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 HALA2019031201614Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN 25.5-37.4, -Y1456 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11. LP 0980971SDR HALA2019031201613Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN 25.5-37.4, -Y2462 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53276421. LP 0980924SDR HALA2019031300122Fuel Line · chafedETOPS SIGNIFICANT SYSTEM - NR 1 ENGINE FUEL LINE FROM HEAT EX-CHANGER CHAFED THRU, LEAKING. REMOVED AND REPLACED FUEL LINE AT HEAT EX-CHANGER IAW AMM 73-11. IDLE RUN LEAK CHECK GOOD.SDR HALA2019031200121Seat Track · corrodedSEAT TRACK BETWEEN FRAME 25 AND 37.4 AT -Y2462 IS CORRODED AT LOCATIONS: 26+16, 29+11, 30+9, 31+7, 32+3, 35+17, 37.1+17. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: 1. FR26+16 CENTRAL L=1.0" W=0.4" D=0.023" IVA UNABLE TO SUFSDR HALA2019031200120Structure · corrodedVERTICAL STAB TRAILING EDGE RHS #2 T CHORD SUSPECT CORROSION AROUND FASTENER HOLES. REMOVAL OF CORROSION C/OUT IAW SRM 51-74-00 REV.98.01. CORROSION STILL EVIDENT IAW NTM 51-10-02-221-001-A REV. 96 AT BLEND DEPTH OF .058". BLEND DEPTH BEYOND 50% MATERIAL THICKSDR HALA2019031200119Structure · corrodedVERTICAL STAB TRAILING EDGE RHS #3 T CHORD SUSPECT CORROSION AROUND FASTENER HOLES. // REMOVAL OF CORROSION C/OUT IAW SRM 51-74-00 REV.98.01. CORROSION STILL EVIDENT IAW NTM 51-10-02-221-001-A REV. 96 AT BLEND DEPTH OF .058". BLEND DEPTH BEYOND 50% MATERIAL THSDR HALA2019031100090Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 40-47, -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F5711057120401. LP 0979474SDR HALA2019031100089Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 25.5-37.4, +Y953 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53276421. LP 0979153SDR HALA2019031200116Seat Track · corrodedSEAT TRACK BETWEEN FRAME 40 AND 47 AT -Y1959 IS CORRODED AT LOCATIONS: FR43, FR44, FR46, FR47. CORROSION REMOVED FROM SEAT TRACK @ FR43, FR44, FR46, FR47 IAW SRM 51-74-00 REV 98.01. DAMAGE DIMENSION: AT FR43 CENTRAL RE-WORK L: 4.5" W: 0.75" D: 0.030", FR44 CENSDR HALA2019031200115Seat Track · corrodedSEAT TRACK BETWEEN FRAME 25.5 AND 37.4 AT +Y953 IS CORRODED AT LOCATIONS: 26, 26+3, 26+8, 26+6, 29+10, 29+15, 29+20, 30+2, 32+13. // CORROSION REMOVED AS SRM 51-71-00 REV 98.01. DAMAGE DIMENSIONS: 1. FR 26"" SUPERIOR L=1.5" W=0.50" DEPTH= 0.030", 2. FR 26 +3"SDR AALA201903129015Valve · burnedFLIGHT CREW REPORTED A CABIN ODOR. THE AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND THE TRIM AIR VALVE BURNED AND HAS SOME CORROSION. DETERMINED THAT IT WAS THE CAUSE OF THE EVENT. REMOVED AND REPLACED THE TRIM AIR VALVE AND NO FURTHER ODORS WERE NOTED.SDR AALA2019031219008Connector · unlockedMAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT AFT OF THE L2 DOOR WAS INOPERATIVE. FOUND GALLEY MODULE WITH AN ELECTRICAL CONNECTOR NOT LOCKED. SECURED THE CONNECTOR AND VERIFIED LOCKED. OPS TESTED OKAY IAW AMM 31-51-00-501.SDR HALA2019031200118Seat Track · corrodedSEAT TRACK BETWEEN FRAME 25.5 AND 37.4 AT -Y1456 IS CORRODED AT LOCATIONS: 33 AND 35. