JASC 3230
Service difficulty reports · 11,179
Reports filed under 3230 · Landing Gear Retraction/Extension System, 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 = '3230' 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 = '3230' 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 HYIA20140415034Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OSDR HYIA20140415033Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OSDR HYIA20140415032Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OSDR GTIA1100007Landing Gear · intermittentON APPROACH, DID NOT GET 3 GREEN FOR LANDING GEAR. FLIGHT EXECUTED GO-AROUND. RE-CYCLED GEAR AND ALL OK - 3 GREEN. FLIGHT LANDED SAFELY AT 1901 LOCAL.SDR REXA201100182Landing Gear · slowGEAR DISAGREE ON LANDING. NOSE LANDING GEAR DIDN'T EXTEND ON 1ST ATTEMPT. AFTER 3 MINUTES GEAR EXTENDED. CREW DECLARED AN EMERGENCY. CW PA 05-018A. NO DEFECTS NOTED.SDR 5APR577Y52Pressure Switch · intermittentUPON LANDING GEAR RETRACTION ON CLIMB AFTER TAKEOFF, LANDING GEAR DID NOT RETRACT. THE LANDING GEAR POSITION INDICATORS REMAINED RED, AND THE HYD CAWS ILLUMINATED. THE PILOT NOTIFIED TOWER THEY WERE RETURNING TO THE FIELD THEN FOLLOWED THE APPROPRIATE CHECKLSDR ASOA201100623Priority Valve · failedNOSE GEAR DISAGREE WARNING ON LANDING COMPLIED WITH QRH AND MANUALLY EXTENDED THE NOSE GEAR. NOSE GEAR DOWN AND LOCKED FROM MANUAL EXTENSION. (ENROUTE, ACFT DIVERTED DUE TO MX -- EMERGENCY DECLARED & VEHICLES STANDING BY. R & R NLG PRIORITY VALVE, OPS CHECK SDR FDEA201103090923Landing Gear · malfunctionedAFTER TAKEOFF AND GEAR RETRACTION, RT MAIN GEAR INDICATED UNSAFE ON BOTH GEAR SYNOPTIC AND INDICATOR LIGHTS. COMPLIED WITH CHECKLIST AND GOT NORMAL INDICATIONS. NO FAULTS IN PSEU. PSEU RTS PASSED. CHECKED SENSOR READOUT IN PSEU AND ALL READINGS FOR RT MAIN SDR CA110310007Control Panel · failed(CAN) PILOT: ATB - AFTER GEAR UP SELECTED, GREEN NOSE REMAINED ILLUMINATED. ALL OTHER INDICATIONS NORMAL. MAINTENANCE: CHECK PSEU FOR FAULTS. NO RELEVANT FAULTS NOTED. DUPLICATED DISCREPANCY BY CYCLING GEAR HANDLE. TAPPING ON GEAR CONTROL PANEL MAKES LIGHT GSDR HSYA20110307001Torque Link · damagedRT MLG TORQUE LINK DISCONNECTED AT START OF ACFT TAXING FROM BLOCKS. UPON INSP, MX DISCOVERED INCORRECT WASHER INSTALLATION AT UPPER AND LOWER TORQUE LINK ATTACH POINT.SDR 2011F00060Spring · out of positionFLIGHT CREW WAS APPROACHING AND ATTEMPTED TO LOWER MLG AT WHICH TIME THE MLG WOULD NOT LOWER. CREW THEN MANUALLY LOWERED MLG AND OBTAINED 3 "GREEN" LIGHTS. CREW MADE AN UNEVENTFUL LANDING. MX WAS THEN NOTIFIED AND FOUND NO OBVIOUS DEFECTS IN THE MLG, NO "POPPESDR VNAA2011030800003Unknown · malfunctionedCREW REPORTED GEAR DISAGREE (UP POSITION) DURING CLIMB AFTER DEPARTURE FROM AVL. GEAR WAS NOT IN TRANSIT AT THE TIME. CREW CONTINUED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECKS ON THE LANDING GEAR EXTENSION / RETRACTION SYSTEM USING THESDR