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 HEEA0011455Cap Assy · pads crackedSKID ASSY MOUNT PADS CRACKED.SDR HEEA0011453Cap Assy · crackedSKID ASSY MOUNT PADS CRACKED.SDR HEEA0011311Skid · corrodedSKID CORRODED BEYOND LIMITS.SDR HEEA0011139Skidtube · corrodedLT SKID TUBE IS CORRODED. (BEYOND LIMITS .033)SDR HEEA0011138Skidtube · corrodedSKID TUBE IS CORRODED. (BEYOND LIMITS .035)SDR HEEA0011123Skidtube · corrodedRT SKID TUBE CORRODED BEYOND LIMITS .040.SDR HEEA0011122Skidtube · corrodedSKID TUBE CORRODED BEYOND LIMITS .034. SENT TO AIRBORNE SUPPLY, INC. FOR INSPECTION AND REPAIR.SDR 97ZZZX4249Gear Leg · failedAFTER AIRCRAFT LANDED ON RUNWAY AND PROCEEDED TO THE TAXIWAY. THE LEFT LANDING GEAR FAILED AT WELD AREA.SDR AU971405Cylinder · cracked(AUS) MAIN LANDING GEAR CYLINDER CRACKED IN TORQUE LINK ATTACHMENTPOINTS.SDR 97ZZZX4190Axle Fitting · crackedCASTING CRACKED IN TWO LOCATIONS. CRACKS WERE LOCATED AT 90 DEGREES TO THE BOLT HOLES, AND PARALLEL TO THE BORE DIAMETER. ONE CRACK APPROXIMATELY 2.500 INCHES LONG WAS LOCATED IN THE WEB SECTION ABOVE THE BOLT HOLES. SECOND CRACK LOCATED IN THE LOWER WEB SESDR 97ZZZX4528Bearing · crackedIN C/W AD 90-02-13, THE MAIN GEAR BARREL INNER BEARING WAS FOUND CRACKED. NEW P/N 5141109-1 BEARING INSTALLED.SDR 97ZZZX4349Crosstube · failedREAR CROSSTUBE FRACTURED DURING GROUND HANDLING OF AIRCRAFT (RAISED ON WHEELS). TOTAL WT. A/C, 13,535 POUNDS. ACCEPTABLE MOVEMENT LIMITATION, 14,500 POUNDS.SDR HEEA0010841Skid Tube · crackedSKID TUBE AT SHOES HAS SIX EACH CRACKS EXTENDING FROM RIVNUT HOLES. SCRAPPED SKID TUBE.SDR HEEA0010778Skidtube · mis drilledSKID TUBE HOLES FOR STEP IN WRONG LOCATION.SDR HEEA0010758Skidtube · corrodedRT SKID TUBE CORROSION BEYOND LIMITS (.018) CORROSION .072.SDR CA970909007Collar · broken(CAN) THE AIRCRAFT IS USED FOR TRANSPORTING SKY DIVERS AND IS SUBJECT TO LONG TAKEOFF RUNS AND CROSSWINDS. THIS CONDITION SUBJECTS THE LANDING GEAR STRUT TO HIGH STRESS LOADS WHICH CONTRIBUTED TO THE STRUT COLLAR FAILURE.SDR ORJA97132Axle Nut · looseLAS - NR 3 BRAKE TEMP 310 DEGREES, ROSE MOMENTARILY TO 350 DEGREES THEN RETURNED TO 310 DEGREES. REMOVED WHEEL ASSY, INSPECTED BRAKE ASSY BRAKES, OPS CHECK NORMAL, NO VISIBLE ABNORMALITIES, FOUND AXLE NOT TORQUED HAND TIGHT, REINSTALLED WHEEL ASSY, AND RE-TORSDR 97ZZZX3986Gear Leg · failedAIRCRAFT EXPERIENCED A FAILURE OF THE RIGHT MAIN GEAR LOWER GEAR SEGMENT. THE LOWER TUBE FAILED AT THE SCISSOR ATTACH POINT CAUSING THE WHEEL TO ROTATE 180 DEGREES.SDR CA970505010Strut · cracked(CAN) ON LANDING LT MAIN GEAR STRUT BOTTOMED OUT. AIR AND HYDRAULIC FLUID ESCAPED. INSPECTION REVEALED A CRACK IN THE MAIN OUTER HOUSING OF THE STRUT AT KNEE FITTING BOSS.SDR 97ZZZX3751Gear Leg · brokeAIRCRAFT WAS IN HANGAR. PILOT WAS ON WING TO CHECK OIL AND LEFT MAIN LANDING GEAR BROKE WHERE THE GEAR ENTERS THE FUSELAGE. CLEAN BREAK. NO SIGN OF CRACKS.SDR 97ZZZX3985Bolt · failedTHE LEFT MAIN GEAR FAILED ON