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 HALA2019040412193Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 53.2-54.5, +Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53326941. LP 1010890SDR HALA2019040320159Seat Track · corrodedSEAT TRACK #19 BETWEEN FRAME 53.2 AND 54.5 AT +Y1959 IS CORRODED AT LOCATIONS: FR53.2+6", FR53.2+7.5", FR53.3+2", FR53.5+11",
FR53.6+15", FR53.7+2" FAULT DESCRIPTION: SEAT TRACK BETWEEN FRAME 53.2 AND 54.5 AT +Y1959 IS CORRODED AT LOCATIONS: FR53.2+6",
FRSDR HALA2019040320158Seat Track · corrodedSEAT TRACK #20 BETWEEN FRAME 53.2 AND 54.5 AT +Y2462 IS CORRODED AT LOCATIONS: FR53.3+3", FR53.3+13", FR53.2 FAULT DESCRIPTION: SEAT TRACK BETWEEN FRAME
53.2 AND 54.5 AT +Y2462 IS CORRODED AT LOCATIONS: FR53.3+3", FR53.3+13", FR53.2. // CORROSION REMOVED ASSDR HALA2019040320157Seat Track · corrodedSEAT TRACK BETWEEN FRAME 62 AND 71 AT -Y1959 IS CORRODED AT LOCATIONS: FR62+12", FR63+11", FR64+2", FR64+18". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01.
DAMAGE DIMENSIONS: FR62+12", FR63+11", FR64+2", FR64+18". CORROSION LOCATED ON ISDR HALA2019040320156Seat Track · corrodedSEAT TRACK BETWEEN FRAME 40 AND 47 AT -Y1959 IS CORRODED AT LOCATIONS: FR46-3". // CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. DAMAGE
DIMENSIONS: FR46-3? L=0.500? W=0.125? EPTH=0.097?. VERNIER CALIPER USED P/N: 505-717 S/N: ITWA17491. ASSESSED ASDR HALA2019040320155Seat Track · corrodedSEAT TRACK BETWEEN FRAME 58 AND 67 AT +Y450 IS CORRODED AT LOCATIONS: FR58+9", FR59+6", FR59+7", FR59+20". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01.
DAMAGE DIMENSIONS: FR58+9", FR59+6", FR59+7", FR59+20". CORROSION LOCATED ON INNER VSDR HALA2019040320154Seat Track · corrodedSEAT TRACK BETWEEN FRAME 58 AND 62 AT -Y1959 IS CORRODED AT LOCATIONS: FR60+10", FR61, FR61+20". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01.
DAMAGE DIMENSIONS: FR60+10" SUPERIOR L=2.0" W=0.750" DEPTH= 0.020", FR61 AND FR61+20" CORROSIOSDR HALA2019040100160Generator · faultedETOPS SIGNIFICANT SYSTEM - APU GEN FAULT. // PERFORMED TSM 24-20-81-810-942-A. REMOVED AND REPLACED APU GEN
PER AMM 24-23-51. OPS NORMAL, NO DEFECTS NOTED. LEAK CHECK OK. OK FOR SVC.SDR HALA2019040412151Sign · brokenDOOR 3R EXIT SIGN TAB BROKEN. REPLACED DOOR 3R OVERHEAD EXIT SIGN LENS. LP 5849813SDR HALA201904043170Oil System · lowETOPS SIGNIFICANT SYSTEM - AFTER STARTING APU OBSERVED LOW OIL LEVEL ECAM. SERVICED APU AS REQUIRED 4 QTS ADDED,APU LOW OIL LEVEL LIGHT EXTINGUISHED. AIRCRAFT OKAY TO CONTINUE.SDR HALA2019032801964Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 40-47, -Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F57112821. LP 1005208SDR HALA2019032800149Seat Track · corrodedSEAT TRACK BETWEEN FRAME 40 AND 47 AT -Y450 IS CORRODED AT LOCATIONS: FR40+2";FR40.3+1"FR45. CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR40+2" INNER VERTICAL: D-0.080" X L-0.400" W-0.120", FR40.3 + 1" O/B LATERAL: D-0.090 X L-1.400: XSDR HALA2019032601924Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 