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 SWAA2012031702005Strut · corrodedRT MLG STRUT UPPER LUGS CORRODED. REMOVED AND REPLACED STRUT PER MM.SDR GQRR2012051027163Lock Ring · misinstalledLT SHOCK ABSORBER LOCKING RING ASSEMBLY INCORRECTLY CLOCKED.SDR UALA2012022401121Actuator · leaking'C' HYD LEAK, FLT DIVERTED. SLOW LEAK CENTER HYD SYS. AFTER LANDING FOUND RT MLG SOAKED WITH HYD FLUID. UNABLE TO DETERMINE IF BRAKE OR A LINE. TOO MUCH SMOKE. RPLC'D RT MLG TRUCK POSITIONER ACTUATOR PER MM.SDR 2012FA0000110Axle · corrodedDURING CLEANING IN PREPARATION FOR RECOVERING OF THE RT LANDING GEAR IT WAS NOTED THAT WOOD PLUG, PN 30941, WAS MISSING. SEVERE CORROSION WAS NOTICED INSIDE LOWER RADIUS OF THE AXLE TUBE. ESTIMATE THE LOWER PORTION OF TUBE WAS CORRODED MORE THEN 50 PERCENT OSDR JR2R2012031000067Strut · corrodedRT MLG OUTER CYLINDER INBD LUG FOR UPPER TORQUE LINK CORRODED. REPAIRED IAW RO CRJ9-32-0102.SDR DXTR20120131010Axle · corrodedCORROSION FOUND ON LT MLG WHEEL AXLE.SDR CA120202009Tube · cracked(CAN) LEFT MLG SHOCK STRUT ASSY, OUTSTOP TUBE FOUND CRACKED DURING O/H. LT MLG SEALS REPLACED AND NEW OUTSTOP TUBE INSTALLED. ACFT RETURNED TO SERVICE.SDR UALA2011121906961O-Ring · leakingRT MLG STRUT FAILED ON TAXI IN, WILL NOT HOLD FLUID. REPLACED RT MAIN LANDING GEAR STRUT SEALS PER MM.SDR AALA20111217TUL05Actuator · leakingSJO - CREW REPORTED MAIN LANDING GEAR DOOR OPEN EICAS MESSAGE. FLIGHT RETURNED SJO LANDED WITHOUT INCIDENT. FOUND LANDING GEAR HYDRAULIC FUSE TRIPPED. REPLACED RIGHT GEAR TRUCK TILT ACTUATOR. SYSTEM GROUND CHECK NORMAL OPERATION.SDR 2011FA0000811Axle · crackedCRACK FOUND IN EAR OF RT AXLE STUB DURING ANNUAL INSPECTION. UNKNOWN IF IT HAS EVER BEEN CHANGED BEFORE. UNKNOWN IF CRACK IS RESULT OF HARD LANDING OR FATIGUE (OR BOTH). ACFT IS INVOLVED IN A FLIGHT SCHOOL OPERATION. R & R PART, RESEALED STRUT. ACFT RELESDR CA111122002Cylinder · cracked(CAN) ASSEMBLY NAME, RT MLG MANUFACTURER, PN 49050-16, SN MA1382. CREW LOGBOOK STATES RT MLG AS STRUCTURAL DAMAGE THAT OCCURRED DURING TOUCHDOWN AFTER NOSE WHEELS CAME DOWN. THE ONLY COCKPIT INDICATION WAS A MASTER CAUTION FOR WOW INPUT & A PROX SYS 1 STATUSSDR MALA110252Strut · failedRIGHT MAIN STRUT HAS STRUCTURAL DAMAGE THAT OCCURRED DURING TOUCHDOWN AFTER NOSEWHEEL CAME DOWN. ONLY COCKPIT INDICATION WAS A MASTER CAUTION FOR WOW INPUT AND A PROX SYS FAULT 1 STATUS MESSAGE. THERE WAS FLUID POOLING AROUND RT MAIN STRUT AND PERSONNEL REPOSDR CA111117004Fitting · used(CAN) CRACK WAS FOUND DURING EDDY CURRENT INSPECTION IAW MM 5, 5-14-28.SDR CA111101005Bolt · undertorqued(CAN) DURING INSPECTION IT WAS FOUND THAT THE BOLTS WHICH ATTACH THE MLG AXLES ON BOTH SIDES HAD LOST