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 CA050610002Fork · cracked(CAN) DURING A WALKAROUND THE PILOT NOTICED THE BRAKE DISC WAS RUBBING AGAINST THE SIDE OF THE GEAR FORK. AFTER THE WHEEL ASSEMBLY WAS REMOVED A CRACK WAS FOUND ON THE AXLE AT THE INNER MOST BEARING RIDE LOCATION. THE CRACK WAS MORE THAN A THIRD OF THE WAY ASDR CA050607001Saddle · cracked(CAN) THE RT OUTER SADDLE CRACKED AT THE AFT SPLIT LINE AT THE RIDGE LINE FOLLOWING THE CONTOUR OF THE SKID TUBE AND CROSS TUBE. THE CRACK TURNS 90 DEGREES FROM THE TOP OF THE SADDLE TO THE REAR. THE PART WAS SENT TO HEADQUARTERS FOR INSPECTION.SDR ASMF200506004Strut · leakingDURING OVERNIGHT SERVICE, WAS DETECTED AN HYDRAULIC LEAK IN SHOCK STRUT OF NOSE LANDING GEAR. THE SEALS WERE REPLACED BUT WHEN TAKING OUT THE PISTON, A BUSHING WAS DETECTED DAMAGED. THE SHOCK STRUT OF NOSE LANDING GEAR SEALS WERE REPLACED IAW MM 32-21-11, TESTSDR MALA050436Strut · damagedAFTER TAKEOFF AT APPROX 100-200 FT RAD ALT THE FD AND AUTOTHROTTLES FAILED AND THE NO CAT 3 LAND ILLUMINATED ON THE FGS ADVISORY. THE LANDING GEAR SELECTOR COULD NOT BE MOVED FROM THE DOWN POSITION UNTIL APPROX 2 MIN AFTER LIFT OFF. THEN THEY WERE ABLE TO SESDR QXEA200500936Strut · scratchedYYC - NOSE LANDING GEAR PISTON ASSEMBLY HAS SEVERAL SCRATCHES AFT FACE OF CHROME. REPAIRED IAW HORIZON AIR EA R-32-188 AND REO 670-32-21-0051.SDR SA05047Strut · lowPIT FLT 219 ENROUTE PIT - TPA, AFTER TAKEOFF, ECAM MESSAGE 'L/G SHOCK ABSORBER FAULT' DISPLAYED. THE FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE SERVICED THE NOSE LANDING GEAR STRUT.SDR CA050503003Saddle · cracked2 PIECE SADDLE, CRACKED ACROSS BOLT HOLE, .250 TO EDGE AND .750 TO BEND STEP RADIUS. FORWARD SIDE, 3RD BOLT HOLE DOWN FROM TOP. PART REPLACED WITH 1 PIECE SADDLE.SDR DXTA200500695Strut · underservicedRIGHT MAIN LANDING GEAR DID NOT FULLY RETRACT AFTER TAKEOFF, CONFIRMED BY FLY BY OF TOWER CONTROLLER. RE-SERVICED RIGHT MLG STRUT IAW HAWKER 800XP AMM 12-32-00, PERFORMED 25 GEAR RETRACTIONS / EXTENSIONS IAW HAWKER 800XP AMM 32-30-00, OP CHECK GOOD.SDR 2005FA0000739Axle · broken(REF: PO0043200R011)AXLE WAS FOUND BROKEN NEAR THE CENTER POINT THAT WAS CONCEALED BY THE TRUCK BEAM DEGES OF THE FRACTURE SHOW SEVERE CORROSION AND PEELED CHROME PLATING. (K)SDR 2005FA0000585Strut · brokenFAILURE OF THE (CAST) MAIN LANDING GEAR STRUT CYLINDER. CRACK IN UPPER SCISSOR ATTACHMENT RESULTED IN LOSS OF GEAR AND STRUT ASSY DURING TAKE-OFF.SDR COMA0560231Axle · wornFLIGHT 