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR 33: L=1.300" W=0.350" D=0.022", FR 35: L=2.00" W=0.650" D=0.038". GAUGE PN: 2417S, SN: VUDSDR HALA2019031300118Seat Track · corrodedSEAT TRACK BETWEEN FRAME 40 AND 47 AT -Y450 IS CORRODED AT LOCATIONS: FR44, FR45, FR46. CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: 1. FR44 CENTRAL REWORK L: 3.5" W: 0.75" D: 0.032", 2. FR45 CENTRAL REWORK L: 5.5" W: 0.75" D: 0.022", 3.SDR HALA2019031200117Seat Track · corrodedSEAT TRACK NR 8 BETWEEN FRAME 40 AND 47 AT -Y450, P/N F57112436201 REQ'S FABRICATING. SEAT TRACK ASSEMBLY P/N F5711243620100 UNABLE TO BE PROCURED DURING THIS MAINTENANCE CHECK. SEAT TRACK ASSEMBLY CONSIDERED TO BE A CATEGORY 3 PART. SEAT TRACK FABRICATED AS PSDR HALA2019030800108Warning System · false activationETOPS SIGNIFICANT SYSTEM - ENG 2 REV FAULT AFTER LANDING. CYCLED NR 2 T/R 3 TIMES PER AMM 78-31-00. MSG CLEARED AFTER THE
FIRST. INSPECTED T/R. NO DEFECTS NOTED. OK FOR SVC.SDR HALA2019030700107Seat Track · corrodedSEAT TRACK BETWEEN FRAME 18 AND 25.5 AT +Y953 IS CORRODED AT LOCATIONS: 19+10, 22+17, 24+18. CORROSION REMOVED IAW SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: 1. FR 18 +2" SUPERIOR L=1.0" W=0.50" DEPTH= 0.022", 2. FR 19 + 10" SUPERIOR L=1.0" W=0.50" DEPTH=0.04SDR HALA2019030700106Support Angle · corrodedDOOR 1R FLOOR SUPPORT STRUCTURE FWD LWR SUPPORT ANGLE @ FR13A Y-2061 IS CORRODED WHERE INDICATED. CORROSION DAMAGE DIMENSIONS: L=0.300" W=0.500" DEPTH=0.020". DEPTH GAUGE USED P/N: 2417 S/N: IRFE5005A9EQ. UNABLE TO FIND SRM LIMITS FOR THIS COMPONENT. RII CARRISDR HALA2019030700105Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 54 AT +Y1959 IS CORRODED AT LOCATIONS: FR53.3, FR53.5+10". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR53.3 CENTRAL REWORK L: 4.5" W: 0.75" D: 0.052", FR53.5(+10") SUPERIOR REWORK L: 3" W:SDR HALA2019030700104Seat Track · corrodedSEAT TRACK BETWEEN FRAME 47 AND 53.2 AT +Y1959 IS CORRODED AT LOCATIONS: FR47+6", FR48+16", FR51+14" AND FR53.1+14". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR47(+6") INNER VERTICAL L: 1" W: 0.2" D:0.020", FR48(+16") CENSDR HALA2019030800109Warning System · false activationETOPS SIGNIFICANT SYSTEM - ON CLIMB ECAM "A. ICE INR WING HIPR LEFT " ON BLEED PAGE AMBER " ANTI ICE AND AMBER TRIANGLE INNER LEFT POSITION. PERFORMED WING ANTI ICE OPS TEST PER AMM 30-11-00-710-801. TEST OK.SDR HALA2019030700102Warning System · false activationETOPS SIGNIFICANT SYSTEM - DURING CRUISE "FUEL OUTER TO INNER FAULT" CAUTION CAME ON. INITIATED MANUAL XFR PER ECAM. FUEL TRANSFER SUCCESSFUL. WITH PFR & TSM 28-26-00 PERFORMED AMM 28-51-00, OPS CHKS OF X-FER VALVE 601QL2 (FIN). ALL OPS CHK FOLLOWED COMMANDESDR HALA2019030700101Sign · unsecure3 L DOOR EXIT SIGN FELL OFF. A/C OK. RE-SECURED 3L DOOR EXIT SIGN LENS. OPS CHECK OK.SDR HALA2019030600099Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 54 AT -Y2462 IS CORRODED AT LOCATIONS: FR53.3. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: (1) FR53.3 SUPERIOR REWORK L: 1.25" W: 0.5" D: 0.035"DEPTH GAUGE USED P/N: 2417 S/N: IRFE5005A9EQ. SDR HALA2019030600098Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 53.4 AT -Y450 IS CORRODED AT LOCATIONS: FR53.2+8" AND FR53.4. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: (1) FR53.2(+8") CENTRAL REWORK L: 1" W: 0.75" D: 0.022"(2) FR53.4 CENTRAL REWORK L: SDR HALA2019030600097Seat Track · corrodedSEAT TRACK NR 7 BETWEEN FRAME 31 AND 35 AT +Y1552 IS CORRODED AT LOCATIONS: 33+4. