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 2016FA0000382Scissor Link · crackedWHEN THE ACFT WAS ON FINAL TO RUNWAY 27, THE CONTROLLER THOUGHT THERE WAS SOMETHING THAT DIDN'T LOOK RIGHT WITH THE ACFT, SO HE UTILIZED BINOCULARS AND NOTICED THAT THE FIXED RT MAIN GEAR APPEARED TO BE HANGING ABNORMALLY FROM THE WING, BY ONLY THE HYDRAULIC BSDR SH5R201609090001Axle · crackedRECEIVED NOTIFICATION THAT DURING TAKEOFF THE NR 1 MAIN WHEEL ASSY DEPARTED THE ACFT. CREW CONTINUED ON WITH TAKEOFF CLIMB AND DIVERTED FOR AN UNSCHEDULED LANDING. AIRCRAFT HAD AN UNEVENTFUL LANDING. UPON INITIAL INSPECTION OF THE AIRCRAFT, IT WAS VISUALLY SDR DALA2016072605569Nut · looseCREW REPORTED THAT THE AIRCRAFT WAS SHAKING VIOLENTLY WHEN BRAKES WERE APPLIED MAKING IT DIFFICULT TO STOP. MAINTENANCE FOUND AXLE NUTS ABOUT 1/2 TURN LOOSE. TORQUED ALL MAIN AXLE NUTS. NO FURTHER ISSUES NOTED.SDR 1CSR201607011Shock Absorber · leakingLEFT LANDING GEAR SHOCK ABSORBER LEAKING INTERNALLY. FOUND GLAND NUT SAFETY WIRE BROKEN. R & R LT LANDING GEAR SHOCK ABSORBER IAW AMM 32-10-14, PAGE 401-406. SERVICED SHOCK ABSORBER IAW AMM 32-10-14, PAGE 301-304.SDR AALA201606279013Shock Absorber · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RT MLG SHOCK ABSORBER AT THE LOWER TORQUE LINK MOUNTING LUGS. REPLACED RT MLG SHOCK ABSORBER.SDR AALA201606279012Shock Absorber · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LT MLG SHOCK ABSORBER AT THE LOWER TORQUE LINK MOUNTING LUGS. REPLACED RT MLG SHOCK ABSORBER.SDR 29GA2016061900001Strut · lowCONFIG ILLUMINATED DURING CLIMBOUT AND THEN WAS INTERMITTENT THROUGHOUT FLIGHT. FOUND MLG STRUTS NOT FULLY EXTENDING, CAUSING WOW SWITCHES TO INTERMITENTLY ACTIVATE CAUSING CONFIGURATION WARNING. FOUND MLG STRUTS UNDER SERVICED. SERVICED BOTH MLG SHOCK STRUSDR ASMF2016072600016Axle · damagedDURING TRANSIT CHECK, IT WAS DETECTED A HIGH TEMPERATURE LOW PRESSURE AT MAIN WHEEL ASSY NUMBER 4. MAINTENANCE PERSONNEL PERFORMED THE FLAT SPOTTED TIRES CONDITIONAL INSPECTION IAW AMM 05-51-16-210-801 DETECTING PAINT ERODED IN THE TRANSDUCTOR HOUSING AND DISSDR 2016FA0000234Axle · failedAXLE FAILURE ON LANDING RESULTING IN GROUND LOOP, PROP STRIKE, AND SUBSTANTIAL DAMAGE TO EMPENNAGE AND LT WING. THE ACFT JUST MODIFIED TO 29 X 11 X 10 AIR HAWKS FROM BUSHWHEELS AND 10" WHEELS. THE AXLE WAS THE STOCK ALUMINUM.SDR AALA20160422007Strut · lowAIRCRAFT WAS GNDED. FLIGHT CREW REPORTS