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 SIMA20180226001Strut · dischargedDURING TAKEOFF ROLL, AROUND 100KTS, THE PLANE SHARPLY VERRED TO THE LEFT. FELT LIKE THE STEERING RE ENGAGED. ABORTED TAKE OFF. SERVICED THE LT STRUT IAW AMM 12-12-07. COMPLETED FIM TASK, NO OTHER FAULTS FOUND. PERFORMED FHDB DOWNLOAD IAW AMM 45-45-00. NSDR SWIA2018021944281Axle · failedNOSE WHEEL STEERING INOPERATIVE CAUTION MESSAGE. FOLLOWED BY WOW CAUTION MESSAGE, THEN A GEAR DISAGREE WARNING. MLG DID NOT RETRACT. COMPLIED WITH QRH, EXTENDED GEAR AND RETURNED TO DEPARTURE. REMOVED AND REPLACED THE PISTON AXLE ASSY IAW CMM.SDR REXA2018020200104Axle · corrodedRIGHT MLG OTBD AXLE IS CORRODED. REPAIRED THE DAMAGE IAW REO 670-32-11-361.SDR JGVR20180126002Axle · corrodedLEFT MLG AXLE HAS CORROSION THAT IS BEYOND SRM LIMITS. REMOVED AND REPLACED THE AXLE.SDR JGVR20180126001Axle · corrodedRIGHT MLG AXLE HAS CORROSION THAT IS BEYOND SRM LIMITS. REMOVED AND REPLACED THE AXLE.SDR 2018FA0000045Bearing · damagedRIGHT LANDING GEAR NITROGEN SUPPORT STRUT (ACME PART NUMBER 24614) LOWER THREADED SPHERICAL BEARING ATTACH FITTING, BROKE OFF INSIDE SUPPORT TUBE UPON LANDING. FACILITATING
RIGHT GEAR WHEEL SUPPORT FRAMING TO COLLAPSE AND BUCKLE UNDER AIRCRAFT. ACCIDENT INVESDR 2018FA0000089Axle · failedON TOUCHDOWN, THE PILOT LOST CONTROL OF THE ACFT. THE ACFT PULLED TO THE LEFT AND CAME TO REST APPROXIMATELY 350 FEED FROM THE TOUCHDOWN POINT IN THE GRASS ON THE LT SIDE OF RNWY. THE INVESTIGATION IDENTIFIED THAT THE LT MLG FAILED AT THE WELD POINT OF THE ASDR FDEA201801120107Strut · failedDURING A POSTFLIGHT INSPECTION, FOUND CENTER LANDING GEAR NOT EXTENDED AND TIRES NOT TOUCHING THE GROUND. PERFORMED GVI OF CENTER GEAR. CENTER GEAR IS DOWN AND LOCKED. PRESSURE RELEASE CAP NEAR TOP OF STRUT IS INTACT AND THE NITROGEN PRESSURE GAUGE IS RESDR T6FA201712142139Axle · corrodedDURING THE FIRST 48MTH MAIN LANDING GEAR AXLE BEAM ASSEMBLY BORESCOPE INSPECTION, CORROSION AND EXCESSIVE PAINT BUBBLING/FLAKING WAS NOTED INSIDE THE RIGHT MAIN GEAR AXLES.SDR JGVR20171206002Axle · corrodedLH MLG AXLE HAS AREAS OF MISSING CHROME AND RUST. REMOVED LH MLG TRAILING LINK FOR AXLE REPLACEMENT AND FOUND BOTH TRUNNION LUGS TO BE CORRODED ON OUTER SURFACES. REPLACE LH MLG TRUNNION AND TRAILING LINK ASSEMBLIES. REMOVED LH MLG TRUNNION AND TRAILING LINK SDR QMLA2017120417134Extension · crackedPERFORMED D 0560-100 HOUR/12 MONTH INSPECTION OF LANDING GEAR AND SKID EXTENSION. FOUND CRACK ON FWD LT CROSS TUBE EXTENSION. CRACK IS LOCATED ON THE BACKSIDE OF THE EXTENSION AND RUNS VERTICAL FROM THE UPPER MOUNTING BOLT TO THE TOP OF THE EXTENSION. REMOVED SDR T6FA201711292136Axle · corrodedDURING THE FIRST 48MTH MAIN LANDING GEAR AXLE BEAM ASSEMBLY BORESCOPE INSPECTION, CORROSION AND BUBBLING PAINT