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 CA190708004O-Ring · failed(CAN) PILOT CALLED OVER PHONE PATCH TO REPORT THAT THEY GOT THE ECAM MESSAGE FOR GREEN SYSTEM HYDRAULIC LOW LEVEL. THEY HAVE PERFORMED THE ECAM AND QRH, SO THE HYDRAULIC PUMPS ARE OFF, AND THE LEVEL ON THE OVERHEAD IS JUST BELOW THE GREEN AREA, AT THE BEGINNINSDR CA190403011Engine · stalled(CAN) AFTER TAKE OFF ENGINE #1 ENCOUNTERED AN ENGINE STALL AT INITIAL CLIMB PASSING 1500FT, THE CREW REPORTS THAT THEY HEARD A COUPLE OF `THUMPS`, AND THEN NOTICED THE N2 DROP. THEY PERFORMED THE QRH AND THEN THE ENGINE WAS FINE, BUT THEY ONLY ATTEMPTED TO 50%SDR CA180925007Fitting · corroded(CAN) STRONG WHISTLE SOUND FROM RL DOOR IN CRUISE. AFTER INVESTIGATION INSIDE OF DOOR,FITTING FOUND CORRODED. FITTING REPLACED. (TC# 20180925007)SDR CA180910001Pump · leaking(CAN) CREW REPORTED DURING FLIGHT: `GREEN HYD QTY SHOW LOW QTY ON THE NEEDLE GAGE QTY ON ECAM IS STEADY` LATER REPORT: `HYD LOW QTY WARNING ON ECAM1 LANDING GEAR GRAVITY EXTENTION NOSE STERING INOP` GREEN HYDRAULIC SYSTEM ENGINE DRIVEN PUMP AND CASE DRAIN FILTSDR CA180423016Computer · false indication(CAN) DURING TAKEOOF ROLL AT 80KTS ECAM ENG INDICATION REJECTED TAKEOFF AT FULL STOP ECAM FWC AMBER CRT CAUTIONS NOT AVAIL. FWC 1 REPLACED AND CHECKED SERV, IAW AMM 31-53-34 ENG TRIM TESTED SERV IAW 73-23-00. (TC# 20180423016)SDR CA151013012Valve · failed(CAN) DURING PUSHBACK OF ACFT FOR DEPARTURE, THE CREW TRIED TO SET THE PARKING BRAKE. THEY WERE UNSUCCESSFULL AND A LEAK WAS NOTED IN THE MAIN WHEEL WELL AREA. PARKING BRAKE VALVE FAILED AND WAS FOUND IN 3 PIECES. HOUSING ON THE VALVE FAILED INTERNAL PLUNGERSDR CA151007011Attach Fitting · broken(CAN) LEFT WING NR 3 SPOILER BROKEN AT ACTUATOR ATTACHMENT. SPOILER WAS FREE TO MOVE EXTEND/RETRACT DURING FLIGHT.SDR CA150820009Skin · delaminated(CAN) THE FLIGHT CREW WAS APPROXIMATELY 4 HRS INTO THEIR FLIGHT WHEN THEY FELT A SIGNIFICANT, SUDDEN VIBRATION THAT LASTED AROUND 3-4 SECONDS AND WAS FELT IN THE CONTROL COLUMN AND RUDDER PEDALS ON THE FLIGHT DECK, AS WELL AS GENERALLY THROUGHOUT THE ACFT. TSDR CA150810001Pump · cracked(CAN) CREW REPORTED HYDRAULIC FLUID ON BLUE SYS LOW LEVEL ECAM WARNING AND FAULT IN CRUISE. CREW DECLARED A PAN PAN, QRH PROCEDURE CARRIED AND ACFT DIVERTED. ACFT LANDING WAS UNEVENTFUL. MAINTENANCE INVESTIGATION FOUND THE NR 1 ENGINE BLUE SYSTEM HYD PUMP CSDR CA140919007Battery · damaged(CAN) DURING ROUTINE VISIT IN