Airbus A310-304
Service difficulty reports · 238
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = 'A310304' 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 aircraft_model_key = 'A310304' 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 CA010105010Fire Bottle · discharged(CAN) A/C 212, DEC 17/2000, FLT 92577, YQM, LOG SEQUENCE 0292319. DURING CLIMB, MAIN DECK (FWD AND MID) SMOKE WARNING OCCURRED. SMELL AND SMOKE AND MIST WAS DETECTED IN COCKPIT. FIRE BOTTLES WERE DISCHARGED AND AIRCRAFT RETURNED TO YMQ. AFTER CREW DEBRIEF, MISSDR CA010205022Actuator · failed(CAN) 1. ON APPRAOCH NLG WOULD NOT EXTEND.2. SEVERAL ATTEMPTS TRIED, THEN MANUAL EXTENSION USED. POSITIVE GEAR DOWN & LOCKED.3. LANDING UNEVENTFUL.4. AIRCRAFT FERRIED TO MAIN BASE. 5. LANDING GEAR (NOSE) ACTUATOR CHANGED I.A.W. M.M. 32-31-24. 6. AIRCRAFT SERVSDR CA001214006Smoke Detector · malfunctioned(CAN) JUST AFTER TAKEOFF, MIN BAY SMOKE INDICATION APPEARED, THEN DISAPPEARED AFTER 10 SECONDS. FLIGHT CREW CHECKED MIN BAY SNIFFER TUBE SYSTEM, NO SMOKE WAS DETECTED. CREW ELECTED TO RETURN TO BASE. ON GROUND NO EVIDENCE OF SMOKE OR BURNING COULD BE FOUND ANDSDR CA001211009Panel · damaged(CAN) DURING WALK-AROUND OF AIRCRAFT, FORWARD CARGO DOOR AFT ACCESS PANEL FOUND BUCKLED AND PEELED BACK, PANEL REPLACED, NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHTS.SDR CA001201002Switch · failed(CAN) AIRCRAFT HAD 2 AIR TURNBACKS DUE TO NR 2 PITCH TRIM LEVER DISENGAGING DURING CLIMB. THE NR 1 PITCH TRIM SYSTEM WAS ON MEL, AT THIS TIME. AFTER THE FIRST TURNBACK, THE NR 2 FLIGHT AUGMENTATION COMPUTER WAS REPLACED. THE NR 2 FAC TESTED SERVICEABLE. NR 1 SDR CA001005013Cable · missing(CAN) NR 1 ENGINE THROTTLE LEVER BINDING WILL NOT GO INTO IDLE POSITION & REVERSE ISNOT SELECTABLE. NR 1 ENGINE THROTTLE CABLE REPLACED DUE TO HEAT DAMAGE. CHANGED AS PER I.A.W. & M.M. 76-11-41. 3. HALF CLAMP & BUSHING FOUND MISSING ANTI-ICING VALVE REPLACESDR CA001005011Computer · false indication(CAN) 1. A/C DEPARTING AT APPROXIMATELY 100 KTS. INTERMITTENT ECAM MASTER WARNING & CHIME MESSAGE DISAPPEARED WITHOUT OBSERVING ECAM. 2. AT APPROXIMATELY 155 KTS MASTER WARNING ON ECAM, MASTER CAUTION & CONDITIONS CHIME.3. SUCCESSFUL REJECTED TAKEOFF CARRIED SDR CA000830041Bolt · loose(CAN) 1.NR2 ENGINE FAILED TAKEOFF AT APPROXIMATELY 100 KNOTS. 2. FOUND 3 BOLTS LOOSE AT NR2 ENGINE MEC FUEL OUTLET MANIFOLD & INJECTOR.3. BOLTS TIGHTENED M.M. 20-21-12. HIGH POWER RUNS CARRIED OUT, THE AIRCRAFT WAS SERVICEABLE AS PER MM 71-00-00. 4. NO FURTHERSDR CA000714028Controller · failed(CAN) WHILE CLIMBING BOTH PX REGULATORS FAILED. AIRCRAFT LANDED WITHOUT INCIDENT. AIRCRAFT SYSTEM TROUBLE SHOOTING FOUND THAT SYSTEM NR 1 CABIN PRESSURE CONTROLLER WAS U/S. NR 1 CABIN PRESSURE CONTROLLER REPLACED. SYSTEM CHECKED SERVICEABLE I.A.W. 21-29-0SDR CA000808014Coupling · broken(CAN) 1. ON TAKEOFF & ROTATION RT ENGINE HIGH EGT. THROTTLE RETARDED. EGT BACK TO NORMAL PARAMETERS. A/C RETURNED TO BASE. 2. ENGINE COWL OPENED & COUPLING FOR H.P. VALVE TO 14TH STAGE BLEED AIR DUCT FOUND BROKEN. 