JASC 3211
Service difficulty reports · 1,177
Reports filed under 3211 · Main Landing Gear Attach Section, 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 = '3211' 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 = '3211' 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 2025FA0000496Bushing · looseRIGHT MAIN GEAR ATTACH BUSHING P/N 0541202-4 LINER BECAME DISBONDED CREATING PLAY IN THE GEAR LEG. THIS AIRCRAFT IS OUTSIDE THE S.N. RANGE OF SEL-32-08 YET HAS THE SAME PROBLEM. THE FAILED BUSHING WAS INSTALLED ON 11/19/2024 AND HAD 291 HOURS IN SERVICE.SDR 2025FA0000411Attach Bolt · brokenTHE BOTTOM MOST BOLT, WASHER, AND NUT, WAS FOUND MISSING ON THE MLG AXLE WHERE THE AXLE ATTACHES TO THE LANDING GEAR LEG. BOLT P/N: LN9037-M6042, WASHER P/N: DIN125A-M6-A2, NUT P/N: DIN985-M6-A2.SDR FDEA202506160965Support Rib · corrodedL/H MLG SUPPORT WING RIB 5 FWD LUG CORROSION NOTED REPAIR PER E.A. 6-5710-T0383717 AND AIRBUS DRAWING R57240425.SDR FDEA202506160964Support Rib · corrodedR/H MLG SUPPORT WING RIB 5 FWD LUG CORROSION NOTED BETWEEN BUSH "D" AND BUSH "E". REPAIR IN ACCORDANCE WITH E.A. 6-5710-T0383720 AND AIRBUS REPAIR DRAWING R57240425.SDR DXTA2025061703900Torque Link · out of positionDURING GEAR RETRACTION CYCLE, NLG TOQUE LINK MADE CONTACT WITH THE L/H AND R/H NLG DOORS. GEAR WERE EXTENDED TO DOWN AND LOCK AND DAMAGE WAS EVALUATED. PER EMB-505 AMM 32-35-00-720-801-A VERIFICATION OF THE NLG TORQUE LINK SHOULD HAVE BEEN DONE . TECHNICIAN LOSDR 2025FA0000540Pivot Pin · dentedDURING ACCOMPLISHMENT OF ADSI IB78J320002-LH, INSPECTION FOUND 2OFF DENT MIDDLE OF OUTER DIAMETER (OD) AREA OF THE GRIP LENGTH (NEAR THE BUSHINGS).SDR CALA2024122401635Spring · missingPDA 1 R/H MAIN LANDING GEAR JURY SPRING FOUND MISSING REPLACED BOTH FWD AND AFT RIGHT MAIN LANDING GEAR JURY STRUT SPRINGS REF AMM 32-32-05-004-001 AND AMM 32-32-05-404-009. SDR FLAGGED FOR PDA 1 REF GMM 02-30-95. PARTS USED: 00-0594-3-2285,QTY :1 76-3211-3-0SDR 2024FA0000940Bushing · looseRIGHT MAIN GEAR ATTACH BUSHING P/N 0541202-4 LINER BECAME DISBONDED CREATING PLAY IN THE GEAR LEG. THIS AIRCRAFT IS OUTSIDE THE S.N. RANGE OF SEL-32-08 YET HAS THE SAME PROBLEM. THIS BUSHING HAD BEEN REPLACED AT THE LAST 100HR INSPECTION, IT LASTED 100HRS.SDR 2024FA0000865Bushing · wornFOUND R/H MAIN LANDING GEAR LEG BUSHING WORN/LOOSE.SDR 2024FA0000863Bushing · wornFOUND R/H MAIN LANDING GEAR LEG BUSHING WORN/LOOSE.SDR AALA202411059462Pin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND MAIN LANDING GEAR UPPER TORQUE LINK PIN. REPLACED TORQUE LINK PIN PER SAFRAN CMM 32-11-33.SDR 2024FA0000787Bolt · brokenRIGHT MAIN LANDING GEAR ATTACHMENT BOLT BROKE. ONE OF TWO THAT HOLD THE OUTBOARD GEAR LEG ATTACHED THE SECOND BOLT WAS BENT FROM BEING THE ONLY BOLT HOLDING THE GEAR LEG IN PLACE. THE PILOTS CAN NOT SEE THE BOLT IS BROKEN DURING PER-FLIGHTS AND COULD MAKE AS MSDR 2024FA0000758Bushing · debondedNEW LANDING GEAR BUSHING 0541202-4 WAS INSTALLED ON 9/5/2015. PART TOTAL TIME IS 1504 HOURS. FOUND INNER BONDED MATERIAL SEPARATED FROM THE METAL BUSHING AND IT HAD MIGRATED OUTSIDE OF THE BUSHING TOWARDS THE WHEEL. N2864Q FLIES ABOUT 200 HOURS PER YEAR AND ISSDR 2024FA0000710Crosstube · crackedCRACKED AFT, LANDING GEAR CROSS TUBE AT STRUT CONNECTION. TSO: 1690.3SDR 2024FA0000591Torque Link · brokenAFTER LANDING, RH MLG LOWER STRUT SEPARATED FROM UPPER STRUT. UPPER TORQUE LINK ATTACHMENT EAR BROKE.SDR 2024FA0000546Bushing · looseLEFT MAIN GEAR ATTACH BUSHING P/N 0541202-4 LINER BECAME DISBONDED CREATING PLAY IN THE