THAT LT WING RAISES UP AT TOUCH DOWN WITH NO CONTROL INPUT. MX CONFIRMS NO FLIGHT ABNORMALITIES. SUSPECT STRUTS NEED SERVICING. ACCOMPLISHED STRUT SERVICING IAW AMM 32-11-02.SDR UIEA2016031900194Jam-Nut · looseEICAS MSG, GEAR DOOR DISPLAYED. WHEN RAISING GEAR AFTER TAKEOFF, THERE WAS AIRFRAME VIBRATION. ACCOMPLISHED QRH PROCEDURES & EICAS MSG CLEARED & VIBRATION STOPPED. TORQUED RT BODY GEAR SHOCK STRUT, INBD DOOR LINKAGE ROD JAM NUT IAW MM 32-14-05. INSPECTED RSDR 2016F00096Bolt · failedLEFT MLG SCISSORS ASSY. THE AN310-5 NUT GALLED OFF THE END OA AN AN175-20 BOLT. RESULTING IN THE FAILURE OF THE LT MLG SCISSORS ASSEMBLY.SDR IPXA2016030500370Skid · damagedDURING GEAR RETRACTION, TAILSKID LIGHT ILLUMINATED, TAILSKID EICAS MSG ILLUMINATED, TAILSKID LIGHT & EICAS EXTINGUISHED UPON GEAR EXTENSION. EVALUATING DAMAGE. R & R TAILSKID ASSY AND OPS CK OF INDICATION IAW AMM 32-71-06-402-001.SDR TIMA20160304004Torque Knee · crackedDISCOVERED A CRACK IN THE RT MLG UPPER TORQUE KNEE, DURING A SCHEDULED INSPECTION. THE CRACK WAS IN THE RADIUS TO THE SINGLE BOSS. REPLACED THE UPPER TORQUE KNEE WITH A NEW PART. CRACK DISCOVERED AT 2772 CYCLES SINCE OVERHAUL.SDR DALA2016030301619Bushing · corrodedCORROSION FWD BUSHING OF PINTLE PIN AT RIB 5 ON RETRACTION ACTUATOR ON LT MLG REPLACED BUSHING, 1 EA OF FWD POSITION ON RETRACTION ACTUATOR ON LT MLG IAW CMM 32-11-33.SDR CA160224010Shaft · fractured(CAN) DURING A ROUTINE LANDING GEAR INSPECTION THE RT UPPER TORQUE LINK SHAFT WAS FOUND TO BE PROTRUDING FROM THE RT TORQUE LINK. THE SHAFT HAD FRACTURED INSIDE THE STRUT. PROTRUDING PORTION WAS APPROX 1 1/2` LONG. THE REMAINING PORTION OF THE SHAFT WAS REMOVESDR CA160315001Axle · cracked(CAN) RIGHT MAIN LANDING GEAR FOUND CRACKED AT TORQUE LINK LOWER ATTACHMENT POINT ON THE STUB AXEL AND OLEO PISTON ASSEMBLY DURING ROUTINE MAINTENANCE. CRACK WAS FOUND BY VISUAL INSPECTION AND IS APPROXIMATELY THREE-QUARTERS OF THE WAY THROUGH THE ATTACHMENT PSDR XCGA560HM21916Strut · stuckLANDING GEAR FAILED TO RETRACT AFTER TAKEOFF WHEN SELECTED TO THE UP POSITION. RED GEAR UNLOCK LIGHT ILLUMINATED BUT ALL 3 GEAR LIGHTS REMAINED GREEN. THE ANTI-SKID LIGHT ALSO BLINKED ON AND OFF. THE FLIGHT CREW SELECTED GEAR DOWN AND ALL INDICATIONS RETURNSDR WPR16LA068Axle · brokenLEFT AXLE BROKEN IN HALF ON LANDING CAUSING ACCIDENT AND SUBSTANTIAL DAMAGE TO ACFT. AXLE FOUND SEPARATED IN 2 INBD OF INNER BEARING RACE