3. COUPLING REPLACED I.A.W. M.M. FUNCTIONED SESDR CA000714027Fitting · worn(CAN) AIRCRAFT WAS CLIMBING WHEN LT NOSE GEAR DOOR WARNING WAS OBSERVED . AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT THE LT NLG DOOR ACTUATING CYLINDER EYE END HAD COME APART FROM THE PISTON. FURTHER INVESTIGATION FOUND THAT EYE ASSY FITTING SDR CA000614002Slide · failed(CAN) AIRCRAFT 204, MAY 17/2000, TRENTON, LOG SEQUENCE 0511852. DURING SCHEDULED TEST DEPLOYMENT OF RT OVERWING SLIDE, IT FAILED TO DEPLOY. SLIDE WAS DEPLOYED BY FURTHER ACTUATION OF AUTOMATIC CABLE. SLIDE DID NOT FULLY INFLATE.SDR CA000802022Frame · cracked(CAN). WHILE AIRCRAFT WAS AT SOGERMA FOR A C12 INSPECTION, EXTENSIVE CRACKING WAS FOUND ON BOTH NR 1 AND NR 2 PYLON LOWER SPAR CANTILEVER STRUCTURE.. MPD INSPECTION TASK WAS RAISED TO COVER THIS AREA Z1421-01-1. REPAIRED WERE CARRIED OUT I.A.W. SRM 54-52-11, FSDR CA000330002Slide · failed(CAN) DURING SCHELDULED DEPLOYMENT OF ESCAPE SLIDE, SLIDE DID NOT COMPLETLY DEPLOY. FABRIC COVER ON THE PACKBOARD JAMMED THE CABLE. SLIDE REPLACED.SDR CA000322017Fcu · malfunctioned(CAN) NR 2 THROTTLE WARN ON ECAM DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RESET SYSTEM, NO FAULT PRESENT. FLIGHT CONTINUED WITH NO OTHER FAULTS.SDR CA991210013Hydraulic Line · ruptured(CAN) LOSS OF GREEN SYSTEM HYD FLUID. INVESTIGATION REVEALED A RUPTUTRED LINE NEAR THE REAR SPAR. LINES REPLACED.SDR CA991210012Connector · dirty(CAN) TRAILING EDGE FLAPS FAILED DURING APPROACH. INSPECTION REVEALED NO FAULT FOUND. CONNECTOR 39 AND 40 CLEANED. FLAP SYSTEM RESET.SDR CA991210011Fairing · missing(CAN) L/H WING NR3 FAIRING, FWD NOSE ASSY FOUND MISSING AFTER FLIGHT.SDR CA991116026Panel · leaking(CAN) PANEL FORWARD OF RIGHT ACU INTAKE FOUND DAMAGED. SUBMITTER SUSPECTED ICE BUILD-UP FROM LAVATORY SERVICE PANEL WHICH WAS LEAKING AT ONE DROP PER SECOND. LEAK REPAIRED, PANEL REPAIRED.SDR CA991027002Switch · out of adjust(CAN) CLIMBING THROUGH FL 280, NR 1 RT CABIN DOOR NOT CLOSED WARNING ILLUMINATED. DOOR SWITCHES ADJUSTED AND TESTED PER AMM 52. NO FURTHER FAULT REPORTED.SDR CA990729002Switch · failed(CAN) NR 2 FUEL CLOG WARNING, DIFFERENTIAL PRESSURE SWITCH REPLACED.SDR CA990729001Escape Slide · failed(CAN) ESCAPE SLIDE FAILED TO DEPLOY DURING TEST DUE TO JAMMING OF THE RELEASE LEVER ON THE EMERGENCY OPERATING CLYINDER. PERCUSSION MECHANISM INSPECTED AND TESTED PER MM.SDR CA990521019Slide · misadjusted(CAN) RIGHT OVERWING SLIDE FAILED TO OPEN WHEN TESTED. ACTUATING CABLE EITHER TOO LONG OR TOO SHORT, YET TO BE DETERMINED.SDR CA990330009Slide · failed(CAN) ESCAPE SLIDE FAILED TO DEPLOY, LEFT AFT DOOR.SDR CA990129021Connector · failed(CAN) IDG HARNESS CONNECTOR IN ENGINE PYLON SEVERELY ARCED ON 3 RECEPTACLE CONNECTORS. REPAIRED/REPLACED.SDR