WAS NOTED INSIDE THE RIGHT MAIN GEAR AXLES. FOUND TO BE BEYOND LIMITS. RIGHT AXLE WAS REPLACED.SDR 2017FA0000614Cylinder · brokenLANDING GEAR OLEO STRUT CYLINDER FAILED AT TORQUE LINK MOUNT EARS AND AT LOWER CYLINDER OUTBOARD EDGE.SDR FDEA201710313115Strut · leakingCENTER MLG STRUT HAS RUNNING LEAK WITH STRUT PRESSURE AT 0 PSI. CTR GEAR RETRACTED. DO NOT OPERATE CTR GEAR. REMOVED THE CENTER GEAR STRUT AND FOUND STRUT DAMAGE. R&R THE CENTER MLG GEAR.SDR DALA2017092507120Pin · corrodedDURING LEFT MAIN LANDING GEAR INSTALLATION, THE AFT PINTLE PIN WAS FOUND TO BE CORRODED, REPLACED THE PINTLE IAW AMDS CARD 3210-9601-LT/002 NR 00011.SDR KQ7R2017081700001Seal · deterioratedOVERHAULED MAIN GEAR DAMPER ASSY LEAKING WITH AND WITHOUT PRESSURE. TEAR DOWN REPORT SHOWS TORN DOWN, PACKING'S AND SEALS DETERIORATED. CLEANED REASSEMBLED AND TESTED GOOD.SDR AALA201708089017Pin · corrodedAIRCRAFT IN BASE MAINTENANCE. RIGHT HAND MAIN LANDING GEAR UPPER TORQUE LINK PIN FOUND CORRODED AND WORN BEYOND LIMITS. REPLACED UPPER TORQUE LINK PIN PER AMM 32-11-27, IPC 32-11-11, AND CARD 26C74032004.SDR V0XD20170802002Axle · corrodedLEFT MAIN LANDIN GEAR AXLE HAS CORROSION. REMOVED AND REPLACED THE AXLE.SDR V0XD2017080101Piston · corrodedEVALUATED AND REPAIRED RT MLG PISTON/AXLE ASSY IAW AMM 32-11-09, NDT MANUAL 51-20-008-230, SERVICE BULLETIN 49200-32-85 DATED 23 JUL 14, REO 670-32-11-361.SDR AALA201707279020Strut · corrodedLT GEAR STRUT CORROSION AND MISSING PAINT. AIRCRAFT FERRIED TO TUL AND INDUCTED INTO BASE MAINTENANCE FOR DISPOSITION. REMOVED LIGHT CORROSION PER AARD 32-00-00-1 AND RESTORED PAINT.SDR AALA201707279019Strut · corrodedRT GEAR STRUT CORROSION AND MISSING PAINT. AIRCRAFT FERRIED TO TUL AND INDUCTED INTO BASE MAINTENANCE FOR DISPOSITION. REMOVED LIGHT CORROSION PER AARD 32-00-00-1 AND RESTORED PAINT.SDR 29GA2017071800001Piston · damagedDURING TAKEOFF, GEAR HANDLE WOULD NOT COME UP WITHOUT PRESSING THE DOWNLOCK RELEASE BUTTON. REMOVED, REPACKED, AND INSTALLED THE MLG STRUT PISTON IAW AMM 32-11-27-04, AND CMM 32-10-06.SDR 2017F00115Ring Assembly · damagedDURING TAKEOFF LIGHT VIBRATION. DURING EXTERIOR INSPECTION AFTER LANDING FOUND MLG RT WITH OIL LEAK. MAIN OLEO STRUT RINGS AND SEALS WERE REMOVED AND REPLACED.SDR DALA2017061204636Brace · corrodedCORROSION ON DRAG BRACE ASSEMBLY AT NLG. THE DRAG BRACE WAS REMOVED AND REPLACED IAW AMM 32-22-05 000-801, AMM 32-22-05 400-802 AND 32-22-05 400-801.SDR AALA201705239008Torque Link · corrodedAIRCRAFT IN BASE MAINTENANCE. CORRODED LEFT LOWER MAIN LANDING GEAR TORQUE LINK. REPLACED TORQUE LINK PER AMM TASK 32-11-27.SDR JGVR20170517001Link · corrodedLT TRAILING LINK INNER BORE HAS LARGE AREA OF CORROSION AND AXLE IS HEAVILY CORRODED. FOUND WHILE PERFORMING TASK 32-11-02-210 MAIN LANDING GEAR INSP AND TASK 