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.

SDR HEEA079966Crosstube · corrodedCORRODED BEYOND LIMITS. SCRAPPED TUBE.Jun 7, 2002 · N8591X · Bell 206L3SDR HEEA079965Crosstube · corrodedCORRODED BEYOND LIMITS. SCRAPPED TUBE.Jun 7, 2002 · N6160Z · Bell 206L3SDR CA020614001Seal · cracked(CAN) RIGHT GEAR HAD LOST ITS NITROGEN CHARGE DURING FLIGHT. REPLACED SEALS IN OLEO AND WHILE SERVICING OLEO IT WAS NOTED HYDRAULIC FLUID WAS APPEARING IN LOWER AREA OF BARREL. ON CLOSER INSPECTION FOUND BARREL CRACKED AT POINT WHERE BARRELL IS FITTED WITH MAIJun 6, 2002 · Cessna 414SDR CA020604006Strut · failed(CAN) A/C SLID DOWN RWY 4,000 FEET AT 21:55. WITH 50 PASSENGERS PLUS CREW. NOBODY HURT. A/C ENROUTE WHEN LDG, LT MLG FAILED JUST BELOW RADIUS BELOW AFT TRUNION FITTING. LT WING TIP LOWER SURFACE CONTACTED RWY AS A/C SLID DOWN RWY. LT INBOARD & OUTBOARD FLAPSJun 2, 2002 · Cndair CL6002B19SDR HEEA079481Crosstube · corrodedCROSSTUBE CORRODED BEYOND LIMITS. SCRAPPED.May 28, 2002 · N6251X · Bell 206L3SDR HEEA079480Crosstube · corrodedCROSSTUBE CORRODED BEYOND LIMITS. DEEP PITS OF CORROSION UNDER CLAMPS. SCRAPPED.May 28, 2002 · N6610C · Bell 206L3SDR HEEA079479Crosstube · corrodedCROSSTUBE CORRODED BEYOND LIMITS. SCRAPPED.May 28, 2002 · N6251X · Bell 206L3SDR HEEA079478Crosstube · corrodedCROSSTUBE CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE.May 28, 2002 · N2753F · Bell 206B3SDR HEEA079477Crosstube · corrodedCROSSTUBE CORRODED BEYOND LIMITS. REPLACED WITH SERVICEABLE CROSSTUBE.May 28, 2002 · N206FS · Bell 206L3SDR HEEA079476Crosstube · corrodedCROSSTUBE CORRODED BEYOND LIMITS. SCRAPPED.May 28, 2002 · N2753F · Bell 206B3SDR AUS20020512Clip · failed(AUS) RT MAIN LANDING GEAR OLEO RETAINING CIRCLIP DISLODGED FROM THE CIRCLIP GROOVE ALLOWING THE STRUT TO SEPARATE. AIRCRAFT DAMAGED DURING EMERGENCY LANDING.May 25, 2002 · Fokker FOKKERFVIIBSDR HEEA079217Crosstube · corrodedFWD CROSSTUBE CORRODED BEYOND LIMITS. TUBE HAS SEVERAL CORROSION PITS OF .012 INCH IN AN AREA WHERE NO CORROSION IS ALLOWED. THESE PITS WERE FOUND ON THE TOP SIDE NEAR THE SADDLE MOUNTS.May 24, 2002 · N6559Z · Bell 412SDR HEEA079181Crosstube · corrodedCORROSION ON AFT CROSSTUBE.May 23, 2002 · N720PH · Bell 407SDR HEEA079119Crosstube · corrodedMLG CROSSTUBE HAS CORROSION IN ZONE 1 & 2 RADIAL DAMAGED AREAS TO BE BEYOND LIMITS.May 21, 2002 · N3911L · Bell 412SDR HEEA079118Crosstube · corrodedCORROSION PITS IN ZONE 1 ON TOP SIDE OF TUBE AT A DEPTH OF .010 OF AN INCH DEEP NEAR SADDLE MOUNT.May 21, 2002 · N3893N · Bell 412SDR HEEA079117Crosstube · corrodedCROSSTUBE CORRODED BEYOND LIMITS.May 21, 2002 · N2258F · Bell 412SDR HEEA079116Crosstube · corrodedCROSSTUBE CORRODED BEYOND LIMITS IN SEVERAL AREAS.May 21, 2002 · N3893P · Bell 412SDR HEEA079115Crosstube · corrodedCROSSTUBE CORRODED BEYOND LIMITS IN SEVERAL AREAS.May 21, 2002 · N22608 · Bell 412SDR HEEA079114Crosstube · corrodedCROSSTUBE CORRODED BEYOND LIMITS IN SEVERAL AREAS.May 21, 2002 · N5759N · Bell 412SDR HEEA079113Crosstube · corrodedCROSSTUBE IS CORRODED