Airbus A310-324
Service difficulty reports · 1,439
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 = 'A310324' 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 = 'A310324' 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 FDEA201409012391Repair · debondedAGING INSPECTION - EXISTING REPAIR ON LT WING I/B FLAP TRAILING EDGE RIB8-10 UPR & LWR SURFACE. REPAIR PATCH DISBONDED. REPORTED TO ENGINEER. REMOVED THE OLD REPAIR PATCH & REPAIRED THE DAMAGE PER A310 SRM 57-52-12 FIG 204 EO 6-5100-7-5000 PART1 WAS COMPLESDR FDEA201408222288Fastener · missingAGING INSPECTION EXISTING REPAIR ON AFT CARGO DOOR SILL BEAM BETWEEN FRAME 59 & 64 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALVATED AND FOUND THE REPAIR WAS MISSING A FASTENER, WAS FOUND COMPARED WITH EA 6-5317-81082 TITLE:FUSELAGE -DEVIATION FRSDR FDEA201408202239Repair · debondedAGING INSPECTION EXISTING REPAIR ON RT WING INBD FLAP TE RIB 5 - 7 LOWER SURFACE, REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR PATCH DISBONDED REMOVED OLD REPAIR PATCH & DAMAGE CORE IT EXCEEDED THE REPAIRABLE LIMIT PER A310SRM57-52-12 FIG 204 REPORTED TO ENSDR FDEA201408202238Repair · debondedAGING INSPECTION EXISTING REPAIR ON RT WING INBD FLAP TE RIB 3 - 5 LOWER SURFACE, REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED AND FOUND THE OLD REPAIR PATCH DISBONDED. REMOVED OLD REPAIR PATCH & DAMAGE CORE REPORTED TO ENGINEER. REPAIRED TSDR FDEA201408202242Repair · corrodedAGING INSPECTION EXISTING REPAIR ON AV COMPARTMENT STRINGER 44 RT BETWEEN FRAME 16 & 17 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS FOUND CORRODED HEVAILY. THE REPAIR ANGLE FITTING WAS REPLACED IN SNRM:N00360 AND COMPLETED TITLE: AV COMPT- STRINGER 4SDR FDEA201408202241Stringer · corrodedAGING INSPECTION EXISTING REPAIR ON AV COMPARTMENT STRINGER 44 RT BETWEEN FRAME 15A & 16 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALVATED AND FOUND THE STRINGER CORRODED HEVAILY. THE OLD REPAIR AND STRINGER WAS REMOVED AND RE-REPAIRED WITH A NEW SDR FDEA201408072106Stringer · corrodedAV COMPARTMENT STRINGER 44 RT FOUND HEAVY CORROSION AT FRAME 16 LOCATION. COMPLIED WITH EA 6-5310-T0310620 PART 1 TITLE :FUSELAGE MAINFRAME SECTION 12. CORROSION ON STRINGER S-44 RH AT FR 16. THE REPAIR WAS CATEGORY "B' AND WAS CLASSIFIED AS MAJOR PER GMM 6SDR FDEA201407281996Computer · failedPASSING 10000 FT TRIM TANK PUMPS ECAM MSG FUEL QTY SHOWED 34K TOTAL, 64.2 TAKEOFF FUEL. ECAM MSG SELF-CLEARED & FUEL SLOWLY ROSE AGAIN, FUEL WAS GOOD. AFTER TAKEOFF PLUS 45 MIN TOTAL LOSS OF FUEL QTY SYS. RTB SENSOR STATUS SHOWED FQ 3 FAIL. R & R FQIC IAW SDR