JASC 3210
Service difficulty reports · 1,882
Reports filed under 3210 · Main Landing Gear, 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 = '3210' 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 = '3210' 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 C2XA00IA365Spring · corrodedIAH-DURING C-CHECK INSPECTION, THE LEFT HAND MAIN LANDING GEAR UPLOCK SPRING WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPRING IN ACCORDANCE WITH EMB145 M/M 32-33-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA00IA366Spring · corrodedIAH-DURING C-CHECK INSPECTION, THE RIGHT HAND MAIN LANDING GEAR UNLOCK SPRING WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SPRING IN ACCORDANCE WITH EMB145 M/M 32-33-10, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR AC2A0000096Rod End · crackedWHILE PERFORMING THE REQUIREMENTS OF ASB 76-32-26, CORROSION INSPECTION OF THE THREADED JOINT, FOUND BEARING CRACKED. REPLACED POSITIONING ROD END. (X)SDR QXEA0002747Support Bracket · chafedPDX- LEFT HAND MAIN LANDING GEAR SIDE TRAY UPPER MEMBER CHAFING ON SUPPORT ANGLE IN OVERHEAD STRUT BAY. REPAIRED IAW FOKKER SRM 51-00-00 PAGE 2 AND HORIZON AIR EA 4-32-201.SDR QXEA0002772Bracket · corrodedPDX- PITTING CORROSION ON RIGHT HAND MAIN LANDING GEAR SIDE STAY BRACKET. REPAIRED IAW FOKKER SRM 51-10-04 PAGE 9 AND 57-01-01 PAGE 3.SDR 20000914SH002Housing · brokenAFT SUPPORTING PORTION OF THE RIGHT GEAR HOUSING BROKE AND ALLOWED THE TIRE POSITION TO SHIFT WHICH CAUSED IT TO HANG UP IN THE WHEELWELL. AIRCRAFT LANDED GEAR UP BECAUSE GEAR COULD NOT BE EXTENDED USING ELECTRIC MOTOR OR MANUAL LEVER. HAD TO PRY GEAR OUT OFSDR QXEA0002368Drag Strut · chafedYXX- LEFT HAND MAIN LANDING GEAR DRAG STRUT FOUND WITH CHAFE MARKS. REPAIRED IAW DHC-8 RD 8-32-474, HORIZON AIR EA 9-32-102 AND CONAIR EO 2869.SDR 20000914SH007Gear · brokenUPON LANDING, RT GEAR LEG, PN 7-1461-R, FAILED AT AREA OF U-BOLT ATTACH CLAMP. FAILURE RESULTED IN DAMAGE TO RT WING, PROPELLER, ENGINE AND COWLING. AIRCRAFT IS USED FOR GLIDER TOWING FROM AN UNPAVED RUNWAY AND AVERAGES 3-5 TAKEOFFS AND LANDINGS PER HOUR. TSDR EISA20000119Bushing · wornDURING ROUTINE C-CHECK INSPECTION, HOLES IN BRAKE MOUNTING FLANGES ARE TOO LARGE TO ACCEPT BRAKE ASSY. FABRICATED BUSHINGS, CAD PLATED AND INSTALLED BUSHINGS, ON I/B AND O/B IAW BOEING SERVICE BULLETIN 727-32-241.SDR 20010305CW002Landing Gear · collapsedGOT RT GEAR UNSAFE LIGHT, UNABLE TO GET LIGHT TO GO OUT. ON LANDING, ROLL OUT RT MAIN GEAR COLLAPSED, DAMAGING THE RT FLOAT. INSPECTION FOUND RT MAIN GEAR ACTUATING CONTROL SHAFT BROKEN. INSTALLED KIT, REPAIRED RT FLOAT KEEL AND SKINS THAT WERE DAMAGED.SDR C2XA00IA234Cap · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT MAIN LANDING GEAR AFT LOWER BEARING CAP WAS FOUND TO BE CORRODED AND PITTED. MAINTENANCE REMOVED AND REPLACED THE LOWER BEARING CAP IAW EMB-145 AMM 32-30-00-700-801-A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA00IA233Cap · corrodedIAH - DURING