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 QXEA2011012400072Strut · damagedFOUND DAMAGE AT RT MLG RT FWD STABILIZER STAY FWD LOWER EDGE APPROX 1" IN LENGTH AND .040 IN DEPTH. FERRIED FOR REPAIRS. REPLACED THE RT MLG STABILIZER STRUT IAW AMM 32-11-16-000-801. RETURNED TO SERVICE.SDR AALA20110120AFW03Support Fitting · corrodedRIGHT WING MAIN LANDING GEAR SIDE STRUT SWIVEL SUPPORT FITTING BORE AND FACE CORRODED. REPAIRED DISCREPANCY PER EA B767-57-014358.SDR ALGA1/14/11RECV40Crosstube · corrodedPITTING, CORROSION, DISTANCE BETWEEN REPAIRS IS LESS THAN 3 INCHES APART AND IS UNACCEPTABLE.SDR ALGA11211AA1306Crosstube · corrodedCROSSTUBE CORROSION DAMAGE AT .007. LIMIT IS .005.SDR F3LA2011011800581Shock Absorber · scratchedLT MLG SHOCK ABSORBER SCRATCHED IN CHROME AREA. 60 TO 80 SCRATCHES 18 INCHES LONG X .003 INCHES DEEP ON FWD SIDE OF STRUT. R & R LT MLG SHOCK ABSORBER IAW AMM 32-11-13-020-058B AND 32-11-13-420-054B.SDR ASMF201101003Strut · damagedDURING TRANSIT CHECK, A HYD SLIP WAS DETECTED IN THE LT MLG SHOCK ABSORBER. DURING MX REVISION, THE MLG SHOCK ABSORBERS WERE COMPRESSED; SO ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL PERFORMED A MLG SERVICE IAW MM 12-15-31, ALL CORRECT AND THE MLG SHOCK STRUSDR 2011FA0000082Strut · failedAFTER LANDING ON 12/10/2010, THE UPPER LINK ATTACH POINT FAILED ON THE MLG STRUT CLYLINDER, PN 65319-002. THIS FAILURE CAUSED THE OLEO STRUT TO BE EJECTED FROM THE CYLINDER CAUSING MAJOR DAMAGE TO ACFT. SB 1311 ADDRESSES THIS ISSUE.SDR 2010FA0001230Strut · damaged(OG5S) DURING ROUTINE (PHASE) INSP, THE NOSE GEAR OLEO STRUT WAS DISASSEMBLED FOR REPLACEMENT OF O-RINGS. DURING DISASEMBLY, THE TECH FOUND THE INNER STRUT TUBE AT THE TOP HAD RETAINING PINS WHICH WERE DAMAGED ALLOWING LOWER PART OF TUBE TO BE WORKED LOOSE FROSDR DXTA2010112904336Strut · leakingON FINAL APPROACH THE LT MLG FAILED TO FULLY EXTEND TO GIVE A GREEN DOWN AND LOCKED LIGHT INDICATION. THE LANDING GEAR WAS BLOWN DOWN IAW THE EMERGENCY CHECKLIST. WHEN PNEUMATIC PRESSURE WAS APPLIED, THE LT MAIN GEAR FULLY EXTENDED GIVING A GREEN LIGHT INDICATSDR CA110318003Lug · cracked(CAN) DURING GEAR INSPECTION, FOUND A CRACK 36 MM LONG BY 5.5MM DEEP ON THE FWD LT LUG OF THE UPPER MEMBER. CYCLE SINCE OVERHAUL 1282.SDR DXTA2010112204313Strut · leakingON LANDING ROLL, BRAKES FELT "GRABBY". UPON POST FLIGHT INSP, FOUND LT MAIN GEAR STRUT WET AND FLUID DRIPPING FROM MAIN STRUT INBD SIDE OF STRUT. LT STRUT IS LESS THAN A CREDIT CARDS WIDTH. RESEALED LT STRUT AND SERVICED. R & R LT BRAKE ASSY. R & R LT MAISDR C2XA10SH391Shock Absorber · damagedSHV - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. LANDING GEAR AIR/GROUND FAIL ON EICAS. REMOVED AND REPLACED RT MAIN LANDING GEAR SHOCK ABSORBER IAW EMB 145 AMM 32-10-02. OPS CHECK GOOD. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR USAA2010120892920Pin · corrodedSAL - S5 - MAJOR REPAIR - CORROSION ON THREADS OF LEFT MAIN LANDING GEAR TORQUE LINK APEX PIN. REPLACED LEFT MAIN LANDING GEAR TORQUE LINK APEX PIN IAW A320 AMM 32-11-29.SDR FCPR201000236Strut · corroded(FCPR) LT LANDING GEAR CYLINDER SEVERELY CORRODED INTERNALLY AT LOWER END.SDR CA101022002Strut · fracturedLT MAIN GEAR LOWER STRUT TORQUE KNEE ATTACH BOSS FRACTURED AND SEPARATED FROM MAIN LOWER ASSY DURING TAXI CAUSING SEVERE SHIMMY.SDR CA100916006Strut · crackedAFTER CHANGING A LANDING GEAR DAMPER FOR LOW PRESSURE, THE ACFT WAS PLACED BACK ON THE GROUND. AFTER IT WAS SITTING ON THE GROUND THE SAME ACFT ORIENTATION PRIOR TO CHANGING THE DAMPER WAS NOTED, TAIL LOW AND LEANING TOWARD THE LT. UPON INSP OF THE LANDING GSDR CA100914006Pump · inoperativeLANDING GEAR DID NOT FULLY EXTEND BECAUSE THE MOTOR/PUMP RAN SHORT AND TRIP THE 60AMP CIRCUT BREAKER. AN EMERGENCY WAS DECLARED BY THE AIR CREW. THE LANDING GEAR WAS THEN DEPLOYED USING THE EMERGENCY HAND PUMP, RESULTING IN 3 GREEN DOWN AND LOCKED INDICATION.SDR C2XA10IA251Shock Absorber · lowIAH - FLIGHT 2219, THE CREW REPORTED A FIVE SECOND LANDING GEAR AIR GROUND FAIL MESSAGE AFTER SELECTING GEAR UP. THE AIRCRAFT LANDED AT OAH WITHOUT INCIDENT WHERE MAINTENANCE SERVICED BOTH MAIN GEAR SHOCK ABSORBERS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TOSDR C2XA10IA250Shock Absorber · lowIAH - FLIGHT 2219, THE CREW REPORTED A FIVE SECOND LANDING GEAR AIR GROUND FAIL MESSAGE AFTER SELECTING GEAR UP. THE AIRCRAFT LANDED AT OAH WITHOUT INCIDENT WHERE MAINTENANCE SERVICED BOTH MAIN GEAR SHOCK ABSORBERS, AND THE AIRCRAFT WAS APPROVED FOR RETURN TOSDR UG8A2010080601Axle · corrodedLT MLG AXLE HAS LIGHT SURFACE CORROSION.SDR HYIA69SCRXL802Axle · crackedUPON TAXING INTO POSITION TO HOLD FOR TAKEOFF,CREW REPORTED EXPERIENCING TAXIING/ BRAKING DIFFICULTIES. MX FOUND RT MAIN GEAR LOWER BARREL AND AXLE ASSY CRACKED. MX R & R RT MAIN GEAR LOWER BARREL AND AXLE ASSY. ACFT RETURNED TO SERVICE.SDR CA100817020Shock Absorber · corrodedDURING AN INSP THE AME FOUND FWD PLATEN (C2UF1219) CORROSION CRACKED, COMPLETED SHOCK ASSY, REPLACED.SDR HALA2010073000349Spacer · missingETOPS SIGNIFICANT SYS - ON ETOPS WALK AROUND FOUND BOTH NLG AXLE NUTS SPACERS (OUTER) MISSING. R & R LT & RT NLG TIRES & INSTALLED OUTTER SPACERS ON BOTH AXLES. SPIN CK GOOD. AMM32-45-02 & HAL CARD M296-767. OK FOR SVC. ALL SPACERS INSTALLED ON BOTH NLG ASDR HYIA402VNRTRUNNBarrel · unserviceableCREW REPORTED, RT MAIN GEAR SHEARED OFF ON LANDING ROLL. MX FOUND RT MAIN GEAR UPPER BARREL AND TRUNNION ASSY SHEARED JUST BELOW MLG ACTUATOR ATTACH POINT. MX IS IN THE PROCESS OF REPLACING RT MLG ASSY, RT ENGINE, RT PROPELLER, RT SIDE INBD AND OTBD FLAP PANESDR HYIA812RAXLEAxle · fracturedON TAKEOFF ROLL, ACFT STARTED TO TURN SHARPLY TO THE RT, ABORTED TAKEOFF. MX FOUND RT MAIN GEAR AXLE BROKEN AT LOWER HALF. MX R & R LOWER BARREL AND AXLE ASSY AND RETURNED ACFT BACK TO SERVICE.SDR CA100720002Damper · cracked(CAN) DURING 1000 HOUR INSPECTION, THE TOP MOUNT OF THE RT MAIN GEAR DAMPER UNIT WAS FOUND TO BE CRACKED THROUGH ONE FLANGE OF THE UPPER MOUNTING. THE CRACK TRAVELS FROM THE BOLT HOLE TO THE UPPER SURFACE OF THE