FDEA201407191860Stringer · corrodedAFT CARGO STRINGER 46R FRAME 63 - 64 STRINGER CORRODED. REPAIRED THE STRINGER PER A310 SRM 53-10-14 PB201 FIG201HSDR FDEA201407171832Windshield · crackedEN ROUTE LT WINDOW HEAT FAULT, FOLLOWED BY WINDSHIELD CRACKING. NUMEROUS CRACKS IN LOWER RT CORNER. QRH FOLLOWED, DIVERTED. REMOVED L1 WINDSHIELD IAW MM 56-11-11-04.SDR FDEA201406281576Pulley · defectiveON DEPARTURE CLIMB WITH AUTO PILOT NR 2 ON WHEN THE SLATS WERE RETRACTED THE ACFT GAVE VERY HARD TO THE RT. THE AILERONS COMPENSATED BY GOING LT 6 UNITS. AT THIS POINT WE CHECKED THE FLIGHT CONTROL POS PAGE & SPOILERS 7, 6 & 5 ON THE LT WING WERE UP. AFTERSDR FDEA201406251546Windshield · crackedCAPTAIN`S COCKPIT WINDOW CRACKED AT FLIGHT LEVEL 340, ARCING BEGAN IMMEDIATELY. NORMAL QRH PROCEDURES STOPPED THE ARCING. REMAINDER OF FLIGHT NORMAL. R & R CAPTAIN'S WINDSHIELD IAW AMM 56 -11-11-04, PERFORMED WINDSHIELD PANEL ANTI-ICING & DEFOGGING. OPERATSDR FDEA201405281215Support · corrodedLEFT MLG RIB 5 FWD LUG HAS CORROSION IN BORE & FWD FACE. COMPLIED WITH EA 6-5710-T0308476 P1 WINGS BASIC WING STRUCTURE LT & RT RIB 5 FWD LUG CORROSION, LT RIB 5.SDR FDEA201405281214Support · corrodedRIGHT MLG RIB 5 FWD LUG HAS CORROSION IN BORE & FWD FACE. COMPLIED WITH EA 6-5710-T0308476 P2 WINGS BASIC WING STRUCTURE LT & RT RIB 5 FWD LUG CORROSION, RT RIB 5.SDR FDEA201405211114Engine · stalledNR 1 ENGINE HAD A SUSPECTED STALL ON ROLLOUT. TOWER REPORTED LT ENGINE ON FIRE. STOWED THRUST REVERSERS BY 60 KIAS & STOPPED ACFT, SHUTDOWN ENGINE, NO OTHER FIRE INDICATIONS, VISUALLY CONFIRM NO SMOKE. ON SHUTDOWN IN RAMP ADC 1 FAULT OCCURRED & STAYED ON. SDR FDEA201405110982Rib · corrodedLEFT RIB 5 FWD LUG HAS CORROSION IN BORE, FWD & AFT FACES. COMPLIED WITH EA 6-5710-T0307941 P-1. MAJOR REPAIR.SDR FDEA201405110981Rib · corrodedRIGHT RIB 5 FWD LUG HAS CORROSION IN BORE, FWD & AFT FACES. COMPLIED WITH EA 6-5710-T0307941 P-2, WING BASIC WING STRUCTURE, LT & RT RIB 5 FWD LUG CORROSION. MAJOR REPAIR.SDR FDEA201405090992Thrust Reverser · damagedNUMBER 1 ENG THRUST REVERSER OTBD TRANSLATING SLEEVE AFT 8 INCHES IS MISSING TOP TO BOTTOM, WHITE COWL. ALL COCKPIT THRUST REVERSER LIGHTS EXTINGUISHED, NORMAL. NR 1 ENG OIL SERVICE DOOR WAS OPEN & BOTTOM HINGE PIN MISSING. INNER BARREL MESH IS MISSING & SDR FDEA201404200759Stringer · corrodedSTRINGER 44L AT FRAMES 41 - 42 IN A/C BAY CORRODED. BLENED IAW SRM 51-74-10, PERFORMED DVI TO VERIFY NO CORROSION FOUND IAW NTM 51-70-00, PERFORMED ROTO TEST TO OPEN HOLES TO VERIFY NO CRACKS FOUND IAW NTM 51-10-01. FABRICATED THE REPAIR PARTS IAW SRM 53-SDR FDEA201404180749Stringer · corrodedSTRINGER 