R61A20110058Uplock Roller · lack of lubeCREW REPORTED RT MLG SHOWED UP EVEN THOUGH IT WAS DOWN, ALONG WITH LG LEVER DISAGREE MSG AND BRAKE CTRL FAULT, CREW DECLARED EMERGENCY AND PERFORMED GO-AROUND. LANDED WITHOUT INCIDENT IN PHL. MAINTENANCE PERFORMED OPS CHECKS AND FUNCTIONAL CHECKS OF UPLOCK ASDR CA110308002Selector Valve · malfunctioned(CAN) PILOTS REPORT, BEGAN TO CONFIGURE ACFT FOR LANDING. ELECTED TO SELECT PROP RPM TO 1200 TO ASSIST SPEED MANAGEMENT DUE SLIGHTLY SHORTER TRACKING THAN ANTICIPATED AND A LITTLE LIGHT TURBULENCE. LANDING GEAR CALLED AND SELECTED DOWN AT APPROXIMATELY 157 KSDR IPXA1M65142Landing Gear · inoperativeON TAKEOFF LT MAIN GEAR DID NOT RETRACT WITH GEAR HANDLE UP. BOTH PRIMARY AND SECONDARY INDICATE GEAR NOT UP AND LOCK. DURING FLT LT GEAR TIRE TEMP INDICATED -25 DEG RT TEMP INDICATED +65 DEG NR420058. SELF TEST OF PSEU & TANGER TEST OF LDG & GEAR DOOR SENSDR IPXA11M65142Landing Gear · malfunctionedON TAKEOFF SDF LT MAIN GEAR DID NOT RETRACT WITH GEAR HANDLE UP. BOTH PRIMARY AND SECONDARY INDICATE GEAR NOT UP AND LOCK. DURING FLT LT GEAR TIRE TEMP INDICATED -25 DEG RT TEMP INDICATED +65 DEG FERRY FLIGHT REQUIRED - DEFERRED ITEM IAW FERRY PERMIT NR 9061SDR CALA2011030400120Printed Ckt Board · defectiveDURING CRUISE AT FL360 205KTS VMC CONDITIONS THE LG SYS XFR VALVE PRI CONT & SEC CONT CB LOCATED ON P6-2 D14 D15 WAS FOUND TRIPPED. FLIGHT CONTINUED AND NO RESET OF CB ATTEMPTED. T/S AND FOUND M1190 CIRCUIT CARD BAD. REMOVED AND REPLACED M1190 CIRCUIT CARD SDR CA110304006Selector Valve · failed(CAN) ACFT PERFORMED AN ALTERNATE LANDING GEAR EXTENSION. TROUBLESHOOTING IN PROGRESS. MX PLUGGED AN EXTERNAL POWER CART TO THE ACFT IN COCKPIT 3 GREEN LIGHTS WERE ON. UNABLE TO CLOSE NOR OPEN GEAR DOOR. LG SELECTOR REPLACED GEAR SWINGS PERFORMED.SDR UALA2011030201036Control Module · faultyEXTREME EFFORT REQUIRED TO RAISE GEAR LEVER TO UP. MUST BE FIXED BEFORE REVENUE FLT. REPLACING LANDING GEAR CONTROL MODULE. NEED 8 BOLTS 926-0380 FOR NOSE JACK FIXTURE. LANDING GEAR CONTROL MODULE HAS BEEN REPLACED. GEAR NEEDS A GEAR SWING PER SFO STATIONSDR DXTA2011030304485Uplock Switch · malfunctionedAFTER TAKEOFF AND GEAR RETRACTION SELECTED, THE 3 GREEN LIGHT EXTINGUSHED, BUT THE RED LIGHT REMAINED ILLUMINATED. CLIMBED TO 6000FT ON THE AUTOPILOT. AFTER 3, 90 DEGREE TURNS ON THE AUTOPILOT WE FELT A HARD BUMP FROM THE UNDERSIDE OF THE AIRPLANE AND THEN THESDR CA110304002Selector Valve · failed(CAN) DURING LANDING, THE NOSE WHEEL STEERING WOULD NOT WORK. THE ACFT WAS TAXIED TO THE BAY USING ASYMMETRIC BRAKE AND POWER. LANDING GEAR SELECTOR VALVE REPLACED. LANDING GEAR SELECTOR VALVE FUNCTIONAL AND LEAK CHECKS CARRIED OUT, IAW AMM 32-31-06 & 29-SDR A6WA201140168Selector Valve · inoperativeON GEAR EXTENSION RECEIVED "GEAR DISAGREE" MSG FOLLOWED WITH DOWN INDICATION OF THE NLG. FOLLOWED QRH MSG CLEARED AND RECEIVED NORMAL DOWN INDICATION AFTER PULLING THE