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 VTZA97099Strut · req'd serviceFLT 6380 - IAD-LGA - DURING CLIMB, MADE AN UNSCHEDULED LANDING DUE TO LEFT MAIN GEAR INTRANSIT LIGHT ILLUMINATED. AIRCRAFT RETURNED TO IAD AND GATE WITH NO FURTHER PROBLEMS. MAINTENANCE INSPECTED AND SERVICED BOTH MAIN GEAR STRUTS. OPS CHECK OK. AIRCRAFT WSDR P5CA9700037Axle · failedFINAL REPORT, AXLE FAILED, SHEARED DURING TRANSIT FUELING AT THE LEFT WING GEAR RIGHT FRONT POSITION NR 2 MAIN. REPLACED THE LEFT WING GEAR TRUCK AND AXLE ASSEMBLY PER BAC MM 32-11-11.SDR MALA975291Strut · req'd serviceFLT 2976 - DID AN AIR TURNBACK DUE TO CONFIGURATION WARNING LIGHT ILLUMINATED AFTER TAKEOFF FROM DTW. WHEN THE CONDITION LEVERS BROUGHT BACK TO MAX THE LIGHT WENT OUT. MAINTENANCE SERVICED LEFT MAIN LANDING GEAR STRUT FLUID. PERFORMED ALL CHECKS. ALL CHECKSDR WWMA9700009Scraper · misinstalledCREW REPORTED, HAD TO USE THE DOWNLOCK RELEASE TO RETRACT THE LANDING GEAR. MAINTENANCE FOUND THE SCRAPER RING INSIDE THE LEFT MAIN LANDING GEAR STRUT INCORRECTLY INSTALLED. REPLACED ALL STRUT SEALS AND PERFORMED GEAR SWINGS IAW SAAB AMM 32-11-25.SDR PNSA970104Strut · reqd serviceLEFT STRUT LOW, SERVICED, NO LEAKS NOTED.SDR MALA975288Strut · req'd servFLT 3006 - DID AN AIR TURNBACK TO DTW AFTER LIFTOFF GOT CONFIGURATION WARNING LIGHT, ICE PROTECTION AND OAT CAUTION LIGHT. MAINTENANCE SERVICED LEFT MAIN STRUT, VERIFIED PROPER OPERATION AT OAT HEAT AND TCAS. ALL CHECKS GOOD. (M)SDR AU970074Cylinder · cracked(AUS) MAIN LANDING GEAR UPPER STRUT CYLINDER CRACKED - FOUND DURING INSPECTION IAW AD/SWSA226/78 (SB 226-32-033)SDR REXA97006Axle · brokenLEFT OUTBOARD MAIN TIRE FELL OFF. PERFORMED INSPECTION AND REPLACED AXLE, TIRES AND BRAKE. (M)SDR MALA975275Strut · req'd serviceAFTER TAKEOFF, FLT 3118, DID AN AIR TURN BACK TO DTW, DUE TO DOWNLOCK RELEASE BUTTON ON LANDING GEAR HANDLE NEEDED TO BE DEPRESSED IN ORDER TO RETRACT RIGHT MAIN LANDING GEAR. MAINTENANCE SERVICED SHOCK STRUT. ALL CHECKS GOOD. (M)SDR WWMA9700004Strut · reqd serviceLANDING GEAR WOULD NOT RETRACT WHEN SELECTED UP. MAINTENANCE FOUND THE LEFT MAIN LANDING GEAR STRUT WAS NOT FULLY EXTENDING . THE LEFT MLG STRUT WAS SERVICED AND GEAR SWINGS WERE PERFORMED.SDR 97ZZZX7Saddle · crackedINSPECTION FOUND LANDING GEAR SADDLE CRACKED AT ACTUATOR ATTACH.SDR CA970109026Oleo Seals · leaking(CAN) AFTER TAKEOFF AND GEAR SELECTED UP, NOSE GEAR UNSAFE LIGHT CAME ON ACCOMPANIED BY A LOUD NOISE COMING FROM NOSE WHEEL WELL AREA. QRH (QUICK REFERENCE HANDBOOK) DRILL CARRIED OUT AND AIRCRAFT LANDED SAFELY. MAINTENANCE TROUBLESHOOTING REVEALED NOSE OLEO FSDR HEEA968660Crosstube · damagedSCRIBE MARKS IN AREA OF CROSSTUBE NOT PERMITTED AS PER BHT412-CR&O.SDR 97ZZZX210Strut · crackedDURING POST-FLIGHT INSPECTION, A CRACK WAS DETECTED EMANATING FROM THE BRACE LOWER ATTACH HOLE EXTENDING 3 INCHES UPWARD TOWARD THE DAMPER ATTACH POINT. RECOMMEND REMOVING BRACE FROM STRUT AND INSPECTING BOLT HOLES EVERY 100 HRS.SDR DL72K962639Strut · crackedRT MLG UNSAFE LIGHT ILLUMINATED ON ROLLOUT AT APPROX 70 KNOTS. FOUND RT MLG CYLINDER CRACKED IN HALF. REPLACED CYLINDER.SDR 97ZZZX3484Washer · failedON LANDING ROLL-OUT, RT MAIN LANDING GEAR ROTATED 90 DEGREES AND BACK AGAIN. INVESTIGATION FOUND MAIN GEAR SCISSOR CENTER BOLT AND BUSHING RETAINING WASHER FAILED AND ALLOWED BUSHING TO 'WALK' AND SCISSOR TO DISCONNECT, ALLOWING TIRE TO ROTATE. NEW