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 C2XA06IA106Shock Absorber · low pressureSTL - FLIGHT 2486, THE CREW REPORTED A LANDING GEAR AIR/GROUND FAILURE ON TAKEOFF. THE AIRCRAFT RETURNED TO STL WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, SERVICED THE LEFT HAND MAIN LANDING GEAR SHOCK ABSORBER, OPERATIONALLY CHECKJul 3, 2006 · N16918 · Emb EMB145LRSDR 01676201Bolt · failedLANDING GEAR COLLAPSED DURING ROLLOUT AFTER LANDING. UPON INSPECTION IT WAS NOTED THAT A BOLT CONNECTING THE DOWNLOCK BELLCRANK TO THE UPPER STRUT ASSEMBLY HAD FAILED. THE BOLT HEAD WAS MISSING ALLOWING ALL OF THE FORCE FROM THE BELLCRANK TO BE APPLIED DIRECTLJun 21, 2006 · N216WA · Cessna 421ASDR 1322062106AAdapter · corrodedDURING INSPECTION RIGHT MAIN GEAR AXLE ADAPTER WAS FOUND CORRODED IN KNEE PIN BORE.Jun 21, 2006 · N422QS · Gulstm GIVSDR 1463960806AAdapter · corrodedRIGHT AXLE ADAPTER WAS FOUND TO HAVE CORROSION AND PITTING DURING INSPECTION.Jun 8, 2006 · N465QS · Gulstm GIVSDR 1463960806Adapter · corrodedLEFT AXLE ADAPTER WAS FOUND TO HAVE CORROSION AND PITTING DURING INSPECTION.Jun 8, 2006 · N465QS · Gulstm GIVSDR 625060606AAdapter · corrodedLEFT MAIN LANDING GEAR AXLE ADAPTER HAS CORROSION AND PITTING.Jun 6, 2006 · N507QS · Gulstm GULFSTREAMGVSDR 625060606Adapter · corrodedRIGHT MAIN LANDING GEAR AXLE ADAPTER HAS CORROSION AND PITTING.Jun 6, 2006 · N507QS · Gulstm GULFSTREAMGVSDR CA060607002Metering Tube · failed(CAN) FRACTURED AT LOWER THREAD WHERE THE TUBE SCREWS INTO THE PISTON. THIS ALLOWED THE UPPER AND LOWER SECTIONS OF THE SHOCK STRUT TO DISENGAGE CAUSING GEAR COLLAPSE. THE FAILED TUBE IS MADE OF ALUMINUM ALLOY. PART AND PICTURES AVAILABLE UPON REQUEST (TC NR 2Jun 5, 2006 · Dhav DHC6300SDR SAI060601Axle · corrodedDURING REMOVAL OF THE LT MLG DEEP CORROSION WAS FOUND ON THE LANDING GEAR AXLE UNDER THE SPACER FOR THE IB BRAKE. THE AXLE REQUIRED REPLACEMENT WITH A REPAIRED UNIT.May 30, 2006 · N370AE · Swrngn SA227ACSDR QXEA200601305Shock Absorber · chafedYYC - C4 RIGHT HAND NACELLE, MAIN LANDING GEAR AREA, SHOCK STRUT HAS CHAFING DAMAGE AT LOWER/FORWARD END OF CYLINDER. CHAFING IS CAUSED BY WEIGHT ON WHEEL WIRING CONDUIT CONTACT. REPAIRED IAW RD8-32-1575 AND EA 2-32-108.May 15, 2006 · N355PH · Dhav DHC8202SDR TSAA0632036Strut · lowDURING CRUISE THE CREW NOTED THAT THE RIGHT MAIN GEAR INDICATION LIGHTS ILLUMINATED BOTH GREEN AND RED (UNSAFE CONDITION). THE CREW MOVED THE LANDING GEAR SELECTOR FROM THE OFF POSITION TO UP POSITION AND THE GEAR INDICATION RETURNED TO GREEN ONLY. THE CREW May 11, 2006 · N1PC · Boeing 7372P6SDR CA060508014Bolt · loose(CAN) DURING THE ACCOMPLISHMENT OF THE ANNUAL INSPECTION OF THE