LOCATION. EVIDENCE NOTED OF POSSIBLE PRIOR DAMAGE IN AREA OF CRACK AND SEPARATION, POTENTIALLY FROM PRIOR ACCIDENT OR USSDR IPXA2016020799002Cylinder · overservicedAFTER TAKEOFF, LANDING GEAR WILL NOT RETRACT. MAINTENANCE BLED AIR FROM LT MLG TRUCK BOGIE TRIM CYLINDER IAW AMM 32-37-01. TRUCK BEAM TRIM INTERLOCK OPS TEST GOOD IN IAW 32-37-00.SDR AALA20160216009Strut · corrodedBORE G2 MACHINED TO 1.685 INCH TO REMOVE CORROSION, MAX REWORK DIMENSION 1.597 INCH. PART SCRAPPED. DOES NOT MEET ULTIMATE STRENGTH LIMITS IAW ENGINEERING. COMPONENT IN SHOP MX.SDR CA160126006Torque Link · defective(CAN) LT MLG TORQUE LINKS FOUND OVER CENTER.SDR JGVR20151230001Pin · brokenWHILE PERFORMING A FACTORY C-INSPECTION, TASK ITEM 32-10-02, REINSTALLING/TORQUEING THE ORIGINAL RT MAIN LANDING GEAR SHOCK STRUT UPPER ATTACHMENT PIN TO THE LANDING GEAR AND THE HEAD BROKE OFF PRIOR TO REACHING THE MINIMUM TORQUE VALUE IAW AMM 32-10-02. VISUSDR CA151214016Torque Link · broken(CAN) FLIGHT CREW CONTACTED MAINTENANCE AFTER LANDING AND EXPERIENCED WHAT THEY THOUGHT WAS A STICKY LT BRAKE. MAINTENANCE REQUESTED THAT THE FLIGHT CREW LOOK AT THE LT BRAKES & GEAR AND SEE IF THEY SAW ANYTHING ABNORMAL. FLIGHT CREW REPORTED BACK THAT WHAT THSDR AALA20151211010Cylinder · corrodedAIRCRAFT WAS GNDED. FOUND CORROSION ON RT MLG STRUT CYLINDER WHILE REMOVING GEAR INSPECTION PATCH. ACCOMPLISHED STEP B THROUGH STEP H OF AARD 32-10-00-4 IAW EA 256707 FOR TIME LIMITED REPAIR.SDR CA151207016Strut · cracked(CAN) A CRACK WAS VISUALLY DETECTED AT THE UPPER END ON THE LT MAIN LANDING GEAR SHOCK ABSORBER STRUT. AT THE TIME THE AIRCRAFT WAS UNDERGOING A MAJOR INSPECTION AS REQUIRED BY THE MANUFACTURE.SDR CA151205001Axle · cracked(CAN) DURING ROUTINE EMMA INSPECTION AXLE P/N C6UM1134-27 WAS FOUND TO HAVE A SUSPECTED CRACK AROUND BARREL APPROXIMATELY 3" LONG. PART WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE.SDR HYIA2015FA0000642Axle · crackedDURING OPERATOR RUTTING MAINTENANCE MECHANIC NOTICED UNUSUAL MARKS ON AXLE. THEN SENT TO NDT AND CRACK FOUND ON INNER AXLE.SDR HYIA20151203001Axle · crackedDURING INSPECTION, A CRACK WAS FOUND ON THE LT MLG AXLE. THE PART WAS REMOVED & SENT FOR NDT INSPECTION, WHERE THE CRACK WAS CONFIRMED.SDR CA151119011Axle · cracked(CAN) WHILE DOING A ROUTINE TIRE REPLACEMENT, UPON REMOVAL OF THE TIRE ASSY FROM THE LT AXLE, THE AXLE WAS CLEANED AND INSPECTION REVEALED WHAT LOOKED LIKE A CRACK OR