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 AALA20070248Seal · inoperativeDTW INFLIGHT T2265/02FEB - NOSE LANDING GEAR FAILED TO RETRACT. RETURNED TO DTW AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING HEAR SHOCK STRUT SEAL. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20070240Piston · inoperativeORD INFLIGHT T1637/02FEB - RECEIVED UNSAFE NOSE GEAR UP INDICATION. COULD HEAR LOUD NOISE WHEN GEAR WAS RETRACTED. SUSPECTED GEAR DOORS WERE OPEN. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NOSE LANDING GEAR STRUT PISTON. SYSTEM GROUND CHECKEDSDR AMWA82406Bolt · missingUPON TAXI, CREW STATED AIRCRAFT WAS SHAKING AND RETURNED TO GATE. RT MAIN LANDING GEAR TORQUE KNEES FOUND TO HAVE PIVOT BOLT MISSING. CAUSE UNKNOWN. SUBSEQUENT INSPECTION OF RT MAIN GEAR SATISFACTORY. REPLACED UPPER AND LOWER TORQUE LINKS AND HARDWARE. AIRCRSDR AALA20070231Strut · inoperativeORD INFLIGHT T2329/31JAN - GEAR UNSAFE LIGHT ILLUMINATED DURING RETRACTION. CYCLED GEAR WITH NO HELP. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. DOWN AND LOCKED INDICATIONS WERE GOOD. REPLACED NOSE LANDING GEAR STRUT. SYSTEM GROUND CHECKED NORMAL OPERATSDR QXEA200700112Unknown · unknownPDX FLIGHT NR 2125, LOUD SCRAPING THUD HEARD WHEN DISCONNECTING FROM TUG RAMP SAID NOSE WHEEL JERKED TO THE SIDE. MAINTENANCE COMPLIED WITH GENERAL VISUAL INSPECTION OF NOSE STRUT ASSEMBLY. NO OBVIOUS DEFECTS NOTED. NO PARTS REPLACED. AIRCRAFT RETURNED TO SDR COMA0770008Strut · corrodedRIGHT MLG I/B UPPER TORQUE LINK ATTACH LUG HAS INTERNAL PITTING CORROSION. REPAIRED IAW BF GOODRICH CONSESSION SCR0073-06 REV A.SDR SWIA200717759O-Ring · damagedNOSE WHEEL WOULD NOT RETRACT, NOSE DOOR OPEN WARNING. RETURNED TO FIELD. REPLACED O-RINGS AND PACKINGS ON NLG FLOATING STRUT PISTON IAW CMM 32-20-04 AND IAW CRJ 200 MM 32-21-25 AND C/W ST12-710-1002. OPERATIONAL CHECKS GOOD.SDR CA070122001Retaining Nut · mismanufactured(CAN) NEW AXLE NUTS FOR THE SERIES AIRCRAFT NOT FULLY ASSEMBLED. THE HOLES FOR THE (2) PINS HAVE BEEN DRILLED BUT NO PINS HAVE BEEN INSTALLED, INCOMPLETE PARTS. MARKING ON NUT WO-04403/1, DEC 07 2006 C6UM1172-27. (TC NR 20070122001)SDR CA070126011Torque Link · failed(CAN) AIRCRAFT WAS DOING TOUCH AND GO`S ON THE 2ND LANDING PILOT REPORTED ABNORMAL LANDING AND NO GEAR UP INDICATION. GEAR CYCLED AND ONLY 2 OUT OF 3 INDICATOR LIGHTS ILUMINATED. RT MAIN, NO INDICATION. GEAR CYCLED AGAIN NO UP INDICATION AND NO RT GREEN DOWN SDR DLM88070045Cylinder · corrodedRT MLG OUTER CYLINDER WAS FOUND WITH CORROSION. LOCALLY BLENDED TO REMOVE CORROSION PITTING AND REFINISHED.SDR CA070117008Seal · leaking(CAN) FLIGHT 