THEIR TORQUE. BOTH ASSEMBLIES DISASSEMBLED AND INSPECTED, NO DAMAGE FOUND. THE WHEEL FAIRING PLATES WHICH WERE INSTALLED AT THOSE LOCATIONS WERE REMOVED, (WHSDR UALA2011102805848Shield · out of positionLT MLG TRUCK BEAM SHIELD FOUND HANGING DOWN. SHIELD REMOVED & PLACED IN LOB. NO DAMAGE TO BEAM. LOWER SURFACE OF THE BEAM MUST BE INSPECTED FOR DAMAGE BEFORE SHIELD IS REPLACED. INSTALLED NEW SHIELD AND HARDWARE.SDR 2011FA0000699Strut · crackedLEFT MAIN GEAR STRUT WAS FLAT, TRIED TO SERVICE, WHEN WE APPLIED NITROGEN PRESSURE HYDRAULIC FLUID CAME OUT OF A 3 INCH LONG CRACK IN THE STRUT BODY AND BEARING ASSY. AFTER TALKING WITH MFG THEY HAVE NEVER SEEN THIS TYPE OF FAILURE BEFORE.SDR IPXA11M69820Cylinder · inoperativeAIR TURN BACK. LANDING GEAR WOULD NOT RETRACT. R & R TRIM CYLINDER FUSE IAW AMM 32-37-06-4, WITNESSED GEAR SWING.SDR CA111024011Strut · cracked(CAN) NDT INSPECTION WAS PERFORMED AS PART OF THE ACFT 2200 HR O/H. TWO CRACKS WERE FOUND ON CENTER BEAM OF STRUT, STRUT REPLACED.SDR UVVR2011101900019Torque Link · bentAFTER TOUCHDOWN THE ACFT EXPERIENCED A VIBRATION IN THE LANDING GEAR. PERFORMED "INSPECTION AFTER LANDING GEAR VIBRATION" IAW THE ACFT FLEXIBLE MX SCHEDULE. INSP REVEALED THAT THE LOWER TORQUE LINK WAS BENT ON THE LT MLG SCISSORS ASSY.SDR CA150702003Seal · damaged(CAN) RH MLG STRUT LEAKING BEYOND AMM LIMITS. AFTER DROPPING THE LOWER BARREL TO REPLACE THE SEALS MAINTENANCE FOUND INTERNAL DAMAGE TO STRUT REQUIRING REPLACEMENT. MAINTENANCE REPLACED RT MLG.SDR C2XA11RI158Shock Absorber · defectiveFLT 2494 EWR-MCI CREW REPORTED 3 BANGS DURING GEAR RETRACTION AFTER TAKEOFF. CREW PERFORMED AIR RETURN BACK TO EWR UNEVENTFULLY. EWR MX REMOVED AND REPLACED THE RIGHT MAIN GEAR STRUT SHOCK ABSORBER AND SERVICED IAW EMB145 AMM 32-10-02 AND EC3210-01184. ACFTSDR SWIA201127958Strut · low pressureGEAR UP DISAGREE. (FLT 4704) SERVICED MAIN LANDING GEAR STRUT.SDR ALGA20110926001Crosstube · corrodedCROSSTUBE CORRODED BEYOND LIMITS IAW ICA D212-664, FIG 5-1.SDR ALGAR919115682Crosstube · corrodedCROSS TUBE CORRDED BEYOND LIMITS IAW AA00061 PAGE 19, FIG 2, TABLE 8.SDR SIMA201124904Strut · failedON FLIGHT 3240 THE CREW REPORTED THE RIGHT MAIN GEAR STRUT FAILED. THE CREW DECLARED AN EMERGENCY INBOUND TO DFW. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR STRUT IAW EMB 14SDR ALGAR82611RECV283Crosstube · corrodedCROSSTUBE HAS CORROSION BEYOND LIMITS.SDR AALA20110822LAX01Axle · shearedLAX - CREW REPORTED THAT AIRCRAFT MAY HAVE BLOWN A TIRE ON TAKEOFF. DEBRIS WAS REPORTED ON RUNWAY AFTER TAKEOFF FROM SDF. EMERGENCY DECLARED FLIGHT LAND LAX WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND NUMBER 3 WHEEL/TIRE/BRAKE ASSEMBLY AND AXLE