44L AT FRAMES 41 - 42 CORRODED.SDR FDEA201404180750Stringer · corrodedSTRINGER 45L AT FRAMES 41 - 42 CORRODED. REPAIRED IAW SRM 51-74-10 REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.SDR FDEA201404010608Rib · corrodedRT RIB 5 BORE & AFT FACE HAVE CORROSION. COMPLIED WITH EA 6-5710-T0307063 P 1 WINGS & BASIC WING STRUCTURE, RT RIB 5 LUG CORROSION.SDR FDEA201404010606Rib · corrodedLT RIB 5 HAS CORROSION IN BORE & FACE. COMPLIED WITH EA 6-5710-T0307003 WINGS & BASIC STRUCTURE, LT RIB 5 LUG CORROSION.SDR FDEA201403190525Sensor · malfunctionedDURING CRUISE FLIGHT, NR 2 RT ENGINE OIL TEMP BEGAN TO FLUCTUATE FROM NORMAL CRUISE TEMP OF 116C UP TO 230C. STAYED ABOVE 160C FOR MORE THAN 9 MINUTES BUT CONTINUED TO FLUCTUATE BETWEEN NORMAL & A HIGH OF 230 C. FINALLY TEMP STAYED ABOVE 160 C FOR MORE THASDR FDEA201403130495Smoke Detector · malfunctionedIAW WRI 26-22 8151 FWD CARGO COMPARTMENT DET INDICATION. AGENT 1 DISCH, NO SECONDARY INDICATION, NO SMOKE INDICATION IN THE COCKPIT. TESTED BOTH SMOKE DET OK & TESTED 26-16-00-05-01, ACFT OK FOR SERVICE. R & R 42WH SMOKE DETECTOR.SDR FDEA201403120491Check Valve · leakingLOST GREEN HYD AIR AT FLT LEVEL 390 IAW QRH QTY WAS MONITORED AFTER 1 MIN GREEN HYD QTY FLUCTUATED & PEGGED AT MAX. IAW QRH GREEN HYD PUMPS 1 & 2 WERE SECURED, IAW QRH LANDED. REPLACED DEPRESSURIZATION RELEIF VALVE IAW AMM 29-11-27-04. ALSO REPLACED GREENSDR FDEA201402140320Tru · faultedESS TR INDICATED 4A NUMEROUS TIMES IN CRUISE. FOUND ONLY 4A ON ESS TR & I ESS TRANSFORMER RECTIFIER IAW MM 24-32-11-04. OPERATIONS CHECK SATISFACTORY RUN NR 2 ENG IAW A310JRH. GOOD DC LOAD DISTRIBUTION, ACFT OK FOR SERVICE.SDR FDEA201402070285Fuel · contaminatedEN ROUTE LT OUTER PUMP 1 & PUMP 2 FAILED IN FLIGHT. BOTH PUMPS SHOWED LOW PRESS. FOLLOWED ECAM TO TURNOFF. THAWED LO FUEL PUMPS & TANK WITH 3 COLD BUSTERS FOR 5 HOURS. PERFORMED LO TANK PUMPS OPERATIONAL TESTED IAW AMM IAW 28-21-00-05, BOTH PUMPS CHECKED NSDR FDEA201401280212Computer · failedDURING FLAP EXTENSION, EXPERIENCED FLAP SYS 1 & 2 FAULT ILLUMINATION, FLAPS FAILED TO EXTEND. PERFORMED QRH PROCEDURE. WHEN FLAP HANDLE MOVED TO 40 DEGREES, FLAPS EXTENDED TO 40. BITE CHECKED BOTH SFCC'S & BOTH PASSED. RESET & TESTED EACH SEGMENT OF BOTH SDR FDEA201401230181Computer · malfunctionedDURING TAKEOFF, TOGA WOULD NOT ENGAGE. NO OTHER WARNINGS, COULD MANUALLY ADVANCE THROTTLES WITH NO RESTRICTIONS. REMOVED AND REPLACED TCC COMPUTOR IAW AMM 22-36-34-04-01 AND REPFORMED A AFS/LAND TEST. ALL SYSTEM TESTED NORMAL.SDR FDEA201401210149Relay · failedDURING DESCENT, RECEIVED AN INTERMITTENT CHIME, WITH NO ECAM ALERT, INVESTIGATION