CA981006026Door · separated(CAN) AIR GROUND DOOR MISSING AND ADJACENT FAIRING PARTIALLY RIPPED OFF. REPAIRED AND DOOR REPLACED. SB 310-52-2030 TO BE CARRIED OUT WHEN PARTS RECEIVED.SDR CA980928032Fuel Door · missing(CAN) DURING INSPECTION, REFUEL DOOR MISSING. REPLACED.SDR CA980909022Pump · leaking(CAN) TWO HOURS INTO FLIGHT, LOST ALL BLUE SYSTEM HYDRAULIC FLUID, APPROXIMATELY 45 MINUTES LATER, THE BLUE SYSTEM HYDRAULIC RESERVOIR OVERHEAT LIGHT CAME ON AND REMAINED ON FOR DURATION OF THE FLIGHT. MAINTENANCE FOUND BLUE SYSTEM ENGINE HYDRAULIC PUMP CASISDR CA980615007Generator · failed(CAN) AFTER TAKEOFF, NR 1 GENERATOR FAILED, UNABLE TO RESET IN-FLIGHT. FAULT ISOLATION PER 24-00-00 P6150 PARTS 1 TO 5 CARRIED OUT. GENERATOR CONTROL UNIT RESET. ENGINE GROUND RUN-UP CARRIED OUT, ALL PARAMETERS NORMAL. HEAVY LANDING AND HEAVY BRAKE INSPECTSDR CA980318051Panel · damaged(CAN) LEFT HAND WHEEL WELL BULK HEAD PANEL FELL OFF AND DAMAGED. PANEL REPLACED. AIRCRAFT TT: 41,402 HOURS.SDR CA980318050Door · missing(CAN) FUEL PANEL DOOR FOUND MISSING AFTER A/C LANDED. NEW PANEL INSTALLED ON RETURN TO HOME BASE.SDR CA971015014Generator Drive · overheated(CAN) DURING CRUISE NR1 I.D.G. HAD AN OVERHEAT TEMPERATURE READING OF 189 DEGREES. I.D.G. DISCONNECTED AND AIRCRAFT RETURNED TO BASE. AS A PRECAUTIONARY MEASURE THE I.D.G. HEAT EXCHANGER AND GENERATOR CONTROL UNIT WERE REPLACED ALONG WITH THE I.D.G.SDR CA970909012Windshield · cracked(CAN) CAPTAINS FORWARD WINDSHIELD OUTER LAYER CRACKED. MAINTENANCE ACTION INVOLVED REPLACING WINDOW.SDR CA970731027Pitot Line · fod(CAN) TAKEOFF ABORTED DUE TO AIRSPEED DISCREPANCY BETWEEN L/H & R/H SIDE OF 40 KNOTS. THE L/H PITOT LINE WAS PURGED AND A WASP WAS REMOVED. PITOT STATIC TEST WAS CARRIED OUT AND CHECKED SERVICEABLE.SDR CA970618019Prox Sensor · failed(CAN) UNABLE TO RETRACT LANDING GEAR ON SYSTEM #1, SYSTEM #2 SELECTED AND GEAR RETRACTED. AFTER PASSING 'TAKE-OFF INHIB' (LIFT OFF PLUS 1 MINUTE) THE FOLLOWING FAILURES OCCURRED. CABIN PRESSURE REG #1 - CAPT. PITOT HEAT AND TAT HEAT - F/O PITOT HEAT - FAC #1 -SDR CA960510101Uplock · lock failed(CAN)DURING WALK AROUND/DAILY CHECK ON AIRCRAFT, RAM AIR TURBINE (R.A.T.) WAS FOUND DEPLOYED. BOTH DEPLOY HANDLES IN THE COCKPIT WERE FOUND WITNESSED WIRED IN THE STOWED POSITION. MAINTENANCE CHECK FOUND TH E UPLOCK MECHANISM INOPERATIVE. UPLOCK REPLACED AND SSDR CA960510102Actuator · jammed(CAN)ON CLIMB OUT, RUDDER TRAVEL #1 AND #2 FAILED QUICKLY IN SEQUENCE, UNABLE TO RESET. MAINTENANCE ACTION INVOLVED CHANGING RUDDER VARIABLE STOP ACTUATOR.SDR CA960208102Handle · worn(CAN)ON CLIMB AT 8,000 FEET DOOR WARNING OCCURRED FOR LOWER ACCESS DOORS. AS THIS WAS FIRST FLIGHT AFTER A "C" CHECK, THE CREW ELECTED TO RETURN TO BASE. MAINTENANCE CHECK REVEALED DOOR HANDLE FOR LOWER AC CESS DOOR WAS FOUND RELEASED. AIRBUS SB A310-52-2040 C
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