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 SWAA080497Fitting · corrodedDURING SCHEDULED MV2 CHECK, FOUND RT MLG TRUNNION FITTING LUGS CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.SDR SWAA080496Fitting · corrodedDURING SCHEDULED MV2 CHECK, FOUND LEFT MLG TRUNNION FITTING LUGS CORRODED. REMOVED AND REPLACED FITTING PER SWA EA.SDR SWAA080466Bolt · corrodedDURING SCHEDULED BRDG CHECK, FOUND LT MLG BOTTLE BOLT CORRODED. REMOVED AND REPLACED BOTTLE BOLT PER MM.SDR SWAA080465Bolt · corrodedDURING SCHEDULED BRDG CHECK, FOUND RT MLG BOTTLE BOLT CORRODED. REMOVED AND REPLACED BOTTLE BOLT PER MM.SDR SWAA080282Fitting · corrodedDURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.SDR SWAA080283Fitting · corrodedDURING SCHEDULED MV2 CHECK, FOUND LT MLG FWD TRUNNION FITTING LUGS CORRODED. REPAIRED FITTING PER SWA EA.SDR SWAA080051Bushing · corrodedDURING SCHEDULED C2 CHECK, FOUND RT MLG TRUNNION LINK HAT BUSHINGS CORRODED. REMOVED AND REPLACED TRUNNION LINK PER MT.SDR SWAA080052Bushing · corrodedDURING SCHEDULED C2 CHECK, FOUND RT MLG STRUT FWD TRUNNION LINK LUG HAT BUSHINGS CORRODED. REMOVED AND REPLACED MLG OUTER CYLINDER AND COLLAR PER MT.SDR SWAA080053Trunnion Pin · corrodedDURING SCHEDULED C2 CHECK, FOUND RIGHT MLG BEAM CLEVIS TRUNNION PIN CORRODED. REMOVED AND REPLACED CLEVIS PER MT.SDR 2007FA0001073Trunnion · crackedRT AFT MAIN TRUNNION CASTING, P/N 67042-013, FOUND TO BE CRACKED DURING INSPECTION. THIS IS A NEARLY IDENTICAL CRACK TO ONE FOUND AUGUST 2006 ON A SISTER SHIP.SDR TRAX200701842Landing Gear · inoperativeLEFT MAIN GEAR WILL NOT RETRACT, EMERGENCY DECLARED. EMERGENCY EQUIPMENT ON STANDBY.SDR HNAA0700270Yoke · bindingON APPROACH TO AIRFIELD, LANDING GEAR DOWN WAS SELECTED AND NR 1 GEAR DOOR AMBER LIGHT ALONG WITH RED GEAR UNSAFE LIGHT ILLUMINATED. UPON VERIFYING THE CONDITION INDICATED, THE CREW THEN DECLARED AN EMERGENCY AND PROCEEDED TO EXTEND THE LANDING GEAR USING THESDR 2007FA0000989Landing Gear · wornPART (A) OF AD 77-13-21 REQUIRES INSPECTION OF LANDING GEAR EVERY 1000 HRS IAW SL 782. AIRCRAFT EXPERIENCED A COLLAPSED RT MLG FOLLOWING A SCENARIO THAT IS IDENTIFIED IN SL 782. THIS SCENARIO INCLUDES A POPPED LANDING GEAR MOTOR CIRCUIT BREAKER RESULTING IN SDR CA071102012Bushing · separated(CAN) THE MAIN GEAR LEG BUSHINGS ARE A STEEL OUTER TUBE, WITH A THICK INNER URETHANE CENTER. DURING PROGRESSIVE CARE OPERATION NR 4, INSPECTION OF THE LT MAIN GEAR LEG REVEALED THAT THAT THE URETHANE INNER BUSHING MATERIAL HAD DEPARTED FROM THE OUTER STEEL BUSDR USAA920071252Link · corrodedMCN - MAJOR REPAIR - C20 CHECK - CORROSION ON LEFT MAIN LANDING