AVIONIC SHOP FOR REGULAR BATTERY CHECK, THE CASE OF EPSU BATTERY WAS FOUND WITH A SMALL BURN. THE ASSY WAS OPENED AND CELLS NR 4 AND 5 WERE FOUND SHORT CIRCUITED AT THE TOP WHERE THE CONNECTING TAB IS POSITIONED. FOLLOWING TWO REASDR CA140903013Coffeemaker · odor(CAN) CREW REPORTED FWD COFFEE MAKER BURNING ODOR IN FLIGHT. CIRCUIT BREAKER WAS PULLED AND ODOR DISSIPATED.SDR FDEA201405211117Fitting · damagedLEFT RIB 5 FWD LUG BORE OUT OF ROUND REPAIRED LT RIB 5 FWD LUG BORE OUT OF ROUND IAW DWG R57249389 & COMPLIED WITH EA 6-5710-T0308275.SDR FDEA201401030015Switch · malfunctionedLEFT CABIN DOOR SHOWED UNLOCKED AT FL 240. LEVELED OFF, PERFORMED QRH & PUSHED ON THE HANDLE. DOOR SHOWED LOCKED. CONTINUED TO CLIMB & DOOR SHOWED UNLOCKED AT FL 340, FINAL ALTITUDE WAS TO BE FL 400, RETURNED TO DEPARTURE. REMOVED AND REPLACED DOOR WARNINSDR FDEA201312142981Jackscrew · lack of lubeON APPROACH, FLAPS DID NOT EXTEND. FLAPS SYS 1 & SYS 2 FAULT LIGHTS ILLUMINATED UPON MOVING FLAP HANDLE TO ANY EXTENDED POSITION. ALTITUDE 6200 FEET AT KGTF, TEMP -5C. RELIEVED LOAD ON LT FLAPS THEN RESET LT FLAP TO LIMITER. RT LIMITER OK IAW A310-300 AMMSDR FDEA201312122966Hinge Fitting · nickedNOSE LANDING GEAR, RT AFT DOOR HINGE FITTING, BEARING HOLE FOUND TWO NICKS. REPAIRED IAW EA 6-5310-99725B PART 2.SDR CA130531004Switch · shorted(CAN) DURING TROUBLESHOOTING OF UPPER BEACON SYSTEM C/B POPPING. C/B WAS PUSHED IN AND A NOISE WAS HEARD & SPARK CAME OUT FROM PANEL 426VU. FOUND TOGGLE SWITCH AT FAULT. TOGGLE SWITCH 2LV AT PANEL 426VU REPLACED IAW AMM 20-45-21 UPPER BEACON TEST C/O IAW AMMSDR FDEA201304240855Wire Harness · failedAFTER TOUCHDOWN, DURING ROLLOUT NR 5 AND NR 6 TIRES BLEW. ACFT REMAINED ON CENTERLINE. REMOVED AND INSTALLED AND ROUTED LT MLG HARNESS LOOM THRU NR 5 AND NR 6 BOGIES IN POSITION IAW MM 32-11-43-04.SDR FDEA201304100772Door · damagedEXTENDING LANDING GEAR, RECEIVED ECAM WARNING THAT NLG DOOR WAS NOT CLOSED. BOTH PANELS SHOWED DOOR. FOLLOWED QRH LANDED UNEVENTFULLY. AFTER TAXING IN NOSE GEAR DOOR LIGHT EXTINGUISHED. FOUND AFT HINGE FITTING FOR RT AFT NOSE GEAR DOOR DAMAGED. REMOVED RTSDR CA130411009Bracket · cracked(CAN) DAMAGE WAS INITIALLY DISCOVERED ON MSN 482 DURING WORK PERFORMANCE IN AVIONIC BAY AS CRACK WAS APPARENT ON ONE FITTING. BASED ON REVIEW OF DAMAGE, REVIEW OF THE 2 OTHER ACFT IN FLEET THAT WERE PRESENT AT LINE MAINTENANCE BS, YTR, WAS DONE AND REQUIREMENSDR CA120827017Control Panel · overheated(CAN) DURING