INCLUSION ON THE AXLE AT THE END OPPOSITE WHERE THE COTTER PIN/NUT SECURE THE WHEEL ASSY. ITSDR AALA20151123010Strut · corrodedRIGHT MLG HAS PITTING & CORROSION IN THE TAPE PATCH AREA REFERENCE MCM CARD 5946, NEEDS REPAIR 32-10-00, REPAIR NR 4. RIGHT GEAR CORROSION REMOVED & TREATED IAW AARD 32-10-00 REPAIR 4 & EA 256111.SDR 2015FA0000612Leg Assy · brokenWHILE EXECUTING A LANDING, PILOT STATED THE MAIN WHEELS TOUCHDOWN FIRST, AS SOON AS NOSE WHEEL TOUCHED DOWN THE NOSE GEAR COLLAPSED CAUSING THE PROPELLERS TO STRIKE THE GROUND AND ACFT SKIDDED TO A STOP WITH PILOT AND 1 PASSENGER EXITING THE AIRCRAFT WITH NO ISDR VQIA2015121100038Strut · malfunctionedLANDING GEAR SHOCK ABSORBER FAULT. ACFT WAS FLOWN AS MAINTENCE FERRY UNDER SPCECIAL FLIGHT PERMIT 52110302015. FOUND PROXIMITY SENSOR 24GA OUT OF LIMITS IAW AMM 32-31-73-200-002-A. REPLACED 24GA AND 25GA PROXIMITY SENSORS AS PRECAUTIONARY IAW AMM 32-31-73-4SDR 2015FA0000637Cylinder · brokenDURING LANDING, THE RT MLG LOWER OLEO PISTON ASSY CAME OUT OF THE UPPER CYLINDER ASSEMBLY. DURING SUBSEQUENT INCIDENT INVESTIGATION IT WAS NOTED THAT THE TORQUE LINK ATTACH LUGS APPEAR TO HAVE FAILED ON THE UPPER STRUT CYLINDER ASSY ALLOWING THE LOWER ASSY TOSDR FDEA201510143210Strut · malfunctionedGEAR HANDLE WOULD NOT RAISE. IT TOOK SEVERAL ATTEMPTS & AFTER WORDS HAD LEVEL 1, ANTI-SKID NO TEST. R & R NLG SHOCK STRUT IAW WC 32T2101. PERFORMED GEAR SWING IAW MM 32-30-00-5. OPERATIONS CHECKED GOOD COMPLIED WITH SECOND WC 32T2701 FOR INSTALLATION. OKSDR SWAA2015110445745Strut · corrodedLEFT MLG FWD LUG, FWD LUG SHOCK STRUT BORE CORRODED. R & R LT LG IAW MT.SDR HYIA20150914001Axle · brokenON TAXI OUT, PILOT REPORTED THE RT MAIN WHEEL BROKEN. PERFORMED VISUAL INSPECTION ON RT MLG & FOUND THE RT MLG AXLE BROKEN & MAIN TIRE WITH DAMAGE. R & R THE RT MLG LOWER BARREL IAW MM CHAPTER 32-10-00. OPERATIONS CHECKED GOOD. R & R RT MLG WHEEL ASSEMBLY SDR CA150916003Cylinder · loose(CAN) THE LT MLG OLEO ASSY DETACHED FROM THE AXLE STRUT ASSY. THE OLEO CYLINDER HAD UNTHREADED FROM THE CAP ON THE AXLE STRUT, THE LOCK NUT WAS STILL ATTACHED TO THE CYLINDER BUT DID NOT PREVENT THE CYLINDER FROM UNTHREADING.SDR 2015FA0000519Bolt · corrodedAFTER LANDING, DURING THE LANDING ROLL THE LT MAIN GEAR WHEEL COLLAPSED. RESULTING IN DAMAGE TO THE LT WING AND LT SIDE OF FUSELAGE. DURING THE INSPECTION OF THE WHEEL ASSEMBLY, IT WAS OBSERVED THAT 2 OF THE LT GEAR WHEEL