5663 DEPARTED WITH 65 PASSENGERS ON BOARD WITH NO ISSUES NOTED. ON APPROACH, AFTER GEAR DOWN SELECTION CREW NOTED A NWS INOP CAUTION MESSAGE. TO GIVE THEMSELVES TIME TO GO THROUGH THE NWS INOP MESSAGE, THEY CARRIED OUT A GO AROUND. AS THEY FLEWSDR AALA20070087Strut · inoperativeTUL INFLIGHT - NOSE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. RETURNED TO TUL AND LANDED WITHOUT INCIDENT. AIRCRAFT TAKEN OUT OF SERVICE FOR EVALUATION. SERVICED NOSE LANDING GEAR STRUT PER MAINTENANCE MANUAL 32 21 02 3. SYSTEM GROUND CHECKED NORMAL OPSDR USAA070037Strut · corrodedNOSE LANDING GEAR UPPER STRUT TORQUE LINK LUGS HAS CORROSION. INSTALLED OVERSIZED BUSHINGS, REAMED HOLES & REMOVED CORROSION PER TYP REPAIR 32-20-01, DEFECT SIZE: .125 INCH.SDR 2007FA0000064Cylinder · damagedDURING AN ANNUAL INSPECTION FO THE LT MLG CYLINDER ASSY PN 6531904, IT WAS FOUND TO BE LOOSE IN THE MAIN WING SPAR. THE LT MLG WAS REMOVED FOR FURTHER INSPECTION OF THE LT MAIN WING SPAR ASSY GEAR ATTACHING BOLT HOSES AND ATTACH POINTS. CLOSE INSPECTION FO TSDR QVFA001Bushing · missingFOUND VERY SLIGHT MOVEMENT IN RT MLG OB PART OF MLG STRUT. UPON FURTHER INVESTIGATION, FOUND THAT P/N 10574X-YR1145 BUSHING WAS NOT INSTALLED IN MLG STRUT. FURTHER INVESTIGATION FOUND THAT THIS AREA HAD NOT BEEN THOROUGHLY INSPECTED SINCE DECEMBER 2004 DURING SDR C90ABushing · missingFOUND VERY SLIGHT MOVEMENT IN RT MLG OB PART OF MLG STRUT. UPON FURTHER INVESTIGATION, FOUND THAT PN 10574X-YR1145 BUSHING WAS NOT INSTALLED IN MLG STRUT. FURTHER INVESTIGATION FOUND THAT THIS AREA HAD NOT BEEN THOROUGHLY INSPECTED SINCE DECEMBER 2004 DURING 6SDR 0602839936Cylinder · malfunctionedAFTER DEPARTURE, THE FLIGHT CREW NOTICED A LOSS OF HYDRAULIC FLUID FROM THE RIGHT HYDRAULIC SYSTEM AND THEN SYSTEM PRESSURE DIMINISHED TO ZERO. COM PROCEDURES WERE COMPLIED WITH AND WHEN THE LANDING GEAR FAILED TO EXTEND NORMALLY CREW UTILIZED THE ALTERNATE ESDR GUUA12230601Strut · lowFLIGHT: 9240 NAS/FLL DURING LANDING UNABLE TO LIFT THROTTLE GATES NO BRAKES OR TILLER ANTI SKID TURNED OFF THEN BRAKES AND TILLER WERE AVAILABLE. SERVICED LT AND RT MAIN LANDING GEAR STRUTS.SDR ABXA070016Bolt · brokenLEFT MAIN LANDING GEAR STRUT LEAKED. FOUND TORSION LINK APEX BOLT DAMAGED/BROKE ON LEFT MAIN LANDING GEAR. REPLACED TORSION LINK APEX BOLT ON LEFT MAIN LANDING GEAR REPACK ON (AVBORNE) NR WX-314, IAW DC8 MM. REPLACED LEFT MAIN LANDING GEAR DOOR RETRACT ACTUSDR COMA0660711Strut · underservicedFLIGHT 5151 - GEAR DISAGREE MESSAGE AFTER TAKEOFF. NOSE GEAR DID NOT RETRACT. RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. FOUND NOSE GEAR WOULD NOT FULLY EXTEND. SERVICED