GEAR LEG. THIS AIRCRAFT IS OUTSIDE THE S.N. RANGE OF SEL-32-08 YET HAS THE SAME PROBLEM.SDR 2024FA0000544Bushing · looseRIGHT MAIN GEAR ATTACH BUSHING P/N 0541202-4 LINER BECAME DISBONDED CREATING PLAY IN THE GEAR LEG. THIS AIRCRAFT IS OUTSIDE THE S.N. RANGE OF SEL-32-08 YET HAS THE SAME PROBLEM.SDR FDEA202312220068Fitting · corrodedLH RIB 5, MLG FWD PINTLE AIRFRAME ATTACH FITTING HAS CORROSION ON AFT SPOT FACE. REPAIRED PER AIRBUS INSTRUCTIONS R57240425SDR FDEA202312220067Fitting · corrodedLH RIB 5, MLG FWD PINTLE AIRFRAME ATTACH FITTING HAS CORROSION ON FWD SPOT FACE. REPAIRED PER AIRBUS INSTRUCTIONS R57240425SDR FDEA202312200066Fitting · corrodedL/H MLG AFT PINTLE FWD LUG HAS SIGN OF CORROSION. REPAIRED PER AIRBUS INSTRUCTIONS R57240425SDR FDEA202311281910Fitting · corrodedL/H MLG RIB 5 HAS CORROSION UNDER SPLIT BUSHINGS FWD LUG. APPROX 10 O'CLOCK LOOKING AFT. REPAIRED PER AIRBUS REPAIR INSTRUCTIONS R57240425.SDR 2023FA0000770Link · brokenAIRCRAFT 9V-SWH WAS UNDERGOING “C06” CHECK IN HANGAR ENVIRONMENT. A LANDING GEAR ALTERNATE EXTENSION TEST WAS SCHEDULED. WHILE ON JACKS, THE INITIAL GEAR LEVER UP RETRACTION TEST
WAS COMPLETED SUCCESSFULLY. HOWEVER, WHILE STILL PERFORMING THE LANDING GEAR ALSDR 2023FA0000759Nut · backed outTHE LEFT MAIN LANDING GEAR FAILED AS A RESULT OF THE NUT ON THE LEFT TORQUE LINK BOLT FAILED. THE TORQUE LINK SEPERATED AND FAILD TO KEEP THE WHEEL ALIGNED WITH THE AIRCRAFT. RESULTING IN DAMAGE TO AIRCRAFT.SDR 2023FA0000752Bolt · brokenRIGHT AFT MAIN LANDING GEAR BOLT BROKE. THIS IS ONE OF TWO OUTBOARD MOUNT BOLTS THIS BOLT WAS INSTALLED NEW 10/03/2018 AND HAD 2764.6 TTSN THE BOLT BROKE IN THE THREADED AREA. THE PILOTS CANNOT SEE THE BOLTS DURING THE PRE-FLIGHT INSPECTION AND CAN MAKE HUNDRSDR CALA2023111003329Spring · missingRT HAND MAIN LANDING GEAR SIDE BRACE DOWNLOCK 1 EA SPRING MISSING. REF IPC 32-11-12-01 ITEM 160. M&E 19-321-3-0075 PIC ADDED SDR FLAGGED. REPLD MSSING SPRING IAW AMM 32-11-22/401, REMOVAL TASK 32-11-22-004-015 & INSTALLATION TASK 32-11-22-404-007.SDR REXA2024110101382Bracket · crackedFWD BRACKET IS CRACKED FOR SYS. 3 BRAKE ACCUMULATOR. REMOVED FWD O/B, I/B CRACKED BRACKET AT SYS. 3 BRAKE ACCUMULATOR .IAW CRJ 900 SRM 51-42-06-001-001-A01. LOCATED, DRILLED AND INSTALLED O/B, I/B FWD BRACKET AT SYS 3 BRAKE ACCUMULATOR . IAW CRJ 900 SRM 51-4SDR 2023FA0000630Bolt · failedMAIN LANDING GEAR LEAF SPRING INNER ATTACH BOLT P/N NAS1106-24 ON LH SIDE OF AIRCRAFT, FAILED MID SHANK ABOVE THE THREADS, 50HR AFTER INSTALLED DURING REPETITIVE INSPECTION BROUGHT ON BY MANDATORY SERVICE BULLETIN-99. BOLT FAILURE CAUSED DEFORMATION OF THE FUSSDR IPXA2023110891070Trunnion · crackedRIGHT AFT TRUNNION, CRACKSSDR JYDR20230607155Flange · brokenUPON RETURN TO SERVICE AT COMPLETION OF LOGGING CYCLE AT 250-FOOT HOVER (GRAPPLE PLACED ON GROUND) R/H MLG STRUT AND WHEEL ASSY DETACHED. THIS IS A PRELIMINARY REPORT TO MEET REPORTING REQUIREMENTS.