P/N S145SDR SIMA963327Trunnion Leg · failed inspORD - LEFT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NO 20317/96 (FCD E-9-32-002). REPLACED GEAR ASSEMBLY IAS ATR 42 JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA963326Trunnion Leg · failed inspORD - RIGHT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER, DOWTY TECHNIQUE A/VT NR 20317/96 (FCD E9-32-002). REPLACED GEAR ASSEMBLY IAW ATR 42 JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA963325Trunnion Leg · failed inspORD - RIGHT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NR 20317/96 (FCD E9-32-002). REPLACED GEAR ASSEMBLY IAW ATR 42 JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA963324Trunnion Leg · failed inspORD - RIGHT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NR 20317/96 (FCD E9-32-002). REPLACED GEAR ASSEMBLY IAW ATR 42 JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA963323Landing Gear · failed inspORD - RIGHT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NR 20317/96 (FCD E9-32-002). REPLACED GEAR ASSEMBLY IAW ATR 42 JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA963322Trunnion Leg · failed inspLEFT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NR 20317/96 (FCD E9-32-002). REPLACED GEAR ASSEMBLY IAW ATR 42-JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA963321Trunnion Leg · failed inspORD - LEFT LANDING GEAR FAILED ULTRASOUND INSPECTION OF TRUNNION LEG AS PER MESSIER DOWTY TECHNIQUE A/VT NR 20317/96 (FCD E9-32-002). REPLACED GEAR ASSEMBLY IAW ATR 42 JIC 32-11-00. OPS CHECK AND LEAK CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR HEEA968567Rubber Ring · deterioratedRUBBER DETERIORATED AND CRACKING. REPLACED WITH NEW RUBBER RINGS.SDR HEEA968542Cross Tube Assy · corrosionCORROSION PITS BEYOND LIMITS WHERE SKID SHOE MOUNTS. REPLACED WITH SERVICEABLE CROSSTUBE.SDR HEEA968504Skid Tube · mis mfgBOLT HOLE IN TOP OF AFT SKID TUBE SADDLE, WAS NOT LINED UP, WOULD NOT MATCH WITH CROSS TUBE MOUNT HOLE.SDR 96ZZZX5997Strut Fork · defectiveINSP OF NEW STRUT FORK FOUND UNUSEABLE DUE TO THREADS FILLED WITH CAD PLATING. ALSO FORK PORTION WAS POORLY MACHINED AND WAS GROOVED.SDR 96ZZZX5816Torque Knee · crackedAFTER AN INCIDENT CAUSED BY AN UPPER TORQUE KNEE FAILURE, OTHER AIRCRAFT IN THE FLEET ARE BEING INSPECTED. DURING THIS INSPECTION THE UPPER TORQUE KNEE ON THE RIGHT GEAR WAS VISUALLY FOUND TO BE CRACKED. A NEW UNIT WAS INSTALLED. BOTH THE NEW UNIT AND THE OSDR 96ZZZX6166Yoke · failedYOKE ASSY FAILED DURING LANDING ALLOWING THE RIGHT MAIN WHEEL ASSY TO ROTATE APPROXIMATELY 90 DEGREES. THIS GROUND THE TIRE, WHEEL ASSY, AND BRAKE DISC TO THE POINT OF RENDERING THESE PARTS UNSERVICEABLE. SUBMITTER RECOMMENDATION: ESTABLISH AN INSPECTION TISDR HEEA968457Skid Shoe · wornSKID PROTECTIVE PLATES WORN THROUGH HARDENED METAL TO AND THROUGH BASE METAL. REPLACED WITH SERVICEABLE SKID PROTECTIVE PLATES.SDR HEEA968438Crosstube · corrodedCROSSTUBE FRETTING CORROSION UNDER MOUNT PADS WHERE NO DAMAGE IS ALLOWED. SCRIBE MARKS AROUND MOUNT PADS.SDR AWXA9600649Strut · fluid lowPHX - FLT 2887 - AIRPLANE ROLLS OFF TO RIGHT UPON LIFT OFF. FLIGHT CONTROLS ARE NORMAL. WIND CONDITIONS LIGHT. ROLL CONTROL NORMAL AFTER TAKEOFF. CHECKED LEFT STRUT SERVICING AS CREW REQUESTED. FOUND FLUID VERY DIRTY AND QTY LOW. FLUSHED STRUT AND SERVICSDR 97ZZZX926Skid Tube · crackedUPON ROUTINE EMERGENCY FLOAT SYSTEM 6 MONTH/500 HOUR