SDR UALA2011082204445Fitting · missingLUBRICATION ZERK FITTING MISSING FROM OTBD END OF RIGHT MAIN GEAR TRUCK PIVOT PIN. HOLE IS WORN TOO LARGE TO INSTALL NEW FITTING. INSTALLED OVERSIZED ZERK FITTING. LUBES OKAY.SDR CA110815009Strut · cracked(CAN) CRACKED LT MLG FITTING (CLOSE TO THE TRUNNION FITTING). AIRLINE HAS A SPARE PART TO REPLACE AND HAVE DOWN LOADED THE FDR TO CHECK FOR HEAVY LANDING.SDR 2011FA0000489Strut · fracturedLT MLG VEE FAILED ON BOTH STRUT TUBES APPROX .5" ABOVE SUPPORT ANGLES ON AXLE CLUSTER. IT APPEARS FROM VISUAL INSP THAT BOTH STRUT TUBES MAY HAVE HAD PREVIOUS STRESS FRACTURES PRIOR TO FAILURE DUE TO DARK CRACK WORKING INDICATIONS ADJACENT TO SHINY FRESH CRACSDR HYIA7037ERTXLAxle · crackedPILOT REPORTED, ON COMPLETION OF FLIGHT 1033, WHILE PARKING AIRCRAFT, RIGHT MAIN GEAR LOCKED UP. MAINTENANCE INSPECTED AIRCRAFT, FOUND RIGHT MAIN LANDING GEAR AXLE CRACKED. MAINTENANCE REMOVED AND REPLACED LOWER BARREL AND AXLE ASSEMBLY. AIRCRAFT RELEASED BSDR 2012FA0000320Housing · crackedACFT ENCOUNTERED A SLIGHTLY HARDER-THAN-NORMAL LANDING. ON PARKING, IT WAS NOTICED THAT FLUID WAS ON THE GROUND BELOW THE RT MAIN GEAR. JACKING THE ACFT, CLEANED AND INSPECTED THE STRUT FOR ANYTHING OBVIOUS. DISASSEMBLED, RESEALED AND REASSEMBLED THE LOWER SDR FCPR20110006Torque Knee · crackedDURING 6 YEAR INSPECTION OF LANDING GEAR, FOUND INDICATION OF CRACK ON TORQUE KNEE.SDR QXEA2011070100475Axle · corrodedDURING THE REMOVAL OF THE NR2 BRAKE, FOUND THE NR1 AXLE TO BE CORRODED AND THE NR2 BRAKE AND WHEEL BEARING LAND. CORROSION WAS PEELING PAINT AND PITTING CORROSION. FERRIED TO REPAIR. R & R NR 1 MLG AXLE IAW 32-11-04-000-801 AND 32-11-04-400-801. RETURNED TO SDR V8Z2011F00000O-Ring · damagedO-RING IN THE LT MLG RETRACT CYLINDER FAILED WHICH ALLOWED THE HYD SYS OIL TO DRAIN. O-RING WAS MOST LIKELY DAMAGED DURING INSTALLATION. DURING INSTALLATION OF THIS PART O-RING LUBE OR HYDRAULIC OIL MUST BE USED TO KEEP UNIT FROM BEING DAMAGED.SDR ALGAR52611AA1201ACrosstube · corrodedCORROSION DAMAGE TO CROSSTUBE BEYOND REPAIR LIMITS IN ZONE "C".SDR ALGAR52611AA1454Crosstube · corrodedCORROSION DAMAGE TO CROSSTUBE BEYOND REPAIR LIMITS IN ZONE "C".SDR CA110427017Strut · crackedWHILE PERFORMING THE 12 MONTH INSPECTION, A CRACK WAS NOTED IN THE LT REAR STRUT. THIS CRACK WAS 7" LONG RUNNING ROUGHLY MIDPOINT AND UP UNDER THE STEP. THE CRACK DID NOT START OR END AT ANY BOLT HOLES. THE CRACK WAS PERPENDICULAR TO THE BOLT HOLES AND RAN PASDR 201100703Strut · fracturedUPON LANDING THE ACFT JUST AFTER TOUCHDOWN, THE RT MAIN GEAR STRUT FAILED AND COLLAPSED ALLOWING THE RT WING STRIKE THE GROUND. THE STEEL STRUT TUBE FRACTURED IN 2 SECTIONS, PROBABLY AT A STRESSED