ONCE MLG IS RECEIVED BY THIS REPAIR STATION AND ANALYZED REPSDR EE4Y2023051517734Unknown · unknownDURING COMPLIANCE WITH THE ALLEGIANT TASK CARD 321101-01-2-002, IT WAS FOUND THE RH MAIN LANDING GEAR SLIDING CHROME WITH SCRATCHES (7EA) AT 14 O’CLOCK POSITION. THE PART WAS REMOVED AND SENT REPAIR SHOP.THIS MAINTENANCE ACTIONS IS COVERED BY COOPESA JOB A1N11SDR QXEA2023052600084Bolt · corrodedDURING C2 INSPECTION, FOUND THE LH MLG RETRACTION ACTUATOR BOLT CORRODED. REPLACED THE LH MLG RETRACTION ACTUATOR BOLT.SDR CALA2023033100955Bracket · unknownSHOCK ABSORBER FAULT DISPLAYED ON UPPER ECAM SCREEN - L-G NLG STRUT PRESSURE IS WITHIN LIMITS SEE LOG PAGES 4197940, 4196147, 4181286, 4181253, FOUND AJUSTMENT OUT OF LIMITS TO NLG PROX SENSORS OUT OF LIMITS. REPLACED BRACKET AND LINKAGE TO SENSOR 25GA AND 24GSDR VNAA202328020011Gland Nut · corrodedCORROSION ON GLAND NUT OF LH MLG PISTON AXLESDR CALA2023021600466Bearing · failedDUE TO DAMAGE ON RH MLG #3 WHEEL , PERFORM CONDITIONAL INSPECTIONS FOR WHEEL BEARING FAILURE, TASK 05-51-17-212-001 AND HEAT DAMAGE OF AXLE INSPECTION, TASK 05-51-17-212-036. DOCUMENT ALL FINDINGS FURTHER FLIGHT. SEE PHOTOS ATTACHED FOR DAMAGE DETAILS. CONDITSDR CALA2022112803239Cap · missingPDA 3 FOUND ON WALK AROUND : RIGHT MAIN LANDING GEAR DAMPER IS MISSING DUST CAP. INSTALLED NEW DUST CAP AT MLG DAMPER PARTS USED: 18-3211-3-0037,QTY :1SDR CALA2022112803238Cap · missingPDA 3 FOUND ON WALK AROUND : LEFT MAIN LANDING GEAR DAMPER IS MISSING DUST CAP. INSTALLED NEW DUST CAP AT MLG DAMPER.PARTS USED: 18-3211-3-0037,QTY :1SDR QXEA2022112100325Spring · brokenLEFT MAIN GEAR SPRING IS BROKEN ( LANDING GEAR RETRACTION SYSTEM ). REMOVED FROM SERVICE. R&R BROKEN IB L/H MLG STABILIZER BRACE LOCK SPRING IAW AMM TASK 32-11-016-000-802/400-802. ALL GEAR PINS HAVE BEEN REMOVED AND FLAGS REATTACHED AND NOSE LOCK HAS BEEN STOSDR YENA2022100600994None · noneFLT#904, SJU-JFK. (AIRCRAFT DECLARED AN EMERGENCY) 'MANUAL GEAR EXTENSION SMOOTH LANDING; MLG GEAR HANDLE RETRACTION STOWED IAW AMM 32-33-00. REQUIRES OPERATIONAL CHECK OF FREE FALL MANUAL EXTENSION REF LP 3437186-2 (PERFORMED OPS CHECK OF FREE FALL MECHANICALSDR V0XR20221101AV2Cap · corrodedLEFT WING MLG AFT LOWER TRUNNION CAP CORRODED AND SCOREDSDR V0XR20221101AV1Cap · corrodedLEFT WING MLG FWD LOWER TRUNNION CAP CORRODED AND SCOREDSDR CALA2022090502271None · nonePDA 1 RIGHT MAIN GEAR FWD JURY STRUT SPRING SNAPPED OFF DURING LANDING. PART RETREIVED BY PORT AUTHORITY AND RETURNED BACK TO MX. NOTIFIED LINE CONTROL AND