LANDING GEAR, MAINTENANCE STAFF NOTICED THAT THE LT IB AND RT OB TORQUE PLATES THAT SECURE THE BRAKE CALIPERS WERE LOOSE. THE 6 BOLTS TAHT SECURE THE TORQUE PLATES TO THE MAIN WHEEL AXLE ASSEMBLY May 8, 2006 · Airtrc AT802ASDR CA060509007Strut · cracked(CAN) WHILE DOING A 100 HOUR INSPECTION OF THE AIRCRAFT THE ENGINEER NOTICED SOME CRACKED PAINT ON THE BOTTOM SIDE OF THE STRUT EMINATING FROM THE LANDING GEAR BRACE BOLT HOLE. HE THEN REMOVED SOME OF THE PAINT AND REVEALED A CRACK 1.5 INCHES LONG GOING OUTWAMay 4, 2006 · Hughes 369DSDR CA060510011Trunnion · crackedTHE RT MAIN LANDING GEAR OLEO WENT FLAT AFTER LANDING. A CRACK WAS NOTICED ON THE UPPER TRUNNION, JUST UNDER THE SIDE BRACE ATTACH FITTING. THE UPPER TRUNNION WAS REPLACED.May 2, 2006 · Cessna 401BSDR 2006FA0000419Strut · brokenLH MLG STRUT BROKE ON TAXIApr 22, 2006 · N838PC · Piper PA44180TSDR 2006FA0000418Strut · brokenLT GEAR STRUT BROKE AT HOUSING.Apr 22, 2006 · N838PC · Piper PA44180TSDR A6WA200640156Strut · dischargedAFTER GEAR SELECTED DOWN, NOSE GEAR WOULD NOT EXTEND, HAD RED GEAR DISAGREE CAS MESSAGE, USED EMERGENCY GEAR EXTENSION, NOSE DOORS OPENED BUT DIDN`T EXTEND. REMOVED AND REPLACED PRIORITY VALVE IAW 32-33-15. REMOVED AND REPLACED SELECTOR VALVE IAW 32-33-10. Apr 18, 2006 · N418AW · Cndair CL6002B19SDR DXTA200601351Nut · looseAFTER TAKEOFF CLIMBING THROUGH FL 250 NOTICE A BUMP OR THUMP APPARENTLY COMING FROM NOSE GEAR AREA FOLLOWED BE GEAR UNLOCKED RED LIGHT. CYCLED GEAR ON APP & LIGHT WENT OUT. LOWER GEAR & NORMAL LAND. FOUND STRUT EXTENSION EXCEEDING MAX. LIMITS. FOUND RETAININApr 18, 2006 · N908QS · Cessna 750SDR CA060410006Cylinder · corrodedAT DISASSEMBLY BY FIRST AIR MAINTENANCE SERVICES (EASA APPROVAL NR 145-7030) THE OUTER CYLINDER WAS FOUND TO HAVE SEVERE CORROSION, VIRTUALLY PERFORATED AND ASSESSED AS INELIGIBLE FOR RETURN TO SERVICE. THE RECORDS INDICATE THE LANDING GEAR ASSEMBLY WAS REMOVApr 6, 2006SDR 000Bolt · departedWHILE TAXING TO PARK THE RT MLG LINK ASSEMBLY BOLT CAME OUT CAUSING THE UPPER AND LOWER LINKS TO SEPERATE. THE RT LANDING GEAR TURNED 90 DEGREES BENDING THE GEAR DOOR COVER.Mar 31, 2006 · N849JB · Cessna 421ASDR 2006FA0000381Strut · brokenLANDING GEAR BROKE JUST OUTSIDE OF THE GEAR BOLT. THE FACE OF THE CRACKED AREA APPEARS TO HAVE RUST ON IT THAT COULD INDICATE A PREVIOUS CRACK. (NE01200603823) (K)Mar 24, 2006 · N739YA · Cessna 172NSDR MASA200600831Strut · dischargedASH 7138 EWR, ABORTED TAKEOFF. SEVERE OSCILLATIONS ON NOSE GEAR STRUT AND THE STRUT WAS LOW. MX SERVICED THE NOSE STRUT.Mar 18, 2006 · N715SF · Cndair CL6002B19SDR COMA0660263Strut · wornFLIGHT 5057 - AFTER TAKEOFF FROM DAY RECEIVED A GEAR DISAGREE/NOSE