C-CHECK INSPECTION, THE LEFT MAIN LANDING GEAR FORWARD LOWER BEARING CAP WAS FOUND TO BE CORRODED AND PITTED. MAINTENANCE REMOVED AND REPLACED THE LOWER BEARING CAP IAW EMB-145 AMM 32-30-00-700-801-A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVSDR C2XA00IA232Cap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR FORWARD LOWER BEARING CAP WAS FOUND TO BE CORRODED AND PITTED. MAINTENANCE REMOVED AND REPLACED THE LOWER BEARING CAP IAW EMB-145 AMM 32-30-00-700-801-A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERSDR C2XA00IA231Cap · corrodedIAH - DURING C-CHECK INSPECTION, THE RIGHT MLG GEAR AFT LOWER BEARING CAP WAS FOUND TO BE CORRODED AND PITTED. MAINTENANCE REMOVED AND REPLACED THE LOWER BEARING CAP IAW EMB-145 AMM 32-30-00-700-801-A. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR 20000816SH026Wheel · crackedWHEEL HALF FOUND CRACKED DURING A ROUTINE INSPECTION. (X)SDR 2000UALA00446Landing Gear · malfunctionedUNABLE TO RETRACT LANDING GEAR. *S/D* ACCOMPLISHED GEAR SWINGS AND CHECKED AIR GROUND SENSOR GAPS. FOUND ALL TO CHECK OUT NORMAL.SDR C2XA00IA215Bearing · corrodedDURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT MLG LEG FORWARD LOWER BEARING CAP WAS FOUND TO BE CORRODED AND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARING CAP IAW EMB145MM 32-10-01-400-9-801A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVISDR C2XA00IA214Bearing · corrodedDURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT MAIN LANDING GEAR LEG AFT LOWER BEARING CAP WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BEARING CAP IAW EMB145MM 32-10-01-400-801A, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. SDR CA000809010Fork · cracked(CAN) DURING A LIQUID PENETRANT INSPECTION TWO CRACKS WERE LOCATED AT THE BASE OF THE RADIUS FORKED END WHICH ACCEPTS THE KNUCKLE JOINT OF THE UPPER TQ KNEE. CRACKS ARE 1/4 INCH LONG AND SEEM TO ORIGINATE FROM MACHINING WHEN PART WAS MANUFACTURED.SDR 20000829SH009Gear · failedDURING TAXI, LANDING GEAR SPRING FAILED AT MATING AREA OF P/N 0541121-2 SUPPORT. CAUSED SUBSTANTIAL DAMAGE TO RIGHT CABIN AFT OF CREW DOOR, RIGHT SIDE OF HORIZONTAL STABILIZER AND ELEVATOR, AND OUTBOARD SECTION OF RIGHT WING. (X)SDR S2YA00019Circuit Breaker · inoperativeMKE-IND - FLT 1052 - SHORTLY AFTER TAKEOFF, THE CREW WAS GOING TO SELECT GEAR UP BUT NOTED THE J HOOK WAS ENGAGED. THE CREW MOVED THE J HOOK AND ATTEMPTED TO RETRACT THE GEAR BUT IT STILL INDICATING DOWN AND LOCKED. THE CREW MADE AN AIR-TURN-ACK AND AN UNEVESDR AALA20001073Pin · installedDFW - FLT 0945 - AFTER TAKEOFF WHEN GEAR HANDLE RAISED, CENTER GEAR LIGHT REMAINED RED. GEAR WAS LOWERED WITH NORMAL PROCEDURES AND INDICATED SAFE. RETURNED AND LANDED WITHOUT INCIDENT. REMOVED CENTER LANDING GEAR PIN THAT WAS STILL INSTALLED. SYSTEM GROUNSDR MWEA00533Panel · crackedMKE - RIGHT MAIN LANDING GEAR BRAKE SHELF LOWER PANEL IS DELAMINATED AND CRACKED. MAINTENANCE INSTALLED NEW BRAKE SHELF PANEL. (X)SDR 20000717SH022Cylinder · crackedRADIUS ROD, PN 1862/F, SN LK-8507326, WAS SENT IN FOR SCHEDULED OVERHAUL WITH CSO OF 32,300 HOURS REPORTED. DURING INSPECTION OF CYLINDER, PN 184811, SN 555, IAW APPH SB 1862-32-07, A FLUORESCENT PENETRANT CRACK INDICATION WAS FOUND AT THE EDGE OF THE ONE-WAYSDR 20000516SH013Relay · inoperativePILOT SELECTED GEAR DOWN, NO RESPONSE. PERFORMED MANUAL GEAR EXTENSION AND LANDED AIRCRAFT. TROUBLESHOT GEAR DOWN CIRCUIT, FOUND ATTACHING SCREENS FOR GEAR DOWN RELAY IN LANDING. GEAR CONTROL BOX HAD COME LOOSE. RE-SECURED RELAY AND PERFORMED GEAR RETRACTSDR UPS00432853Support Bracket · damagedINSPECTION TYPE:C, HOLES ELONGATED IN AFT INNER BLG DOOR STRUCTURE AT AFT HINGES LT AND RT. NEW SECTIONS OF DOOR SUPPORT STRUCTURE FABRICATED AND FITTED. NEW FITTINGS DRILLED AND INSTALLED. REF Q/NOTE 13/00.SDR MZZA00011Landing Gear · collapsedYAP - DURING LANDING IN THE ISLAND OF YAP, THE LEFT MLG COLLAPSED AND RESULTED IN THE LEFT WING STRIKING THE RUNWAY. L-1 SLIDE WAS DEPLOYED. THE L-1 SLIDE ASSEMBLY P/N 1461100-4DG WAS REMOVED AND REPLACED PER B727 MM 25-60-15. (M)SDR UPS00832406Duct · failedINSPECTION TYPE:N/A, AFTER LANDING GEAR HANDLE SELECTED UP, A LARGE BANG WAS HEARD WITH A FOUL SMELL THROUGHOUT THE COCKPIT, NO OTHER ABNORMAL INDICATIONS. EMERGENCY DECLARED WITH CENTER CONTROLLER. INSPECTED AIRCRAFT FOR DAMAGE CHECKED INLETS FOR FOD AND SDR DLL19000750Control Valve · inoperativeAFTER TAKEOFF WHEN GEAR HANDLE PUT IN THE UP POSITION, THE RED DOOR LIGHT AND THE RED INTRANSIT LIGHT ON FWD PNL REMAINED ILLUMINATED. ON THE S/O PNL THE LT GEAR DOOR AMBER LIGHT WAS ON. DID POM PROCEDURE, RE-CYC GEAR, NO HELP. REPLACED LT MAIN GEAR PHASSDR 20000407SH025Stud · wornON ANNUAL INSPECTION (AD 97-01-01R1), FOUND BOTH MAIN LANDING GEARS SIDEBRACE STUDS WORN, RT 0.624 INCH AND THE LT, 0.524 INCH AND SIDEBRACE BUSHING WORN. REPLACED BOTH SIDE BRACE STUDS WITH .6250 INCH, P/N 78717-002, AND REAMED EXISTING BUSHING TO 0.624 INCHSDR 20000426SH007Retainer · damagedVISUAL INSPECTION SHOWED RING RETAINER AREA DAMAGED BEYOND LIMITS AND HEAVY CORROSION AT BOLT HOLE AREAS. (X)SDR LS1R066571Strap · tornSTRAP IS TORN. (RUBBER COMING APART).SDR LS1R066570Strap · tornSTRAP IS TORN. (RUBBER COMING APART).SDR C2XA00IA058Landing Gear · malfunctionedGSP - FLT 4370 - THE CREW REPORTED THAT THE MAIN LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO GSP WHERE IT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRY FLOW TO TYS WHERE MAINTEANCE JACKED, INSPECTED AND OPERATIONALLY TESTED THE GEAR WITH NO DESDR JBXA0000152Selector Valve · malfunctionedUPON SELECTING GEAR DOWN, RIGHT MAIN DID NOT GET A DOWN AND LOCKED INDICATION (RECIEVED LEVEL THREE ALERT). CYCLED GEAR AND BOTH MAIN GEAR DID NOT DOWN AND LOCK. EXECUTED MISSED APPROACH. CYCLED GEAR AGAIN AND GOT THREE GREEN, LANDED NORMALLY. REMOVED AND SDR L1GA200000308Brace · corrodedRIGHT MLG SIDE BRACE CORRODED 3 X 5 INCHES AND BOLT HOLE ELONGATED.SDR 2000ZZZX311Fitting · damagedTHREE