LANDING. THE LOWER SCISSOR ATTACH BOLT, BELLANCA PN 19404-4, APPEARED TO HAVE FAILED ALLOWING THE LOWER GEAR SEGMENT TO ROTATE 180 DEGREES.SDR 97ZZZX3756Bolt · brokenDURING INSTRUCTIONAL FLIGHT INVOLVING TAKEOFF AND LANDINGS, THE PILOT WAS INFORMED VIA RADIO FROM ANOTHER AIRCRAFT THAT THE ACFT NOSE WHEEL HAD FALLEN OFF. HE PROCEEDED TO SEE WHERE HE MADE A SUCCESSFUL EMERGENCY LANDING. INSPECTION OF THE ACFT NLG ASSY INDISDR 97ZZZM781Strut · crackedFLT 7173 - NAS-MIA - LEFT MAIN GEAR TORQUE LINK BROKE. REPLACED LEFT MAIN UPPER AND LOWER TORQUE LINKS AND PISTON AXLE ASSEMBLY. CYCLE CONTROLLED ITEM, CSO, 3987 CYCLES. (M)SDR COMA9710329Lock Washer · bentDURING E-5 INSPECTION TASKS 721-012, 731-012, FOUND BOTH MAIN GEAR OUTBOARD TRUNNION BEARING RETAINING NUTS LOOSE (FINGER TIGHT). AFTER REMOVAL, FOUND EXTERNAL LOCKING TABS DISTORTED / BENT OUT OF PLACE, ALLOWING NUT TO LOOSEN. INSTALLED SERV LOCKING WASHER SDR 97ZZZX3346Bogie Beam · crackedTHE MLG BOGIE BEAM WAS RECEIVED IN OVERHAULED CONDITION WITH TWO LARGE CRACKS AT THE TOW LUG. THE BEAM WAS SUBMITTED TO BOEING FOR A REPAIR PROCEDURE AAG-MIA-97-0133TR.SDR CA970424006Support · damaged(CAN) CROSSTUBE SUPPORT STRUCTURE DAMAGED. REPAIR CARRIED OUT.SDR HEEA0010331Skid Tube · defectiveFORWARD TIE DOWN FITTING HOLES MISALIGNED.SDR HEEA0010307Cap Assy Aft · delaminatedLANDING GEAR CAP ASSY AFT HAS DELAMINATED RUBBER.SDR HEEA0010212Skid Tube Assy · corrodedSKID TUBE CORROSION.SDR AU970683Pivot · cracked(AUS) LH MAIN LANDING GEAR PIVOT LUGS CRACKED - AIRCRAFT HAD BEEN MODIFIED 28 HOURS PREVIOUSLY BY FITMENT OF HEAVY DUTY OUTBACK LANDING GEAR KIT - COMPARISON OF THE LH AND RH MAIN LANDING GEAR LUGS FOUND THAT THE MATERIAL THICKNESS ON THE CRACKED LH LUGS WAS OSDR 97ZZZX3036Strut · crackedA CRACK WAS FOUND IN THE FILLET AREA ABOVE THE PIVOT OF THE TOP SCISSOR ARM.SDR 97UAL900483Sleeve · looseON REMOVAL OF NR 2 FORWARD TIRE ASSEMBLY, FOUND AXLE SLEEVE MIGRATED AND LOOSE. *S/D* ACCOMPLISHED SLEEVE MIGRATION CHECK PER MM 32-41-01. NO FURTHER DISCREPANCIES HAVE OCCURRED.SDR 97ZZZX3031Side Strut · crackedTHE 707 MLG SIDE STRUT WAS RECEIVED FOR OVERHAUL. AFTER BUSHING REMOVAL AND PAINT REMOVAL, PEENTRANT INSPECTION DETECTED TWO 3-INCH CRACKS AT THE CENTER SECTION (WEB REGION).SDR 97ZZZX3028Strut · crackedTHE TWO 707 MLG INNER CYLINDERS WERE RECEIVED FOR EVALUATION IN SERVICEABLE CONDITION. DURING MAGNETIC PARTICLE INSPECTION, NUMEROUS REGIONS OF UNTEMPERED AND OVERTEMPERED MARTENSITE WITH LADDER CRACKS WERE FOUND UNDER THE CHROME PLATING. PN 65-22112-1, SN 1SDR 97ZZZX3027Strut · crackedTHE TWO 707 MLG INNER CYLINDERS WERE RECEIVED FOR EVALUATION IN SERVICEABLE CONDITION. DURING MAGNETIC PARTICLE INSPECTION, NUMEROUS REGIONS OF UNTEMPERED AND OVERTEMPERED MARTENSITE WITH LADDER CRACKS WERE FOUND UNDER THE CHROME PLATING. PN 65-22112-1, SN 1SDR 97ZZZX2895Gear Leg · failedPRIVATE PILOT REPORTED DURING LANDING ROLL, 20 TO 25 KNOTS, APPLIED LIGHT BRAKING. ACFT