INSPECTION, THE SKID TUBE WAS FOUND CRACKED IN THREE PLACES AS SKETCHED. UPON FURTHER INSPECTION OF TUBE, THE CRACKS APPEAR TO ORIGINATE FROM THE INSERTS DUE TO IMPROPER INSTALLATION OR HOLE PREPARATION RATSDR 97ZZZX89Skid Tube · crackedUPON ROUTINE EMERGENCY FLOAT SYSTEM 6 MONTH/500 HOUR INSPECTION, THE SKID TUBE WAS FOUND CRACKED IN THREE PLACES. UPON FURTHER INSPECTION OF TUBE, THE CRACKS APPEAR TO ORIGINATE FROM THE INSERTS DUE TO IMPROPER INSTALLATION OR HOLE PREPARATION RATHER THAN DAMSDR 97ZZZX1694Bolt · detachedBOLT CAME OUT OF JUNCTURE OF UPPER AND LOWER TORQUE LINK ASSY ON NOSE GEAR ALLOWING NOSEWHEEL TO TURN 90 DEGREES RIGHT OF CENTER AND COLLAPSE. SUBMITTER SUGGESTED TO SPECIAL CHECK THIS BOLT AS PART OF PILOT'S PRE-FLIGHT INSPECTION.SDR P5CA9600845Strut · corrodedLEVEL 1 CORROSION ON FORWARD BASE PORTION OF RIGHT WING GEAR STRUT. REMOVED CORROSION AND REPAINTED PER BAC SRM 51-10-01.SDR ABXA9700413Strut · corrodedDURING C-CHECK, FOUND RIGHT MAIN LANDING GEAR SHOCK STRUT CORRODED UNDER THE SERVICING PLACARD. REPAIRED IAW ABX REA Y132-16914-MR.SDR 96ZZZX5554Trunnion Assy · crackedINSP FOUND RT MLG TRUNNION ASSY UPPER BARREL CRACKED.SDR 96ZZZX5571Bushing · wornDURING AN ANNUAL INSPECTION, VERTICAL FREE PLAY OF THE RIGHT MAIN LANDING GEAR TRUNNION PIN TO BUSHING TO PIN CLEARANCE MEASURED .025 INCH GREATER THAN THE LEFT MAIN LANDING GEAR. NO TOLERANCE FOR VERTICAL MOVEMENT COULD BE FOUND IN THE AIRCRAFT MANUFACTURERSSDR 97ZZZX730Abrasion Strip · wornSKID ABRASION STRIP WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 97ZZZX729Abrasion Strip · wornSKID ABRASION STRIP WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.SDR 96ZZZX5477Fork End · shearedLT GEAR JACK STRUT LOOSE WHEN USING ENTRY STEP. FOUND FORK END SHEARED OFF (IN THREADED AREA) WHERE JACK STRUT ATTACHES TO MAIN GEAR LEG.SDR CA970311055Skid Tube · punctured(CAN) PUNCTURE OF BOTTOM OF SKID TUBE, FORWARD OF SADDLE.SDR CA961025012Torque Knee · cracked(CAN) BOLT P/N 99-810061-3 FOUND LOOSE AT THE TORQUE KNEE UNION. WHEN DISASSEMBLED TO ADD WASHERS FOR SHIMMING, THE LOWER KNEE WAS FOUND CRACKED AT THE INSIDE RADIUS OF KNUCKLE. LPI CONFIRMED CRACK. BUSHING AT STRUT ATTACH POINT WAS WORN, POSSIBLY RESULTING INSDR CA961022013Yoke · cracked(CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BEEN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGUE AS SOME NEW YOKES SDR CA961022011Yoke · cracked(CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BEEN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGUE AS SOME NEW YOKES SDR CA961022009Yoke · cracked(CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BEEN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGUE AS SOME NEW YOKES HAVE BEEN SDR CA961022007Yoke · cracked(CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BEEN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGUE AS SOME NEW YOKES SDR CA961022006Yoke · cracked(CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BEEN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGUE AS SOME NEW YOKES SDR CA961022003Yoke · cracked(CAN) ULTRASONIC INSPECTION OF LANDING GEAR YOKES AS PER AD 96-19-05. OF 41 YOKES INSPECTED 12 HAD CRACKS. ALL 12 HAD BEEN FOUND OK ONE YEAR PREVIOUS. ALL ARE FAIRLY HIGH TIME. SUBMITTER SUGGESTS THAT CRACKING NOT ENTIRELY RELATED TO FATIGUE AS SOME NEW YOKES
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