Airbus A330-243
Service difficulty reports · 5,645
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 = 'A330243' 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 = 'A330243' 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 AALA201811239007Floorbeam · corrodedCORROSION FOUND ON FLOOR SUPPORT BETWEEN FRAMES 73 - 74. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11 AND DRAWING F53478040.SDR AALA201812269007Seat Track · corrodedCORROSION ON THE SEAT TRACK, -Y1456, FRAME 33. REPAIRED THE SEAT TRACK IAW SRM 53-21-15-300-002, PAR 2A, FIG 20102.SDR AALA201812119010Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 272JF IN THE AFT GALLEY. REPLACED THE FLOOR PANEL IAW EA 286929, SRM 53-02-00-300-009, AND IRM 9701, REVISION I.SDR AALA201812119008Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 272HF, BETWEEN FRAMES 72 - 77. REPLACED THE FLOOR PANEL IAW EA 286929, SRM 53-02-00-300-009, AND IRM 9701, REVISION I.SDR AALA201812119009Floor Panel · delaminatedDELAMINATION FOUND ON FLOOR PANEL 272KF, FRAMES 72 TO 77, -YA -TC, IN THE AFT GALLEY AREA. FABRICATED AND INSTALLED A NEW FLOOR PANEL IAW EA 286929, SRM 53-02-00-300-009, AND IRM 9701, REV I.SDR AALA201812039013Floor Panel · crackedFLOOR PANEL 232KG WAS CRACKED FROM FRAMES 25 TO 29, Y-1959 TO Y2462. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-009, PARA 2, FIGURE 20109, AND IRM 9701 REV.I.SDR AALA201811289012Seat Track · corrodedCORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 31-35 IN THE PASSENGER CABIN. REPLACED THE SEAT TRACK IAW SRM 51-72-11 AND DRAWING F53275877.SDR HALA2018112656752Skin · gougedWHILE IN THE LINE IN HNL, MAINTENANCE FOUND A GOUGE ON THE INNER SKIN OF THE AFT CARGO DOOR (P/N F5237231500000) BETWEEN FR 62 AND FR 62A. WHILE ACCOMPLISHING HAL A330 SRM 52-32-00-300-008, MAINTENANCE REQUIRED FASTENER SUBSTITUTIONS SINCE THE FASTENERS REQUIRSDR AALA201812039012Seat Track · corrodedCORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 25+12 - 37.4+12. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DRAWINGS F53328090, AND F5397939.SDR AALA201811299004Seat Track · corrodedCORROSION FOUND WAS ON THE SEAT TRACK, FRAMES 26 - 37.4+9", Y1959. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DWG F53276421.SDR AALA2018112989011Seat Track · corrodedCORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 38-39.2 IN THE PASSENGER CABIN. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53311114.SDR AALA2018112639005Seat Track · corrodedCORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 31 - 35.SDR AALA201811239008Seat Track · corrodedCORROSION FOUND ON THE SEAT TRACK BETWEEN FRAMES 47 - 53.2 IN THE PASSENGER CABIN. REPLACED THE SEAT TRACK IAW SRM 51-42-11, 51-72-11, DRAWING F53325687 AND F53325686.SDR AALA201811069010Battery · no testEMERGENCY POWER SUPPLY BATTERIES AT THE L4 DOOR FAILED A CAPACITY CHECK. REPLACED THE BATTERIES IAW AMM 33-51-38. OPS CHECKED OK.SDR AALA201811069005Battery · no testEMERGENCY POWER SUPPLY BATTERIES AT THE R2 DOORSFAILED A CAPACITY CHECK. REPLACED THE BATTERIES IAW AMM 33-51-38. OPS CHECKED OK.SDR HALA2018110500365Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ON LANDING. ENG 1 AIR EXCHANGER FAULT. ENG 1 MINOR FAULT.