ATTACH BOLTS WHICH HAD SHEARED OFF, SDR SWAA2015091543925Link · corrodedLEFT MLG SWING LINK ATTACH UPPER & LOWER AFT POSITION CORRODED. REPAIRED SWING LINK IAW CMM.SDR 7C7A20150715056Yoke · chafed0.25 INCH DIAMETER CHAFE DAMAGE TO RT MLG GEAR YOKE.SDR DALA2015062403983Strut · damagedRT MLG TRUCK ASSY DAMAGED. R & R PISTON ASSY AND TRUCK ASSY IAW CMM 32-11-36, REV 21.SDR CA150623004Piston · damaged(CAN) WHILE MAINTENANCE WERE CARRYING OUT SCHEDULED PHASE INSPECTION, PHASE 2, 400 HOUR, IT WAS DISCOVERED THAT THE RT SIDE MLG OLEO PISTON WAS DAMAGED. THE PISTON CHROME WAS FLAKING OFF & THERE WERE SCORES & SCRATCHES IN THE PISTON FWD AREA. R & R THE LG UNSDR CA150618005Torque Knee · broken(CAN) AFTER TOUCHDOWN THE PILOTS FELT A VIBRATION, ACFT STOPPED THEN TAXIED TO THE RAMP & IT WAS FOUND THAT THE LT MLG, UPPER & LOWER TORQUE LINK WERE FOUND BROKEN OFF AT ATTACH POINT. THE TORQUE LINKS WERE REPLACED. ACFT INSPECTED & RETURNED TO SERVICE. WSDR VQIA2015072400025Strut · underservicedACFT EXPERIENCED DIFFICULTY RETRACTING THE LANDING GEAR. AFTER TAKEOFF, THE LANDING GEAR HANDLE WOULD NOT RELEASE AND MOVE TO THE UP POSITION. AFTER APPROXIMATELY 1 MINUTE, THE GEAR HANDLE RELEASED AND THE LANDING GEAR RETRACTED NORMALLY. THE ACFT CONTINUEDSDR 2015FA0000201Axle · looseFOUND THE AXLE BOLTS LOOSE THAT ATTACH THE AXLES TO THE MLG. RIGHT AXLE BOLTS WERE LOOSE TO THE POINT OF MOVEMENT BETWEEN THE AXLE AND THE MAIN GEAR AND LT AXLE BOLTS COULD NOT BE FELT LOOSE BY MOVEMENT IN THE AXLE, BUT WERE NOT TIGHT WHEN CHECKED WITH A WRENSDR SWAA2015051439663Strut · crackedLEFT MLG SHOCK STRUT LUG OTBD HOLE, HAT BUSHING CRACKED. R & R STRUT IAW CMM & AMM.SDR CA150511007Torque Link · broken(CAN) UPON LANDING, PILOT FELT LIKE HE HAD A FLAT. NO FLAT NOTED BUT UPON INSPECTION, IT WAS NOTED THAT THE RT MLG UPPER TORQUE LINK WAS FOUND TO BE BROKEN IN HALF ABOUT ONE INCH FROM THE ATTACH POINT TO THE LOWER TORQUE LINK. SPECIAL INSPECTION HAS BEEN INISDR CA150506011Axle · corroded(CAN) CORROSION FOUND ON THE NR 1 MLG AXLE. CMM 32-11-03 PAGE 605 STATES IN PART ON NON-WEAR SURFACES THE DEFECTS TO BE POLISHED OUT, MUST NOT EXCEED 0.005 INCHES & FOR WEAR SURFACES DEFECTS MUST NOT EXCEED 0.0005 INCHES. INSPECTION REVEALED PITTING ON NON-WSDR SWIA201541091Axle · corrodedRIGHT MLG NR 4 AXLE CORRODED, C-CHECK, RO 4/21/15, REPAIRED RT MLG NR 4 AXLE REF REO.
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