LOCATION. THE LANDING WAS DESCRIBED AS NORMAL WITH NO UNUSUALSDR USAA2011050391739Pin · corrodedSAL - S4 - CORROSION ON LEFT MAIN LANDING GEAR UPPER TORQUE LINK PIN. REPLACED LEFT MAIN LANDING GEAR UPPER TORQUE LINK PIN IAW A319 AMM 32-11-27.SDR QXEA2011041200282Bearing · failedLT MAIN BRAKE, OTBD WHEEL, WAS SMOKING AFTER FLIGHT WITH METAL FILINGS IN WHEEL SLOTS. REMOVED NR 1 AND NR 2 MLG TIRE AND WHEEL ASSY AND BRAKE ASSY IAW MX 6324101 AND 6324201. REMOVED NR 1 AND NR 2 WHEEL SPEED TRANSDUCERS IAW AMM TASK 32-46-11-000-801. REMOSDR UALA2011031501238Strut · underservicedTOOK 3 TRIES TO GET THE LANDING GEAR HANDLE TO MOVE TO GET THE GEAR TO RETRACT. FOUND BOTH MAIN GEAR STRUT UPPER CHAMBERS LOW. ACP FULL SVC ON MAIN GEAR. ACP GEAR SWING 3 TIMES, OPS GOOD.SDR 2011FA0000190Cylinder · brokenRT MLG LOWER STRUT FELL OFF WHEN ACFT LIFTED OFF THE RUNWAY AT 2H2. STUDENT PILOT FLEW AND LANDED RESULTING IN DAMAGE TO THE UPPER LANDING GEAR STRUT HSG. WHEN LOWER STRUT DEPARTED UPPER HSG, IT STRUCK THE FLAP, DAMAGING FLAP SKIN. RT MLG UPPER TORQUE LINK SDR SWAA111202Bolt · corrodedDURING SCHEDULED 22Y CHECK, FOUND LT MLG SHOCK STRUT T-BOLT ATTACH BOLT BORE CORRODED. REMOVED AND REPLACED T-BOLT PER MM.SDR DXTA2011022304475Strut · leakingGEAR WOULD NOT RETRACT AFTER TAKEOFF, HANDLE WOULD NOT MOVE. HEARD A LOUD "THUMP" IN THE NOSE WHEEL AREA PRIOR TO LANDING AT OUR DIVERSION AIRPORT. CHECKED VOLTAGE AT GEAR HANDLE CONNECTOR PLUG VOLTAGE WAS LESS THAN REQUIRED, CHANGED LANDING GEAR LOGIC MODULESDR 2011FA0000133Axle · shearedDURING DISASSEMBLY OF THE LANDING GEAR AT O/H. WHILE ACCOMPLISHING THE UNTORQUE CHECK IAW SP 145-32-0097, THE NUT FELL OFF THE SUBJECT AXLE AS TORQUE WAS APPLIED TO THE UPPER ATTACH AXLE. THE AXLE HAD SHEARED AT THE POINT WHERE THE THREADS ENTERED THE NUT. SDR DXTA2011021404466Strut · out of limitsAFTER LANDING FROM THE RT SEAT, BRAKE PEDALS WENT TO THE FLOOR. THEY EVENTUALLY GRABBED BUT LOW TO THE FLOOR. ON TAXI IN FROM THE LT SEAT, THE BRAKES PULLED HARD RT; TRIED THE BRAKES AGAIN FROM THE RT SEAT, THEY GRABBED VERY LOW. FOUND MLG STRUTS FULLY EXTESDR USAA2011020890594Pin · corrodedSAL - MAJOR REPAIR - S4 CHECK - CORROSION ON LEFT MLG BOTTOM TORQUE LINK PIN. REPLACED LEFT MLG BOTTOM TORQUE LINK PIN IAW A319 AMM 32-11-27.SDR USAA2011020890584Pin · corrodedSAL - MAJOR REPAIR - S4 CHECK - CORROSION ON THE LEFT MLG TORQUE LINK APEX PIN. REPLACED THE LEFT MLG TORQUE LINK APEX PIN IAW A319 AMM 32-11-29.SDR AALA20110124AFW01Swivel Fitting · corrodedLEFT MAIN LANDING GEAR SIDE STRUT SWIVEL FITTING CORRODED. REMOVED A MAX OF 0.150" CORROSION ON THE LUG FACE PER EA B767-57-014875.
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