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR33+4? L=1.250", W=1.0 ", D+.044". DEPTH GAUGE USED P/N: 2417 S/N: IRFE5005A9EQ. DAMAGE ASSESSED SDR HALA2019030600096Seat Track · corrodedSEAT TRACK BETWEEN FRAME 25 AND 337.4 AT +Y1456 IS CORRODED AT LOCATIONS: 35+17. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR35+17 SUPERIOR L=2.0", W=0.5", D+.030" & OUTER VERTICAL WALL DEPTH = .050". ASSESSED AS OUTSIDE OSDR HALA2019030600095Seat Track · corrodedSEAT TRACK BETWEEN FRAME 25+5 AND 37.4 AT +Y1959 IS CORRODED AT LOCATIONS: 33.1. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: DAMAGE DIMENSION AT LOCATION FRAME 33 + 1" SUPERIOR L = 1.5" W = 0.5" D = .040". IVA UNABLE TO SUFSDR HALA2019030600094Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 54 AT -Y1959 IS CORRODED AT LOCATIONS: FR53.3, FR53.5+9" AND FR53.9+12". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR53.3 SUPERIOR REWORK L: 2" W: 1" D: 0.040", FR53.5(+9") INNER VERTICAL SDR ANCF2019030502Acm · damagedMAR 5. DURING FINAL APP TOUCH DOWN AND TAXI, SMOKE WAS PRESENTED INSIDE PAX CABIN DETECTED BY F/A MODERATE SMOKE. CORRECTIVE ACTIONS: MAR 5. IAW TSM 24-00-00-810-947-A ELECTRICAL BURNING SMELL OR FUMES FOUND IN THE CABIN COCKPIT CARGO OR AVIONICS COMPARTMENT ASDR HALA2019030600093Cids · malfunctionedEMERGENCY LIGHT SIGNS @ 1L AND 2R ON THROUGHOUT FLIGHT. REBOOTED CIDS1+2 AND CHECKED EMERGENCY LIGHT SYSTEM AS PER AMM 33-50 FOUND NORMAL. AC OK FOR SVC.SDR HALA2019030600092Warning System · false activationETOPS SIGNIFICANT SYSTEM - ENG 2 OIL CHIP DETECTED CAME ON AT TOUCHDOWN. GROUND CHECKED NR 2 ENG CHIP DETECT NO METAL NOTED. EMCD TEST OK. REF: TSM 79-20-00. CHECK OK FOR SVC.SDR HALA2019030600091Unknown · malfunctionedETOPS SIGNIFICANT SYSTEM - APU FAULT ON START ATTEMPTS, 2 ATTEMPTS TO START MADE. T/S PER TSM 49-00-00-810-829-A REF POST FLIGHT REPORT "IGNITER PLUG(59KA31)/IGNITION EXCITER (59KA10)" PERFORMED APU TEST, TESTED OK. PERFORMED OPS TEST AMM 49-00. APU STARTED NOSDR HALA2019030600090Blade · damagedETOPS SIGNIFICANT SYSTEM - FOUND DAMAGE ON NR 15 COMPRESSOR BLADE ON NR 2 ENG. 5 INCHES FROM BLADE TIP DENT DIMENSION X AT .162 INCH DIMENSION Y .094 DIMENSION Z 1.04 INCH. FOUND DIM X=.162 DIM Y=.094 DIM Z= 1.04. FOUND TO BE OUT OF LIMITS PER AMM 72-31-41-000SDR HALA2019030600089Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 54 AT -Y2462 IS CORRODED AT LOCATIONS: FR53.3. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: (1) FR53.3 SUPERIOR REWORK L: 1.25" W: 0.5" D: 0.035"DEPTH GAUGE USED P/N: 2417 S/N: IRFE5005A9EQ. SDR HALA2019030600088Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 53.4 AT -Y450 IS CORRODED AT LOCATIONS: FR53.2+8" AND FR53.4. // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: (1) FR53.2(+8") CENTRAL REWORK L: 1" W: 0.75" D: 0.022"(2) FR53.4 CENTRAL REWORK SDR HALA2019030400084Unknown · odorINBOUND CABIN CREW REPORTED WET SOCK-ACRID ODOR ON TAXI-TAKEOFF-CLIMB. ODOR DISSIPATED BUT RETURNED AGAIN DURING DESCENT. PERFORMED TSM 71-00-81 - OPERATED ENG 1 & 2 INDEPENDENTLY - ISOLATED PACKS 1 & 2 DURING ENGINE RUNS - APU ISOLATED - NO ODORS NOTED - OK SDR HALA2019030100080Warning System · false activationETOPS SIGNIFICANT SYSTEM - ON SHORT FINAL FUEL L STBY PUMP LO PRES ECAM. NO FAULTS NOTED SYSTEM 1 & 2. NO CLASS 3 MESSAGES. PERFORMED FCMC SYSTEM TEST. FCMC 1 SYSTEM TEST OK. FCMC 2 SYSTEM TEST OK. OPERATED L STBY PUMP. OPS NORMAL. NO LOW PRESS INDICATION.SDR HALA2019030100079Unknown · malfunctionedEMERG EXIT LIGHTS CAME ON WITH SWITCH IN OFF. CIDS 1 & 2 RESET CARRIED OUT. EPSU SYSTEM TEST CARRIED OUT OK. SUBSEQUENT OPS CHECKED NORMAL AS PER AMM 23-73-00.SDR HALA2019030100078Warning System · false activationSMOKE LAVATORY DET FAULT IN LAV 35 BY 2L DOOR. PERFORMED BITE OF CIDS SDF. TEST OK. NO FAULTS NOTED.SDR AALA2019030419002Unknown · odorFLIGHT CREW REPORTED A FUME EVENT SHORTLY AFTER TAKEOFF, STRONG ODOR OF DIRTY SOCKS. RETURNED TO DEPARTURE. THE AIRCRAFT WAS GROUNDED. PERFORMED CARDS 33L00021002, 33L00021001, 33L00071001, 33L20021002, AND EA 290664. ACCOMPLISHED TSM 71-00-81-812-805-ASDR AALA2019030489013Apu · odorDURING DESCENT, EXPERIENCED A FUME EVENT. DIRTY SOCK, MUSTY, OIL ODOR IN THE COCKPIT, CONTINUED DESCENT THRU 16,000 FT, IDLE POWER AND WING ANTI-ICE ON, OIL QUANTITY 17 QTS. FUMES SEEMED TO CONTINUE THRU ENGINE SHUTDOWN. MAINTENANCE TRACKED THE SOURCESDR HALA2019022800075Cids · malfunctionedEMERGENCY EXIT LIGHTS CAME ON WITH SWITCH IN OFF. CIDS 1 & 2 RESET CARRIED OUT. EPSU SYSTEM TEST CARRIED OUT OK.
SUBSEQUENT OPS CHECKED NORMAL AS PER AMM 23-73-00.SDR HALA2019022760049Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 25-37, -Y450 FOUND CORRODED. REPLACED SEAT TRACK. LP 0960057SDR HALA2019022700073Seat Track · corrodedSEAT TRACK BETWEEN FRAME 25 AND 37.4 AT -Y450 IS CORRODED AT LOCATIONS: 31+19, 31+11, 32+14, 34+1, 37.3+13. // CORROSION REMOVED FROM SEAT TRACK BY
GRINDING AT LOCATION ?Y450 FR31+19?, FR 31+11?, FR 32+14?, FR 34+1?,FR 37.3+13? IAW A330 SRM 51-74-00 PASDR AALA201902269016Unknown · odorCREW REPORTED AN ODOR IN THE CABIN AND COCKPIT. RETURNED TO DEPARTURE. AN EMERGENCY WAS DECLARED AND LANDED W ITHOUT INCIDENT. TROUBLESHOT IAW JOB CARDS 33L00021001, 33L00071001 RIGHT ENGINE, 33L20021002 RIGHT ENGINE, NO FINDINGS.SDR HALA2019022750050Sign · detachedDOOR 3L EXIT SIGN FELL OFF. RE-SECURED DOOR 3L EXIT SIGN. LP 3224359SDR HALA2019022500064Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ENG 2 REV FAULT- DURING LANDING. UPON ARRIVAL AT A/C FAULT NOT PRESENT. NO FAULTS PRESENT ON GROUND SCAN. PREV FLIGHT FAULTS DISPLAYED FAULT CODE 783113 TR STOW SW. T/S PER A330 TSM 78-30-00-810-874-A. T/R DEPLOYED & STOWED NORMALSDR HALA2019022500067Warning System · false activationOPEN - ETOPS SIGNIFICANT SYSTEM - ENG 2 OIL CHIP DETECTED ECAM ILLUMINATED AFTER ENG 2 SHUTDOWN. PER TSM 79-20-00-810-824 INSPECTED OIL CHIP DETECTOR ON NR 2 ENGINE. NO DEBRIS NOTED. CLEARED PER AMM 79-22-46-100-802. FUNCTIONAL CHECK OF EMCD. AMM 79-22-46-720-SDR HALA2019022500068Controller · malfunctionedOPEN - ETOPS SIGNIFICANT SYSTEM - FLIGHT DECK TEMP DIFFICULT TO CONTROL EITHER TO HOT OR TOO COLD. ZONE TEMP INDICATION OVERSHOOTS TO HIGH OR LOW. COCKPIT ZONE TEMP ROTARY SELECTOR, DOES NOT SEEM TO RESPOND IN THE MID RANGE 12 O'CLOCK POSITION. RESET PACK CONT
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