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 R61A201401150116Bolt · corrodedDURING HEAVY CHECK, RT MLG SIDE STAY ATTACH BOLT CORRODED AT BOLT HOLE. MAINTENANCE R & R BOLT IAW AMM 32-11-05.SDR R61A201401150114Bolt · corrodedDURING HEAVY CHECK, LT MLG SIDE STAY ATTACH BOLT CORRODED. MAINTENANCE R & R ATTACH BOLT IAW AMM 32-11-05.SDR CA140108002Damper · collapsed(CAN) WHILE ATTEMPTING THE FIRST START OF THE DAY THE ACFT SUDDENLY SHIFTED TAIL LOW AND TO THE RIGHT. IT WAS DETERMINED THAT THE RT REAR LANDING GEAR DAMPER HAD COLLAPSED TO THE FULLY RETRACTED POSITION AND OIL WAS LEAKING FROM THE PISTON CAP AREA. THE DAMPSDR CA131219016Pin · cracked(CAN) PIN IS CRACKED. REPORTED TO MFG AND WAITING FOR MFG INSTRUCTIONS.SDR R61A201312141333Pin · damagedDURING HEAVY CHECK, LEFT MLG FWD PINTLE PIN HAS A LARGE PIECE OF MISSING PLATING AND RUST. MX R & R LT MLG FWD PINTLE PIN IAW AMM 32-11-01.SDR R61A201311221260Bolt · corrodedDURING HEAVY CHECK, LT MLG LOWER SIDE STAY TO SHOCK STRUT HARDWARE CORRODED. MX R & R HARDWARE IAW AMM 32-11-05.SDR C77A20131111004Attach Fitting · gougedNICK IN LT MLG SIDE BRACE HOUSING ON FUSELAGE. BLENDED DAMAGE SMOOTH IAW SRM II 51-10-03.SDR V0DR20130912001Pin · crackedMLG CAME IN FOR OVERHAUL. DURING DISASSEMBLY UPPER TORQUE KNEE PIN WAS VISUALLY INSPECTED. FOUND WHAT APPEARED TO BE A CRACK. ON FUTHER INSPECTION, CRACK CONFIRMED. CRACK RUNS FROM A GREASE GROOVE ON THE PIN, ALONG THE LENGTH OF THE PIN FOR APPROXIMATELYSDR REXA2013082501120Lug · corrodedLEFT MLG SIDE STAY INBD LUG HAS MINOR SURFACE CORROSION IN THE AREA BETWEEN THE FORWARD AND AFT BUSHINGS MEASURING 0.0005" DEEP. REPAIRED IAW SRM 51-21-06.SDR CA130904010Angle · cracked(CAN) LEFT MLG TRUSS ANGLE NOTED TO HAVE CRACK APPROXIMATELY 0.7" LONG IN RADIUS. CRACK DISCOVERED BY VISUAL INSPECTION AND CONFIRMED USING FLPI. THIS ANGLE PROVIDES SECONDARY ATTACHMENT OF THE MLG TRUSS FORGING TO THE LOWER WING SKIN. CRACK WAS REPAIRED USISDR SWIA201334161Trunnion · crackedLT MLG TRUNNION AFT GREASE HOLES ARE CRACKED. C-CHECK R&R LT MLG TRUNNION IAW REO.SDR UALA2013060503894Cover · missingLEFT MLG MISSING PLASTIC COVER WHERE L-G MEETS AC. REPLACED RUBBER CUP. OK TO CONTINUE.SDR MTNA20130409021Pin · out of limitsDISCOVERED A BASE METAL CHANGE THAT WAS OUT OF LIMITS ON LEFT MAIN LANDING GEAR AFT PINTLE PIN P/N D61000. THIS WAS DESCOVERED DURING AN ATTEMPT TO EXTEND THE TBO FOR THE LANDING GEAR COMPONENTS. THE LEFT LANDING GEAR ASSEMBLY IS GOING TO BE SENT TO AN OVERHSDR MTNA20130409020Universal · out of limitsDISCOVERED A BASE METAL CHANGE THAT WAS OUT OF