NOSE STRUT. NO FURTHER DEFECTS.SDR COMA0660700Strut · underservicedAFTER TAKE-OFF AT APPROXIMATELY 145 KTS, GEAR DISAGREE MESSAGE ILLUMINATED, NOSE GEAR HAD RED HASH MARKS AND AFTER 10 SECONDS NOSE GEAR RETRACTED. AIRCRAFT RETURNED AND LANDED SAFELY. INSPECTED AIRCRAFT AND FOUND NOSE STRUT DID NOT FULLY EXTEND DURING JACKINSDR GUUA12060602Strut · lowFLIGHT: 5200 FLL/FLL UPON LANDING NO REVERSE NO TILLER NO BRAKES. USED EMERGENCY BRAKES. SERVICED STRUTS. TEST FLIGHT SATISFACTORY.SDR CA061205001Yoke · cracked(CAN) DURING SCHEDULED A CHECK, RT MLG YOKE WAS FOUND TO HAVE A CRACKED FITTING AT THE AUX ACTUATOR ATTACH POINT. (TC NR 20061205001)SDR 2006FA0001112Axle · crackedDURING A SCHEDULED 100 HOURS INSPECTION OF THE LANDING GEAR, THE MECHANIC FOUND A CRACK ON RT MAIN LANDING GEAR UPPER PART. IT IS SUSPECTED THE FATIGUE OR STRESS CORROSION CRACKING COULD BE THE CAUSE. ANOTHER REASON WHY MOST OF RT MAIN LANDING GEAR WERE FOUND SDR 2006UALA02150Cylinder · corrodedLT MLG OUTER CYLINDER INNER SURFACE IS CORRODED BETWEEN GLAND NUT THREADS AND CHROME PLATED SURFACE. LEFT MLG OUTER CYLINDER INNER SURFACE IS CORRODED BETWEEN GLAND NUT THREADS AND CHROME PLATED SURFACE, ITEM ROLLED FORWARD APPROX 270 DEGREES. REPLACED MAIN SDR 2006FA0001145Drag Link · misinstalledAIRCRAFT CAME IN FOR FIRST ANNUAL AFTER INSTALLATION. ON INSPECTION FOUND MAIN GEAR DRAG LINK HAD NOT BEEN PROPERLY SEALED AT THE LOWER END ALLOWING WATER TO ENTER THE ASSEMBLY. BECAUSE OF THE SEALANT WE ARE UNABLE TO TELL IF THE INSIDE OF THE TUBE HAS SOME SDR 2006FA0001078Strut · departedWHILE PRACTICING TAKEOFF AND LANDINGS, THE TOWER INFORMED PILOT THERE WAS A PROBLEM WITH LEFT LANDING GEAR. THE INSTRUCTOR ELECTED TO RETURN TO TAKEOFF AIRPORT. UPON LANDING THE BRAKEHOSE SEPARATED, AND THE WHEEL, BRAKE ASSY, STUB AXEL AND OLEO PISTON DEPARTSDR WRNA200600036Axle · overtempAFTER LANDING, NR 4 BRAKE TEMPERATURE REACHED 600 DEGREES, FUSE PLUG DISCHARGED AFTER PARKING. PERFORMED BRAKE OVERHEAT INSPECTION IAW AMM 05-51-16, FOUND AXLE DISCOLORATION IN BEARING AREA OUT OF LIMITS. REPLACED AXLE IAW CMM REV.8 DATED 03/02/1998. A/C RETUSDR CA061016004Strut · cracked(CAN) DURING 100 HOUR INSPECTION THE RT REAR FLOAT STRUT WAS FOUND TO HAVE A 6` STRESS CRACK ORIGINATING AT THE TOP FORWARD SIDE OF THE STRUT. TIME IN SERVICE IS UNKNOWN. TAT 22,057 HOURS. THE AIRCRAFT IS OPERATED EXCLUSIVELY ON FLOATS IN A CORROSIVE ENVIRONSDR CA061016002Strut · cracked(CAN) DURING 100 HOUR INSPECTION, THE L/H MIDDLE FLOAT STRUT WAS FOUND TO HAVE A 4" STRESS CRACK EXTENDING DOWN THE LEADING EDGE FROM THE TOP OF THE STRUT. THE AIRCRAFT IS OPERATED EXCLUSIVELY