N393HA
Service difficulty reports · 185
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N393HA' AND registry_match = 'registration' 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 n_number = 'N393HA' AND registry_match = 'registration' 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 HALA2019040400171Seat Track · corrodedSEAT TRACK BETWEEN FRAME 58 AND 62 AT +Y1959 IS CORRODED AT LOCATIONS: FR58+20", FR60+9", FR61+20". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01.
DAMAGE DIMENSIONS: FR58+20" SUPERIOR L=1.0" W=0.500" DEPTH=0.038", FR60+9" CORROSION SPREADSDR HALA2019040402197Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 58-62, +Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F534772112040. LP 1015425SDR HALA2019040400093Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 54-58, -Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53476200. LP 1015421SDR HALA2019040400167Seat Track · corrodedSEAT TRACK BETWEEN FRAME 54 AND 58 AT -Y450 IS CORRODED AT LOCATIONS: FR56+4", FR56+18", FR57+14", FR57+16". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01.
DAMAGE DIMENSIONS: FR56+4", FR56+18", FR57+14", FR57+16". CORROSION LOCATED ON INNSDR HALA2019040432150Tee Fitting · corrodedDURING H CHECK, VERTICAL STAB TRAILING EDGE RIGHT HAD SIDE VERTICAL PROFILE ABOVE NBR 3 T CHORD FOUND CORRODED. REPLACED CHORD TO VERTICAL STAB TRAILING EDGE PER SRM 51-42-47 AND AIRCRAFT DRAWING F55371707. LP 1013986SDR HALA2019040432147Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 58-62, -Y2462 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53477040. LP 1013982SDR HALA2019040432146Floor Support · corrodedDURING H CHECK, AFT CABIN FLOOR STRUCTURE LONGERON AT FR 76, -Y445 FOUND CORRODED. REPLACED LONGERON PER SRM 51-72-11 AND AIRBUS DRAWING F53478040. LP 1013979SDR HALA201904043092Tee Fitting · corrodedDURING H CHECK, VERTICAL STAB TRAILING EDGE RIGHT HAD SIDE VERTICAL PROFILE ABOVE NBR 3 T CHORD FOUND CORRODED. REPLACED CHORD TO VERTICAL STAB TRAILING EDGE PER SRM 51-21-00, 51-46-11, 51-76-11, AND 51-42-11. LP 1013988SDR HALA2019040432196Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 54-58, +Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53476200. LP 1013984SDR HALA2019040300166Floor Support · corrodedAFT CABIN FLOOR STRUCTURE LONGERON AT FR76 -Y445 HAS SUSPECT CORROSION. // CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. DAMAGE
DIMENSIONS: L=1.000? W=0.600? DEPTH=0.110? (FULL THICKNESS). DEPTH GAUGE USED P/N: 2417 S/N: IRFE5005A9EQ. ASSESSED AS SDR HALA2019040300165Seat Track · corrodedSEAT TRACK BETWEEN FRAME 58 AND 62 AT -Y2462 IS CORRODED AT LOCATIONS: FR59, FR60+7.5", FR60+9", FR62. // CORROSION REMOVED AS PER SRM 51-74-00 REV 98.01. DAMAGE AT
LOCATIONS FR59", FR60+7.5", FR60+9", FR62" ALL CORROSION LOCATED IN THE INNER VERTICAL PSDR HALA2019040300164Seat Track · corrodedSEAT TRACK BETWEEN FRAME 54 AND 58 AT +Y450 IS CORRODED AT LOCATIONS: FR56, FR57+16", FR57+18". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01.
DAMAGE DIMENSIONS: FR56, FR57+16", FR57+18". CORROSION LOCATED ON INNER VERTICAL WALL AREA. UNASDR HALA2019040300163Tee Fitting · corrodedVERTICAL STAB TRAILING EDGE RT NR 3 TEE FITTING CORRODED AROUND FASTENER HOLES. REMOVAL OF CORROSION CARRIED OUT IAW SRM 51-74-00, REV 98.01. CORROSION STILL EVIDENT IAW NTM 51-10-02-221-001-A REV 96. BLEND DEPTH OF .054" IS BEYOND 50% MATERIAL THICKNESS. SDR HALA2019040300162Skin · corrodedVERTICAL STAB TRAILING EDGE RHS #3 T CHORD SUSPECT CORROSION AROUND FASTENER HOLES. // REMOVAL OF CORROSION CARRIED OUT IAW HAL A330 SRM 51-74-00 REV
98.01. CORROSION STILL EVIDENT IAW HAL A330 NTM 51-10-02-221-001-A REV 96. BLEND DEPTH OF .054" IS BEYOND 5SDR HALA2019040422138Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 26-37-4, -Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53276421. LP 1012345SDR HALA2019040422137Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 62-71, -Y2462 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53477040. LP 1012341SDR HALA2019040320153Seat Track · corrodedSEAT TRACK BETWEEN FRAME 62 AND 71 AT -Y2462 IS CORRODED AT LOCATIONS: FR63+10", FR65, FR65+2", FR66+13". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01.