EMERGENCY EXTEND HANDLE. R & R NLG SELECTOR VALVE IAW AMM 32-33-10.SDR QXEA2011030400202Bypass Valve · out of rigAFTER T/O, GEAR DID NOT COME UP. GEAR HANDLE LIGHT REMAINED ILLUMINATED ALONG WITH RED GEAR UNSAFE LIGHTS FOR MAIN GEAR AND NOSE GEAR. PERFORMED MANUAL GEAR EXTENSION TO GET GREEN LIGHTS. RETURNED TO FIELD AND ACCOMPLISHED A UNEVENTFUL LANDING. CHECKED PSSDR VNAA2011030200016Priority Valve · malfunctionedCREW REPORTED THE NOSE WHEEL MADE A LOUD CLANGING NOISE ON GEAR EXTENSION ON APPROACH TO IND. GEAR EXTENSION TOOK LONGER THAN NORMAL. CREW LANDED IN IND WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE NOSE LANDING GEAR (NLG)SDR SIMA201106003Landing Gear · malfunctionedON FLIGHT 4469 THE CREW REPORTED THAT AFTER TAKE OFF DURING GEAR RETRACTION THE LANDING GEAR FAILED TO RETRACT FOLLOWED BY A LANDING GEAR LEVER DISAGREE MESSAGE. THE CAPTAIN ELECTED TO DIVERT TO IAD. CRASH, FIRE AND RESCUE WERE CALLED FOR THE LANDING. THE ASDR IPXA1164937Switch · inoperativeWHEELS WILL NOT COME UP AFTER T/O IAW PROC, RETURNED. DID NOT RECEIVE AN ECAM MESSAGE OR CHIME. NO WARNING. R & R LANDING GEAR NORMAL CONTROL SWITCH UNIT IAW 32-31-11-04. T/S IAW TSM 32-30-00, FIG 1091, FIG 107 AND TECH. PERFORMED MLG SAFETY CONTROL TESTSSDR AXSA194WA02/23/11Motor · burnedLEW - WHILE LANDING AT LEW ON A 2 MILE FINAL, PILOT SELECTED A NOTCH OF FLAPS AND STARTED TO SMELL ELECTRICAL SMOKE. THE CABIN FILLED WITH SMOKE. PILOT SHUT BATTERY AND GENERATORS OFF. AIRCRAFT HAD THREE GREEN LIGHTS WHEN GEAR WAS EXTENDED. AIRCRAFT LANDEDSDR AXSA191WA02/23/11Circuit Breaker · trippedMHT - ON APPROACH TOT MHT PILOT SELECTED GEAR DOWN. NO MOVEMENT NOTED. CHECKED GEAR CIRCUIT BREAKER AND NOTICED IS WAS OUT. PILOT PUSHED BREAKER IN AND IT WOULD NOT STAY IN. PILOT PUSHED BREAKER IN WITH GEAR HANDLE SELECTED DOWN AND GEAR CAME DOWN, WITH THSDR CA110223001Selector Valve · failedON 21 FEB. 2011, THE ACFT DEPARTED. AFTER GEAR UP SELECTION THE CREW GOT A "GEAR DISAGREE" MESSAGE AND NOTED THAT THE NOSE GEAR HAD NOT RETRACTED. THE ACFT RETURNED AND LANDED NORMALLY. THE FAULT COULD BE DUPLICATED IN THE HANGAR ON JACKS. T/S REVEALED THAT TSDR A6WA201140089Landing Gear · malfunctionedON TAKEOFF, AFTER RETRACTING GEAR, GOT GEAR UNSAFE/ NOSE DOOR OPEN WARNING. PERFORMED QRH. NOSE GEAR DID NOT SHOW UP AND LOCKED. EVERYTHING WORKED NORMALLY AFTER GEAR EXTENDED. OPENSDR ASOA201100332Selector Valve · failedGEAR DISAGREE AFTER PUTTING THE GEAR HANDLE IN THE DOWN POSITION ON APPROACH. BOTH MAINS WERE NOT DOWN AND LOCKED. NOSE GEAR INDICATED DOWN AND LOCKED. FOLLOWED QRH. PULLED MANUAL GEAR EXTENSION RECEIVED 3 GREEN. EMERGENCY DECLARED - TOWER HAD EQUIPMENT STASDR CA110225002Landing Gear · failedTHE GEAR WOULD NOT EXTEND. THE GEAR WAS EXTENDED MANUALLY. THE CREW REPORTED WHEN THEY SELECTED THE GEAR LEVER DOWN, NOTHING HAPPENED FOR ABOUT 4 SECONDS THEN THEY GOT A CYAN PROX SYS FAULT AND AMBER GEAR DISAGREE