GEAR SUPPORT BEAM SWING LINK. REPLACED LEFT MAIN LANDING GEAR SUPPORT BEAM SWING LINK IAW B737 AMM 57-15-00-4.SDR K11A2008123172311Beam · corrodedLT MLG BEAM LOWER SURFACE CORROSION HAS CORROSION IN AND AROUND FASTENER HOLES.SDR CA070919009Landing Gear · misoverhauled(CAN) (AD)2006-0087 WAS REVIEWED AS PART OF THE NEW AIRCRAFTS BRIDGING INSPECTION. DURING REVIEW OF THIS AD IT WAS FOUND THAT THE RT MAIN LANDING GEAR HAD BEEN REASSEMBLED AT OVERHAUL WITH THE WRONG PART NUMBER UPPER AND LOWER TOGGLES INSTALLED. THE INSTALLEDSDR CA071114009Brace · cracked(CAN) FLIGHT CREW CONDUCTED A CROSSWIND LANDING, SHUTDOWN, AND PASSENGERS DEPLANED ON REMOTE RAMP LOCATION. UPON TAXIING TO THE TERMINAL FOR THE NEXT FLIGHT, CREW NOTICED THE AIRCRAFT FELT DIFFERENT. MAINTENANCE WAS CALLED, AND A VISUAL INSPECTION FOUND THAT TSDR SWAA074268Drag Brace · corrodedDURING SCHEDULED SERVICE CHECK, FOUND LEFT MLG LOWER DRAG BRACE BUSHING AND TEE FITTING CORRODED. REMOVED AND REPLACED DRAG BRACE PER MM.SDR SROM200700009Support Fitting · damagedNR269 - WEAR DAMAGE RIGHT MAIN LANDING GEAR FUSE TO TRUNNION SUPPORT BEAM ATTACH FITTING. REPAIRED IN ACCORDANCE WITH BOEING APPROVED FAA FORM 8100-9 MESSAGE 1-515849678-6, DATED AUGUST 23, 2007.SDR 2007UALA02878Brake · fireON ARRIVAL HAD BRAKE FIRE ON NR 1 FWD MLG BRAKE ASSY.SDR MALA070092Pin · failedAFTER TAKEOFF FROM MSP, THERE WAS A LOUD CLUNK IN THE NOSE GEAR AREA AND THE INTRANSIT LIGHT REMAINED ILLUMINATED. CREW FOLLOWED THE QRH AND RETURNED TO MSP. REPLACING NOSE LANDING GEAR ACTUATOR RETRACT PIN, PN: AIR127298.SDR CA070703001Trunnion · cracked(CAN) DURING A SCHEDULED LAYOVER, ON POST FLIGHT WALK AROUND THE PILOTS NOTICED THAT THE LT GEAR STRUT WAS DEFLATED. EXAMINATION BY MAINT SHOWED THAT THE TRUNNION HAD CRACKED ALONG THE WELD THAT HOLDS THE (2) HALVES OF THE TRUNNION TOGETHER. IT HAD CRACKED UP SDR DLM88070457Fitting · corrodedLT MAIN LANDING GEAR SUPPORT FITTING, EXFOLIATION CORROSION ON INNER BORE OF BUSHING. CORROSION REMOVED, PERMANENT REPAIR PERFORMED FOLLOWING INSTRUCTIONS AND RECOMMENDATIONS CONTAINED IN THE BCAG SR09570087 AND BCAG SR-ID 1-301794190.SDR 2007FA0000308Pin · brokenUPON EXTENDING THE LANDING GEAR, THE PILOTS GOT A RED GEAR UNSAFE LIGHT IN THE HANDLE, AND THE LT DOWN AND LOCKED LIGHT WAS NOT LIT UP. THE PILOTS TRIED TO EXTEND THE GEAR MANUALLY, BUT THE HANDLE WOULD NOT EXTEND THE GEAR ANY FURTHER, THE PILOTS RETRACTED THESDR AWXA200700433Pin · corrodedSAL - CORROSION ON RIGHT MAIN LANDING GEAR REAR PINTLE PIN THREADS. REPLACED RIGHT MAIN LANDING GEAR REAR PINTLE PIN IAW AWA TASK CARD R4M32304.SDR AALA20070039Damper · inoperativeJFK INFLIGHT T1375/09JAN BDL TO SJU - LANDING GEAR WOULD NOT RETRACTION SYSTEM ONE AND TWO. CREW CONFIRMED GEAR WAS DOWN AND LOCKED. LANDED JFK WITHOUT INCIDENT. REPLACED LEFT MAIN LANDING GEAR PITCH DAMPER. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR 2007UALA00027Pin · corrodedLEFT MLG AFT MAIN BEAM O/B ATTACH PIN CORRODED. MAJOR REPAIR: REPLACED ATTACH PIN.SDR UPS07548821Trunnion · bentNLG OPERATING SEQUENCE SLIDE ROD & TRUNNION ASSY BENT. A/C FERRIED TO MAE FOR REPAIR. REPLACED ROD ASSY & R&R TRUNNION ASSY IAW MM 32-34-06.NR930536 REPLACED SUPPORT ASSY IAW MM 32-34-06. PERFORM NLG EXTEMSION/RETRACTION TEST IAW MM 32-34-00 TEST GOOD. REPLASDR KY7A11409Drag Brace · crackedDRAG BRACE P/N OAS55-1-5, CRACK LUG FOR UPLOCK.SDR SWAA064486Fitting · corrodedDURING SCHEDULED MV2 CHECK, FOUND LT MLG WALKING BEAM HANGER FITTING CORRODED. REMOVED AND REPLACED FITTING PER MM.SDR SWAA064485Fitting · corrodedDURING SCHEDULED MV2 CHECK, FOUND RIGHT MLG WALKING BEAM HANGER FITTING CORRODED. REPAIRED FITTING PER SWA EA.SDR CA061122006Trunnion · cracked(CAN) AT INSPECTION NOTICED CRACK RIGHT THROUGH TRUNNION ASSY 67042-013.SDR NACA20060058Fitting · corrodedFOUND RIGHT MAIN LANDING GEAR TEE BOLT FITTING HAS PITTING CORROSION AROUND BASE RADIUS. REMOVED AND REPLACED MAIN LANDING GEAR DRAG STRUT TEE BOLT ASSEMBLY IN RIGHT MLG IAW BOEING 737-200 MM CHAPTER 32-11-42. OP CHECKED GOOD ON FCD2006-28 ITEM 23.SDR SWAA064119Link · wornVIBRATION FELT DURING TAKEOFF AND LANDING. REMOVED AND REPLACED RT MLG UPPER AND LOWER TORSION LINKS PER MM.SDR QXEA200602914Attach Bracket · corrodedC3 YYC - LEFT MAIN LANDING GEAR SHOCK STRUT ASSY ACTUATOR ATTACH BRACKET OUTBOARD MOUNT HAS CORROSION. REPAIRED IAW REO670-32-11-213.SDR ERH2006F00000Casting · brokenSKIPLANE LANDED ON GLACIER. AFTER LANDING, AIRCRAFT TAXIED OVER A SNOW COVERED CREVASSE. PILOT HEARD A LOUD BANG. THE AIRCRAFT LANDED TO THE LEFT AS HE STOPPED. PILOT UNLOADED PASSENGER, AND INVESTIGATED THE LT GEAR BOX AREA. INVESTIGATION OF THIS AREA RESDR 06FDEA03098Trunnion · corrodedCENTER LANDING GEAR, RT TRUNNION AFT HOLE UPPER SURFACE FOUND CORRODED. COMPLIED WITH FEDEX E.A 1-5340-103487, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 2006FA0000765Trunnion · crackedDURING MAINTENANCE INSPECTION OF THE GEAR, THE MECHANIC FOUND THE AFT MAIN GEAR TRUNNION CRACKED. DYE PENETRANT CONFIRMED CRACK. CAUSE IS UNDETERMINED BUT THE AIRCRAFT IS USED FOR FLIGHT TRAINING.SDR 2006FA0000669Cone Bolt · failedLT LANDING GEAR STRUT IB ATTACHMENT BOLT HEAD POPPED OFF DURING TAXI CAUSING PARTIAL GEAR COLLAPSEDSDR 