37.4-39.2, -Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53311114. LP 1002038SDR HALA2019032601923Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 53.2-79.3, FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53275878. LP 1002036SDR HALA2019032601922Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 31-35, -Y1552 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53275878. LP 1002031SDR HALA2019032601921Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 26-37.4, +Y1456 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND DRAWING F53276421. LP 1002025SDR HALA2019032600148Seat Track · corrodedSEAT TRACK BETWEEN FRAME 26 AND 37.4 AT +Y1456 IS CORRODED AT LOCATIONS: FR36. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR36 SUPERIOR REWORK L: 3" W: 0.3" D: 0.115" DIAL INDICATOR P/N 2417 S/N IRFE5005A9EQ. ASSESSED AS OUSDR HALA2019032600147Seat Track · corrodedSEAT TRACK BETWEEN FRAME 31 AND 35 AT -Y1552 IS CORRODED AT LOCATIONS: FR32+17", FR33+4". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS: FR32(+17") SUPERIOR REWORK L: 3.5" W: 0.3" D:0.045", FR33(+4") CENTRAL REWORK L: 3.5" W: 0SDR AALA201903269006Bottle · low pressureL1 DOOR ASSIST BOTTLE HAD LOW PRESSURE. THE AIRCRAFT WAS GROUNDED. MAINTENANCE SERVICED THE DOOR ASSIST BOTTLE IAW AMM 52-10-00-600-801A, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.SDR AALA201903259021Bottle · low pressureCIDS PANEL DISPLAYED THE L1 DOOR LOW PRESSURE. THE AIRCRAFT WAS GROUNDED. MAINTENANCE SERVICED THE DOOR ASSIST BOTTLE IAW JC 33C80052002, AND PERFORMED A SATISACTORY OPERATIONAL CHECK.SDR AALA201903259020Bottle · low pressureCIDS PANEL DISPLAYED THE L1 DOOR HAD LOW PRESSURE. THE AIRCRAFT WAS GROUDNED. MAINTENANCE SERVICED THE L1 DOOR ASSIST BOTTLE IAW JC 33C80052002, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.SDR CA190325011Interface Unit · faulted(CAN) L/G GEAR NOT DOWN LOCKED WARNING IN FINAL APPROACH WITHOUT GREEN TRIANGLE ON LDG GEAR PANEL. LDG GEAR GRAVITY EXTENSION PROCEDURE EXECUTED ACCORDING TO ECAM AND QRH. LANDING GEAR SET TO NORMAL EXTENSION SYSTEM AFTER FREE FALL DURING FLT IAW A,, 32-00-00-SDR HALA2019032500145Oil System · lowETOPS SIGNIFICANT SYSTEM - APU OIL LEVEL LOW. SERVICED APU PER AMM 12-13-49, 1 QT. CHECKS GOOD, OK FOR SERVICE.SDR HALA2019032500144Fcu · faultedETOPS SIGNIFICANT SYSTEM - ECAM AUTO FLT FCU FAULT- BARO REF CHECK ILLUMINATED AT FL230 IN LEVEL FLIGHT. POST FLT REPORT SHOWS AUTO FLT FCU FAULT & FCU (3CA) CLASS 1 FAULT. T/S PER TSM 22-81-00-810*801A. PERF AFS SYS TEST. TEST OK. OK FOR SVC.SDR AALA201903259031Sensor · inoperativeAN ECAM BLEED PAGE NR 2 PACK OUTLET TEMPERATURE INDICATION INOPERATIVE. SD PAGE INDICATE XX. AFTER TAKEOFF, THE NR 2 PACK SHUTDOWN AGAIN. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. THE AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE RIGHT PSDR HALA2019032200140Warning System · false activationETOPS SIGNIFICANT SYSTEM - ECAM AUTO FLT FCU FAULT- BARO REF CHECK ILLUMINATED AT FL230 IN LEVEL FLIGHT. POST FLT REPORT SHOWS AUTO FLT FCU FAULT & FCU (3CA) CLASS 1 FAULT. T/S PER TSM 22-81-00-810*801A. PERFORMED AFS SYSTEM TEST. TEST OK. OK FOR SERVICE. NO 3SDR HALA2019032200139Unknown · malfunctionedETOPS SIGNIFICANT SYSTEM - HF NR 1 NO TRANSMIT. PULLED AND RESET HF1 C/B AND OPERATION RETURNED TO NORMAL. OK FOR SERVICE. NO PROMPTS WERE AVAILABLE TO PERFORM BITE TEST. AFTER RESETTING THE C/B THE PROMPTS RETURNED AND SYSTEM OPS CHECKED NORMAL.SDR HALA2019032200138Warning System · false activationETOPS SIGNIFICANT SYSTEM - FUEL T TANK XFR- FAULT. T/S PER TSM 28-27-00-810-828-A PERFORMED A BITE OF FCMC 1 AND FCMC 2 PER AMM 28-51-00-700-801-A BOTH TESTS PASSED, NO CURRENT FAULTS. AC OK FOR SVC.SDR AALA201903259007Seat Track · corrodedCORROSION FOUND ON THE SEAT TRACK AT FRAME 37, +Y1959. REPLACED THE SEAT TRACK IAW SRM 53-21-15.SDR AALA201903259006Seat Track · corrodedCORROSION FOUND ON THE SEAT TRACK AT FRAME 37, +Y1959. REPLACED THE SEAT TRACK IAW SRM 53-21-15.SDR HALA2019032100091Not Reported · missingFLOOR LIGHT STRIP IN AFT GALLEY IS MISSING PARTS. REPLACED EMERGENCY LIGHT STRIP IN AFT GALLEY. LP 5847373SDR AALA2019040490003Engine · odorTHERE WAS AN ODOR STILL NOTICABLE DURING CLIMB, CRUISE WAS FINE, ALSO NOTICED INTERMINAL AREA FOR APPROACH. NOT ABLE TO ISOLATE TO EITHER PACK. THE AIRCRAFT WAS GROUNDED. MAINENANCE REMOVED AND REPLACED THE NR 1 ENGINE IAW JC 33L40071003.SDR HALA2019031901820Tire · defectiveAIRCRAFT 379 ATO - ABORTED TAKEOFF AT 90-100 KNOTS DUE TO SEVERE NOSE GEAR VIBRATION. CORRECTIVE ACTION: REPLACED LEFT AND RIGHT NOSE TIRES, AND LUBED NOSE GEAR LOWER AREAS. LP 5875735SDR HALA2019031900137Tire · defectiveATO - SEVERE NOSE GEAR VIBRATION. BEGAN APPROX 60 KNOTS. AGGRESSIVELY WORSE W/SPEED. RTO @ 90-100 KTS. T/S IAW TSM 32-20-00-810-801-A DUE TO RTO & RTB. FOUND A HOP ON LT NLG TIRE AFTER JACKING AND SPINNING WHEELS. REMOVED & REPLACED LT & RT NLG TIRE ASSY IAW ASDR HALA2019031800131Line · unsecureETOPS SIGNIFICANT SYSTEM - DURING PDC, FOUND HP/IP BEARING OIL LINE LEAKING. SERVICED NR 2 ENGINE PER AMM 12-13-79, ACCOMPLISHED ENGINE IDLE RUN 5 MINS. RE-SECURED HP-IP OIL LINE PER CMM/EM 72-10-51. NO LEAKS NOTED EXTERNALLY AROUND AREA. AFTER ENGINE RUN NOTESDR ANCF2019031701Hydraulic System · low pressureGREEN HYDRAULIC SYSTEM LO PRESS DURING LANDING. PENDING CORRECTIVE ACTIONS.SDR HALA2019031800135Warning System · false activationETOPS SIGNIFICANT SYSTEM - AFTER STARTING NR 2 ENG ECAM ENG2 OVSP PROT FAULT, ENGINE PARAMETERS NORMAL. MAINT CONTROL TOLD US TO SHUT DOWN ENG 2 AND RESTART. AFTER RESTART NO ECAM OR FURTHER MESSAGE ALL INDICATIONS NORMAL. SYSTEM TEST OF EEC 2 OK NO FAULTS NOTSDR HALA2019031800133Warning System · false activationETOPS SIGNIFICANT SYSTEM - AFTER TAKEOFF ENGINE ONE BLEED FAULT. RESET ENG 1 BLEED, OPS NORMAL. PERFORMED BMC 1 BITE PER AMM 36-11-00-740-804-A. BITE PASS, NO DEFECTS NOTED. OK FOR SVC.SDR HALA2019031800132Warning System · false activationETOPS SIGNIFICANT SYSTEM - ON CLIMB ECAM "FUEL T TANK XFR FAULT". FUEL AFT XFR VALVE 1 CLASS 1 FAULT IN PFR & PER TSM 28-