OVERSIZED HOLES IN THE RT MAIN LANDING GEAR FITTING. REPAIRED RIGHT MAIN LANDING GEAR FITTING OVERSIZED HOLES PER EIA ECRA 941-57-055-2.SDR 2000ZZZX304Fitting · corrodedCORROSION DAMAGE FOUND IN 5 BOLT HOLES COMMON TO THE LT AND RT MAIN LANDING GEAR FITTINGS. REPAIRED LT AND RT MAIN LANDING GEAR FITTINGS PER EIA ECRA 941-57-065-2 REV A.SDR CALA0000108Circuit Breaker · trippedBOTH MLG GREEN INDICATION LIGHTS DID NOT ILLUMINATE WHEN LG WAS EXTENDED ON APPROACH. THE AIR/GROUND RELAY AND LIGHTS CB WAS FOUND TRIPPED DURING GO-AROUND. THE CB WAS RESET AND BOTH MAIN GEAR RED AND GREEN LIGHTS ILLUMINATED. THE CHECKLIST FOR UNSAFE GEAR SDR DHL2000705001Landing Gear · malfunctionedRIGHT MAIN LOCKED IN THE UP POSITION. REQUIRED MANUAL GEAR EXTENSION. RESET MANUAL GEAR EXTENSION, LUBED RT MAIN LANDING GEAR AND DOORS JACKED AIRCRAFT AND CYCLED GEAR SIX TIMES. OPS CHECK NORMAL PER M/M 32-32-0.SDR C2XA00CL010Mlg · malfunctionedAZO - FLT 3010 - AFTER TAKEOFF FROM AZO, LANDING GEAR WOULD NOT RETRACT. RETURNED TO AZO AND LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED SEVERAL UP AND DOWN CYCLES WITHOUT FAILURE, SIMULATING AIRLOAD AND VIBRATION ON WIRING. SYSTEM OPS CHECKED GOOD IAWSDR C2XA00CL009Mlg · malfunctionedCLE - FLT 3027 - AFTER TAKEOFF FROM PIT, LANDING GEAR FAILED TO RETRACT INITIALLY. AFTER 30-60 SECONDS, GEAR CAME UP. CONTINUED ON TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED GEAR SEVERAL TIMES IAW BEECH 1900D MM CHAP 32-30-00. SYSTEM OPS CHECKEDSDR 20000426SH037Tube · crackedDURING OVERHAUL OF MLG, PN B00A702925A, SN BADL-475, SLIDE TUBE PN 101A703013, SN BA66, WAS FOUND TO HAVE A CRACK EXTENDING FROM THE TOP OF THE TUBE THROUGH THE HOLE FOR THE SOCKET SET SCREW, PN 741M1-4D, AND DOWN THE TUBE FOR AN ADDITIONAL 6.102 INCHES. THISSDR AGQA065542Damper · weakMLG DAMPER IS WEAK.SDR AGQA065541Damper · weakMLG DAMPER IS WEAK.SDR 2000ZZZX25Fitting · brokenFOUND BROKEN PART ON RAMP. INSPECTED AIRCRAFT ON RAMP AND NO PROBLEM FOUND. CALLED OUT STATION AND FOUND THE AIRCRAFT IN DALLAS HAD THE BROKEN FITTING ASSY. GROUNDED AIRCRAFT AND HAD IT REPAIRED BEFORE FLYING AIRCRAFT AGAIN.SDR QXEA0000119Bracket · crackedPDX - LEFT-HAND WING MAIN LANDING GEAR BACK UP UPPER BRACKET WAS CRACKED AT LOWER BOLT, WITHIN PANEL 81X. REPAIRED IAW FOKKER SRM 57-07-09.SDR CA000128044Block · mismanufactured(CAN) ONE OF OUR NEWLY MNUFACTURED COMPRESSION BLOCKS SAGGED WHEN INSTALLED DURING REGULAR MAINTENENACE. BLOCK REMOVED AND NEW ONES INSTALLED WITHOUT PROBLEM. BLOCKS SENT FOR TESTING & CHEMICAL ANALYSIS. HAVE ISOLATED BLOCKS TO WHAT BATCH AND POUR.SDR HEEA065353Hose · kinkedHOSE ASSY KINKED.SDR 2000ZZZX180Bolt · mismanufacturedDURING REPLACEMENT OF RT MLG ATTACH FITTING (TRUNNION) WHILE INSTALLING LOWER REAR AUXILIARY SPAR CAP TO TRUNNION, 'NEW CONDITION' BOLT, P/N NAS-638-39, CRACKED WHILE TURNING INTO POSITION. THIS BOLT WAS ONLY BEING RUN IN AT TIME OF FAILURE, NOT TORQUED. ACF
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