N392HA

Service difficulty reports · 159

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 = 'N392HA' 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 HALA2018101700506Angle · corrodedSUSPECT CORROSION LOCATED AFT OF DOOR 4L ON FLOOR "Z" ANGLE 6" AFT OF FRAME 75 AS MARKED. CORROSION REMOVED FROM "Z" ANGLE 6" AFT OF FRAME 75 IAW SRM 51-74-00 REV 97. DAMAGE DIMENSION: 2.5"L X 1.5"W X MAX DEPTH 0.045". DEPTH GAUGE USED P/N: 2417 S/N: IRFE5005AOct 16, 2018 · N392HA · Airbus A330243 · Fuselage Miscellaneous StructureSDR HALA2018101700505Angle · corrodedSUSPECT CORROSION (2 OFF) LOCATIONS AFT OF DOOR 4R AT FLOOR LEVEL 6" AFT OF FRAME 75 AS MARKED. CORROSION REMOVED IAW SRM 51-74-00 PARA 6 A. THRU 6 B.(3) REV 98.00. REMAINING THICKNESS ESTABLISHED ON Z ANGLE IAW SRM 51-74-00 PARA 6B. (6) REV 98.00 FOR BLENDED Oct 16, 2018 · N392HA · Airbus A330243 · Fuselage Miscellaneous StructureSDR HALA2018101700510Seat Track · corrodedSEAT TRACK BETWEEN FRAME 31 AND 35 AT -Y1552.5 IS CORRODED AT LOCATIONS: FR32+18.5", FR33+3". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98. UNABLE TO FULLY REMOVE CORROSION DAMAGE OR ACCURATELY MEASURE DEPTH. DAMAGE LOCATIONS -Y1552.5 FR32+18.5 & FOct 15, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018101700509Seat Track · corrodedSEAT TRACK BETWEEN FRAME 26 AND 37.4 AT +Y2462 IS CORRODED AT LOCATIONS: FR26+15", FR30+10", FR31+3", FR32+5", FR35+7". CORROSION REMOVED IAW SRM 51-74-00 REV 98. DAMAGE DIMENSION: AT FR26+15", FR30+10", FR31+3", FR32+5", FR35+7" LOCATED ON SEAT TRACK INNER VEOct 15, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018101700507Seat Track · corrodedSEAT TRACK BETWEEN FRAME 40 AND 47 AT -Y450 IS CORRODED AT LOCATIONS: FR40.1+16", FR41+0", FR41+12", FR46+8". CORROSION REMOVED IAW SRM 51-74-00 REV 98. DAMAGE DIMENSION: FR40.1 + 16", FR41 + 0", FR41 + 12" AND FR46 + 8. LOCATED ON SEAT TRACK INNER VERTICAL AROct 15, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018101700508Seat Track · corrodedSEAT TRACK BETWEEN FRAME 40 AND 47 AT -Y1959 IS CORRODED AT LOCATIONS: FR40.3+0", FR41+3", FR41+4", FR42+16", FR45+5". CORROSION REMOVED PER SRM 51-74-00 REV 98. UNABLE TO FULLY REMOVE CORROSION DAMAGE OR ACCURATELY MEASURE DEPTH. DAMAGE LOCATED AT FR40.3, FR4Oct 15, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018101700521Seat Track · corrodedSEAT TRACK BETWEEN FRAME 47 AND 53.2 AT -Y1959 IS CORRODED AT LOCATIONS FR51+14", FR52+6", FR53+3", FR53.1+12". CORROSION REMOVED IAW SRM 51-74-00 REV 98. DAMAGE DIMENSION: FR 37.3, FR31+17'', FR31, FR30, FR29+9'' AND FR 29+6" LOCATED ON SEAT TRACK INNER VERTIOct 12, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018101700520Seat Track · corrodedSEAT TRACK BETWEEN FRAME 26 AND 37.4 AT -Y450 IS CORRODED AT LOCATIONS: FR37.3,+0", FR31+17", FR31+0", FR30+0", FR29+9", FR29+6". CORROSION REMOVED IAW SRM 51-74-00 REV 98. DAMAGE DIMENSION FR 37.3, FR31+17'', FR31, FR30, FR29+9'' AND FR 29+6'' LOCATED ON SEATOct 12, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018101700519Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 53.5 AT +Y450 IS CORRODED AT LOCATIONS: FR53.2+8", FR53.3+17", FR53.4+0", FR53.4+7". CORROSION REMOVED IAW SRM 51-74-00 REV 97. DAMAGE DIMENSION: AT FR53.2 + 8", FR53.3 + 17", FR53.4 + 0" AND FR53.4 + 7" LOCATED ON SEAT TRACK Oct 12, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018101700518Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 53.5 AT -Y450 IS CORRODED AT LOCATIONS: FR53.2+8", FR53.3+1", FR53.3+17", FR53.3+19". CORROSION REMOVED IAW SRM 51-74-00 REV 97. DAMAGE DIMENSION: FR53.2 + 8" AND FR53.3 + 1" LOCATED ON SEAT TRACK INNER VERTICAL AREA. UNABLE TOct 12, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018101700517Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 54 AT +Y1959 IS CORRODED AT LOCATIONS: FR53.5+11". CORROSION REMOVED IAW SRM 51-74-00 REV 97. DAMAGE DIMENSION: AT FR53.5+11" SUPERIOR, L=1.0", W= 0.250", D=0.60". CONFIRMED AS LEVEL 2 CORROSION, PART REPLACEMENT REQUIRED. SEAOct 12, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018101700516Seat Track · corrodedSEAT TRACK BETWEEN FRAME 58 AND 68 AT -Y450 IS CORRODED AT LOCATIONS: FR59, FR62+4". CORROSION REMOVED FROM SEAT TRACK -Y450 AT FR59" AND FR62+4" IAW SRM 51-74-00 REV 98. DAMAGE DIMENSION: ATFR62+4": SUPERIOR L=1.0", W=0.250, D=0.080", & FR 59 L=1.0", W=0.250,Oct 12, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018101700515Seat Track · corrodedSEAT TRACK BETWEEN FRAME 58 AND 62 AT -Y1959 IS CORRODED AT LOCATIONS: FR59, FR62. CORROSION REMOVED IAW SRM 51-74-00 REV 98. DAMAGE DIMENSION: AT FR59 L: 2.5" W:0.75" D: 0.022" CENTRAL REWORK, FR62 L: 3" W: 0.25" D: 0.060" LATERAL REWORK. ASSESSED TO BE OUT OOct 12, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018101700514Seat Track · corrodedSEAT TRACK BETWEEN FRAME 31 AND 35 AT +Y1552.5 IS CORRODED AT LOCATIONS: FR32+15", FR33+3". CORROSION REMOVED IAW SRM 51-74-00 REV 98. DAMAGE DIMENSION: AT FR32+15" AND FR33+3''LOCATED ON SEAT TRACK INNER VERTICAL AREAS, UNABLE TO SUFFICIENTLY REMOVE CORROSIOOct 12, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018100500474Seat Track · corrodedSEAT TRACK BETWEEN FRAME 18 AND 26 AT +Y953 IS CORRODED AT LOCATIONS: FR 19+9". CORROSION REMOVED FROM SEAT TRACK +Y953 AT FR19+9" IAW SRM 51-74-00 REV 97. DAMAGE DIMENSION: AT FR19+9" 1"L X 0.400"W X 0.051"D ON SUPERIOR AREA. DEPTH GAUGE USED P/N: 2417 S/N: IOct 5, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018091305603Light · unsecureEMERGENCY LIGHT STRIP LOOSE AT SEAT 1HJ. SECURED THE LIGHT STRIP.Sep 12, 2018 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2018090805536Power Supply · no testWHILE PERFORMING SLIDE CHANGE ON THE L4 DOOR, THE EPSU 17WL SYSTEM TEST FAILED. REPLACED THE EPSU.Sep 7, 2018 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2018071600023Drain · disconnectedETOPS - NR 1 ENG LEAK FUEL FROM FUEL DRAIN TANK OVERFLOW DRAIN MAST. RECONNECTED FUEL MANIFOLD