FOUND LOW FUEL TANK AT 1.5 & RO AT 1.7. THE CENTER TANK WAS FEEDING & TRIM TANK TRANSFERRING FWD. UNABLE TO RECOVER INNER FUEL TANK & APPROXIMATELY 17600 LBS OF FUEL WAS TRAPPSDR FDEA201401030016Sequence Valve · failedRIGHT MLG WOULD NOT GO DOWN. UTILIZED CRANK HANDLE & RT MLG LOWERED. RT MLG SEQUENCE VLV LOCKED UP & WOULD NOT MOVE. R & R RT MLG SEQUENCE VLV IAW AMM A310-300 32-31-37-04. OPERATIONS CHECK & LEAK CHECKED GOOD.SDR FDEA201312253039Sequence Valve · out of rigGEAR LEVER RAISED, RT MAIN GEAR DID NOT RETRACT. GREEN DOWN INDICATION, GEAR DOOR AMBER. PUT GEAR HANDLE BACK DOWN ALL INDICATIONS BACK TO NORMAL FOR DOWN & LOCKED. JACKED ACFT, SWUNG RT MAIN GEAR, GEAR DID NOT RETRACT. FOUND RT MAIN GEAR SEQUENCE VALVESDR FDEA201311302913Floor Support · crackedMDIS 807 53-00 0008007 30NOV13 BQN CLOSE R FOUND FWD FUSELAGE FLOOR SUPPORT MEMBER BETWEEN C9 & C10, ONE FRAME LT 09 88 WITH SEVERAL CRACKS. A536 11977200 ID WEB IAW SRM 53-11-15 PAGE 4 ITEM 475 PN A53611977200 & ATTACHED FITTING ITEM 185 PN A53610270220. SDR FDEA201311122736Skin · corrodedLEFT WING UPPER SKIN INBD JET FUEL GROUND CONNECTOR POINT AROUND AREA HAS SLIGHT CORROSION AT STR 7 AND STR 8 POSITION. REPAIRED IAW EA 6-5720-T0303769. REPAIR WAS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201311012663Beam · crackedONE CRACK WAS FOUND ON THE NR 33 FASTENER OF THE INNER LONGERON BEAM FLANGE AT STRINGER 11 BETWEEN FRAMES 73A AND 75A (LT SIDE). CRACK LENGTH IS 1INCH IAW E6-5310-7-3314, PT3. DRILLED OUT AFFECTED FASTENER AND CUT OUT DAMAGE PORTION OF BEAM FLANGE. NDI WAS SDR FDEA201310252617Controller · malfunctionedCABIN NR 2 PRESSURE REGULATOR INITIALLY ROUGH DURING TAKEOFF AND CLIMBOUT, EVENTUALLY SMOOTHED OUT. FAULTED AT FL 310. HAD TO TURN BOTH NR 1 & NR 2 OFF & USE MANUAL PRESSURIZATION CONTROL TO RECOVER, EMERGENCY DECLARED, CONTINUED TO DESTINATION. TESTED NSDR FDEA201310162517Skin · dentedFUSELAGE SKIN DENTED ON BELLY FWD OF FRAME 4. REPAIRED DENT IAW EA 6-5330-T0302970A.SDR FDEA201310152506Limiter · trippedDURING FINAL, TRIED LOWERING FLAPS AND RECEIVED A FLAPS 1/2 SYS FAULT. CYCLED HANDLE NO FLAPS EXTENDED. FOUND WHEEL WELL TORQUE LIMITER FOR RT WING FLAP DRIVE TRIPPED. RESET LIMITER. INSPECTED RT WING FLAP TRANSMISSION TORQUE LIMITERS NOT TRIPPED. NR 1 SFSDR FDEA201310012366Smoke Detector · failedEQUIPMENT BAY SMOKE INDICATION, SEVERAL MINUTES AFTER, HEARD A LOUD BANG. UNKNOWN WHERE SOUND COME FROM. FIRE WARNING ILLUMINATED SEVERAL TIMES. DID NOT SMELL SMOKE. PERFORMED SMOKE DETECTION OPS TEST IAW AMM 26-15-00-05, FOUND SMOKE ECAM WARNING AND COUSDR FDEA201309132202Fitting · corrodedRT