N380HA

Service difficulty reports · 276

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 = 'N380HA' 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.

SDR HALA2012082800214Oxygen Bottle · depletedSMALL O2 WALKAROUND BOTTLE AT 3H STORAGE COMPARTMENT EMPTY, COMPLETE DISCHARGE AT 41000 FT. R & R PORTABLE OXYGEN CYLINDER ASSY AND REPLACE WITH SERVICABLE ASSY IAW AMM 35-32-42, PG 401. INBOUND LOCATION AT 3H STORAGE COMPARTMENT. OK FOR SERVICE.Aug 28, 2012 · N380HA · Airbus A330243 · Portable Oxygen SystemSDR HALA2012030300097Unknown · odorOIL ODOR IN CABIN. OPENMar 3, 2012 · N380HA · Airbus A330243 · Air Distribution SystemSDR HALA2012030200094Valve · failedDURING ENGINE START, AFTER ENGINE START SELECTOR TO IGNITION START AIR PRESSURE DROP FROM 45 TO 0, ABORTED START ON 2ND ATTEMPT APU FAILED. TROUBLESHOT AND FOUND SURGE CONTROL VALVE FAILED. R & R SURGE VALVE IAW AMM 49-51-52-000-801-A. THEN PERFORMED OPS Mar 2, 2012 · N380HA · Airbus A330243 · APU ControlsSDR HALA2012011700040Wire · damagedOPEN - ETOPS SIGNIFICANT SYSTEM - LEFT WINDSHIELD HEAT ECAM ILLUMINATED PRIOR TO ENTERING ETOPS AIRSPACE. RETURNED . BITE OF WINDSHIELD HEAT CONTROLLER NR 1 FAULTED CLASS 1-L WINDSHIELD SENSOR (3DG1) WINSHIELD HEAT CCONTROLLER NR 1 (2DG1) FAULT SWAPPED CONTROJan 17, 2012 · N380HA · Airbus A330243 · Ice/Rain Protection System WiringSDR HALA2012011600033Heater · inoperativeETOPS SIGNIFICANT SYS -LEFT WINDSHEILD HEAT INOPERATIVE. PERFORMED TSM TASK 30-42-00-810-867A AND OPS CHECKED IAW AMM 30-42-00-710-810-A. NO FAULTS DURING TEST NOTED. OK FOR SERVICE.Jan 16, 2012 · N380HA · Airbus A330243 · Windshield/Door Rain/Ice RemovalSDR HALA2012011400021Fire Loop · chafedETOPS SIGNIFICANT SYS - NOTED ENGINE NR 1 FIRE LOOP A, FAULT MESSAGE. PERFORMED TSM REF-26-12-00-801-93J. FOUND FIRE LOOP A ZONE 3 BOTH LOOPS CHAFED. R & R ZONE 3 LOOP ASSY IAW AMM REF 26-12-00. MESSAGE CLEARED, OK FOR SERVICE.Jan 14, 2012 · N380HA · Airbus A330243 · Smoke DetectionSDR HALA2012010700011Blade · damagedETOPS SIGNIFICANT SYS - WHILE PERFORMING PDC DURING WALK AROUND FOUND FAN BLADE DAMAGE ON NR 2 ENG 18.5" FROM TIP, 0.9" L, .4" D, .1250" R. REPLACED NR 2 BLADE AND RESHUFFLED ALL OTHER BLADES IAW RR FAN BLADE SHUFFLE PROGRAM. R & R IAW MM 72-31-41 & 72-35-41Jan 7, 2012 · N380HA · Airbus A330243 · Turbine Engine Compressor SectionSDR HALA2011120800571Light · looseEMERGENCY LIGHT FLOOR STRIP COMING OFF NEAR FIRST CLASS LAVATORY. REPLACED EMERGENCY LIGHT STRIP NEAR THE FIRST CLASS LAV. SECURITY CHECKED GOOD.Dec 8, 2011 · N380HA · Airbus A330243 · Emergency LightingSDR HALA2011101000447Computer · faultedETOPS SIGNIFICANT SYS - FLIGHT CONTROL COMPUTER FAULTED. R & R FLIGHT CONTRL COMPUTER IAW AMM 27-93-34. OPS CHECKED & TESTED GOOD IAW AMM 27-93-00.Oct 10, 2011 · N380HA · Airbus A330243 · Flight ControllerSDR HALA2011100500428Warning Light · illuminatedETOPS SIGNIFICANT SYS - "AUTO FLT FM 1 FAULT" IN FLIGHT AT CRUISE. STATUS CAT 3 SINGLE ONLY INOPERATIVE SYS API FM1 CAT 3 DUAL. ACCOMPLISHED TSM 22-70-00. NO FAULTS NOTED. TEST PASS.Oct 5, 2011 · N380HA · Airbus A330243 · Auto Flight SystemSDR HALA2011081200362Inlet · damagedON PREFLIGHT FOUND LIGHTING STRIKE UNDER NR 2 ENGINE. DAMAGE LOCATED ON NR 2 ENGINE INLET 6 O'CLOCK POSITION 20" AFT OF THE INLET L/E. MEASURES 1.0 X .350 X 020 AT DEEPEST POINT. CARBON FIBER IS EXPOSED, BUT NOT DAMAGED. PERFORMED LIGHTING STRIKE INSP AMM 0Aug 12, 2011 · N380HA · Airbus A330243 · Nacelle/Pylon, Main FrameSDR HALA2011062300279Coffeemaker · burnedABOVE 10,000 FT. ALL EXIT SIGNS EXCEPT FOR THE 2L EXIT SIGN WENT OUT. THE F/A'S NOTICED A BURNING SMELL FROM THE 2L GALLEY AREA AND THE AFT GALLEY AREA. PERFORMED OPERATIONAL TEST OF THE OVERHEAD EXIT SIGNS CONTROL UNIT IAW AMM 33-51-00-710-804A. TEST GOODJun 23, 2011 · N380HA · Airbus A330243 · Buffet/GalleysSDR HALA2011062200278Fitting · looseETOPS SIGNIFICANT SYS - UPON WALK AROUND FOUND HYD FLUID LEAKS FROM RT OTBD FLAP DRIVE 34CV-A PRESSURE LINE. RESECURED LOOSE FITTING ON PRESSURE LINE. RESERVICED HYD GREEN AND YELLOW SYSTEMS. RAN HYD PUMPS. LINE LEAK CHECKED GOOD. ACFT OK FOR SERVICE.Jun 22, 2011 · N380HA · Airbus A330243 · Hydraulic System, MainSDR HALA2011061100257Control Panel · malfunctionedETOPS SIGNIFICANT SYS - RADAR 1 & 2 NO RETURN AND NO TILT ANGLE INDICATION IN BOTH AUTO AND MANUAL. RADAR INOP. REPLACED CONTROL PANEL IAW AMM 34-41-12 AND PERFORMED BITE PROCEDURE IAW AMM 34-41-00. ACFT OK FOR SERVICE.Jun 11, 2011 · N380HA · Airbus A330243 · Weather Radar SystemSDR HALA2011060400248Radar · multiple failSUP - ETOPS SIGNIFICANT SYS - WEATHER RADAR NR 2 INOP. BEGAN TS PROCEDURES IAW TSM 34-41-00 FOR FAULT WXR MOUNTING TRAY (5SQ). CLEANED CONNECTIONS ON WXR CTRL PANEL, WAVE GUIDE SWITCH AND WCXR 1 AND 2 PERFORMED WEATHER RADAR BITE TEST IAW AMM 34-41-00-740-80Jun 4, 2011 · N380HA · Airbus A330243 · Weather Radar SystemSDR HALA2011060400247Radar · multiple failETOPS SIGNIFICANT SYS - WEATHER RADAR NR2 INOP. BEGAN TS PROCEDURES IAW TSM 34-41-00 FOR FAULT WXR MOUNTING TRAY (5SQ). CLEANED CONNECTIONS ON WXR CTRL PANEL, WAVE GUIDE SWITCH AND WCXR 1 AND 2. PERFORMED WEATHER RADAR BITE TEST IAW AMM 34-41-00-740-801, TEJun 4, 2011 · N380HA · Airbus A330243 · Weather Radar SystemSDR HALA2011051000186Warning Light · illuminatedETOPS SIGNIFICANT SYS - ENG 2 MINOR FAULT ECAM AFTER LANDING. PERFORMED EECS2 CHAN B SYS TEST, LAST LEG CLASS 3 FAULT AND GROUND REPORT TEST, TESTED OK. PERFORMED TSM 73-22-00-740-815, TESTED