUTION OF THE PUT THE AIRPLANE BACK TO SERVICE. DEPRESERVING PROCEDURE (DMC-B787-A-10-11-07-03A-820A-A), CORROSION WAS DETECTED ON THE RH SHOCK STRUT (PN 51010-38, SN S00VC) DURING THE EXAMINE THE LANDING GEAR COMPONENTS FOR CSDR FXTA20250408001Strut · leakingNO CHROME SHOWING ON RIGHT LANDING GEAR STRUTSDR IPXA2025032270655Cylinder · corroded**SUPPLEMENTAL SDR** FAULT - CORROSION - FOUND CORROSION ON INNER SURFACE OF R/H MAIN LANDING GEAR OUTER CYLINDER. (REPAIR). ACCOMPLISHED JOB I.A.W UPS EO-93133-REQ1 REV1. REVIEW COMPLETESDR IPXA2025031870655Cylinder · corroded**SDR FILED OPEN** FOUND CORROSION ON INNER SURFACE OF R/H MAIN LANDING GEAR OUTER CYLINDER. (REPAIR) PERFORMED NDT/PT FOR THE REWORKED AREA I.A.W SOPM 20-20-02 REV.29.<BR>RESULT: NO CORROSION INDICATION WAS FOUND.SDR 2025FA0000153Strut · brokenLEFT HAND REAR LANDING GEAR STRUT ASSEMBLY BROKEN AT BRACE ASSEMBLY ATTACHMENT BOLT DURING LANDING. OTHER MINOR DAMAGE TO SURROUNDING AREA OCCURRED. TOTAL TIME ON PART IS UNKNOWN.SDR DALA2025020700964Shock Absorber · dischargedSHIP 3248 - GEAR/ATB - DUE TO A L/G SHOCK ABSORBER FAULT THAT PREVENTED GEAR RETRACTION. CORRECTIVE ACTION: ACCOMPLISHED A FULL SERVICE OF THE NLG SHOCK STRUT. NLG 24GA AND 25GA PROXIMITY SENSORS REPLACED AS A PRECAUTION. (LP: 6821962)SDR QXEA2025010600003Strut · leakingREJECTED TAKE OFF AT ROUGHLY 100 KNOTTS FO MAY HAVE ADVANCED THROTTLE A HAIR TOO FAR. REMOVED FROM SERVICE. NO SIGNS OF HIGH ENERGY STOP OR ANY SIGNS OF TIRE DAMAGE - REF AMM 05-50-12-200-801-A 1(B). FOUND LEAKING MLG STRUT ON INSPECTION AT LEFT SIDE. C/W MCN
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