BEYOND LIMITS ON TOP SIDE BETWEEN SADDLES.May 21, 2002 · N22347 · Bell 412SDR HEEA079112Crosstube · corrodedCROSSTUBE HAS SEVERAL AREAS OF PITTED CORROSION BETWEEN SADDLES.May 21, 2002 · N108X · Bell 412SDR HEEA079111Crosstube · corrodedCROSSTUBE HAS SEVERAL AREAS OF PITTED CORROSION BETWEEN SADDLES.May 21, 2002 · N3893L · Bell 412SDR HEEA079110Crosstube · corrodedCROSSTUBE HAS SEVERAL AREAS OF PITTED CORROSION BETWEEN SADDLES.May 21, 2002 · N800Y · Bell 412SDR CA020527011Socket · cracked(CAN) DURING INSPECTION OF MLG LOWER SOCKETS THEY WHERE FOUND TO BE CRACKED AS PER COMMUNIQUE NR 27 DATED FEB 1993. BLENDING IS ALLOWED UP TO .050 INCH BUT DUE TO LOW HOURS SINCE NEW THEY WHERE SENT TO AN OVERHAUL FACILITY FOR EVALUATION OF REPAIR OR REPLACE.May 16, 2002 · Beech 1900DSDR CA020523017Fork · cracked(CAN) BOTH BOW WHEEL FORKS HAVE TWO CRACKS EACH UP TO 1.5 INCHES LONG LOCATED ON THE AFT UPPER EDGE OF FORK. THE CRACKS ARE RUNNING FROM EDGE OF THE FORK FORWARD THE TWO 5/16 INCH REAR MOUNTING BOLT HOLES. ONE OF THE CRACK HAD GONE BEYOND THE HOLE.May 16, 2002 · Cessna A185FSDR HEEA078967Crosstube · damagedLANDING GEAR CROSSTUBE SPREAD OUT OF LIMITS.May 15, 2002 · N406PH · Bell 407SDR HEEA078959Crosstube · corrodedFOUND PITS OF CORROSION UNDER "T" BOLT AT A DEPTH OF .032. SCRAPPED CROSSTUBE.May 15, 2002 · N4999 · Bell 407SDR HEEA078958Crosstube · damagedLANDING GEAR CROSSTUBE SPREAD OUT OF LIMITS.May 15, 2002 · N406PH · Bell 407SDR HEEA078957Crosstube · damagedCROSSTUBE IS SPREAD ON RT SIDE.May 15, 2002 · N406PH · Bell 407SDR HEEA078956Crosstube · corrodedCROSSTUBE IS CORROSION OUT OF LIMITS.May 15, 2002 · N612PH · Bell 407SDR HEEA078955Crosstube · corrodedFWD CROSSTUBE CORRODED AT RT SADDLE ZONE A2 MAXIMUM ALLOWED .005 INCH MEASURED CORROSION .008 INCH.May 15, 2002 · N408PH · Bell 407SDR HEEA078916Crosstube · corrodedCORROSION ON CROSSTUBE.May 13, 2002 · N408PH · Bell 407SDR HEEA078884Crosstube · corrodedMLG CROSSTUBE HAS CORROSION.May 10, 2002 · N4999 · Bell 407SDR QXEA0200808Strut · chafedPDX - LEFT-HAND MAIN LANDING GEAR SHOCK STRUT CHAFED AT UPLOCK HOOK ROLLER LUGS. REPAIRED IAW HORIZON AIR EA 2-32-49.May 8, 2002 · N359PH · Dhav DHC8202SDR FC52004F00000Ring · corrodedPILOTS POST FLIGHT INSPECTION REVEALED DAMAGE TO THE NOSE LANDING GEAR LOWER DOOR LINKAGE. FURTHER INVESTIGATION REVEALED THIS DAMAGE CAUSED BY THE NOSE STRUT NOT FULLY EXTENDING AND THE NOSE TIRE FORK STRIKING THE LINKAGE. THIS WAS FOUND TO BE CAUSED BY EXCMay 7, 2002 · N77FC · Cessna 402CSDR 2002FA0000635Stud · brokenDURING SCHEDULED REPLACEMENT OF THE MLG STRUT CYLINDERS, THE HYD ACTUATOR ATTACH STUD WAS BEING REMOVED FOR RE-USE. UPON APPLYING A TENSION LOAD ON THE STUD TO REMOVE IT, PER MM, THE STUD SEPARATED ALONG THE THREADS WELL BELOW THE MAX TORQUE LIMIT, THE CRACK BMay 3, 2002 · N87SF · Cessna 550SDR AUS20020418Bolt · broken(AUS) MAIN LANDING GEAR TORQUE LINK BOLT FAILED. LOWER HALF OF OLEO STRUT, TORQUE LINKS, AXLE AND WHEEL ASSEMBLY POPPED OUT AFTER TAKEOFF.Apr 22, 2002 · Newze FU24A954SDR 2002FA0000570Snap