LIMITS ON RIGHT MAIN LANDING GEAR UNIVERSAL P/N D61036. THIS WAS DISCOVERED DURING AN ATTEMPT TO EXTEND THE TBO FOR THE LANDING GEAR COMPONENTS. THE RIGHT LANDING GEAR ASSEMBLY IS GOING TO BE SENT TO AN OVERHAULSDR MTNA20130409019Pin · out of limitsDISCOVERED A BASE METAL CHANGE THAT WAS OUT OF LIMITS ON RIGHT MAIN LANDING GEAR AFT PINTLE PIN PN D61000. THIS WAS DISCOVERED DURING AN ATTEMPT TO EXTEND THE TBO FOR THE LANDING GEAR COMPONENTS. THE RIGHT LANDING GEAR ASSEMBLY IS GOING TO BE SENT TO AN OVERSDR COEA2013040401801Mount Bolt · crackedFSR FOUND A CRACK IN THE RIGHT MLG FWD TRUNNION MOUNTING PIN, P/N D60999. THIS WAS A SCHEDULED INSPECTION FOR THE PURPOSE OF EXTENDING THE TBO FOR THE LANDING GEAR COMPONENTS. THE PART IS TO BE REPLACED WITH SERVICEABLE PART PRIOR TO AIRCRAFT OPERATION.SDR 2013FA0000078Bushing · galledAFTER VISUAL INSPECTION, RT MLG FOUND HAS A GALLED BUSHING ON RETRACTION TRUNNION SLEEVE. FOUND THE AREA OF THE PITTING ON THE SLEEVE. AREA IS WIDTH APPROX 2 CM AROUND THE SLEEVE. PERFORMED IAW RECOMMEND TO REMOVE THE BRONZE TRANSFER WITH SCOTCHBRITE , THE SDR CA130205003Fitting · cracked(CAN) DURING REASSEMBLY AFTER REPAIR, THE LT MAIN GEAR SADDLE WAS FOUND TO HAVE CORROSION ON LOWER FORWARD EDGE. UPON A CLOSER INSPECTION OF THE AREA, A STRESS CRACK WAS DISCOVERED UNDER THE CORROSION. THE GEAR SADDLE WAS R & R WITH NEW TO RECTIFY THE DEFECTSDR A6WA20134676Bracket · crackedSUPPORT BRACKET ON RIGHT MLG AFT TRUNNION I/B SIDE IS CRACKED. REPLACED WITH NEW SERVICEABLE SUPPORT BRACKET P/N 601R10205-30 IAW CRJ SRM 51-42-21.SDR COEA2013030802913Trunnion · corrodedHEAVY CHECK COE/MAJOR REPAIR: LEVEL 2 CORROSION. RIGHT MLG TRUNNION UPPER FLANGE UNDERSIDE HAS A SMALL SPOT OF CORROSION. BLEND OUT CORROSION PER SRAS.SDR COEA2013030801913Trunnion · corrodedHEAVY CHECK COE/MAJOR REPAIR: RIGHT MLG TRUNNION UPPER FLANGE HAS A SMALL SPOT OF LEVEL 2 CORROSION AT CENTER ON TOP AT FRAME 16. BLEND OUT CORROSION PER SRAS.SDR IPXA13M76723Support · damagedAFTER GEAR RETRACTION, PRIMARY & SECONDARY IND GEAR INDICATES LT MAIN GEAR WAS UNSAFE. AIR TURNBACK DUE TO GEAR UNSAFE CONDITION AFTER TAKEOFF. R & R LT MLG SENSOR SUPPORT IAW AMM 32-34-03.SDR 2013FA0000008Leg Assy · corrodedDURING THE ANNUAL INSPECTION, LT AND RT TUBULAR STEEL LANDING GEAR LEGS HAD CORROSION. REPLACED THE LANDING GEAR LEGS.SDR CA121121007Bushing · mismanufactured(CAN) THE VENDOR THAT SUPPLIES BUSHING, HAS NOTIFIED MFG THAT 2 BATCHES OF THE BUSHING WERE NOT HEAT TREATED TO THE FINAL HARDNESS SPECIFICATION AS REQUIRED IAW THE MFG DWG.SDR SWIA201232262Trunnion · crackedCRACK DISCOVERED ON LEFT MLG TRUNNION COMMON TO STEEL STRAP IDENTIFIED AS HOLE NR 1 ON AIRCRAFT, THIRD HOLE AFT FROM MOST FWD LOCATION. (C-CHECK) COMPLETED REPAIR ON LEFT TRUNNION NR 1 HOLE AS IDENTIFIED IAW REO.SDR R61A201210060588Pin · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE LEFT MLG FORWARD PINTLE PIN CORRODED. MAINTENANCE REMOVED AND REPLACED THE LEFT MLG FORWARD PINTLE PIN IAW EMB 190 AMM 32-11-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR MTNA201210050001Trunnion Pin · crackedDURING THE OVERHAUL OF MAIN LANDING GEAR S/N MN16 A TRUNNION PIN S/N MN46 WAS FOUND TO BE CRACKED.SDR R61A201209190519Pin · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT MLG FORWARD TRUNNION PIN BOLT HOLE CORRODED. MAINTENANCE REMOVED AND REPLACED RIGHT MLG TRUNNION PIN IAW EMB 175 AMM 31-11-01. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR SWIA201231804Trunnion · crackedONE CRACKED HOLE ON RIGHT TRUNNION. (C-CHECK) REPAIRED PER REO.SDR SWIA201231803Trunnion · crackedTHREE CRACKED HOLES ON LEFT TRUNNION. (C-CHECK) REPAIRED PER REO.SDR CA120901002Eyebolt · cracked(CAN) DURING THE 5 YEAR LANDING GEAR INSPECTION, A CRACK WAS DISCOVERED IN THE EYEBOLT BY THE NDT TECH. THE NDT OF MANY ITEMS ON THE LANDING GEAR ARE NOT REQUIRED BY THE MFG BUT WE DO IT PROACTIVELY AND HAVE HAD SOME FINDINGS. THE TYPE CERTIFICATE HOLDER WANTSDR MASA2012082035054Bushing · damagedCOMPLIED WITH PERM REPAIR TO RIGHT FWD MLG TRUNNION BUSHING TO 1 RST OVERSIZE. COMPLIED WITH IAW REO 601R-57-21-003 REV B. REF RO# CRJ-57-4003.SDR MASA2012082035053Bushing · damagedCOMPLIED WITH PERM REPAIR TO RIGHT AFT MLG TRUNNION BUSHING TO 1 RST OVERSIZE. COMPLIED WITH IAW REO 601R-57-21-003 REV B. REF RO# CRJ-57-4002.SDR MASA2012082035052Bushing · damagedCOMPLIED WITH PERM REPAIR TO LEFT FORWARD MLG TRUNNION BUSHING TO 1 RST OVERSIZE. COMPLIED WITH IAW REO 601R-57-21-003 REV B. REF RO# CRJ-57-4001.SDR MASA2012082035051Bushing · damagedCOMPLIED WITH PERM REPAIR TO LEFT AFT MLG TRUNNION BUSHING TO 1 RST OVERSIZE. COMPLIED WITH IAW REO 601R-57-21-003 REV B. REF RO# CRJ-57-4000.SDR A6WA201240825Bushing · gougedRIGHT MLG SIDE STAY BUSHING GOUGED. REPAIRED IAW REO 601R-32-11-1240.SDR CNQR2012080886796Pin · backed outRIGHT MLG COLLAPSED WHILE ACFT WAS TAXING IN FROM LANDING. AFT TRUNNION PIN WAS INSTALLED INCORRECTLY, THE AN3-42 RETAINING BOLT WAS NOT THROUGH THE PIN AS NEEDED TO RETAIN THE TRUNNION PIN IN THE TRUNNION ASSY. A REVIEW OF ACFT ONSITE AT THE REPAIR STATION SDR R61A201207060372Pin · corrodedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND CORROSION AROUND THE BOLT HOLES FOR THE LEFT MAIN GEAR FORWARD PINTLE PIN. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN LANDING GEAR FORWARD PINTLE PIN IAW EMB 190 AMM 32-11-01. THE AIRCRAFT IS OUT OF SERSDR ASOA2012071101885Bracket · unserviceableGEAR DISAGREE WARNING MESSAGE CLIMBING THROUGH 14,000 FT. COMPLETED QRH PROCEDURE. EMERGENCY DECLARED, ACFT RETURNED TO DEPARTURE, LANDED NORMALLY. R & R NLG WOW AND CENTERING SENSOR HARNESS BRACKET IAW AMM 32-61-25. ADJUSTED IAW AMM 32-61-05. PERFORMED GSDR UVVR2012062500021Attach Fitting · brokenRT MLG SIDE STAY WING ATTACH FITTING FOUND BROKEN DURING VISUAL INSPECTION AFTER PILOT COMPLAINED ABOUT A VIBRATION DURING LANDING.SDR SWAA2012071705918Pin · corrodedLEFT MLG FWD TRUNNION PIN CORRODED. REMOVED AND REPLACED PIN IAW DWG.SDR USAA2012061100003Beam · wornRON CHECK - WEAR ON LEFT MAIN LANDING GEAR WALKING BEAM, BETWEEN RS STA 135 TO RS STA 259, WBL 120. REPLACED LEFT MAIN LANDING GEAR WALKING BEAM, BETWEEN RS STA 135 TO RS STA 259, WBL 120 IAW B737 AMM 32-32-11.SDR CA120625002Leg Assy · cracked(CAN) DURING INSPECTION IAW SB 1131, RT MLG LEG WAS FOUND CRACKED AT THE UPPER INBD TORQUE LINK ATTACH LUG. THIS LG STRUT CYLINDER WAS CAST TYPE.SDR CA120508001Trunnion · misinstalled(CAN) DURING AN ANNUAL INSPECTION , IT WAS FOUND OUT THAT ON THE RT MLG UPPER MEMBER, THE AFT TRUNNION WAS INSTALLED REVERSED. THE SOILD END WAS INSTALLED ON THE OUTSIDE BUT IT SHOULD HAVE BEEN INSTALLED ON THE INSIDE TO MATE WITH THE UPPER MEMBER FUSELAGE FISDR CA120507016Brace · cracked(CAN) OPERATOR WAS INCORPORATING AN SB AND ON REMOVAL, THE MLG SIDE BRACE SHAFT FITTINGS WERE FOUND HEAVILY CORRODED AND CRACKED.SDR DALA1227119261Support Fitting · corrodedRT MLG RETRACT SUPPORT FITTING BUSHING BORE HAS CORROSION, PITTING ON SURFACE. MACHINED RT RETRACT BUSHING BORE TO 2.381 AND REMOVED .068 FROM BUSHING BORE INNER FACE. EXCEEDED LIMITS OF EA 02-093855-03 REV A. FABRICATED OVERSIZED BUSHING PER ERA 487463-14ASDR DALA1210993771Trunnion · corrodedACCOMPLISHED EA 12-487906-12 REV A, ME03 OPN0301 ON LMLG TRUNNION FITTING.SDR DALA1210983771Trunnion · corrodedEA 12-487906-12 REV A, ACCOMPLISHED ON R/S MLG PER ME06 OPN 0601.SDR ERAA201200017Pin · corrodedRIGHT MLG DRAG STRUT TO SHOCKSTRUT ATTACH PIN REPLACED DUE TO PITTING.SDR 2012FA0000099Bearing · crackedGEAR WAS REMOVED FOR OTHER MX AND RT FORWARD MAIN LANDING TRUNNION PIN WING FITTING BEARING ASSY WAS REMOVED DUE TO PHENOLIC LINING DAMAGE. TECH WAS INSPECTING BEARING AND FOUND BEARING CRACKED.
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