DOOR OPEN MESSAGE, FLIGHT RETURNED TO THE FIELD. REPLACED THE NLG STRUT LOWER CYLINDER.Mar 18, 2006 · N712CA · Cndair CL6002B19SDR ABXA060149Strut · corrodedRIGHT MAIN LANDING GEAR STRUT CYLINDER SHOWED PITTING ALONG THE INNER SURFACE AT LOWER FLANGE AT CHROME AREA. DAMAGED GLAND THREADS. RIGHT MAIN LANDING GEAR STRUT ASSEMBLY REMOVED AND REPLACED WITH SERVICABLE UNIT IAW MM 32-40-1-02, 32-42-01-4 AND 32-43-02-2Mar 15, 2006 · N813AX · Doug DC863SDR DXTA200601301Strut · out of rigONCE LANDING GEAR WAS RETRACTED, RED UNLOCK LIGHT REMAINED ILLUMINATED. FOUND NOSE EXTENSION OUT OF LIMITS AND NOSE UPLOCK CABLE RIGGING TOO TIGHT. ADJUSTED NOSE GEAR RELEASE CABLE IAW 750 M/M 32-30-00. REPLACED NOSE STRUT IAW 750 COMPONENT M/M 32-20-02. OMar 15, 2006 · N943QS · Cessna 750SDR 2006FA0000372Axle · crackedCRACKS IN BOTH UPPER BOLT HOLES THAT SECURE AXLE TO STRUT ASSEMBLY ON BOTH LT AND RT MLG. PROBABLE CAUSE MAYBE HARD LANDING OR FATIGUE CRACKS DO TO NORMAL USE. (K)Mar 9, 2006 · N9219X · Piper PA34220TSDR 06FDEA0857Strut · crackedON FINAL APPROACH TO IND LT MAIN LANDING GEAR FAILED TO EXTEND FULLY DOWN AND LOCK. FWD PANEL GEAR HANDLE SHOWING RED DOWN ARROW, LT GEAR INDICATION SHOWS RED -UNLK-, WD GEAR PANEL INDICATION AND OVERHEAD WERE IN AGREEMENT LT GEAR NOT DOWN AND LOCKED. FLIGHTFeb 27, 2006 · N675FE · Airbus A300F4605RSDR 2006FA0000865Strut · damagedWHEN CHANGING SHOCK CORDS ON THIS AC, NOTICED A DISCOLORATION OF THE INNER STRUT TUBE (LONGER ONE, SUB PN 1180400) AND REMOVED IT FROM THE OUTER TUBE (SHORTER, SUB PN 1180300) ONE OF THE INNER STRUT TUBES WAS CORRODED APPROX 50 PERCENT OF CIRCUMFERENCE. THE OFeb 26, 2006 · N4879H · Piper PA17SDR 2006FA0000447Strut · corrodedCHANGING SHOCK CORDS, DISCOLORATION OF INNER STRUT TUBE (LONGER ONE), REMOVED IT FROM OUTER TUBE (SHORTER ONE) OF INNER STRUT TUBES WAS CORRODED APPROX 50 PERCENT OF CIRCUM. OTHER INNER STRUT HAD MULTIPLE CORROSION HOLES THROUGH METAL. BOTH SHORT TUBES (OUTEFeb 26, 2006 · N4879H · Piper PA17SDR DXTA200601263Strut · malfunctionedAFTER TAKEOFF DURING GEAR RETRACTION, THE GEAR HANDLE WAS DIFFICULT TO MOVE OUT OF THE DOWN DETENT BUT EVENTUALLY DID MOVE TO THE UP POSTION. MAINS RETRACTED NOSE DID NOT. STILL HAD GREEN NOSE LIGHT AND RED UNSAFE LIGHT. HANDLE WAS MOVED TO GEAR DOWN AND 3 Feb 26, 2006 · N903QS · Cessna 750SDR AMTA200600134Strut · unknownINSPECTED LT MLG IB STRUT IB LEG IAW CMM. FABRICATED 2 EA BUSHINGS, CAD PLATED, PEENED BORE IAW CMM. INSTALLED BUSHINGS IAW BSOPM. (K)Feb 13, 2006 · N514AT · Boeing 75723NSDR DHL2006804543Bolt · crackedLT MLG UPPER TORQUE LINK BOLT THREADED AREA CRACKED 0.500". REMOVED AND REPLACED LT MLG UPPER TORQUE LINK