MESSAGE.SDR FDEA201102180607Mechanism · out of rigON FINAL APPROACH, AFTER PUTTING GEAR HANDLE DOWN AND WAITING TWICE THE NORMAL TIME FOR GREEN INDICATION, ALL 3 GEAR WERE STILL RED, HANDLE WAS CHECKED IN AND HYDRO QTY AND PRESSURE WERE BOTH GOOD. ELECTED TO CYCLE GEAR AFTER A LONG PAUSE AGAIN, THE GEAR FISDR REXA201100127Landing Gear · malfunctionedGEAR DISAGREE ON FINAL RT MAIN WAS RED DURING APPROACH 3 PREVIOUS FLTS IT TOOK LONGER FOR IT TO COME DOWN THAN OTHER GEAR RAN QRH CYCLED GEAR ALL CAME DOWN NORMAL. PERFORMED OK CHECK OF LANDING GEAR SYS BY PERFORMING GEAR SWING IAW AMM 32-30-00 AND C/W PA 05-SDR 2011F00037Landing Gear · failedAFTER T/O, GEAR WOULD NOT COME UP. HANDLE WOULD NOT RAISE PAST 1/2 TRAVEL.SDR CA110221004Roller · wornGEAR FAILED TO RETRACT AFTER GEAR HANDLE SELECTED UP. RED LT, NOSE, RT GEAR UNSAFE ILLUMINATED MX: INTERROGATED PSEU, FOUND NW CTR UNREASONABLY FAR ON PAST 2 FLIGHT LEGS. CHECKED INDUCTANCE VALUES IAW 32-61-00-280-801. ALL VALUES GOOD. FOUND WORN ROLLER BEARISDR HYIA20140415031Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OSDR HYIA20140415030Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OSDR HYIA20140415029Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OSDR HYIA20140415028Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OSDR UALA2011021100753Interface Unit · malfunctionedLANDING GEAR DID NOT RETRACT, RTFL. ONCE TSM HAS BEEN ACCOMPLISHED ALSO WILL ALSO REPLACE PROX SENSORS 24GA AND 25GA. ACP TSM FOUND 28VDC AT CON "A" PIN "W". FOUND 28VDC AT CON "B" PIN "J", REPLACED LANDING GEAR CTL LEVER. REPLACED BOTH LGCIU'S. REPLACED SDR C2XA11CL045Electronic Unit · faultyORD FLT 6156 - THE CREW REPORTED A LOUD BANGING NOISE WHEN GEAR RETRACTED. MAINTENANCE INSPECTED AND REPLACED THE LANDING GEAR ELECTRONIC UNIT. OPERATIONAL CHECKS WERE GOOD.SDR DXTA2011021004463Landing Gear · malfunctionedRED GEAR HANDLE LIGHT REMAINED ILLUMINATED IN THE GEAR UP POSITION. VISUALLY INSPECTED LANDING GEAR. PERFORMED GEAR SWING. FOUND MLG INBD DOORS NOT CLOSING DURING RETRACTION CLEANED LT AND RT NLG UPLOCK SWITCHES. OPS CHECKED NORMAL. PERFORMED OPS CHECK OSDR HYIA20140415027Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OSDR HYIA20140415026Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OSDR HYIA20140415025Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OSDR HYIA20140415024Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OSDR HYIA20140415023Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OSDR HYIA20140415022Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE OSDR HYIA20140415021Drag Brace · crackedAT SCHEDULED INSPECTION, NLG DRAG BRACE OEM PN 5142002-5 WAS FOUND TO BE CRACKED IN THE AREA OF NLG ACTUATOR ATTACH POINT. METHOD OF INSPECTION WAS DYE PENETRANT. THIS CRACK WAS FOUND TO BE WITHIN ALLOWABLE LIMIT. THIS UNIT HAS BEEN REPAIRED IAW PROCEDURE O
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