DRAIN TO FMU PER AMM 73-21. REMOVED AND REPLACED LUBRICATION FLOW FILTER ASSY PER AMM 73-12. LEAK CHECK GOOD.Jul 16, 2018 · N392HA · Airbus A330243 · Fuel Controlling SystemSDR HALA2018062700314Warning Light · false activationNR 1 ENGINE AIR EXCHANGER FAULT. PERFORMED TSM TASK 79-20-00-810-809-A. NO DEFECTS NOTED. OK FOR SERVICEJun 26, 2018 · N392HA · Airbus A330243 · Engine (Turbine/Turboprop)SDR HALA2018062700313Fault Light · false activationNR 1 ENGINE MINOR FAULT. PERFORMED FADEC/EEC 1 SYS TEST. NO FAULTS NOTED. OK FOR SERVICE.Jun 26, 2018 · N392HA · Airbus A330243 · Engine (Turbine/Turboprop)SDR HALA2018060800289Pump · leakingETOPS SIGNIFICANT SYSTEM - ON PDC WALK AROUND FOUND HYDRAULIC LEAK ON NR 2 ENGINE HYDRAULIC PUMP. REMOVED AND REPLACED NR 2 EDP (GREEN). C/W OPS, LEAK AND SERVICE PER AMM 29-11-51-400-805-A. OK FOR SVC.Jun 7, 2018 · N392HA · Airbus A330243 · Hydraulic Pump (Electric/Engine), MainSDR HALA2018051600230Irs · malfunctionedNR 2 ENGINE, FADEC SYS FAULT. LAST LEG & GROUND REPORT FAULT OPUS E2-4072KS, CHANNEL A & B. FAULT CLEARED ON EEC RESET. TROUBLESHOT IAW TSM 73-21-71-810-889-A. INSPECTED CONNECTOR 4071KS-C, AND FOUND SOCKETS 1, 5, & 6 DIRTY. CLEANED THE SOCKETS & INSTALLEMay 5, 2018 · N392HA · Airbus A330243 · Turbine GovernorSDR HALA2018010200002Cover · missingDOOR 2R EXIT SIGN LIGHT COVER IS MISSING. DEFERRED PER MEL 25-22-3. REPLACED DOOR 2R EXIT SIGN LIGHT COVER.Jan 1, 2018 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2017122700326Frame · damagedOPEN - FOUND DAMAGE ON FRAME 24 BETWEEN STRINGER 28 & 29L. HFEC DAMAGED AREA. NO DEFECTS NOTED. INTERNAL DETAILED VISUAL CHECK OK. ACCOMPLISHED U.T.Dec 25, 2017 · N392HA · Airbus A330243 · Fuselage Main, FrameSDR HALA2018010400003Skin · damagedFOUND A GOUGE AND DENT DAMAGE TO THE LEFT SKIN BETWEEN FRAMES 21 - 26, STRINGERS 28 - 29L. INSPECTION REVEALED NO CRACKS. BLENDED IAW ERA 564572-14.Dec 25, 2017 · N392HA · Airbus A330243 · Fuselage Main, Plate/SkinSDR HALA2017121300294Oil System · lowETOPS SIGNIFICANT SYSTEM - UPON ENGINE SHUTDOWN AT GATE WITH APU RUNNING APU GENERATOR DID NOT TRANSFER POWER FROM ENGINE GENERATOR. AIRCRAFT LOST POWER, PERFORMED ECAM APU GEN RESET, OPS NORMAL. // PERFORMED APU BITE PER AMM 49-00-00-740-801A & OPS TEST OF Dec 12, 2017 · N392HA · Airbus A330243 · APU Oil SystemSDR HALA2017111308097Sign · detachedL3 DOOR EXIT SIGN DETACHED. SECURED THE SIGN.Nov 12, 2017 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2017110808003Light · unsecureEMERGENCY PATH LIGHTING TORN BETWEEN DOOR 4L AND 4R. RESECURED PATH LIGHT.Nov 7, 2017 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2017070500178Detector · out of limitsDURING CRUISE, AN ECAM MESSAGE NR 2 ENGINE FIRE LOOP A FAULT DISPLAYED. TROUBLESHOT THE NR 2 FIRE LOOP A IAW TSM 26-12-00-810-937A. BITE TESTED OK. FOUND PYLON DETECTOR, 2WD2, OUT OF LIMITS. REMOVED & REPLACED THE PYLON DETECTOR IAW AMM 26-12-16. OPS CHECJul 2, 2017 · N392HA · Airbus A330243 · Smoke DetectionSDR