FLANGE.SDR 2010FA0000723Strut · damagedDURING LANDING THE RT OLEO PN 3-665 SPRING AND SHAFT POPPED AND CAUSED OLEO TO OVSR EXTEND AND BEND REARWARD. THIS ALLOWED THE WHEEL AND BRACE TO COLLAPSE.SDR VGQY2010060700044Sleeve · crackedRIGHT BODY LANDING GEAR FOUND WITH HYDRAULICS LEAKING. DURING SEAL REPLACEMENT FOUND INNER SLEEVE CRACKED AND METAL CHIPS FALLING OUT FROM STRUT, INNER CYLINDER. REMOVED AND REPLACED RT BODY LANDING GEAR AS PER AMM 32-13-01, REV 90.SDR CA100708001Strut · brokenLT MLG STRUT SNAPPED IN HALF OUTBOARD OF SADDLE/CLAMP, WHILE PARKED/TIED DOWN. NO EVIDENCE OF HARD LANDING OR DAMAGE TO A/C EXCEPT SMALL DENT ON LOWER WING-SKIN FROM CONTACT WITH WHEEL FAIRING.SDR 2010FA0000901Strut · corrodedLANDING GEAR STRUT ASSY FAILED DUE TO INTERNAL CORROSION RESULTING IN COLLAPSE OF RT GEAR DURING LANDING. MINOR DAMAGE TO WING, COWLING AND GEAR. PROP STRIKE. AGING ACFT ISSUE.SDR SIMA201017303Strut · lowON FLIGHT 3248 ON APPROACH THE CREW REPORTED AN EXCESSIVE RUBBING NOISE FROM THE MAIN GEAR AREA DURING RETRACTION. THE CREW DECLARED AN EMERGENCY WHEN AMA TOWER ADVISED OF POSSIBLE BLOWN TIRE. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTIOSDR HYIA618CARHAXLEAxle · brokenON TAKEOFF ROLL, CREW EXPERIENCED A YAW WHICH CAUSED THE TAKEOFF TO BE DISCONTINUED AT LOW SPEED. CREW TAXIED BACK TO THE RAMP. MX FOUND RT MAIN GEAR AXLE ASSY BROKEN AT LOWER HALF. MX R & R AXLE ASSY, AND RETURNED THE ACFT BACK TO SERVICE.SDR HYIA36911RHAXLEAxle · crackedON TAXI, CREW REPORTED LOAD "POP" FROM RT GEAR, ACFT BECAME DIFFICULT TO TAXI. MX FOUND RT MAIN GEAR AXLE ASSY CRACKED AT LOWER HALF. R & R AXLE ASSY. RELEASED ACFT BACK TO SERVICE.SDR 2ARF201006005Seal · leakingDURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED ON THE RIGHT MAIN LANDING GEAR SHOCK ABSORBER. MAINTENANCE PERSONNEL REPLACED THE SEAL AND RING IAW MM 32-17-02 AND SERVICE WAS PERFORMED TO THE SHOCK ABSORBER IAW MM 32-11-02, TESTED CORRECT.SDR MASA2010052000527Gland Nut · corrodedCORROSION FOUND IN MLG OUTER CYL GLAND NUT THREADS AND IN CHROME OF STRUT ASSY IN EXCESS OF LIMITS PER BOMBARDIER REO 670-32-11-221-REV A, AND GOODYEAR SCR 0003-07 REV NC. MX REPLACED OUTER CYLINDER ASSEMBLY.SDR CA100525021Strut · misinstalled(CAN) AIRCRAFT WAS BROUGHT IN FOR CONFORMANCE INSPECTION. EDO 4580 FLOATS HAVE BEEN MODIFIED TO EDO 679-4930 FLOATS UNDER SEAFLIGHT STC SF92-1. THE FLOATS DO NOT MEET THE AIRWORTHINESS REQUIREMENTS FOR THE FOLLOWING REASONS. 1. NO STC TO INSTALL 679-4930 FLOSDR UALA2010051401645Seal · failedLGCIU 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. LOUD BANG ON TAKEOFF. WILL REPLACE SEALS. ACFT JACKED, STRUT REMOVED, REPLACED STRUT SEALS AND STARTED LEAK CHECK. STRUT HAS 275 PSI AIR CHARGE STARTING AT 1325. NEED TO COMPLETE STRUT INSTALLATION IAW SAME MMSDR F3LA2010052200430Strut · corrodedREF HEAVY MX NON ROUTINE N0538. RT MLG INNER BARREL (CYL) HAS CORROSION. REMOVED CORROSION AND REPAIRED IAW EA 3 AC-32R-31779.SDR AALA20100326ORD01Strut · low pressureORD - INFLIGHT DAY-DFW. CREW