27-00. PERFORMED VLV TEST & TEST OK. NO ECAM MSG NOTED. A/C OK FOR SVC.SDR HALA2019031800134Warning System · false activationETOPS SIGNIFICANT SYSTEM - FUEL RIGHT PUMP 2 LO PR PER ECAM. TURNED OFF RIGHT 2 PUMP. TROUBLE SHOOT PER TSM 28-21-00-810-852-A NO C/B TRIPPED, FCMC LAST LEG NO FAULT FOUND, PERFORMED GROUND FUEL TRANSFER WITH RIGHT 2 PUMP PER AMM 28-21-00-710-801, FUEL TRANSSDR HALA2019031800130Actuator · failedETOPS SIGNIFICANT SYSTEM - DURING FUEL ECAM "FUEL T TANK XFR FAULT". FUEL VALVES TEST SHOWS OUTER TANK INLET VALVE 1 FAILED OPEN. REMOVED AND REPLACED INLET VALVE ACTUATOR PER AMM 28-25-57-400-801-A. OPS CHECK OK.SDR HALA2019031800129Computer · malfunctionedATB - ETOPS SIGNIFICANT SYSTEM - AUTO FLT AUTO THRUST OFF DURING CLIMB OUT. AUTO THRUST WAS ACTUALLY WORKING THOUGHT FOLLOWED PROCEDURES - ALL MESSAGES (STATUS ETC) WENT AWAY. CONTINUED FLT, THEN AUTO THRUST QUIT, RETURNED TO AIRPORT. REMOVE AND REPLACE FMG ECSDR AALA201903189002Heat Exchanger · leakingFLIGHT CREW REPORTED A STRONG ODOR DURING CLIMB. ISOLATED TO THE LEFT A/C PACK. MAINTENANCE ACCOMPLISHED A BORESCOPE OF THE LT ENGINE LP & HP, NO OIL NOTED. REMOVED AND REPLACED THE HEAT EXCHANGER AND THE LT PACK COMPONENTS.SDR HALA2019031500127Rvdt · faultyETOPS SIGNIFICANT SYSTEM - AFTER ENG START STATUS MSG PAGE INDICATING CAT 3 SINGLE ONLY/INOP SYS CAT 3 DUAL. PERFORMED OPERATIONAL TEST OF THE THS SERVO LOOPS PER AMM 27-96. TEST FAILED FOR PRIM2. T/S PER FIM TASK 27-40-00-810-811-A DRIFT OF THE RVDT MON. R/R SDR HALA2019031300124Structure · corrodedBULK CARGO FLOOR STRUCTURE AT FR 67 AND APPROX -Y600 SUSPECT CORROSION AS MARKED. CORROSION REMOVED BY BLENDING. BLEND MEASURED AND FOUND TO BE BEYOND SRM LIMITS, CORROSION REPORTED AS LEVEL 2. STRUCTURE COMPONENTS REPLACED. ALL IAW SRM 51-74-00, 51-42-11, 51-SDR HALA2019031300123Seat Track · corrodedSEAT TRACK BETWEEN FRAME 25 AND 37.4 AT -Y450 IS CORRODED AT LOCATIONS: 29+9, 31+2, 31+5, 31+19, 32+14. CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01. DAMAGE DIMENSIONS:1. FR 29+9" IVA L=.50" CORROSION ALSO SPREAD TO INNER VERTICAL WALL AREA. UNASDR HALA2019031500126Relay · failedETOPS SIGNIFICANT SYSTEM - AFTER START STATUS PAGE INDICATING CAT 3 SINGLE ONLY/INOP SYSTEM, CAT3 DUAL NOTE AND GROUND POWER FAILED AT GATE PRIOR TO APU START. AS PER CREW MSG CLEARED AFTER ENGINE SHUTDOWN, UNABLE TO DUPLICATE FAULT, RESTARTING ENGINE AT GATE SDR HALA2019031201617Structure · corrodedVERTICAL STABILIZER TRAILING EDGE LT #2 T CHORD CORRODED. REPLACED T CHORD PER SRM 51-44-11, 51-21-11, AND 51-46-11. LP 0980976SDR HALA2019031201616Structure · corrodedVERTICAL STABILIZER TRAILING EDGE RT NR 3 T CHORD CORRODED. REPLACED T CHORD PER SRM 51-44-11, 51-21-11, AND 51-46-11. LP 0980967SDR HALA2019031201615Structure · corrodedVERTICAL STABILIZER TRAILING EDGE RT NR 2 T CHORD CORRODED. REPLACED T CHORD PER SRM 51-44-11, 51-21-11, AND 51-46-11. LP 0980963
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