Airbus A330-243

Service difficulty reports · 5,645

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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"

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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 0980971Mar 12, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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 0980924Mar 12, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Mar 12, 2019 · N375HA · Airbus A330243 · Engine Fuel DistributionSDR 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 SUFMar 12, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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 THICKMar 12, 2019 · N390HA · Airbus A330243 · Vertical Stabilizer Miscellaneous StructureSDR 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 THMar 12, 2019 · N390HA · Airbus A330243 · Vertical Stabilizer Miscellaneous StructureSDR 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 0979474Mar 11, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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 0979153Mar 11, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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 CENMar 11, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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"Mar 11, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Mar 10, 2019 · N290AY · Airbus A330243 · Air Distribution SystemSDR 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.Mar 10, 2019 · N287AY · Airbus A330243 · Light System WiringSDR 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: VUDMar 8, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Mar 8, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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 PMar 8, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Mar 7, 2019 · N383HA · Airbus A330243 · Engine Thrust ReverserSDR 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=0.04Mar 7, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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 CARRIMar 7, 2019 · N390HA · Airbus A330243 · Fuselage Miscellaneous StructureSDR 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:Mar 7, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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") CENMar 7, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Mar 6, 2019 · N383HA · Airbus A330243 · Airfoil Anti/De-ice SystemSDR 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 COMMANDEMar 6, 2019 · N389HA · Airbus A330243 · Fuel Transfer ValveSDR HALA2019030700101Sign · unsecure3 L DOOR EXIT SIGN FELL OFF. A/C OK. RE-SECURED 3L DOOR EXIT SIGN LENS. OPS CHECK OK.Mar 6, 2019 · N383HA · Airbus A330243 · Emergency LightingSDR 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. Mar 6, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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: Mar 6, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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 Mar 6, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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 OMar 6, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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 SUFMar 6, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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 Mar 6, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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 AMar 5, 2019 · N342AV · Airbus A330243 · Cabin Cooling SystemSDR 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.Mar 5, 2019 · N374HA · Airbus A330243 · Emergency LightingSDR 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.Mar 5, 2019 · N374HA · Airbus A330243 · Engine Oil Indicating SystemSDR 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 NOMar 5, 2019 · N370HA · Airbus A330243 · APU Start/Ignition SystemSDR 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 72-31-41-000Mar 5, 2019 · N360HA · Airbus A330243 · Turbine Engine Compressor SectionSDR 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. Mar 5, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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 Mar 5, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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 Mar 3, 2019 · N374HA · Airbus A330243 · Air Distribution SystemSDR 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.Feb 28, 2019 · N384HA · Airbus A330243 · Aircraft Fuel Distribution SystemSDR 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.Feb 28, 2019 · N383HA · Airbus A330243 · Emergency LightingSDR HALA2019030100078Warning System · false activationSMOKE LAVATORY DET FAULT IN LAV 35 BY 2L DOOR. PERFORMED BITE OF CIDS SDF. TEST OK. NO FAULTS NOTED.Feb 28, 2019 · N383HA · Airbus A330243 · Smoke DetectionSDR 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-AFeb 27, 2019 · N289AY · Airbus A330243 · Air Distribution SystemSDR 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 SOURCEFeb 27, 2019 · N291AY · Airbus A330243 · Airborne Auxiliary Power Unit (APU) SystemSDR 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.Feb 27, 2019 · N383HA · Airbus A330243 · Audio/Video MonitoringSDR HALA2019022760049Seat Track · corrodedDURING H CHECK, SEAT TRACK BETWEEN FR 25-37, -Y450 FOUND CORRODED. REPLACED SEAT TRACK. LP 0960057Feb 26, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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 PAFeb 26, 2019 · N390HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR 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.Feb 24, 2019 · N289AY · Airbus A330243 · Air Distribution SystemSDR HALA2019022750050Sign · detachedDOOR 3L EXIT SIGN FELL OFF. RE-SECURED DOOR 3L EXIT SIGN. LP 3224359Feb 24, 2019 · N374HA · Airbus A330243 · Emergency LightingSDR 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 NORMALFeb 24, 2019 · N373HA · Airbus A330243 · Engine Thrust ReverserSDR 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-Feb 23, 2019 · N382HA · Airbus A330243 · Engine Oil Indicating SystemSDR 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 CONTFeb 22, 2019 · N393HA · Airbus A330243 · Cabin Temperature Controller
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