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 CA030130008Cylinder · corrodedAFTER A VERY COLD OPERATION DAY, A/C TOWED TO HANGAR. DURING INSPECTION, MECH FOUND LT MLG WITH NO CHROME PORTION VISIBLE AND AREA WET. LT MLG INNER CYLINDER REMOVED TO GAIN ACCESS FOR INSPECTION AND SEAL REPLACEMENT. FOUND LWR INNER CYLINDER WHERE LOWER BESDR CA030129002Fitting · cracked(CAN) INTERGRANULAR CORROSION AT FORWARD FLOAT STRUT ATTACH HOLE ON 585926. LT FITTING FOUND DURING ROUTINE 100 HOUR INSPECTION. FLOAT DATE OF MANUFACTURE 1-11-51 HOUR ON PART UNKNOWN. TTAF 11,951.4 HOURS.SDR HEEA083977Crosstube · damagedMLG CROSSTUBE SPREAD.SDR HEEA083382Clamp · brokenLT OUTBOARD CLAMP ON FWD CROSSTUBE HAS BROKEN T-BOLT. SCRAPPED.SDR HEEA083277Crosstube · corrodedCROSSTUBE HAS CORROSION. SCRAPPED.SDR HEEA083276Crosstube · corrodedCROSSTUBE HAS CORROSION. SCRAPPED.SDR HEEA083275Crosstube · corrodedCROSSTUBE HAS CORROSION IN ZONE ONE. SCRAPPED.SDR HEEA083196Crosstube · corrodedCROSSTUBE HAS CORROSION. SCRAPPED.SDR HEEA083193Crosstube · corrodedFOUND AFT CROSSTUBE CORRODED BEYOND LIMITS NEAR AND UNDER SADDLES. SCRAPPED.SDR HEEA083192Crosstube · corrodedFOUND CROSSTUBE CORRODED BEYOND LIMITS NEAR AND UNDER SADDLES. SCRAPPED.SDR HEEA083154Fitting · wornMLG CROSSTUBE FITTING ASSY WORN AND CORRODED. SCRAPPED.SDR HEEA083153Fitting · wornCROSSTUBE FITTING ASSY WORN AND CORRODED. SCRAPPED.SDR HEEA083152Fitting · wornCROSSTUBE FITTING WORN AND CORRODED. SCRAPPED.SDR BMAC020026Strut · dischargedPILOT REPORTED 'CABIN' CAP LIGHT ILLUMINATED DUIRNG FLIGHT AT 11,300 FEET. PERFORMED EMERGENCY CHECKLIST ACTIONS, DESCENDED TO 9,000 FEET. CABIN CAP LIGHT OUT CABIN DOES NOT PRESSURIZE. MAINTENANCE DEFERRED PER MEL 21-14. LATER TROUBLE-SHOOTING DETERMINED SDR AC2A081582Crosstube · corrodedCORROSION ON AFT CROSSTUBE, RIGHT HAND SIDE JUST OUTBOARD OF CLAMP. REPLACED WITH SERVICEABLE CROSSTUBE.SDR AUS20021345Landing Gear · transposed(AUS) LT MAIN LANDING GEAR AND RT MAIN LANDING GEAR TRANSPOSED. PERSONNEL/MAINTENANCE ERROR.SDR AUS20021344Washer · unapproved part(AUS) LT AND RT MAIN LANDING GEAR SHOCK ABSORBERS FITTED WITH PLASTIC AUTOMOTIVE TYPE BUSHES ALONG WITH PNO 169-810000-119 WASHERS. UNAPPROVED PART. PERSONNEL/MAINTENANCE ERROR.SDR AUS20021343Rod · worn(AUS) LH AND RH MAIN LANDING GEAR SHOCK ABSORBER RODS SEVERELY WORN. LH MLG RODS WORN APPROXIMATELY 0.863MM (0.034IN). RH MLG RODS WORN APPROXIMATELY 0.457MM (0.018IN). FOUND DURING INSPECTION IAWAD/BEECH23/13. AIRCRAFT HAD OPERATED FOR 20.7 HOURS SINCE LASTPESDR QXEA0201915Strut · chafedPDX - RIGHT MAIN LANDING GEAR SHOCK STRUT CHAFED ON FORWARD SIDE APPROXIMATELY 6 INCHES BELOW LUG FOR BARREL NUT AND LOWER END. REPAIRED IAW CHH 32-10-01, PAGES 668-669, PARAGRAPH 5.SDR QXEA0201896Strut · chafedPDX - RIGHT HAND MAIN