5907 DURING CLIMBOUT OF CVG, RECEIVED A LANDING GEAR DISAGREE WARNING MESSAGE, CREW DECLARED AN EMERGENCY AND RETURNED TO THE FIELD, LANDING WITHOUT INCIDENT. REPLACED THE NLG LOWER STRUT. ASSEMBLY.SDR 05FDEA00801Strut · damagedON TAKEOFF FROM MEM, CENTER GEAR INDICATED UNSAFE UP. BOTH DISPLAYS SHOWED UNSAFE UP. COMPLIED WITH ALL CHECKLISTS AND LANDED KMEM 36C. REMOVED CENTER LANDING GEAR SHOCK STRUT, PER FEDEX WORK CARD 32T7101. REMOVED THE CTR LDG AFT W/W LT AND RT GEAR DOORS SDR BB05026Axle · fracturedSJU - FL596 - UPON LANDING, CREW FELT SLIGHT PULL TO THE RIGHT ON ROLL OUT AND TAXI. ON POST-FLIGHT INSPECTION, THE NR 8 WHEEL WAS CANTED.SDR DXTA200500641Strut · underservicedAFTER TAKEOFF ON GEAR RETRACTION GOT ALL 3 GREEN LIGHTS AND THE RED UNLOCK LIGHT STAYED ON. COULD HEAR THE LOUD AIR NOISE AND THE GEAR CYCLING AT LEAST 4 TIMES. FINALLY THE GEAR CAME COMPLETELY UP AND THE UNLOCK LIGHT WENT OUT. JACK AIRCRAFT & CONFIRMED DISSDR DXTA200500633Strut · underservicedAFTER DEPARTURE FROM MIDWAY, GEAR HANDLE WOULD NOT RELEASE FROM THE DOWN POSITION, COULD NOT BE RAISED, AIRCRAFT RETURNED FOR LANDING. JACKED ACFT AND FOUND THE NOSE STRUT NOT EXTENDING PROPERLY. CHECKED SERVICING AND FOUND THAT THE AIR PRESSURE WAS LOW. SESDR CA050318003Bolt · broken(CAN) DURING THE WALK-AROUND FOR A SERVICE CHECK, THE MECHANIC DISCOVERED THE HEAD OF THE BOLT BROKEN OFF AND MISSING FROM THE RT MAIN LANDING GEAR SIDE STRUT. THIS BOLT ATTACHES THE SIDE STRUT UPPER AND LOWER SEGMENTS AT THE PIVOT. THE BOLT WAS REMOVED AND SDR 2005FA0000407Strut · damagedDURING 300 HOUR INSPECTION (GEAR SERVICE) THE INNER STRUT CHROME WAS FOUND DAMAGED APPROXIMATELY .001 INCH DEEP. PROBABLE CAUSE: WEAR OF SEALS CAUSING THE UPPER CAM TO CONTACT THE INNER CYLINDER. INSPECTION REPACK OF THE NOSE LANDING GEAR ASSY AT 3,000 LANDISDR ARWA20050301Link · crackedLEFT MAIN GEAR SCISSOR CRACKED AT BOLT HEAD OF BOLT BROKEN FOUND AT POST FLIGHT AT MSLP. REMOVED AND REPLACED BOLT AND UPPER LINK IN ACCORDANCE WITH MM 32-11-4.SDR A6WA200540076Strut · dischargedAFTER TAKEOFF, THE NOSE GEAR DID NOT RETRACT. SERVICED HYDRAULIC FLUID AND NITORGEN TO THE NOSE STRUT. ADJUSTED THE NOSE OLEO CENTER EXTEND SENSOR WITHIN LIMITS. (M)SDR MASA200500136Strut · damagedASH 2762 FROM PHL TO ALB RETURNED TO THE FIELD DUE TO A GEAR DISAGREE. MAINTENANCE IS IN THE PROCESS OF TROUBLESHOOTING. MAINTENANCE REPLACED THE NOSE LANDING GEAR STRUT ASSY, OPS CHECKED GOOD ON THE GROUND.SDR AWXA200500233Bearing · disintegratedUPON ARRIVAL, ACFT WAS TAXIING TO GATE A RAMPER OBSERVED SPARKS COMING OUT OF LT OUTBOARD WHEEL ASSEMBLY AND NOTICED THE BRAKE FAN WAS RUNNING. MAINTENANCE REMOVED THE NR 1 WHEEL ASSEMBLY AND FOUND THE INNER BEARING HAD DISINTEGRATED; THE OUTER BEARING WAS NOSDR CA050216003Pin · corroded(CAN) WHEN MLG TRAILING LINK WAS REMOVED FOR TREATING MINOR CORROSION THE LINK PIN WAS FOUND CORRODED INSIDE AT THE LOCK NUT END. THE LINK PIN IS OPEN AT THE IB END WHEN INSTALLED AND HAD ACCUMULATED SAND AND OTHER DEBRIS AND WATER CAUSING THE CORROSION. THE SDR CA050216001Pin · corroded(CAN) WHEN THE MLG TRAILING LINK WAS REMOVED TO DEAL WITH A MINOR CORROSION ISSUE THE LINK PIN ASSY WAS FOUND CORRODED INSIDE AT THE LOCKING NUT END. THE LINK PIN IN QUESTION IS OPEN AT THE IB END WHEN INSTALLED AND IT HAD ACCUMULATED SAND, OTHER DEBRIS AND WSDR 2005FA0000339Axle · cracked(MDR05-073) FOUND CRACKED DURING NDT INSPECTION. CRACK IS APPROXIMATELY 1 INCH IN LENGTH AND IS IN THE KEY GROOVE. THIS IS FIRST KNOW DEFECT OF THIS TYPE FOR THIS PART. CAUSE IS UNKNOWN AND NO RECOMMENDATIONS TO PREVENT RECURRENCE AT THIS TIME. (K)SDR GTIA050019Strut · leakingFLL - FLT 395 - FOUND NOSE GEAR BOTTOMS OUT DURING TAXI, AIRCRAFT TAIL SWAP. REMOVED AND REPLACED VALVE BODY AND O-RING, SERVICED STRUT, LEAK CHECK OK. (M)SDR GTIA050011Strut · leakingDTW - FLT 1039 - NOSE GEAR WOULD NOT RETRACT. REPACKED NOSE STRUT, LEAK CHECK GOOD, SWUNG NOSE GEAR, OPS CHECK GOOD. (M)SDR GTIA050010Strut · icedFLT 202 - DTW - AFTER TAKEOFF GEAR WOULD NOT RETRACT, RETURNED TO DTW, NORMAL LANDING WEIGHT FOR LANDING, AIRCRAFT TAIL SWAP. UPON INSPECTION, FOUND NOSE STRUT PACKED WITH ICE, CLEANED, REPACKED AND SERVICED. (M)SDR QXEA200500102Strut · bindingON LIFT-OFF, THE CREW RECEIVED A WOW INPUT CAUTION MESSAGE. THE OVERRIDE WAS USED TO RAISE THE GEAR. WHEN THE GEAR WAS RAISED, THE WOW INPUT CAUTION WAS EXTINGUISHED FOLLOWED BY A GEAR DISAGREE CAUTION WHICH REMAINED ILLUMINATED FOR APPROXIMATELY 5 SECONDS. SDR CA050117006Axle · failed(CAN) UPON TAXI TO PARKING, GROUND CREWS NOTICED THE NR 1 MAIN WHEEL WAS MISSING. UPON FURTHER INVESTIGATION, IT WAS DISCOVERED THAT THE NR 1 AXLE HAD SHEARED OFF, ALLOWING THE WHEEL TO DEPART THE A/C. THE WHEEL WAS FOUND JUST OFF OF THE TAXIWAY STILL ATTACHEDSDR CA050125006Link · wrong part(CAN) MLG WAS REMOVED FOR MODIFICATION IAW STC. NR SA00487SE. ON RE-INSTALLATION THE MLG TRAILING LINK P/N 5741140-5 - LT WAS INSTALLED ON THE RT MLG, AND P/N 5741140-6 