WING MLG FITTING OF RIB 5 FORWARD LUG CORRODED, COMPLY WITH EA6-5710-T0302341A.SDR FDEA201309132201Fitting · corrodedLT WING MLG FITTING OF RIB 5 FORWARD LUG FOUND CORROSION, COMPLY WITH EA 6-5710-T0302340.SDR FDEA201308191952Jackscrew · wornAFTER TAKEOFF DURING FLAP RETRACTION, RECIEVED A WARNING BELL AND FLAP SYS 1, FLAP SYS 2FAULT. FLAPS WERE STUCK BETWEEN 15-20, CYCLED HANDLE AND DID NOT CLEAR RAN QRH AND RTB. DURING AFTER LANDING CHECK, FLAPS RETRACTED. REVIEWED FAULT CODE FORM NR 1 SFCCSDR FDEA201308151902Unknown · unknownON APPROACH, FLAPS SYS 1 AND 2 FAULTED. RECYCLED FLAPS, RETRACTED BUT ON EXTENSION STOPPED AT APPOX 18. RAN QRH AND ON FINAL WITH FLAP HANDLE EXTENSION TO 30/40 SLATS EXTEND TO 30 BUT FLAPS REMAINED LESS THAN 20'. BITE TEST ON SFCC NR 1 GOT FAULT CODE 011SDR FDEA201308131865Windscreen · crackedDURING CRUISE AT FL340, CAPT'S WINDSCREEN CRACKED. ARCING NOTED TOP RT CORNER AFTER CRACKING. COMPLIED WITH QRH, PROCEED TO DESTINATION IAW GOC GUIDANCE. ENTERED IN ERROR, PREVIOUSLY REPORTED ON 13-1864. THIS DUPLICATE OCCURED AFTER A DOUBLE CLICK OF MOUSE OSDR FDEA201308131864Windscreen · crackedDURING CRUISE AT FL340, CAPTAIN'S WINDSCREEN CRACKED. ARCING NOTED TOP RT CORNER AFTER CRACKING. COMPLIED WITH QRH, PROCEED TO DESTINATION IAW GOC GUIDANCE. TEXT REMAINS OPEN FOR WINDOW COMPONENT(S) R & R IAW AMM 30-42-11-04. LEFT WINDOW HEAT PROTECTION UNSDR FDEA201308021750Jackscrew · contaminatedNR 1 & 2 SLAT SYSTEMS FAULTED ON APPROACH. COMPLIED WITH PHASE 1, NO HELP. COMPLIED WITH ECAM AND QRH. ON CONFIGURING FOR LANDING IAW QRH SLAT EXTENDED NORMALLY. SFCC 1 & 2 FAULT INDICATES SLAT 01111 SLAT BINDING IAW TSM 27-80-02, FIG 101. FOUND LT L/E TOSDR FDEA201308011728Computer · failedDURING TAKEOFF ROLL, APPROX 10 SECONDS INTO ROLL, ATS LEVER TRIPPED OFF. ENGINE NR 2 EPR MODE FAULTED, ENGINE NR 2, N1 MODE, ATS OFF ON ECAM. CLEARED RUNWAY. RESET CIRCUIT BREAKER ON OUH 31 PANEL AS DIRECTED BY MX. ALSO RESET NR 2 ENGINE EPR MODE FAULT, ASSDR FDEA201307041476Drain · obstructedSTANDBY AIRSPEED INDICATORS INOPERATIVE. AT 250 KTS ON BOTH PFD'S BOTH STANDBY AIRSPEED INDICATORS SHOWED 180 KTS, THIS WAS AT 10,000 FT, BOTH STANDBY AIRSPEED INDICATORS SLOWLY DECREASED DURING THE CLIMB TO FL 380, AT FL 380 BOTH PFD'S SHOWED 255 KTS, BOTH SSDR FDEA201305070933Wire · damagedWHEN SETTING TAKEOFF POWER, NR 1 ENGINE REVERSE UNLOCK LIGHT ILLUMINATED. DURING REACTIVATION OF NR 1 THRUST REVERSER, FOUND WIRE CHAFING IN WIRING BUNDLE 21W4082-509 NEXT TO CONNECTOR DS307, FOUND THE WIRE ROUTING TO PIN 4 ON DS307 TO NR 1 THRUST REVERSER
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