06FDEA2385Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND RT TRUNNION MATING SURFACE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL THICKNESS = 2.500", TOP SPOTFACE MATERIAL REMOVED = 0.007" (FWD), TOP SPOTFACE MATERIAL REMOVED = 0.0125" (AFT), LOWER MASDR 06FDEA2384Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND RIGHT HAND TRUNNION ALIGNMENT PIN HOLE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL HOLE DIAMETER = 1.502", FINAL HOLE DIAMETER = 1.6502", MAXIMUM ALLOWABLE LIMIT DIAMETER = 1.680" AND FOUND WITHINSDR 06FDEA2383Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND RIGHT HAND TRUNNION AFT MOUNTING HOLE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL HOLE DIAMETER = 1.280", FINAL HOLE DIAMETER = 1.3776", MAXIMUM ALLOWABLE DIAMETER = 1.385" AND FOUND WITHIN LIMISDR 06FDEA2382Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND RIGHT HAND TRUNNION FORWARD MOUNTING HOLE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL HOLE DIAMETER = 1.280", REWORKED HOLE DIAMETER = 1.3768", MAXIMUM ALLOWABLE DIAMETER = 1.385" AND FOUND WISDR 06FDEA2381Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND LEFT HAND TRUNNION MATING SURFACE CORRODED. REWORKED AS PER FEDEX E.A. 1-5340-99703, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA2380Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND LEFT HAND TRUNNION ALIGNMENT HOLE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL BORE DIAMETER = 1.502", FINAL BORE DIAMETER = 1.6766", MAXIMUM ALLOWABLE DIAMETER = 1.680" AND FOUND WITHIN LIMIT AS PSDR 06FDEA2379Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND LEFT HAND TRUNNION AFT MOUNT HOLE CORRODED. TRUNNION REWORKED AS PER FEDEX EA 1-5340-99703, REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA2378Trunnion · corrodedCENTER LANDING GEAR WHEEL WELL, FOUND LEFT HAND TRUNNION FORWARD HOLE CORRODED. REMOVED AS PER SRM 53-40-00 FIGURE 15 VOLUME I. ORIGINAL BORE DIAMETER = 1.281", FINAL BORE DIAMETER = 1.3685", MAXIMUM BORE DIAMETER = 1.385" AND FOUND WITHIN LIMIT AS PER SRM SDR 2006FA0000582Bolt · looseNOSE GEAR RETRACTED ON LANDING. FOUND BOLT PN 401-421 (AN6-41A) LOOSE WHERE NOSE GEAR MOUNT BOLTS TO BULKHEAD AT STA 49.5. THIS RELEAVED DOWNLOCK LINK OVER CENTER POSITION. BOLTS SHOULD BE CHECKED EACH 500 HRS. (K)SDR CA060511004Bolt · shearedPILOT REPORTED LOSS OF GREEN LIGHT AND TRANSIT LIGHT ON THE NOSE GEAR DURING TAXI INTO AIRPORT. PILOT SHUTDOWN AC AND EMPTIED AIRCRAFT. MAINTENANCE MOVED AIRCRAFT TO SAFE LOCATION AND WHILE JACKING THE AIRCRAFT NOTICED THAT NOSE WHEEL PIVOTED SIDEWAYS. UPON
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