DAMAGE DIMENSIONS: FR63+10", FR65", FR65+2", FR66+13" LOCATED ON INNER VERTICAL SURFASDR HALA2019040320152Seat Track · corrodedSEAT TRACK BETWEEN FRAME 26 AND 37.4 AT -Y450 IS CORRODED AT LOCATIONS: FR34, FR37+15". // CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98.01.
DAMAGE DIMENSIONS: FR34 SUPERIOR REWORK L: 1" W: 0.5" D: 0.030", FR37(+15") LATERAL REWORK L: 0.5" W: 0SDR HALA2019040412130Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN 58-67, +Y450 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53477044. LP 1010907SDR HALA2019040412129Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 40-47, -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F57112824. LP 1010902SDR HALA2019040412128Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 62-71, -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53477040. LP 1010897SDR HALA2019040412195Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 58-62, -Y1959 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53477040. LP 1010908SDR HALA2019040412194Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 53.2-54.5, +Y2462 FOUND CORRODED. REPLACED SEAT TRACK PER SRM 51-72-11 AND AIRBUS DRAWING F53326931. LP 1010893SDR 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 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 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 CONTSDR HALA2019022100059Controller · malfunctionedETOPS SIGNIFICANT SYSTEM, COCKPIT TEMP SYSTEM INOP. VERY HARD TO CONTROL TEMP IN COCKPIT IT EITHER TOO HOT OR TOO COLD. CKPT TEMP SHOWS 80*F BUT FEELS LIKE 70*F. RESET PACK CONT 1/2 AND ZONE CONT. PERFORMED ECS "BITE". NO FAULTS NOTED. OK FOR SVC.SDR HALA2019022100060Sensor · defectiveETOPS SIGNIFICANT SYSTEM - COCKPIT TEMP CONTROLLER INOP. ITS EITHER 52 DEGREES OR 132 DEGREES ON COND SYNOPTIC PAGE FOR HOT AIR 2. REMOVED AND REPLACED COCKPIT TEMP SENSOR 650HK PER AMM 21-63-17-400-802-A. OPS TEST GOOD. COCKPIT TEMP CONTROL NORMAL. OK FOR SERSDR HALA2019021100054Brake · overheatedATO, NR 5 BRAKE WAS RAPIDLY CLIMBING & REACH MAX OF 520 DEGREES. REPLACED NR 5 BRAKE.SDR HALA2019010900020Unknown · malfunctionedETOPS SIGNIFICANT SYSTEM - COCKPIT TEMPERATURE TRIM AIR VALVE, TEMPERATURE UNCONTROLLABLE, TRIM AIR TEMP GOES FROM 42C TO 124C WITH COCKPIT CONTROLLER SET ON INDEX MAKE. RESET THE C/B OF ZONE CONTROLLER AND PERFORMED THE SYSTEM TEST OF COCKPIT AND CABIN TEMP CSDR HALA2018112760607Fire Loop · brokenATB - ENG 2 FIRE LOOP A FAULT ENG 2 FIRE LOOP A/FDU2. // FOUND ENGINE PYLON LOOP 6WD2 BROKEN AT DETECTOR. REMOVED AND REPLACED ENG 2 FIRE LOOP A AND SUPPORT ASSEMBLY PER
AMM 26-12-16. OPS CHECK GOOD. OK FOR SVC.SDR HALA2018111900598Light · missingEXIT FLOOR LIGHTING MISSING IN FIRST CLASS. // RE-SECURED EXIT FLOOR LIGHTING STRIP IN FIRST CLASS AREA.SDR HALA2018111500587Terminal · looseAIR DIVERSION - ENG 2 FIRE LOOP A FAULT. // PER A330 TSM TASK 26-12-00-810-937-A INSPECTED FIRE LOOP ON ENG 2, FOUND FIRE DET- LOOP 2L (4012WD) 3 TERMINAL LOOSE AND FOUND
FIRE DET PYLON (6WD2) RESISTANCE CHECK VERIFIED OPEN. REMOVED FIRE DET LOOP (6WD2) WORSDR HALA2018111400584Motor · making metalETOPS SIGNIFICANT SYSTEM - METAL CHIPS IN #2 STARTER CHIP DETECTOR. // REMOVED AND REPLACED #2 STARTER ASSEMBLY IAW A330 AMM TASKS 80-11-41-000-803-A & 80-11-41-400-803A, LEAK AND OPS CHECKS GOOD.SDR HALA2018091800223Light · inoperativeDOOR 1L EMERGENCY LIGHT INOP. RELAMPED DOOR 1L EMERGENCY LIGHT.SDR HALA201809175604Lens · detachedR3 DOOR EXIT SIGN LENS DETACHED. SECURED THE EXIT SIGN LENS.SDR HALA2018061800288Probe · faultedETOPS SIGNIFICANT SYSTEM. UPON LANDING, ECAM ENGINE 1 MINOR FAULT. PFR 732111 P20T20 PROBE (E1-4014KS) T20 A AT ENG START. T/S PER
TSM 73-21-71-810-865-A NO FAULTS, NO PREV LEG FAULTS. OK FOR SVC.
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