LANDING GEAR DRAG STRUT IS CHAFED IN TWO PLACED ABOVE LOWER ATTACH POINT. REPAIRED IAW DHC-8200 CMM 32-10-01, PAGES 668-669, PARAGRAPH 5.SDR 2003F00081Strut · lowON CLIMB-OUT FROM FWA, COULD NOT RETRACT LANDING GEAR WITHOUT DEPRESSING DOWN LOCK RELEASE. UPON BRINGING CONDITION LEVERS BACK IN CLIMB, CONFIG WARNING HORN SOUNDED. AFTER GEAR RETRACTION, OAT WARNING LIGHT ILLUMINATED. FLIGHT 4505 RETURNED TO FWA, MAINTENASDR 2002FA0001289Frame · crackedTHE LEFT FRAME WAS NOTED TO HAVE CORROSION PREVENTATIVE OOZING IN THE EXACT AREA OF THE INSPECTION, IN A LINE THAT APPEARED AS A CRACK. THE AREA WAS CLEANED AND A CRACK WAS APPARENT BY USING A GOOD LIGHT AND 10 POWER GLASS. A DYE CHECK OF THE AREA FAILED TO SDR AUS20021272Bolt · separated(AUS) LT MAIN LANDING GEAR OLEO STRUT PISTON SEPARATING FROM AXLE. SHEAR BOLT HAD SHEARED AND THE PISTON HAD MIGRATED OUT BY APPROXIMATELY 25MM (0.98IN).SDR AC2A081232Crosstube · corrodedCORROSION WAS FOUND UNDER THE SADDLE SUPPORT CLAMP AND PART HAD ONLY 581 HOURS ON IT. REPLACED THE CROSSTUBE.SDR QXEA0201779Strut · chafedPDX - LT MLG LOWER STRUT INBOARD SIDE HAS CHAFE MARKS. REPAIRED IAW DHC-8 SRM 51-20-16 AND SRM 51-20-26, PAGE 7.SDR WVE2002F00022Bearing · corrodedDURING 3000 LANDING INSPECTION THE LOWER BEARING OF THE LEFT AND RIGHT MAIN LANDING GEAR STRUT ASSEMBLIES WERE FOUND CORRODED.SDR 0202999919Cylinder · failedTHE RIGHT MAIN LANDING GEAR COLLAPSED DURING TAXI TO RUNWAY. PRELIMINARY INVESTIGATION REVEALED A FAILED MAIN LANDING GEAR STRUT CYLINDER BARREL.SDR 2002FA0001307Bolt · failedBOLT (NR 32) IS ONE OF FOUR. THREE APPARENTLY WERE PROBABLY SHEARED FROM PAST ACCIDENT. SAFETY WIRE HELD 211 BOLTS FROM ROTATING. REMAINING BOLT TORE OUT END OF UPPER TUBE, CAUSING COMPLETE DISASSEMBLY OF UPPER PART OF STRUT. UPPER ATTACH BOLT (NR 17) AND SDR 2002FA0001089Axle · crackedPISTON/ AXLE ASSEMBLY HOUSING HAS AN INDICATION OF A CRACK ON BOTH SIDES AT THE CASTING LINE. ONE SIDE HAS AN INDICATION APPROXIMATELY 2 INCHES LONG. THE OTHER SIDE HAS AN INDICATION APPROXIMATELY 0.5 INCH LONG THESE INDICATIONS WERE FOUND DURING A ROUTINE 6SDR CA020910006Link · corroded(CAN) THE WORN TRAILING LINK BUSHINGS WERE SCHEDULED TO BE REPLACED DURING THE ANNUAL INSPECTION. UPON REMOVING THE BUSHINGS FROM THE RT TRAILING LINK, SEVERAL SPOTS OF CORRORSION WERE DISCOVERED IN THE MAIN BUSHING BORE. TECH REP. DIRECTED A CHANGE OUT OF DEFSDR ARWA20020808Cylinder · crackedDURING DAILY INSPECTION FOUND RIGHT HAND CYLINDER CRACKED AT LOWER OUTBOARD SIDE. REMOVED AND REPLACED RT MLG STRUT ASSEMBLY. OPERATIONAL CHECK NORMAL.SDR DHL2002363523Sleeve · flakingC-CHECK, NR 8 AXLE PROTECTIVE SLEEVE HAS INTERNAL BLISTERING AND FLAKING ON NICKEL PLATING. REMOVED AND REPLACED DAMAGED PROTECTIVE SLEEVE IAW A300 AMM 32-42-22.SDR DHL2002363514Sleeve · wornC-CHECK, NR 4 AXLE PROTECTIVE SLEEVE HAS PITTING ON EXTERNAL SURFACE AND NICKEL PLATING WORN. REMOVED AND REPLACED PROTECTIVE SLEEVE IAW A300 AMM 32-42-27.SDR 2002F01118Gland Nut · failedHNL FLT 7670 - AFTER LANDING AT HNL, THE AIRCRAFT WAS LEANING TO THE RIGHT SIDE. THE LEFT MLG SHOCK STRUT GLAND NUT FAILED ALLOWING THE SHOCK STRUT TO OVER EXTEND, AND BIND IN THAT POSITION. THE LEFT MLG FAIRING SUSTAINED DAMAGE DUE TO THE OVER EXTENSION. SSDR JK12002F00000Cylinder · crackedUPON ROUTINE RESEALING OF THE STRUT, A SMALL CRACK WAS FOUND ON LOWER END OF THE SHOCK STRUT CYLINDER. THIS HELICOPTER IS USED FOR CORPORATE TRANSPORTATION AND ENTERED INTO SERVICE ON DEC. 1990, CURRENTLY HAS 12,110 LANDINGS. THERE HAVE BEEN NO HARD OR OVERWSDR DHL2002363513Axle · gougedC-check/#8 axle has worn nickel plating and gouged.Corrective action/Smooth an blended out area to a .2 mm radius in ref. to repair approval sheet from Messier-Dowty OE-085-08-02-003,NDT inspected per CMM 32-09-01 section 42 no cracks found. See NDT report seeSDR 2002FA0000974Axle · brokenRIGHT GEAR AXLE BROKE (MAIN) ON LANDING, CAUSING SUBSTANTIAL DAMAGE TO FUSELAGE GEAR ATTACH AREA.SDR ABXA020101Bushing · corrodedRIGHT MAIN LANDING GEAR LOWER AFT SIDE STRUT, LOWER FORWARD BUSHING WAS CORRODED. REPLACED THE RIGHT MAIN LANDING GEAR LOWER AFT SIDE STRUT IAW BOEING B767 MM 32-11-05.SDR CA051109004Torque Link · crackedUPON INSPECTION DISCOVERED MLG TORQUE LINKS CRACKED AT CENTER BOLT ATTACH POINTS. TORQUE LINKS SUBSEQUENTLY REPLACED.SDR AUS20020748Strut · cracked(AUS) LT MAIN LANDING GEAR STRUT CRACKED FROM RIVET HOLE. CRACK LENGTH 9.525MM (0.375IN).SDR 2002FA0000823Bushing · debondedDURING A PHASE INSPECTION FOUND THE RUBBER TYPE BUSHING HAD BECOME LOOSE AND SLID DOWN THE LEFT GEAR LEG, RESULTING IN METAL TO METAL CONTACT OF THE GEAR LEG AND BUSHING SLEEVE. JACKED A/C, REMOVED GEAR LEG AND OLD BUSHING. INSPECTED GEAR LEG, FOUND DAMAGE LIMSDR CA020718008Support · broken(CAN) AFTER LANDING THE AIRCRAFT, THE PILOT HEARD A LOUD BANG. THE AIRCRAFT DID NOT MOVE AND THERE WAS NO INDICATON OF ANY MALFUNCTION ON THE INSTRUMENTS. THE PILOT OPENED THE CREW DOOR AND SAW THE RT SKID TUBE SLIPPED OUT TO THE RIGHT. INSPECTION REEALED THATSDR HEEA079974Crosstube · corrodedCROSSTUBE HAS CORROSION. SCRAPPED TUBE.SDR HEEA079973Crosstube · corrodedCORROSION. SCRAPPED TUBE.SDR HEEA079972Crosstube · corrodedCORROSION. SCRAPPED TUBE.SDR HEEA079971Crosstube · corrodedCORROSION. SCRAPPED TUBE.SDR HEEA079970Crosstube · corrodedCORROSION. SCRAPPED TUBE.SDR HEEA079969Crosstube · corrodedCORROSION. SCRAPPED TUBE.SDR HEEA079968Crosstube · corrodedCORROSION PITTING IN CURVE. SCRAPPED TUBE.SDR HEEA079967Crosstube · corrodedCORRODED BEYOND LIMITS. SCRAPPED TUBE.
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