// PERFORMED TROUBLE SHOOT PER TSM 79-20-00-810-809-A. VISUAL INSPECTED AIR OIL/HEAT EXCHANGER, NO DAMAGE FOUND. PERFORMED FADEC SYSTEM TEST PER AMM 73-21-00. SYSTEM TEST OK. SDR HALA2018110500364Sensor · dirtyETOPS SIGNIFICANT SYSTEM - COCKPIT TEMP DIFFICULT TO CONTROL WITH A FIXED TEMP SETTING,SUPPLY AIR VARIES FROM VERY COLD TO VERY HOT.// CLEANED FLIGHT DECK TEMP SENSOR AND LINE PER A330 AMM 21-63-17 PERFORMED SYSTEM TEST PER A330 AMM 21-63-00 OP CHECK NORMAL OSDR HALA2018110500362Switch · malfunctionedETOPS SIGNIFICANT SYSTEM - AT 3000' ON DESCENT APU FAILED TO START "AUTO SHUT DOWN." AFTER LANDING 2ND START ATTEMPT FAILED ALSO.// FOUND APU OUT OF SEQUENCE (APU INLET OPEN WHEN MASTER SWITCH WAS OFF) CYCLED APU FIRE P/B SWITCH TO CLOSE INLET. APU STARTED FIRSDR HALA2018112656756Skin · gougedWHILE ON THE LINE IN HNL, MAINTENANCE FOUND DAMAGE COMMON TO THE INNER SKIN OF THE AFT CARGO DOOR (P/N: F5237231500000, FTN: 4E4870). THE DAMAGE CONSISTS OF A DENTED GOUGE LOCATED BETWEEN FR 63 AND FR 63A ON THE AFT CARGO DOOR. THERE IS AN EXISTING REPAIR COMMSDR HALA2018110400322Skin · damagedDURING CARGO LOADING, CARGO LOADER REPORTED INNER SKIN DAMAGE ON AFT CARGO DOOR BETWEEN FR 61-6A AND BEAM 4-5. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER PER ER/A 572826-14 AND SRM 52-32-00-300-008.SDR HALA2018110500567Skin · damagedCARGO LOADER REPORTED INNER SKIN DAMAGE OF AFT CARGO DOOR BETWEEN FRAMES 62-62A AND BEAM 4-5. DENT IS 3" FROM FR62 & 2 7/8" FROM FR62A. APPROX 3/4" FROM BEAM 5. LENGTH APPROX 2". HEIGHT APPROX 1 1/4". DEPTH APPROX 1/8". TWO CRACKS NOTED. LENGTHS OF 7-16" FWD ASDR HALA2018110500366Oil System · lowETOPS SIGNIFICANT SYSTEM - APU LOW OIL LEVEL. SERVICED 3 QT OF APU OIL PER AMM 12-13-49. C/W VISUAL INSPECTION OF APU & NO LEAK NOTED, RAN APU & OPS CHK GOOD. OK FOR
SVC.SDR HALA2018110500363Engine · oil consumptionETOPS SIGNIFICANT SYSTEM - #2 ENGINE OIL CONSUMPTION INTAKE ABOVE AVERAGE.// OPENED #2 ENGINE COWLS PERFORMED VISUAL INSPECTION OF OIL SYSTEM FOR LEAKS. NONE NOTED. OK FOR SVC.SDR HALA2018110100559Skin · corrodedFUSELAGE EXTERIOR SKIN HAS LIGHT CORROSION AROUND 3 RIVETS IN FRAME 78 3" ABV STR 42L. CORROSION LEVEL 2, REPAIRED PER PRI 543570-14 REV 1 / ERA 543570-14 REV 0 AND 1/ ERA 543570-14 REV C.SDR HALA2018103000552Unknown · odorLOWER CREW REST SMELLS OF SMOKE, ELECTRICAL. INSPECTED CREW REST LIGHTS/CIRCUIT BREAKERS, EYEBALL VENTS, DOORWAY AND SURROUNDING AREA. NO BURNING SMELLS NOTED. OK FOR SVC.SDR HALA2018103000551Light · brokenON PARKING - ELECTRICAL SPARK FROM ABOVE CAPTAIN'S SEAT WITH AUDIO "POP" AND VISIBLE SPARK. INSPECTED FLIGHT DECK WITH VERBAL FROM CREW. FOUND BROKEN DOME LIGHT ABOVE CAPT SEAT. RELAMPED CAPT SIDE DOME LIGHTS WITH MPN 8GH004554-28 PER AIPC 33-12-08-01A ITEM 1SDR