ON FLOATS IN A CORROSIVE ENVIRONMENT IN GENERALLY ADVERSE LANDING SDR 2006FA0001203Strut · failedTHIS PART FAILED AT THE WELD THAT ATTACHES PN 12020( UNIVERSAL) TO THE LANDING GEAR SHOCK STRUT. THIS PART IS LOCATED AT THE POINT WHERE THE SHOCK STRUT ATTACHES TO THE LANDING GEAR TO FUSELAGE SUPPORT TUBE AT THE FRONT OF THE RT WING MAIN SPAR. THIS PART FASDR DHL2006802002Strut · underservicedDURING INITIAL T/O ROLL, UNABLE TO MAINTAIN DIRECTIONAL CONTROL WITH FULL RUDDER PLUS TILLER INPUT. ALL ENG'S INDICATED EQUAL N1. CLOCKS RECORDED 7 SEC OF FLT. TIME INDICATING NOSE STRUT EXTENSION. ATIS WIND REPORTED AT 050 7 KTS RUNWAY 04L WAS USED. SERSDR AALA20060732Schrader Valve · inoperativeRDU - AFTER TAKEOFF LANDING GEAR RETRACTED AND RED NOSE GEAR LIGHT STAYED ON. LANDED RDU WITHOUT INCIDENT. INSPECTED NOSE STRUT PISTON. REPLACED NOSE SCHRADER VALVE AND O-RING AND REPACKED NOSE STRUT. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR ASMF200609010Cylinder · leakingAIRCRAFT RETURNED, DUE TO NOSE LANDING GEAR DID NOT RETRACT. AT PLATFORM AIRCRAFT WAS JACKED IAW MM 07-11-00 AND 3 EXTENSION AND RETRACTION CYCLES WERE PERFORMED, DETECTING THE NOSE LANDING GEAR STRUT LOW AND WITH LOW AIR LEVEL. NOSE LANDING GEAR STRUT SEALS WSDR CA061018005Seal · torn(CAN) ON CLIMB OUT, NOSE GEAR RED WARNING LIGHT STAYED ON; GEAR CYCLED TWICE, NIL CURE. AIRCRAFT PROCEEDED TO AIRPORT, LANDING WAS NORMAL. ON GROUND, NOSE GEAR SERVICED, SUBSEQUENT TAKEOFF NORMAL. ON RETURN TO BASE, ONE SEAL FOUND TORN, ALL SEALS REPLACED, FULSDR CA060925008Strut · underserviced(CAN) AFTER TAKEOFF LANDING GEAR WAS SELECTED UP AND ALL LANDING GEAR NOT-UP AND LOCKED LIGHTS DID NOT EXTINGUISH. AIRCRAFT DIVERTED AND AFTER LANDING IT WAS DISCOVERED THE NOSE STRUT WAS COMPLETELY COLLAPSED. THE NOSE STRUT WAS RE-SERVICED WITH NITROGEN AND GSDR 2006FA0000951Axle · cracked(REF NR: MDR06-091) UPON DISASSEMBLY, AXLE WAS FOUND TO BE CRACKED AND RUNS AROUND THE CIRCUMFERENCE. THE TRACTURE APPEARS TO ROIGINATE IN THE WELD ON THE CENTER OF THE AXLE SHAFT. THE AXLE WAS FRACTURED UNDER THE SOCKET, PN 6425-50202-101, AS EVIDENCED BY ASDR CA060920010Strut · broken(CAN) ON LANDING IN ROUGH WATER THE RT FRONT FLOAT STRUT BROKE AT THE UPPER END. STRUT REPLACED. (TC NR 20060920010)SDR CA060920009Strut · broken(CAN) ON TAKEOFF IN ROUGH WATER THE LT FRONT FLOAT STRUT BROKE AT THE UPPER END. STRUT REPLACED. (TC NR 20060920009)SDR YENA200670Packing · cutLANDING GEAR WOULD NOT RETRACT. FOUND NLG STRUT BOTTOM CHAMBER SHRADER VALVE PACKING CUT AND NO AIR IN THE STRUT. REPLACED PACKING AND SERVICED NLG STRUT IAW AMM 12-12-09 AND GREASED NLG AND SCISSOR LINKS. CYCLED GEARS SEVERAL TIMES IAW 32-33-00-501. FUNCTSDR AALA20060599Cylinder · inoperativeINFLIGHT T1107/22AUG CREW REPORTED NOSE GEAR VIBRATION AFTER GEAR RETRACTION THAT INCREASED AS THEY ACCELERATED. LANDED TPA WITHOUT INCIDENT. REPLACED LT AND RT GEAR DOOR CYLINDERS. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)SDR 2006FA0000839Brace · misdrilledTHIS IS A NEW PART PURCHASED THRU MFG (RAPID). BRACE ASSEMBLY HAS 4 BOLT HOLES THAT ARE NOT DRILLED TO THE REQUIRED SIZE TO ACCOMMODATE THE BOLT THAT IS TO BE INSTALLED. HOLE I.D. SIZE IS 0.185. BOLT O.D. SIZE IS 0.310.SDR 2006FA0000898Axle · corrodedLT MLG TRAILING ARM AXLE FOUND TO HAVE CORROSION ON TAPERED WASTELAND AREAS AT BOTH WHEEL POSITIONS. (K)SDR IXXA060598OCylinder · bypassingDURING CLIMB FROM KSEA, AFTER LANDING GEAR RETRACTION, THE GEAR AND DOOR UNSAFE LIGHT REMAINED ON. THE CREW COMPLIED WITH THE APPLICABLE CHECK LIST, DURING THE UP-LATCH CHECK THE GEAR FAILED TO UP-LATCH. THE CREW DIVERTED TO KPDX. MAINTENANCE INSPECTED THE SDR DXTA200601511Strut · underservicedUNLOCK LIGHT STAYED ON AFTER GEAR RETRACTION, CYCLED GEAR AND UNLOCK LIGHT WENT OUT AFTER 20 SECONDS. ON POST FLT, FOUND DAMAGE TO A/C AT ENTRY POINT FOR RIGHT MAIN TIRES. DAMAGE TO WHEEL WELL WAS CAUSED BY THE RT OLEO NOT FULLY EXTENDING AFTER TAKEOFF AND TSDR C2XA06BT031Shock Absorber · lowCREW REPORTED, LANGING GEAR AIR/GROUND FAILED AFTER TAKEOFF MAINTENANCE REMOVED AND REPLACED THE LGEU DID NOT FIX PROBLEM, INSPECTED AIR/GROUND PROXIMITY SWITCHES AND HARNESS FOR CONDITION AND SECURITY, NO DEFECTS NOTED, PERFORMED LANDING GEAR RETRACTION AND ESDR 06FDEA02470Axle · gougedLT MLG NR 1 AXLE FOUND WITH MINOR GOUGE ON MID UPPER AREA AS MARKED. LT MLG NR 1 AXLE ON MID UPPER MINOR GOUGE MARK AREA REWORKED TO LENGTH: 0.437", WIDTH: 0.312" AND DEPTH: 0.003" PER CMM 32-12-11 PAGE 414 (REF EARN N523FE-059), CLASSIFIED MINOR REPAIR AS PESDR CA060710002Seal · cut(CAN) ON THE RAMP AFTER REFUELLING, PILOTS NOTED THE LT MLG OLEO WAS LEAKING FLUID AND DEFLATING. MAINTENANCE FOUND THE LT OLEO COMPLETELY DEFLATED AND APPROX. 1 LITRE OF HYDRAULIC FLUID ON THE RAMP UNDER THE LT OLEO. AFTER OLEO REMOVAL, FOUND THE LOWER OLEO BSDR 06FDEA2470Axle · gougedFOUND LT MLG NR 1 AXLE FOUND WITH MINOR GOUGE ON MID UPPER AREA AS MARKED.SDR CA060808009Strut · cracked(CAN) DURING THE YEARLY INSPECTION, THE LT AFT LANDING GEAR STRUT WAS INSPECTED AND FOUND TO BE CRACKED, FROM THE LOWER DRAG BRACE ATTACH HOLE. THE CRACK WAS APPROX. 1.250 INCH LONG, AND EXTENDED LENGTHWISE TOWARDS THE BEND IN THE STRUT (TC NR 20060808009)
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