TOMC. INSTALLED NEW RIGHT MAIN GEAR FWD JURY STRUT SPRING PER AMM 32-32-05-404-009; ADD EMP:U393384SDR CALA2022071501743Packing · damagedLH MAIN LANDIG GEAR STRUT CYILINDER HYDRAULIC LEAKING. CONFIRMED. LH M.L.G SHOCK STRUT COLLAPSED ACCOMPLISHED ACTIVE SEAL REPLACEMENT WITH SPARE SEALS I.A.W AMM 32-11-25-962-342. NO LEAK NOTED.SDR YENA2022070500643None · noneFLT#1692, LIR-JFK. (AIRCRAFT DECLARED AN EMERGENCY ) 'HYD GREEN RSVR LOW-LEVEL ECAM IN FLIGHT PERFORMED ECAM AND QRH PROCEDURES HEARD VIBS NOISE; REF LOG PAGE 3370186 ITEM 2 (INSTALLED ENGINE #1 HYDRAULIC PUMP IAW AMM 29-11-51 UP TO SUBTASK 29-11-51-865-052-A)SDR GTIA2022062736501None · fault messageL/G GEAR NO DOWN LOCKED BOTH LGCIU'S INDICATED NOSE GEAR NOT DOWN AND LOCKED-R/R NLG LOCKSTAY ASSY IAW AMM 32-21-17. LEAK AND OPS TEST C/W. NO FAULTS DETECTEDSDR 2022FA0000339Attach Bolt · brokenDURING THE 100 HR / ANNUAL INSPECTION OF THE SUBJECT AIRCRAFT WE FOUND 4 BROKEN BOLTS IN THE LEFT HAND MAIN LANDING GEAR. UPON ARRIVAL OF THE AIRCRAFT FOR INSPECTION ONE BOLT WAS OBSERVED TO BE MISSING A NUT AND PORTION OF THE BOLT WHEREUPON IT WAS DECIDED TO SDR 2022FA0000334Attach Bolt · brokenDURING THE 100 HR / ANNUAL INSPECTION OF THE SUBJECT AIRCRAFT WE FOUND 4 BROKEN BOLTS IN THE LEFT HAND MAIN LANDING GEAR. UPON ARRIVAL OF THE AIRCRAFT FOR INSPECTION ONE BOLT WAS OBSERVED TO BE MISSING A NUT AND PORTION OF THE BOLT WHEREUPON IT WAS DECIDED TO SDR 2022FA0000265Attach Fitting · corrodedUPON LH MLG OLEO INSTALLATION, FOUND LH MLG TRAILING LINK/AXLE ASSY. P/N: 7441030-3, S/N: 27693055 LOCATED AT L/H MLG OLEO ATTACH FITTING PITTED AND CORRODED AROUND OUTBOARD SIDES OF LUGS. TEXTRON AVIATION STRUCTURES ENGINEERING ORDER: DQ34849M1 DATE:5/19/2022SDR CALA2022050401138None · collapsedLH MLG SHOCK STRUT COLLAPSED AT THE GATE. ACCOMPLISHED LEFT MAIN GEAR SHOCK STRUT SERVICING PER AMM TASK 12-15-01-613-021 TO CONFIRM SHOCK STRUT LEAKING. CONFIRMED LEAKING NEEDS PACK SET REPLACMENT. DELAY BECAUSE LEFT MLG OIL LEAK. ACCOMPLISHED LH M.L.G ACTIVESDR 2022FA0000233Landing Gear · debondedRIGHT MLG BRACE RIB WAS FOUND TO BE DEBONED FROM THE UPPER SHELL OF THE CENTER WING SECTION, THUS CAUSING THE GEAR ASSEMBLY TO SHIFT FROM ITS FIXED POSITION AND FORCE THE OVER CENTER LINK TO PREMATURELY RETRACT.SDR CALA2022030100540Hub Cap · missingPDA 1 #1 MLG TIRE HUBCAP MISSING. HUBCAB PLACED ON CDL 32W & O/B ANTI SKID PLACED ON MEL 3202C. INSPECTED RIM ASSY, OK INSTALLED NEW HUB CAP ASSY REF AMM 32-42-11-420-003
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