HALA2018102900550Structure · damagedLINE SVC REPORTS DAMAGE ON RH WINGLET. // RH WINGLET REPAIRED AND INSTALLED IAW AMM 57-31-22-400-801A. OK FOR SERVICE.SDR HALA2018103000553Warning System · false activationETOPS SIGNIFICANT SYSTEM - ENG 2 MINOR FAULT ECAM ON LANDING ROLLOUT. PERFORMED FIM TASK 73-21-71. NO FAULTS FOUND. MESSAGE CLEARED. OK FOR SERVICE.SDR AALA201810319001Bottle · low pressureL4 DOOR EMERGENCY DOOR ASSIST CYLINDER PRESSURE WAS LOW. THE CYLINDER WAS SERVICED IAW AMM 52-10-00-600-802A. NO LEAKS EVIDENT.SDR HALA2018102606315Sign · unsecureDOOR 3R EXIT SIGN FELL OFF. SECURED SIGN.SDR HALA2018102600547Sign · unsecure3R DOOR EXIT SIGN FELL OFF. SECURED SIGN CHECK OK.SDR HALA2018101900532Seat Track · corrodedSEAT TRACK BETWEEN FRAME 26 AND 37.4 AT -Y1959 IS CORRODED AT LOCATIONS: FR26+14", FR32+0",FR32+16", FR33+4", 37.3+0". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98. UNABLE TO FULLY REMOVE CORROSION DAMAGE OR ACCURATELY MEASURE DEPTH. DAMAGE LOCATEDSDR HALA2018101900531Track · not reportedAFT CARGO ROLLER TRAY -Y1470, C58 - 60 REQUIRES REMOVAL FOR ACCESS. ROLLER TRAY REMOVED, DAMAGED BLENDED AND ASSESSED. FOUND TO BE OUT OF LIMITS DUE TO DAMAGE LARGER THAN 25MM DIAMETER AT ZONE 1, DAMAGE ALSO WITHIN 150MM LIMIT BETWEEN BLENDS AND OUT OF LIMIT DSDR HALA2018101900530Seat Track · corrodedSEAT TRACK BETWEEN FRAME 40 AND 47 AT +Y1957 IS CORRODED AT LOCATIONS: FR41+5", FR42+17", FR44+6", FR45+18".// CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98. DAMAGE DIMENSIONS: CENTRAL AREA FR41+5?= 1" X 1" X 0.005", CENTRAL AREA FR44+6? = 2" X 0.5SDR HALA2018101800528Seat Track · corrodedSEAT TRACK BETWEEN FRAME 47 AND 53.2 AT +Y1957 IS CORRODED AT LOCATIONS: FR47+6", FR50+3", FR53.1+13". CORROSION REMOVED IAW SRM 51-74-00 REV 97. DAMAGE DIMENSION: AT FR47 + 6" AND FR50 + 3" LOCATED ON SEAT TRACK INNER VERTICAL AREAS, UNABLE TO SUFFICIENTLY RESDR HALA2018101800527Seat Track · corrodedSEAT TRACK BETWEEN FRAME 26 AND 37.4 AT +Y1959 IS CORRODED AT LOCATIONS: FR26+16", FR30+0", FR30+9", FR32+4". CORROSION REMOVED IAW SRM 51-74-00 REV 98. DAMAGE DIMENSION: AT FR26+16", FR30+0", FR30+9", FR32+4" LOCATED ON SEAT TRACK INNER VERTICAL AREAS, UNABLESDR HALA2018101800526Roller Tray · corrodedBULK CARGO ROLLER TRAY FR65 TO FR68 +Y301 HAS CORROSION EVIDENT. ROLLER TRAY REMOVED IAW MM 25-51-21 R61.05 IAW CMM 25-51-83 REV4. CORROSION ON FLANGE BLENDED AROUND FASTENER HOLES. BLEND EXCEEDS ALLOWABLE LIMITS. EVIDENCE OF (LEVEL 2) CORROSION STILL PRESENT SDR HALA2018101800525Seat Track · corrodedSEAT TRACK BETWEEN FRAME 26 AND 37.4 AT -Y1959 IS CORRODED AT LOCATIONS: FR26+14", FR32+0",FR32+16", FR33+4", 37.3+0". CORROSION REMOVED PER SRM 51-74-00 REV 98. UNABLE TO FULLY REMOVE CORROSION DAMAGE OR ACCURATELY MEASURE DEPTH. DAMAGE LOCATED AT -Y1959 FR26SDR HALA2018101800524Not Reported · faultedETOPS SIGNIFICANT SYSTEM. ENG 2 MINOR FAULT. T/S PER TSM 73-21-71-810-952-A. PERFORMED GROUND REPORT NO FAULTS NOTED. OK TO CONTINUE.SDR AALA2018101879012Ballast · burnedFUMES AT AFT CABIN (ROWS 25-30) LEFT. ODOR INTERMITTENT, OCCURING ROUGHLY EVERY 10 MINUTES. THE AIRCRAFT WAS GROUNDED. TROUBLESHOT IAW CAR 33L00021001, FOUND NO ODOR COMING FROM ENGINE BLEED OR PACK SYSTEM. DID FIND FAULTY LIGHT BALLAST AT ROW 30 CEILING. SDR HALA2018101700513Heater · odorON CLIMB FLIGHT ATTENDANTS SMELLED ELECTRICAL ODOR TURNED OFF FLOOR HEATERS DISSIPATED IN FEW MINS. VERIFIED 2L FLOOR HEATER CAUSING ELECTRICAL BURNING SMELL OK TO CONTINUE PER MEL. MAINTENANCE PROCEDURES C/W, PLACARD INSTALLED, LIDS UPDATED. C/B H07 PULLED ANSDR HALA2018101700512Fmu · leakingETOPS SIGNIFICANT SYSTEM, ENG NR 2 LEAKING FUEL FROM DRAIN MAST WHILE AT IDLE. REMOVED AND REPLACED NR 2 ENG FMU PER AMM 73-21-52-000-802-A AND 73-21-52-400-802-A. OK FOR SVC.SDR HALA2018101700511Hf Comm · malfunctionedETOPS SIGNIFICANT SYSTEM, NR 2 HF WON'T TUNE. RESET HF2 ON 722VU. OPS CHK OKAY.SDR HALA2018101700506Angle · corrodedSUSPECT CORROSION LOCATED AFT OF DOOR 4L ON FLOOR "Z" ANGLE 6" AFT OF FRAME 75 AS MARKED. CORROSION REMOVED FROM "Z" ANGLE 6" AFT OF FRAME 75 IAW SRM 51-74-00 REV 97. DAMAGE DIMENSION: 2.5"L X 1.5"W X MAX DEPTH 0.045". DEPTH GAUGE USED P/N: 2417 S/N: IRFE5005ASDR HALA2018101700505Angle · corrodedSUSPECT CORROSION (2 OFF) LOCATIONS AFT OF DOOR 4R AT FLOOR LEVEL 6" AFT OF FRAME 75 AS MARKED. CORROSION REMOVED IAW SRM 51-74-00 PARA 6 A. THRU 6 B.(3) REV 98.00. REMAINING THICKNESS ESTABLISHED ON Z ANGLE IAW SRM 51-74-00 PARA 6B. (6) REV 98.00 FOR BLENDED SDR HALA2018101700510Seat Track · corrodedSEAT TRACK BETWEEN FRAME 31 AND 35 AT -Y1552.5 IS CORRODED AT LOCATIONS: FR32+18.5", FR33+3". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98. UNABLE TO FULLY REMOVE CORROSION DAMAGE OR ACCURATELY MEASURE DEPTH. DAMAGE LOCATIONS -Y1552.5 FR32+18.5 & FSDR HALA2018101700509Seat Track · corrodedSEAT TRACK BETWEEN FRAME 26 AND 37.4 AT +Y2462 IS CORRODED AT LOCATIONS: FR26+15", FR30+10", FR31+3", FR32+5", FR35+7". CORROSION REMOVED IAW SRM 51-74-00 REV 98. DAMAGE DIMENSION: AT FR26+15", FR30+10", FR31+3", FR32+5", FR35+7" LOCATED ON SEAT TRACK INNER VESDR HALA2018101700507Seat Track · corrodedSEAT TRACK BETWEEN FRAME 40 AND 47 AT -Y450 IS CORRODED AT LOCATIONS: FR40.1+16", FR41+0", FR41+12", FR46+8". CORROSION REMOVED IAW SRM 51-74-00 REV 98. DAMAGE DIMENSION: FR40.1 + 16", FR41 + 0", FR41 + 12" AND FR46 + 8. LOCATED ON SEAT TRACK INNER VERTICAL ARSDR HALA2018101700508Seat Track · corrodedSEAT TRACK BETWEEN FRAME 40 AND 47 AT -Y1959 IS CORRODED AT LOCATIONS: FR40.3+0", FR41+3", FR41+4", FR42+16", FR45+5". CORROSION REMOVED PER SRM 51-74-00 REV 98. UNABLE TO FULLY REMOVE CORROSION DAMAGE OR ACCURATELY MEASURE DEPTH. DAMAGE LOCATED AT FR40.3, FR4SDR HALA2018101600503Warning System · false activationETOPS SIGNIFICANT SYSTEM - ENG 1 MINOR FAULT ON LANDING. PERFORMED EEC 1 BIT TEST PER AMM 73-21-00-710-812-A. NO FAULTS NOTED. GROUND SCANNING GOOD. NO HISTORY WITHIN LAS 15 FLIGHT DAYS. OK FOR SERVICE.
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