OK.May 10, 2011 · N380HA · Airbus A330243 · Engine Indicating SystemSDR HALA2011021000089Unknown · unknownETOPS SIGNIFICANT SYS - NO FUEL TRANSFER FROM TRIM TANK. PERFORMED FCMC 1 & FCMC 2 SYS TEST. NO FAULTS NOTED. PERFORMED FCMC 1 & FCMC 2 FUEL VALVE TEST. NO FAULTS NOTED. PERFORMED FCMC 1 & FCMC 2 LEVEL SENSE TEST. NO FAULTS NOTED. NO FAULTS NOTED ON POSFeb 10, 2011 · N380HA · Airbus A330243 · Aircraft Fuel Distribution SystemSDR HALA2011012200039Autopilot Sys · malfunctionedETOPS SIGNIFICANT SYS - AUTO FLT FM 1 FAULT. PERFORMED AFS TEST RESET POWER TO FMGEC 1 IAW 22-83-00, MSG CLEARED. NO HISTORY.Jan 22, 2011 · N380HA · Airbus A330243 · Autopilot SystemSDR HALA2011010100006Reservoir · leakingECAM: HYD G RESERVIOR LEAK DETECTED, MESSAGE CAME ON DURING DESCENT. LEAK CONFIRMED ENG 1 & 2 G PUMPS TURNED OFF. FOUND FITTING AT PRESS MANIFOLD "G" SYS 2 TURNS LOOSE. G SYS FOUND 90 PERCENT EMPTY. TIGHTENED PRESS MANIFOLD FITTING. SVCD W/ 4 GALLONS HYD FJan 1, 2011 · N380HA · Airbus A330243 · Hydraulic Accumulator, AuxiliarySDR HALA122700596Fitting · looseCAPTAIN REPORTED HYD SYS QUANITY DROPPING, DECLARED AN EMERGENCY LANDING AND RETURNED TO BASE RE-SECURED FITTING ON HYD LINE. FROM 5102JM HP FILTER MODULE ON GREEN HYD SYS ACCUMULATOR. LEAK CHECK GOOD IAW TSM 29-11-00. OPS CHECK GOOD IAW AMM 29-00-00. SERVDec 27, 2010 · N380HA · Airbus A330243 · Hydraulic System, MainSDR HALA121700595Power Supply · inoperativeDURING EMERGENCY LIGHT TEST, DOOR 3 LT EXIT LIGHT WAS INOPERATIVE. THE EMERGENCY POWER SUPPLY UNIT (EPSU), BATTERY AND DOOR 3 EXIT SIGN WERE REPLACED AND TESTS OK.Dec 17, 2010 · N380HA · Airbus A330243 · Emergency LightingSDR HALA2010121600589Warning Light · illuminatedETOPS SIGNIFICANT SYS - BTB: ECAM MESSAGE F/CTRL PRIM 1 PITCH FAULT. T/S IAW TSM 27-30-00-810-815 F/CTRL PRIM 1 PITCH FAULT AND F/CTRL ELEV SERVO CNTR POS XDLR L&R &FAULT CLEARED, SYS CHEKS GOOD OK FOR SVS.Dec 16, 2010 · N380HA · Airbus A330* · Central WarningSDR HALA2010111200536Monitor · odorREPLACED MONITOR DUE TO F/A REPORTED ELECTRICAL ODOR IAW 23-32-10, P4001.Nov 12, 2010 · N380HA · Airbus A330243 · Entertainment SystemSDR HALA2010072400328Warning Light · false activationETOPS SIGNIFICANT SYS - BTB, ECAM MESSAGE FLT CONTROL SEC 2 PITCH FAULT AFTER ENGINE START. COMPLIED WITH FCSC OPS TEST IAW AMM 27-94-00-710-801, OPS TEST OK, NO FAULT NOTED. OK FOR SERVICE.Jul 24, 2010 · N380HA · Airbus A330243 · Central WarningSDR HALA2010071600308Warning System · false activationBTB: SMOKE FWD CARGO BOTTLE 1&2 FAULT / AFT CARGO BOTTLE 1&2 FAULT. RESET SDF1 & SDF2. OK FOR SERVICE. SDF SYSTEM TEST OKAY.Jul 16, 2010 · N380HA · Airbus A330243 · Fire Bottle, Fixed
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