32-30-00-210 MLG TRAILING LINK INTERNAL BORE INSP. AS PART OF THE PHASE 5 INSPECTION. REMOVED AND REPSDR RAIA201705120001Bolt · brokenLG LEVER DISAGREE EICAS WARNING AFTER DEPARTURE WITH A RED HATCHED BOX OVER LEFT MAIN LANDING GEAR INDICATOR. REMOVED AND REPLACED BROKEN TOP BOLT OF LT SHOCK ABSORBER. FERRIED AIRCRAFT TO STL. REMOVED AND REPLACED LT MAIN LANDING GEAR LEG STRUCTURE ASSY DUE TSDR CALA2017051201362Strut · crackedPRIOR TO AIRCRAFT MOVE, WHEN MOVE TEAM RAISED THE NOSE GEAR, RIGHT MAIN GEAR LOWER SHOCK STRUT CRACKED. RH MLG ASSY REPLACED REF AMM 32-11-11-401. ALL WORK AND INSPECTION REQUIREMENTS ARE DOCUMENTED.SDR V0XD2017051101Axle · corrodedCORROSION FOUND ON INBD AND OTBD LT AXLES. PERFORMED SB 49200-32-95 IAW SB 670BA-32-048 AND REO 670-32-11-361, NDT PERFORMED, NO DEFECTS NOTED.SDR 7C7A201741900305Drag Strut · chafedCHAFE DAMAGE TO DRAG STRUT FROM FWD DOOR ATTACH HARDWARE. TWO LOCATIONS BEYOND LIMITS OF CMM 32-10-02. REPAIRED IAW ECO 008.32-17-01SDR B4VR201704140001Bushing · debondedLANDING GEAR CROSS LINK JOINTS THAT WERE BONDED IN TO THE LANDING GEAR TRAILING ARM PER MSB 42-088/3 AND AD 2011-11-07 SHIFTED DURING NORMAL OPERATION. THIS RESULTED IN
METAL ON METAL CONTACT BETWEEN THE LANDING GEAR CROSS LINKS AND THE TRAILING ARMS.SDR 2017FA0000121Strut · chafedACCOMPLISHED MINOR REPAIR TO OLEO IAW MEMO DQ7482.SDR AALA201703319037Shock Absorber · damagedCRACKED, AND FLAKING CHROME ON SLIDING TUBE SHOCK ABSORBER FOR THE LEFT MAIN LANDING GEAR. REPLACED SLIDING TUBE SHOCK ABSORBER AMM 32-11-13.SDR DALA2019022601224Spherical Bearin · damagedRH MLG SPHERICAL BEARING FOUND SIGNS OF ROTATION, REPLACED BEARING C/W ERA 567722-14 (LP 2907406)SDR ASMF20170301001Gland Nut · corrodedDURING TRANSIT CHECK, IT WAS DETECTED CORROSION ON THE SHOCK STRUT GLAND NUT AND CYLINDER OF THE LEFT MAIN LANDING GEAR; THEREFORE THE LEFT MAIN LANDING ASSY WAS REPLACED IAW AMM 32-11-00, ADDITIONALLY LEFT MLG TEST WAS PERFORMED IAW AMM TASK 32-32-00-710-801,SDR C77A20170203001Strut · dischargedRECIEVED A LANDING GEAR WEIGHT ON WHELLS SYSTEM FAIL MESSAGE ON GEAR RETRACTION, DECLARED AN EMERGENCY, AND PERFORMED AN AIR RETURN. ON GEAR EXTENSION THE MESSAGE CLEARED AND THE FLIGHT LANDED WITHOUT INCIDENT. OPERATIONAL TEST WAS PERFORMED IAW AMM 3262-00 TASDR ASOA201701163003Axle · brokenDURING ROUTINE MAINTENANCE, THE RIGHT MAIN LANDING GEAR SHOCK ABSORBER LOWER AXLE WAS FOUND BROKEN. MAINTENANCE REPLACED THE RIGHT SHOCK ABSORBER LOWER AXLE SPECIAL BOLT.SDR AC2R2016120601Bearing · crackedCRACKED BEARING ON SHORTENING ACTUATOR. CRACKED BEARING ON SHOCK ABSORBER.SDR DALA2016120209505Piston · corrodedWHILE UNDERGOING L-CHECK, THE SUBJECT AIRPLANE WAS FOUND WITH CORROSION ON THE SLIDING PISTON LOCATED ON LEFT MAIN LANDING GEAR SHOCK STRUT CAPSULE. LOCALLY BLEND