HALA2017060900145Apu · malfunctionedAPU GENERATOR FAULT ON APU START. TWO START ATTEMPTS UNSUCCESSFUL. PERFORMED TSM 24-23-00-810-816-A. APU TESTED OK. RAN MULTIPLE TIMES & USED TO RUN NR 1 ENGINE. ALL OPS NORMAL. OK FOR SERVICE.Jun 8, 2017 · N392HA · Airbus A330243 · Airborne Auxiliary Power Unit (APU) SystemSDR HALA2017060900144Fire Detector · malfunctionedNR 2 ENGINE FIRE LOOP -A- FAULT. TROUBLESHOT IAW TSM 23-12-00-810-937-A. BITE TESTED IAW AMM 26-12, & TESTED OK. RANG OUT CONNECTOR (1WD2-A) PINS J TO K & HAD 1498 OHMS. RANG-OUT, CLEANED, & INSPECTED NR 2 ENG ALL X5 LOOPS A & B FIRE DETECTORS. NO DISCREPAJun 8, 2017 · N392HA · Airbus A330243 · Fire DetectionSDR HALA2017060600141Fire Loop · malfunctionedDURING FLIGHT ECAM MESSAGE FOR NR 2 ENGINE FIRE LOOP A FAULT. CAME ON INTERMITTENTLY THEN DISAPPEARED. FIRE LOOP A / FDU2 ON PLF. PERFORMED FDU 2 BITE TEST OK IAW AMM 26-12-00. ACFT OK FOR SVC.Jun 5, 2017 · N392HA · Airbus A330243 · Smoke DetectionSDR HALA2017060600140Warning Light · false activationAPU BLEED FAULT ECAM ON INITIAL START. RECYCLED APU BLEED SWITCH O CHANGE. // ACCOMPLISHED TSM TASK 49-62-00-810-841-A. OPS CHECK OF THE APU IAW AMM 49-00-00-710-801, OK. TEST OF THE APU BLEED VALVE OK IAW AMM 49-51-51-710-803-A, OK. CYCLED APU BLEED VALVE SWIJun 4, 2017 · N392HA · Airbus A330243 · APU Bleed Air SystemSDR HALA2017041200150Light · unsecureFLOOR EMERGENCY LIGHT AT LEFT ROW 37 NOT ATTACHED. SECURED FLOOR LIGHT STRIP AT SEAT 37C.Apr 11, 2017 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2017032700086Valve · faultedECAM FOR TRIM TANK TRANSFER FAULT. REMOVED AND REPLACED THE LEFT OUTER TANK INLET VALVE IAW AMM 28-25-57. OPS NORMAL.Mar 27, 2017 · N392HA · Airbus A330243 · Aircraft Fuel Distribution SystemSDR HALA2017021600040Light · looseAFT GALLEY EMERGENCY LITE STRIP RUNNING FROM A/C L TO RIGHT IS LOOSE. RESECURED FLOOR STRIP.Feb 15, 2017 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2016111900208Cover · looseAFT GALLEY FLOOR LIGHT NEEDS SECURING. SECURED AFT GALLEY FLOOR LIGHT COVER.Nov 19, 2016 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2016111700515Fuel Filter · cloggedNR 1 ENG FUEL FILTER CLOG LIGHT ILLUMINATED. REMOVED AND REPLACED THE NR 1 FUEL FILTER IAW AMM 73-11-41 AND LEAK CHECKED OK. OK FOR SERVICE.Nov 17, 2016 · N392HA · Airbus A330243 · Engine Fuel DistributionSDR HALA2016110900207Light · looseFLOOR LIGHTING STRIP AT LEFT ROWS 25 AND 26 ARE LOOSE. REMOVED DEBRIS FROM UNDER FLOOR LIGHTING AND RE-SECURED LIGHT STRIP.Nov 7, 2016 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2016081000327Oil System · underservicedAPU FAULT WHEN STARTING IAW ECAM SHUTDOWN APU, SECOND START ATTEMPT, APU OK. G.V.I. OF APU COMPARTMENT, FOUND APU OIL QTY LOW AT ADD LINE. SERVICED APU OIL TO FULL. INSPECTED COMPARTMENT FOUND NO DISCREPANCIES AT THIS TIME. ALSO INSPECTED EXHAUST AREA. N.T.Aug 10, 2016 · N392HA · Airbus A330243 · APU Oil SystemSDR HALA2016073100312Exciter · malfunctionedAPU INFLIGHT START AT FL 