THEN VEERED TO THE RT INTO A GROUND LOOP. LT MAIN GEAR COLLAPSED. EXAMINATION OF MLG REVEALED HEAVY CORROSION WITHIN THE INNER BORE OF LOWER LEG STRUT WHERE IT JOINS TSDR HEEA0010095Set Screw Ring · unbondedRUBBER COLLAR NOT PROPERLY BONDED TO ALUMINUM RING.SDR HEEA0010094Set Screw Ring · unbondedRUBBER COLLAR NOT PROPERLY BONDED TO ALUMINUM RING.SDR HEEA0010093Set Screw Ring · unbondedRUBBER COLLAR NOT PROPERLY BONDED TO ALUMINUM RING.SDR HEEA0010092Set Screw Ring · unbondedRUBBER COLLAR NOT PROPERLY BONDED TO ALUMINUM RING.SDR 97ZZZX3486Bearing · wrong partPULLED STRUTS TO RESEAL. DISCOVERED UPPER BEARING BLOCKS, AD 90-02-13, REQUIRES MAGNAFLUX EACH 1,000 HOURS, BUT SERIAL NUMBER DOES NOT APPLY TO 414A AFTER 0340. THESE WERE NOT BROKEN, BUT HAVE FOUND SEVERAL ON EARLIER AIRCRAFT COVERED BY THE AD BROKEN.SDR W8PA971163Cylinder · corrodedRIGHT MLG OUTER CYLINDER TRUNNION LUG CORRODED AND CHROME PLATING CHIPPING AWAY ON THE FWD TRUNNION LUGS. REPLACED THE RT MLG OUTER CYLINDER. (M)SDR AU970650Washer · faulty(AUS) MAIN LANDING GEAR SCISSOR LINK CENTRE BOLT PULLED THROUGH LOWER LINK ALLOWING WHEEL TO ROTATE LATERALLY - DURING LANDING THE TYRE AND TUBE BLEW OUT - SUSPECT CAUSED BY FAULTY WASHER AND/OR BUSHINGSDR 97ZZZX2774Skid Tube · crackedCRACKS WERE DISCOVERED IN THE SKID TUBE DURING A DAILY INSPECTION. THE CRACKS EXTENDED THROUGH TWO OF THE RIVNUT HOLES FOR THE FIRST SKID SHOE AFT OF THE FORWARD CROSS TUBE. THE OPERATOR REPORTED THAT THIS IS THE FOURTH SKID TUBE THEY HAVE FOUND CRACKED IN TSDR 99ZZZM10Bolt · improper partFOUND INCORRECT HARDWARD HAD BEEN INSTALLED IN THE UPPER END OF THE LEFT REAR LIFT STRUT. THE BOLT THROUGH THE UPPER END OF THE LIFT STRUT WAS APPROXIMATELY 1.5 INCHES PLUS TOO LONG. THE NUT HAD BEEN TIGHTENED UNITL IT BOTTOMED OUT ON THE THREADS, LEAVING THSDR HEEA0010009Skid Tube · corrodedSKID TUBE CORRODED BEYOND LIMITS AT THIS REPAIR STATION AS MARKED .040.SDR WWMA9700081Strut · reqd serviceCONFIGURATION WARNING LIGHT ILUMINATED AND THE LANDING GEAR REQUIRED THE USE OF OVERRIDE TO RETRACT THE GEAR. MAINTENANCE SERVICED THE LEFT MAIN LANDING GEAR STRUT AND PERFORMED GEAR SWINGS.SDR P5CA9701091Strut · chafedRT WING LANDING GEAR SHOCK STRUT INNER CYLINDER O/B BRAKE EQUALIZING ROD ATTACH LUG DEEP CHAFE MARK. REF BOEING TELEX PAO-HKG-97-0008RE, 0011RE LOCAL BLENDING C/O, NDT INSPECTED SHOT PEENING AND STYLUS CADIUM PLATED. THE CYLINDER AND BRAKE ROD REQ OVERHAUL WSDR AU970573Bolt · loose(AUS) NO1 AND NO14 MAIN LANDING GEAR WHEEL AXLE NUT SAFETY BOLTS (ONE OF TWO PER WHEEL) LOOSE - WHEEL HUB CAPS HAD BROKEN ATTACHMENT LUGSSDR P2EA97058Torsion Links · corrodedPAE - FOUND C-CHECK MAINTENANCE VISIT, RIGHT MLG UPPER AND LOWER TORSION LINKS HAVE WORN BUSHING SAT STRUT ATTACH POINTS. REMOVED WHEELS AND BRAKES, DAMPER, UPPER AND LOWER TORSION LINKS. REPLACED UPPER AND LOWER TORSION LINKS. REPLACED UPPER LINK ATTACH BO
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