REPORTED AFTER TAKEOFF THE NOSE LANDING GEAR WOULD NOT RETRACT. EMERGENCY DECLARED FLIGHT DIVERTED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. SERVICED NOSE GEAR STRUT. SYSTEM GROUND CHECK NORMAL OPERATION.SDR DXTA2010032304049Strut · malfunctionedON DEPARTURE, LANDING GEAR HANDLE COULD NOT BE MOVED TO THE UP POSITION, LANDING GEAR REMAINED DOWN AND LOCKED. APPROX 1-2 MINS LATER THE "WOW MISCOMPARE" CAS MSG ILLUMINATED FOR 30 SECONDS THEN EXTINGUISHED. REMOVED LOWER STRUT, CLEANED AND REPACKED WITH NEWSDR WRLA20100316348Strut · damagedDUE TO HARD LANDING, INSP A PERFORMED AND FOUND CENTER LANDING GEAR STRUT DAMAGED. CENTER LANDING GEAR AND ADDITION BRAKES AND WHEELS REPLACED.SDR FDEA201003040644Cylinder · overservicedLANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. RAN QRH AND STILL UNABLE TO BRING GEAR LEVER TO UP POSITION. BURNED OFF EXCESS FUEL AND LANDED WITHOUT INCIDENT. UNABLE TO MOVE GEAR HANDLE OUT OF DOWN DETENT WITH OR WITHOUT OVERIDE BUTTON. FOUND TRIM CYLINDESDR FDEA201002250529Strut · corrodedDURING SERVICE CHECK AT HANGAR, FOUND LT MLG OUTER SLEEVE GLAND THREADS ARE CORRODED ON INSIDE OF CYLINDER. SEVERE CORROSION OF ALL THREADS FOR 360 DEGREES. EXTREME EROSION OF THREADS OF UP TO 40 PERCENT FROM 4:00 TO 7:00 POSITION. REMOVED AND REPLACED LT MSDR FDEA201002250525Strut · corrodedRIGHT MLG SHOCK STRUT (OUTER CYLINDER) LOWER CURCUMFERENTIAL INTERNAL THREADS ARE CORRODED/PITTED. ALSO, THE SHOCK STRUT GLAND NUT THREADS FOR MLG OUTER CYLINDER (SHOCK CYLINDER) ARE CORRODED/PITTED (REF SNRM 872). RIGHT MAIN OUTER CYL.-LOWER CIRCUMFERENTIALSDR FDEA201002250524Strut · corrodedLEFT MLG SHOCK STRUT (OUTER CYLINDER) LOWER CIRCUMFERENTIAL INTERNAL THREADS ARE CORRODED/PITTED. ALSO, THE SHOCK STRUT GLAND NUT THREADS FOR MLG OUTER CYLINDER (SHOCK STRUT) ARE CORRODED/PITTED. LT MAIN OUTER CYL.-CIRCUMFERENTIAL INTERNAL THREAD CORROSIOSDR FDEA201002250523Strut · contaminatedWATER FOUND IN UPPER LT MLG STRUT "B" CHAMBER EXT WATER FOUND IN UPPER LT MLG STRUT "B" CHAMBER EXTENSION TUBE AREA. DURING SIGHT ROD ASSY. R & R. (REF NR0002) INVESTIGATE AS REQ. REPLACED NEW GEAR INSTALLED REF. W/C 32T1902SDR DXTA2010022404002Strut · underservicedGEAR HANDLE WAS MOVED TO "UP" POSITION, NOSE GEAR RETRACTED WHILE BOTH MAIN GEAR LIGHTS STAYED ILLUMINATED WITH GEAR "UNLOCK" LIGHT ON. MAIN GEAR CYCLED SEVERAL TIMES IN A 20-25 SECOND TIME PERIOD. FINALLY MAIN GEAR RETRACTED, AND UNLOCK LIGHT EXTINGUISHED. FSDR UALA2010022200657Strut · corrodedFOUND CORROSION ON INNER WALL OF OUTER STRUT. NEW OUTER CYLINDER REPLACED, REASSEMBLING GEAR AND ALL COMPONENTS BEFORE INSTALL.SDR MALA100011Strut · dischargedGEAR DISAGREE WARNING DURING RETRACTION. SERVICED STRUT; INSPECTED; GEAR SWINGS, NO FAULTS FOUND.SDR USAA2010020890300Strut · crackedPHX - MAJOR REPAIR - WEEKLY - RIGHT MAIN LANDING GEAR UPPER STRUT FAILED ULTRASONIC INSPECTION, NUMEROUS CRACK INDICATIONS WERE NOTED. REPLACED RIGHT MAIN LANDING GEAR ASSEMBLY.
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