RT WAS INSTALLED ON THE LT MLG. THIS ERROR WAS NOT OBVIOUS DURING LANDING GEAR FUNCTIONAL RSDR 2005FA0000120Bushing · wornDURING NORMAL ANNUAL INSPECTION RT MAIN GEAR WAS JACKED AND CHECKED FOR ATTACHMENT FREEPLAY. EXCESSIVE FREEPLAY WAS NOTED AND UPON FURTHER VISUAL INSPECTION, IT WAS DETERMINED THAT RUBBER EXTRUDING OUT FROM THE GAP BETWEEN THE RT MAIN GEAR LEG AND PN 05912024SDR DL76S050015Axle · brokenNR 8 MAIN LANDING GEAR TIRE FOUND AT 30 DEGREE ANGLE UPON WALKAROUND INSP BY MTC, FOUND AXLE BROKEN. REPLACED SAME. REPAIRED WIRING HARNESS.SDR DXTA200500524Strut · dischargedAFTER TAKEOFF GEAR HANDLE WOULD NOT COME UP. FOUND NOSE STRUT NOT PROPERLY SERVICED. SERVICED NOSE STRUT IAW CESSNA 750 MM 12-10-38. CYCLED GEAR MULTIPLE TIMES, OPS CHECKS GOOD.SDR MALA050110Strut · underservicedLANDING GEAR INTRANSIT LIGHT REMAINED ON WELL AFTER GEAR HANDLE WAS SELECTED UP. PERFORMED QRH. CONDITION REMAINED. AIR RETURN TO CID. MAINTENANCE SUSPECT NLG NEVER EXTENDED FULLY TO ENGAGE CENTERING CAM. AFTER PROPER SERVICING STRUT RAN GEAR EXTENSION/RESDR 20030778Axle · crackedRT MAIN GEAR LOWER STRUT AXLE ASSY LUG HAS (2) CRACKS APPROX .05 AND .06 LONG WHERE LOWER TORQUE KNEE ATTACHES TO LUG.SDR 2005FA0000681Strut · looseDURING INSPECTION OF NOSE GEAR STRUT HARDWARE IT WAS FOUND TO HAVE LOOSE STRUT MOUNTING HARDWARE. (K)SDR HYTA2M5004Strut · debondedTUBE OF NOSE GEAR STRUT TUBE ASSY PN 26430161, CAME LOOSE FROM UPPER END CAP ALLOWING TUBE TO FLOAT WITH NOSE GEAR STRUT MOVEMENT. VENT TUBE INSIDE STRUT TUBE WAS CRUSHED AND SHOVED TO UPPER END OF TUBE. EXAMINATION OF TUBE AND END CAP REVEALED THAT END CAP SDR A6WA200440233Strut · dischargedAFTER ROTATION AND GEAR UP RECEIVED SEVERAL MESSAGES NOSE DOOR, GEAR DISAGREE, WOW INPUT AND STEERING INOP. FOLLOWED QRH PROCEDURES LANDED WITH NOSE STEERING INOPERATIVE. SERVICED NLG STRUT IAW CRJ AMM 12-12-32B REFERENCE AWAC W/O NR 77064 FOR DETAILS OF WORSDR GTIA040868Packing · leakingDTW - FLT 503 - DURING PREFLIGHT, FOUND HYDRAULIC FLUID ON RT MLG, AIRCRAFT SWAP. RE-PACKED RT MAIN GEAR STRUT, LEAK CHECK GOOD. (M)SDR 2004FA0000931Strut · brokenTHE LT MAIN GEAR STRUT FAILED AT THE LOWER WELDMENT WHERE THE STRUT ATTACHES TO THE FORK. THIS DAMAGE HAD PROGRESSED AROUND THE ATTACHMENT IN THE FORM OF A CRACK UNTIL WEEKEND TO THE POINT OF FAILURE. THIS PART HAD BEEN FABRICATED BY THE KIT MANUFACTURER.SDR MALA040864Strut · dischargedAFTER TAKEOFF THE GEAR WOULD NOT RETRACT, THE AUTO SPOILER AND AUTO THROTTLES DISCONNECTED. AIR RETURN TO DTW. MAINTENANCE UPON INSPECTION NOTED RT MLG STRUT FLAT. REPLACED RT SHOCK ABSORBER IAW TASK CARD 3210-503. PERFORMED LANDING GEAR FUNCTIONAL CHECKS SDR ABXA040400Bearing · seizedRIGHT MAIN LANDING GEAR INNER BEARING RACE SEIZED TO AXLE. AXLE CHROME MISSING. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR FORWARD AXLE BEARING ASSEMBLY IAW DC-9 MM.SDR RX8R2004002Strut · crackedRIGHT MAIN LANDING GEAR STRUT CRACKED AT ATTACH POINT TO ACTUATING BRACE. CRACK IS 2.5 INCHES LONG ALONG AFT SIDE OF AFT ATTACH POINT LUG. CRACK IS AT SAME LOCATION THAT GETS INSPECTED IAW PIPER SERVICE BULLETIN 969. AREA WAS INSPECTED PER SB 65.2 HRS. AGO,SDR CA041126010Axle · broken(CAN) ACFT 684 ON LANDING, DISCOVERED RT ML GEAR AFT AXLE BROKEN, IT SEEMS THAT HAPPEN DURING TAKEOFF IN XXX, BECAUSE FLIGHT CREW REPORT ANTI- SKID LIGHT WAS ON DURING WHOLE FLIGHT. MORE INFO AND PICTURES WILL FOLLOW AS IT BECOME AVAILABLE.SDR 2005FA0000157Axle · brokenLT MAIN GEAR WHEEL AXLE BROKE BETWEEN GEAR LEG AND WHEEL RACE. (GL11200505686) (K)SDR 2005FA0000372Housing · crackedAFTER LANDING, TAXIIED TO REPAIR SERVICE, THE NOSE STRUT BOTTOMS OUT, STOPPED AT RAMP. EXITED AC, NOTED A LARGE PUDDLE OF HYDRAULIC FLUID AROUND NLG. JACKED AC UP, NOTICED THE LARGE CRACK IN THE LOWER STRUT HOUSING, STARTING FROM BACK SIDE OF TORQUE KNEE ATTSDR 2005FA0001271Collar · separatedCOLLAR SEPARATING FROM TUBE DUE TO INSUFFICIENT PENETRATION WHEN PART WAS FURNACE BRAZED OR SILVER SOLDERED TOGETHER, WORKING COLLAR CAUSED PART TO WORK AND CRACKED BOSS. RECOMMEND INSPECTION OF COLLAR AT BOTTOM OF GEAR STRUT FOR ANY MOVEMENT OR WORKING BETWSDR 2005FA0001270Cylinder · crackedCOLLAR SEPARATING FROM TUBE DUE TO INSUFFICIENT PENETRATION WHEN PART WAS FURNACE BRAZED OR SILBER SOLDERED TOGETHER- WORKING COLLAR CAUSED PART TO WORK AND CRACK BOSS. RECOMMEND INSPECTION OF COLLAR AT BOTTOM OF GEAR STRUT FOR ANY MOVEMENT OR WORKING BETWEENSDR 2005FA0001269Cylinder · crackedCOLLAR SEPARATING FROM TUBE DUE TO INSUFFICIENT PENETRATION WHEN PART WAS FURNACE BRAZED OR SILVER SOLDERED TOGETHER-WORKING COLLAR CAUSED PART TO WORK AND CRACK BOSS. (K)SDR A6WA200440186Strut · dischargedGEAR DISAGREE AFTER TAKEOFF, COMPLIED WITH QRH LANDING WEIGHT 47,000 LBS. JACKED AIRCRAFT AND OBSERVED NLG NOT SELF-CENTERING SERVICED HYDRAULIC FLUID IN STRUT AND NITROGEN CHARGE IAW MM 12-1232. JACKED AIRCRAFT AGAIN, NLG CENTERS ON ITS OWN. SWUNG ALL 3 GE
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