Ring · failedAIRCRAFT WAS PARKED IN HANGAR, NO MAINTENANCE BEING PERFORMED. UPON 1ST INVESTIGATION LT MAIN LANDING GEAR STRUT WAS BOTTOMED. UPON FURTHER INVESTIGATION UPPER STRUT CAP SNAP RING HAD COME LOOSE AND CAP EJECTED THROUGH UPPER WING SKIN CAUSING A 3 INCH HOLE Apr 16, 2002 · N632Z · Beech D50SDR 2002FA0000517Nut · misinstalledDURING ANNUAL INSPECTION, MAIN AXLE NUTS WERE INSTALLED BACKWARDS. ONLY WAY COTTER KEY HOLES WOULD ALIGN, WAS TO BACK OFF NUT TO WHERE MAIN WHEEL WAS NOT TIGHT ON AXLE. ONLY THING RETAINING WHEEL ONTO AXLE WAS BRAKE ASSEMBLY. MAIN AXLE TABS WERE DEEPLY GROOApr 16, 2002 · N8288L · Piper PA28RT201SDR HYI2002F00012Strut · damagedDURING TAXI, RIGHT MAIN LANDING GEAR STRUT ASSEMBLY BROKE AT ACTUATOR ATTACH COLLAR. UPON INSPECTION, FOUND STRUT HAD LOST NITROGEN CHARGE AND HAD BEEN TAXIED IN THE FULLY DEPRESSED POSITION, POSSIBLY DAMAGING THE STRUT INTERNALLY. THE LANDING GEAR DID NOT RApr 9, 2002 · N618CA · Cessna 402CSDR AUS20020351Strut · cracked(AUS) LH MAIN LANDING GEAR LEG ASSEMBLY CRACKED AT THE UPPER FORWARDWELD JOINT.Apr 8, 2002 · Mooney M20CSDR C2XA02TY063Housing · gougedTYS DURING A SCHEDULED INSPECTION THE RIGHT HAND MAIN LANDING GEAR FORWARD SIDE-BRACE BEARING HOUSING WAS FOUND GOUGED ON THE INNER SURFACE. MAINTENANCE ACCOMPLISHED A BLEND OUT REPAIR IAW EMB GST-113/02. THE DYE PENETRANT INSPECTION WAS SATISFACTORY AFTER Apr 7, 2002 · N22971 · Emb EMB145SDR HEEA078542Crosstube · failedDURING PASSENGER LOADING (ENGINES SECURED) AFT CROSSTUBE FAILED ONE INCH OUTBOARD OF RIGHT HAND ATTACHMENT POINT (STRESS MARKS ON TUBE INDICATES FAILURE STARTED AT THE 12 O`CLOCK POSITION). AIRCRAFT SETTLED TO THE RIGHT RESULTING IN DAMAGE TO RIGHT HAND AFT FApr 1, 2002 · N5736J · Bell 212SDR MEX2002086Strut · leakingFLT 6142 - MEX-PVR - DURING OVERNIGHT SERVICE A LEAK WAS DETECTED IN RIGHT MAIN LANDING GEAR. MAIN GEAR STRUT WAS REPLACED IAW MM 32-11-02. (M)Mar 27, 2002 · N168PL · Doug MD88SDR CA020326010Bolt · worn(CAN) DUE TO PREVIOUS EXPERIENCE REMOVED LEFT AND RIGHT AXLE BOLTS EVEN THOUGH AIRCRAFT WAS POST S/B 32-006 AND DID NOT REQUIRE REMOVAL. BOLT WAS FOUND TO BE WORN AND STEPPED EVEN THOUGH AIRCRAFT WAS LOW TIME.AS BEFORE THERE IS NO REQUIREMENT TO REMOVE THIS BOMar 25, 2002 · Pilats PC1245SDR 2002FA0000462Strut · damagedDURING A FLEETWIDE NDT INSPECTION OF OUR MAIN LANDING GEAR STRUTS, FOLLOWING A STRUT FAILURE ON T-86 (N433DF SN 149855) A CRACK WAS FOUND IN THIS HOUSING. IT WAS INSTALLED ON THE RIGHT SIDE STRUT ASSEMBLY. IT WAS FOUND BY INSPECTION OF THE DISASSEMBLED STRUMar 22, 2002 · N404DF · Gruman FIRECATSDR HEEA078397Crosstube · corrodedMLG CROSSTUBE HAS CORROSION PITS. SCRAPPED AND REPLACED WITH SERVICEABLE ASSY.Mar 22, 2002 · N404PH · Bell 407SDR HEEA078351Tube · corrodedCORROSION UNDER SLEEVE.Mar 21, 2002 · N457PH · Bell 407SDR HEEA078341Crosstube · damagedCROSSTUBE SPREAD BEYOND LIMITS.Mar 21, 2002 · N724PH · Bell 407SDR HEEA078340Crosstube · corrodedCROSSTUBE HAS CORROSION BEYOND LIMITS.Mar 21, 2002 · N457PH · Bell 407
Back to JASC 3213