410, OAT -60 WAS UNSUCCESSFULL AFTER 3 ATTEMPTS. REMOVED AND REPLACED THE APU IGNITION EXCITER IAW AMM 49-41-38. OPS CHECKED OK. VERIFICATION FLIGHT FOR APU COMPLETED. APU OPERATES NORMALLY. VERIFICATION OF COLD SOAK START VERIFJul 31, 2016 · N392HA · Airbus A330243 · APU Start/Ignition SystemSDR HALA2016061900244Regulator · faultedETOPS SIGNIFICANT SYSTEM, AIR PACK REGULATOR 2 FAULT. T/S IAW TSM 21-53-00-810-850A. RESET PACK TEMP CONTROLS. NO FAULTS. OK FOR SERVICE.Jun 19, 2016 · N392HA · Airbus A330243 · Cabin Cooling SystemSDR HALA2016052400223Controller · inoperativeECAS, CABIN AUTO INOPERATIVE. CLIMBING OUT OF 20,000 FT. REPLACED THE NR 2 AUTO PRESSURE CONTROLLER IAW AMM 21-31-02. OPS CHECK GOOD, OK FOR SERVICE.May 24, 2016 · N392HA · Airbus A330243 · Cabin Pressure ControllerSDR HALA2016042200033Transformer · failedCREW DIVERTED THE ACFT DUE TO TR 2 APPEARED IN AMBER. SDAC NR 1 AND 2 RESET IAW MCC, NO HELP. MAINTENANCE REPLACED THE NR 2 TRANSFORMER RECTIFER.Apr 21, 2016 · N392HA · Airbus A330243 · DC Generating SystemSDR HALA20160309076Power Supply · failedDURING LOCAL TEXT, DOOR 1L EMERGENCY POWER SUPPLY UNIT FAILED TEST. REPLACED DOOR 1L EPSU POWER SUPPLY. R & R 1L EPSU REF AMM 33-51-38. OPS CHECK GOOD.Mar 9, 2016 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2016021900022Skin · damagedDURING WALK AROUND INSPECTION, AFT CARGO DOOR INNER SKIN DAMAGED AT FR 63-63A BETWEEN BEAM 4 AND 5 WITH A CRACK ON THE BACK SKIN. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER IAW ER/A 544076-14.Feb 19, 2016 · N392HA · Airbus A330243 · Cargo/Baggage DoorsSDR HALA2015031600038Generator · unknownETOPS SIGNIFICANT SYSTEM - APU GENERATOR FAULT ON ECAM. FAULT LIGHT ON APU GENERATOR P/B SW. R & R APU AIR INTAKE DUCT IAW AMM 49-16-46. R & R APU GENERATOR IAW AMM 24-23-51. OPS, LEAK, CONDITION & SECURITY CK GOOD. APU OIL LEVEL FULL. SECURED APU ACCESSMar 16, 2015 · N392HA · Airbus A330243 · AC Generator-AlternatorSDR HALA2015030700031Computer · malfunctionedETOPS SIGNIFICANT ITEM, ECAM PRIM 1 FAULT, PRIM 1 SWAPPED TO PRIM 3 POSITION. OK TO CONTINUE IAW MEL 27-93-1B, DMI 50574. NO HISTORY 14 LEGS, FAULT TRANSFERRED FROM 1 TO 3. PRIM IN POSITION 3 IS FAULTY. PERFORMED BITE TEST OF EFCS. CHECK OK IAW AMM 27-96-0Mar 7, 2015 · N392HA · Airbus A330243 · Flight Control SystemSDR HALA2014110700184Limiter · malfunctionedAIR TURNBACK, ELEC BATTERY 2 SYS FAULT. ALL 3 BATTERIES NOT CHARGING. PERFORMED TSM 24-30-00-810-816-A. REPLACED BCL2 IAW AMM 24-38-34 -000-801-A. OPS TEST OK. OPS TEST BCL1 AND APU TEST OK.Nov 7, 2014 · N392HA · Airbus A330243 · Battery/Charger SystemSDR HALA2014090500129Idg · malfunctionedNR 2 GENERATOR FAULT, TROUBLESHOT IAW TSM 24-20-00-810-942-A. SWAPPED GCU'S AND RAN ENGINES, CONDITION SAME. IDG WIRE CHECKED GOOD. R & R NR 2 ENGINE IDG IAW AMM 24-21-51-400-804-A. OPS CHECKED GOOD, NO FAULTS NOTED. OK FOR SERVICE.Sep 5, 2014 · N392HA · Airbus A330243 · AC Generator-Alternator
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