CRUISE FLIGHT, FLIGHT CREW REPORTED SMOKE COMING OUT OF ADF NR 2 CONTROL PANEL. ADF2 CIRCUIT BREAKER WAS PULLED BUT SMOKE CONTINUED TO COME OUT OF PANEL. PANEL WAS REMOVED AND DISCONNECTED AND SMOKE STOP FROM COMING OUT OF PANEL. PANEL IS BEING SDR CA120504003Bulkhead · corroded(CAN) FOUND BULKHEAD AT FRAME 39, CORRODED AND PERFORATED BETWEEN STRINGERS 54-55L AND BELOW WATERLINE Z-2557.SDR CA120330005Tank · ruptured(CAN) ACFT RETURNED TO BLOCK AFTER A LOUD BANG HEARD IN CLIMB FOLLOWED BY WATER QTY AND PRESSURE INDICATE ZERO ON FAP PANEL. ON ARRIVAL, FOUND WATER TANK RUPTURED.SDR FDEA201203160978Shear Plate · corrodedFWD END SHEAR PLATE FOUND CORRODED AT SEVERAL LOCATIONS FROM BS 410 TO 440, BL 0 TO LBL 24.75 FWD END SHEAR PLATE REPAIRED IAW EA F-5310-157901.SDR CA120224006Actuator · cracked(CAN) CLOSE TO 90KTS, ECAM MESSAGE "SPEED BRAKE WARNING", ENGINE SETTING WAS 96 PERCENT N1, REJECTED TAKEOFF CALLED, AFTER A FEW SECONDS, A SECOND ECAM MESSAGE DISPLAYED "HYD BLUE RESERVOIR LOW LEVEL". ALSO ECAM F/CTL PG DISPLAYED "SPOILER 2 EXTENDED". ACFT SDR FDEA201202160591Computer · malfunctionedAPPROX 1.5 HRS INTO FLIGHT, RT OTBD FUEL TANK QTY BEGAN TO DECREASE RAPIDLY. TANK WENT TO EMPTY, XX, AND REMAINED UNTIL IN DESCENT AT 16,000 FT, THEN QTY RETURNED TO 6.42. TROUBLESHOOTING VERIFIED FUEL LEVEL IN RT OTBD TANK ON RT NR 2 & NR 3 MAGNETIC LEVELSDR FDEA201112155280Fuel Cell · leakingRT WING BOTTOM SKIN HAD FUEL SEEPAGE AT SLAT TRACK NR9 CANISTER DRAIN PORT FASTENER. REMOVED AND CLEANED THE DAMAGED SEALANT AREA. RE-APPLIED NEW SEALANT FOR REPAIRING IAW EO 6-5710-7-3304 PT3 AND EA 6-5710-149029 (FOR REPAIR OF FUEL TANK SEALING). THE REPAIR SDR FDEA201112155276Fuel Cell · leakingRT WING FRONT SPAR HAD FUEL SEEPAGE AT RIB 18. REMOVED AND CLEANED THE DAMAGED SEALANT AREA. RE-APPLIED NEW SEALANT FOR REPAIRING IAW EO 6-5710-7-3304, PT3 AND EA 6-5710-149029. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201112155274Canister · leakingRT WING SLAT JACKSCREW NR 3 CANISTER DRAIN PORT HAD FUEL SEEPAGE IAW EA 6-5710-149029. REMOVED FUEL PANEL 540BB, 540CB IAW AMM 28-11-22. RE-SEALED SCREWJACK CANISTER IAW EO 6-5710-7-3304C PT1. RE-INSTALLED FUEL PNL 540BB, 540CB IAW AMM 28-11-22. LEAK CHSDR FDEA201112025116Skin · dentedRT WING T/E OTBD FLAP UPPER SURFACE DENTED. REPAIRED IAW SRM 57-53-12 FIG 210. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR FDEA201112025115Door · gougedFOUND CREW DOOR GOUGED. REPAIRED IAW EA 6-52-50-149021 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR FDEA201111295067Fitting · crackedLEFT NOSE SECTION/ FR 12A STIFFENER FITTING WAS FOUND 1 EA CRACK ABOUT .7500" IN LENGTH . ON ZONE B,J AREA IAW NTM 51-10-08, PART 1. REMOVED STIFFENER FITTING AND JUNCTION FITTING. INSTALLED STIFFENER FITTING AND JUNCTION FITTING WITH NEW PART REFER TO EO 6SDR FDEA201111224994Floor Panel · damagedAFT CARGO COMPARTMENT FLOOR PANEL 162AF HAS EDGE IMPACT DAMAGED. FOUND OUT OF LIMITS. REPLACED THE FLOOR PANEL BY FABRICATION OF A NEW PANEL WITH ADHESIVE AND INSERTS IAW SRM 53-10-20 & DWG A53279966. REPAIR MINOR PER GMM 6-2-100.SDR CA111116008Mec · failed(CAN) AFTER NORMAL ENGINE NR 2 START, NO THROTTLE RESPONSE N1 15 PERCENT, TGT 660 DEGREES, N2 60 PERCENT, FF 0.05. NR 2 ENGINE, MAIN ENGINE CONTROL (MEC) REPLACED IAW 73-21-01 AND MADE SERVICEABLE.SDR FDEA201110154538Power Supply · no testEMERGENCY LIGHTS WOULD NOT TEST PROPERLY. R & R EMERGENCY LIGHT POWER SUPPLY AND BATTERY IAW MM 33-51-14-04-09. OK FOR SERVICE.SDR FDEA201107032558Floorbeam · damagedBULK CARGO COMPARTMENT, FR 63 FLOORBEAM BOTTOM CEILING PANEL ATTACHMENT BETWEEN SEAT TRACK 1 AND 2L HAS A DRILL START. COMPLIED WITH EA 6-5310-145342 PT1.SDR FDEA201107012531Stringer · gougedAFT CARGO COMPARTMENT LT SIDE FWD OF FR 54.1, STR 37 HAS GOUGE. REMOVED, REPAIRED AND RE-INSTALLED STRINGER SECTION IAW SRM 53-10-14, PGS 201 THROUGH 231 SRM 51-21-10, PG 2, SRM 51-40-44, PG 1 AND SRM 51-75-10, PG 204.SDR FDEA201107012532Seal · crackedMETALLIC VAPOR SEAL CRACKED ON LT SIDE AT FR 42-43, R & R METALLIC VAPOR SEAL ON LT SIDE FR 42-43.SDR FDEA201106142246Web · damagedAFT PIT FR 69 RBL 26 VERTICAL WEB PUNCTURED AT CARGO FLOOR LEVEL REMOVED AND REPLACED VERTICAL WEB AT FR 69 RBL 26 IAW SRM 51-40-21SDR FDEA201106122211Seat Track · crackedSEAT TRACK NR 3 LT CORRODED AT FR 19. REMOVED CORROISON FROM NR 3 SEAT TRACK AT FR 19 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED AND REPLACED NR 3 LT SEAT TRACK SECTION AT FR 19 IAW SRM 51-72-10.SDR FDEA201106122212Seat Track · corrodedMDCC SEAT TRACK, NR 6, RT CORRODED INSIDE TRACK. REMOVED LEVEL 1 CORROSION ON SEAT TRACK NR 6 AT FR 19 AND FOUND TO BE OUT OF LIMITS IAW AIRBUS SRM 53-10-16. REPAIRED NR 6 SEAT TRACK AT FR 19 IAW EA 6-5310-145630.SDR FDEA201106122210Seat Track · corrodedRIGHT SEAT TRACK NR6 BETWEEN FRAME 19 & 20 HAS CORRSION 1 SQ INCH. REMOVED LEVEL 1 CORROSION FROM RT NR 6 SEAT TRACK BETWEEN FRAME 19 & 20 AND FOUND BEYOND LIMITS IAW SRM 53-10-16. REPAIRED IAW EA 6-5310-145630.SDR FDEA201106122213Floorbeam · corrodedMDC UNDERFLOOR TEE HAS 1 SQ INCH OF CORROSION FWD OF SEAT TRACK NR LT AT FR 12A. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-00. REMOVED AND REPLACED TEE FWD OF SEAT TRACK NR 3 AT FR 12A IAW SRM 51-72- 10.SDR FDEA201106102204Seat Track · damagedSEAT TRACK 4L AT FRAME 54.3 HAS DAMAGE TO TACK AND SCALLOPS. BLENDED DAMAGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 4L SECTION AT FR 54.3 IAW SRM 51-72-10.SDR FDEA201106102201Seat Track · damagedMDC SEAT TRACK 5R HAS 2 GOUGES AT SCALLOPS, 1 AT 54.2 AND 1 7 INCHES AFT OF 54.2. BLENDED DAMAGED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 5R SECTION AT FR 54.2 INCLUDING 17 INCHES AFT OF FR 54.2.SDR FDEA201106102203Seat Track · damaged2 EA GOUGES ON SEAT TRACK 3R FROM FRAME 54.2 TO FRAME 55/58. BLENDED GOUGED AREAS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 3R SECTION AT FR 54.2SDR FDEA201106102202Seat Track · damagedSEAT TRACK 2R AT FRAME 54.2 HAS GOUGE AT SCALLOP. BLENDED GOUGED AREA AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK 2R SECTION AT AT FR 54.2 IAW SRM 51-72-10.SDR FDEA201106052123Fitting · corrodedNR2 PYLON SPIGOT RECEPTACLE FITTING HAS PITTING CORROSION ON UPPER PLATE. REMOVED NR 2 PYLON IAW AMM 54-50-00-4 REMOVED AND REPLACED UPPER AND LOWER SPIGOT FITTING IAW S/B 54-20-20 PAR. B(6) REINSTALLED NR 2 PYLON IAW AMM 54-50-00-4 COMPLIED WITH FEDEX EA 6SDR FDEA201106052121Fitting · corrodedNR 1 PYLON SPIGOT RECEPTACLE FITTING HAS PITTING CORROSION ON UPPER PLATE. REMOVED NR 1 PYLON IAW AMM 54-50-00-4. REMOVED AND REPLACED UPPER AND LOWER SPIGOT FITTINGS IAW S/B 54-2020 PARA B(6). REINSTALLED NR 1 PYLON IAW AMM 54-50-00-4. COMPLIED WITH EA-5450-SDR FDEA201106012083Seat Track · misinstalledMAIN CABIN SEAT TRACK NR 2 LT Y450 BETWEEN FRAMES 47/48 TO 49 HAS AN EXISTING REPAIR WITH INCORRECT FASTENERS INSTALLED ON TOP FLANGE. REMOVED AND REPLACED 20 EACH RIVETS AND INSTALLED 20 EACH LOCK FASTENERS ON TOP FLANGE OF SEATTRACK REPAIR BETWEEN FRAMES SDR CA110513007Bushing · seizedWHEN PERFORMING TASK 292500-16-1 (OPS CHECK OF RAT UPLOCK MECHANISM) DURING A-06 CHECK, RAM AIR TURBINE (RAT) FAILED TO DEPLOY FROM EITHER THE CAPTAINS` AND FIRST OFFICERS` RELEASE HANDLE. AFTER INVESTIGATION IT WAS FOUND THAT THE UPLOCK ROLLER ON THE RAT WAS
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