BOLT IAW MM 32-11-4 PG 201. REFER TO JC 8-32-20-007 FOR OPS CHECK.Feb 9, 2006 · N804DH · Doug DC873FSDR DHL2006804542Bolt · crackedRT MLG UPPER TORQUE LINK BOLT THREADED AREA CRACKED 0.500". REMOVED AND REPLACED RT MLG UPPER TORQUE LINK BOLT IAW MM 32-11-4 PG. 201. REFER TO JC 8-32-20-007 FOR OPS CHECK.Feb 9, 2006 · N804DH · Doug DC873FSDR DHL2006804534Link · crackedRIGHT MLG LINK NR 7 CRACKED 3.250 INCH LENGTH. REMOVED AND REPLACED RIGHT MLG BRAKE LINK NR 7 IAW MM 32-11-1 PG 401.Feb 6, 2006 · N804DH · Doug DC873FSDR 2006FA0000587Cylinder · unserviceableMLG HYD CYL, PN TB2047007/SN WO300497 WAS REMOVED AND SENT FOR INTERNAL LEAK AND A VERY STIFF SPOT ABOUT CENTER OF TRAVEL. CYL WAS RETURNED, REPAIRED, WARRANTY AS IS. INSTALL CYL ON LT MLG. INTERNAL LEAK NO LONGER EXISTED. UPON TESTING EMERGENCY EXTENSION Feb 2, 2006 · N2808W · Socata TB20TRINIDADSDR AALA20060059Schrader Valve · inoperativeSAN INFLIGHT T400/31JAN - NOSE GEAR WOULD NOT RETRACT. RETURNED TO SAN AND LANDED WITHOUT INCIDENT. FOUND NOSE STRUT FLAT. REPLACED SCHRADER VALVE AND SERVICED STRUT WITH FLUID AND AIR. SYSTEM GROUND CHECKED NORMAL OPERATION.Jan 31, 2006 · N9677W · Doug DC983SDR DXTA200601222Strut · underservicedLANDING GEAR HANDLE WOULD NOT MOVE AFTER TAKEOFF AND LANDING GEAR COULD NOT BE RETRACTED. FOUND NOSE STRUT STICKING END NOT FULLY SERVICED. SERVICED NOSE STRUT. PERFORMED GEAR SWINGS. OPERATIONAL CHECK OF GEAR SATISFACTORY. ALL WORK IAW CH 12-10-38 AND 32Jan 30, 2006 · N946QS · Cessna 750SDR MASA200600225Strut · overservicedASH 7273 IAD, ON APPROACH CAPTAIN REPORTED FLAPS 1/2 SPEED, PITCH FEEL FAULT, RUDDER LIMIT FAULT STATUS MSGS ON FINAL APPROACH. MX DE-SERVICED NOSE STRUT AND ALL FAULTS CLEARED. ACFT CONTINUED OPERATIONS.Jan 27, 2006 · N510MJ · Cndair CL6002C10SDR DXTA200601215Strut · underservicedAFTER TAKEOFF GEAR WOULD NOT RETRACT. PLACED ACFT ON JACKS AND NOTED NOSE STRUT WOULD NOT FULLY EXTEND ALLOWING THE NOSE WOW SWITCH TO MAKE CONTACT. COMPLIED WITH NOSE STRUT SERVICING IAW 750 AMM 12-10-38. LOWERED ACFT ON GROUND THEN PLACED BACK ON JACKS ANJan 25, 2006 · N948QS · Cessna 750SDR QXEA200600293Cylinder · corrodedYYC - C3 NOSE LANDING GEAR CORROSION ON OUTER CYLINDER. REPAIRED IAW HORIZON AIR EA R-32-197 AND REO 670-32-21-083 SCR 0001-06 REV NC.Jan 24, 2006 · N606QX · Cndair CL6002C10SDR 4516601262006Strut · overservicedCREW RECEIVED A NWS CAS MESSAGE AFTER ROTATION. TOWER FLY-BY INDICATED NOSE WHEELS 45 DEGREES OFF CENTER. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. ON LANDING, NOSE WHEELS CASTORED TO CENTER WITHOUT DAMAGE. LANDING UNEVENTFUL. SECOND INSTANCE OF THIS Jan 23, 2006 · N430FX · Lear 45LEARSDR 2006F00010Torque Shaft · brokenLT MAIN GEAR UPPER TORK LINK SHAFT (P/N 27-51540-003) BROKE ON LANDING, AIRCRAFT WAS UNABLE TO TAXI, LT MAIN WHEEL DIRECTION UNCONTROLLABLE. TORK LINK SHAFT BROKE AT BOTH OB ROLL PIN HOLES. SERVICE BULLETIN 227-32-46 ADDRESSES THE PROBLEM. THE SERVICE BULLETJan 21, 2006 · N184SW · Swrngn SA227ACSDR BIK2006F00000Cylinder · crackedDURING INSPECTION, FOUND ONE OF THE TORQUE LINK ATTACH EARS CRACKED FROM BOTTOM UP .7500 TOTAL LENGTH OF EAR. THIS AIRPLANE WAS USED PRIMARILY FOR FLIGHT TRAINING FOR LAST 1300 HOURS. WING WAS REPLACED IN 1981, BUT FOUND NO RECORD OF LANDING GEAR REPLACEMENTJan 20, 2006 · N8ML · Piper PA28180SDR DXTA200601208Strut · out of adjustIN CRUISE, A THUMP OF NOSE GEAR REPRESSURIZING. UNLOCK LIGHT FOR GEAR WAS ON AND REMAINED ON TILL GEAR WAS PUT DOWN. REPEAT WRITE UP. FOUND NLG STRUT TO MEASURE 9.92 INCHES. MAX STRUT EXTENSION SHOULD ONLY BE 9.75 INCHES. SUSPECT LOWER ORIFICE CAP COMING Jan 20, 2006 · N916QS · Cessna 750SDR COMA0560819Strut · dischargedFLIGHT 5468 - GEAR DISAGREE WARNING. SERVICED THE NLG SHOCK STRUT.Jan 19, 2006 · N999CA · Cndair CL6002B19SDR 4516601172006Strut · dischargedON TAKEOFF, NOSE GEAR WOULD NOT RETRACT. ATC FLY-BY CONFIRMED NOSE WHEELS COCKED 45 DEGREES. DIVERTED AIRCRAFT TO BDL. LANDING UNEVENTFUL. MAINTENANCE FOUND STRUT WITH NO APPRECIABLE AIR CHARGE AND OVER-SERVICED BY 17 OUNCES OF FLUID. SIMILAR PREVIOUS INCJan 17, 2006 · N430FX · Lear 45LEARSDR VNAA0601005Shock Absorber · failedAFTER TAKEOFF THE LANDING GEAR WOULD NOT RETRACT AND THE CREW REPORTED A GEAR DISAGREE WARNING. THE CREW DECLARED AN EMERGENCY, FOLLOWED THE QRH, AND RETURNED TO CLT. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THAT THE NOSE LANDING GEAR SHOCK FAILED TO EXTJan 9, 2006 · N719PS · Cndair CL6002C10SDR 2006FA0000071Cylinder · crackedCOLLAR SEPARATING FROM TUBE DUE TO INSUFFICIENT PENETRATION WHEN PART WAS FURNACE BRAZED OR SILVER SOLDERED TOGETHER WORKING COLLAR CAUSED PART TO WORK AND CRACK BOSS. RECOMMEND INSPECTION OF COLLAR AT BOTTOM OF GEAR STRUT FOR ANY MOVEMENT OR WORKING BETWEEN Jan 2, 2006 · N91VK · Piper PA60601PSDR DXTA200601178Strut · dirtyAFTER TAKEOFF, GEAR WOULD NOT RETRACT. JACKED AIRCRAFT, CYCLED GEAR 10 TIMES, COULD NOT DUPLICATE DISCREPANCY. CLEANED LOWER NLG STRUT OF FOREIGN STICKY SUBSTANCE. RECYCLED GEAR 5 TIMES, COULD NOT DUPLICATE. WORK PERFORMED IAW CE750 M/M CH 32-00-01.Jan 2, 2006 · N934QS · Cessna 750SDR MASA200501067Strut · leakingNOSE GEAR DISAGREE AFTER TAKEOFF UPON GEAR UP SELECTION. AIRCRAFT WAS FERRIED TO CLT. MAINTENANCE REPACKED NOSE STRUT.Dec 21, 2005 · N593ML · Cndair CL6002B19
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