CORRODED AREA, FLAP PEEN THE REWORKED AREA, APPLY CADMIUM PLATING AND APPLY 2 COATS OF PRIMER PASDR DALA2016120209504Piston · corrodedWHILE UNDERGOING L-CHECK, THE SUBJECT AIRPLANE WAS FOUND WITH CORROSION ON THE SLIDING PISTON LOCATED ON R/H MAIN LANDING GEAR SHOCK STRUT CAPSULE. LOCALLY BLEND CORRODED AREA, FLAP PEEN THE REWORKED AREA, APPLY CADMIUM PLATING AND APPLY 2 COATS OF PRIMER PAISDR ASMF201612013Axle · out of limitsDURING TRANSIT CHECK, THE MLG WHEEL NUMBER 3 WAS REPLACED IAW AMM 32-45-07 BY NORMAL WEAR, DETECTING THE STATOR DISKS WITH DAMAGES BY THERMAL OXIDATION AND DISCOLORATION ON AXLE CHROME WITH EVIDENCE OF HIGH TEMPERATURE; INSPECTION PERSONNEL EVALUATED THE DAMAGSDR DALA2016111408777Pin · damagedLEFT MLG PIVOT PIN WORN AND DAMAGE TO CHROME. REPLACED THE PIN IAW AMDS 3211-01182-07A.SDR ASOA20161106110Sleeve · corrodedALL FOUR INBD MLG PISTON AXLES ARE CORROCED. REMOVED AND REPLACED THE SLEEVE IAW SB 49200-32-85 SECTION 11 STEPS 3(A-C). AIRCRAFT APPROVED FOR RETURN TO SERVICE.SDR C85R20170202001Scissor Link · crackedDURING 100 HR INSPECTION, FOUND BOTH EARS CRACKED THAT SCISSORS LINK ATTACHES TO ON UPPER END OF LEFT MAIN GEAR STRUT.SDR HYIA20161020001Strut · separatedPILOT REPORTED "NO INDICATION ON POSITION OF RIGHT MAIN GEAR. HAD TO CONDUCT A LANDING ON THE AIRCRAFT FLOAT SKIDS ON A HARD SURFACE RUNWAY." UPON INSPECTION, MAINTENANCE DISCOVERED THE RIGHT MAIN GEAR STRUT INNER PISTON & OUTER CYLINDER HAD SEPARATED. THIS SDR HALA2016092900364Strut · lowWHEN LANDING, RIGHT MAIN STRUT FEELS LIKE IT COMPRESSES MUCH FURTHER THAN LEFT STRUT, THEN IT SPRINGS BACK UP QUICKLY CAUSING A ROLLING MOTION TO THE LEFT. ON TAKEOFF, RIGHT WING DIPS BUT AIRCRAFT RETURNS LEVEL & TRIM AIRBORNE. SERVICED BOTH MAIN LANDING GEASDR HYIA20160917001Torque Link · brokenPILOT REPORTED RT MAIN GEAR WHEEL BRACE BROKEN. MAINTENANCE PERFORMED A DETAILED VISUAL INSPECTION OF THE RT MLG SYSTEM AND COMPONENTS TO INCLUDE RT CLOSE OUT RIB AND TRUNNION FITTING AREA. R & R THE RT MLG TRUNNION, LOWER BARREL, TORQUE LINKS AND WHEEL ASSYSDR ASOA20160910114Sleeve · corrodedDURING C CHECK FOUND ALL 4 I/B MLG PISTON AXLES PITTED/CORRODED. MTC R & R ALL 4 AXLE SLEEVES REFERENCING SB 49200-32-85 SECTION II STEPS 3(A-C)SDR 2016FA0000454Strut · crackedDURING 100 HOUR INSPECTION CRACKS WERE FOUND ON THE RIGHT MAIN LANDING GEAR STRUT LOCATED AT THE ATTACHMENT POINT OF THE LOWER SCISSOR. THE AIRCRAFT WAS TAKEN OUT OF SERVICES UNTIL PARTS COULD BE PROCURED.SDR 2016FA0000453Scissor Link · crackedTHE UPPER SCISSOR LINK ATTACHMENT SUPPORT (INBOARD SIDE) OF THE CYLINDER (P/N: 65319-04) WHICH IS CASTED METAL SUFFERED A FATIGUE CRACK. THIS SCISSOR LINK IS PART OF THE RIGHT MAIN LANDING GEAR (MLG) STRUT P/N: 35644-05. CRACKING APPEARS TO HAVE OCCURRED OVE
Back to JASC 3213