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 HALA2022050200168None · noneSHIP 392 EXIT SIGN OVER 3L DOOR FELL OFF. CORRECTIVE ACTION: RESECURED 3L EXIT SIGN. (8447139)May 2, 2022 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2022033000083Filter · cloggedETOPS - FWD CRG VENT AND BULK VENT ECAM APPEARS INTERMITTENTLY // T/S PER A330 TSM 21-23-00-810-804-A POST FLIGHT REPORT MSG GALLEY LAV DUCT CLOGGED. REMOVED AND REPLACED LAV + CABIN+GALLEY FILTERS SYSTEM TEST PASS.Mar 29, 2022 · N392HA · Airbus A330243 · Air Conditioning SystemSDR HALA2022031500081None · noneSHIP 392 FOUND EMER LIGHT MISSING SEAT 26 R/H SIDE ON OVERHEAD PANEL. CORRECTIVE ACTION: INSTALLED DOME EMER LIGHT PER HAL A330 AMM 33-51-00.Mar 15, 2022 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2022022300069None · noneSUPPLEMENTAL INFORMATION SHIP 392 - ATB - DUE TO ENGINE FAILURE OCCURRED AT 100 FT AFTER TAKE OFF. ENG #2 AGENT 1 DISCHARGED. CORRECTIVE ACTION: PERFORMED INSPECTION AFTER ENGINE FAILURE, NACELLE GVI AND FIRE EXTINGUISHING SYSTEM. REMOVED AND REPLACED #2 ENG. Mar 2, 2022 · N392HA · Airbus A330243 · Powerplant SystemSDR HALA2022030300065None · noneATB - ENGINE FAILURE OCCURRED AT 100 FT. AFTER TAKE OFF // REMOVED AND REPLACED #2 ENG. ( RIGHT HAND ) PER TASK CARD # 7100-9401-02-HAL QEC, & ACCESSOR OFF 43-7299-9-0005 S/N 42009 ON 43-7110-9-0010 S/N 42192Mar 2, 2022 · N392HA · Airbus A330243 · Powerplant SystemSDR HALA2022022200051Engine · failedATB - #2 ENGINE FAILURE OCCURRED AT 100FT AFTER TAKEOFF // PER AIRBUS RECOMMENDATION DOSSIER REFERENCE 81029165, PERFORMED INSPECTION AFTER ENGINE FAILURE PER AMM 05-51-26, NACELLE GVI PER AMM 05-34-00, AND ADDITIONAL CHECKS OF FIRE EXTINGUISHING SYSTEM PER AMFeb 18, 2022 · N392HA · Airbus A330243 · Engine Emergency Shutdown SystemSDR HALA2022020700041None · noneAFTER TAKE-OFF ECAM ENG 1 CTL SYS FAULT // REMOVED AND REPLACED VSV CONTROLLER #1 ENG IAW AMM 75-33-51 REQUIRES LEAK CK WORK STILL IN PROGRESS. 789181 E.SOTO. PERFORMED FUEL AND OIL LEAK TEST PER A330 AMM 71-00-00, NO LEAK NOTED, NO FAULT ON ECAM, A/C OK FOR Feb 6, 2022 · N392HA · Airbus A330243 · Fuel Control/Reciprocating EnginesSDR HALA2022011800024Strip · defectiveSHIP 392 AFT GALLEY FLOOR TRIM COMING OFF MIDDLE WALKWAY. CORRECTIVE ACTION: REMOVED AND REPLACED PHOTO LUMINESCENT FLOOR STRIP. (7717149)Jan 16, 2022 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2021122000194Inverter · defectiveETOPS - WORKING W/C 2518-01001-01 INSPECT STATIC INVERTER; REPLACE // REMOVED AND REPLACED (3NA) STATIC INVERTER PER A330 W/C 2518-01001-01. OPS CHKS NORMAL INVERTER, STATI OFF 43-2420-9-0001 35479 ON 43-2420-9-0001 36122Dec 18, 2021 · N392HA · Airbus A330243 · AC InverterSDR HALA2021121600190Control Unit · inoperativeETOPS - ENG 2 CTL SYS FAULT // ACCOMPLISHED TSM 71-00-00-810-924-A, ON #2 ENG RUN FOUND VSV CONTROL FAULT (VSV SYSTEM/ VSV CONTROL UNIT. 2283142 13 DEC 21. PERFORMED TSM 75-33-00-810-808-A UP TO STEP 4.(4)(C) WIRE CHECKED OK 2438457 12/13/2021 REMOVED AND RDec 15, 2021 · N392HA · Airbus A330243 · Engine Fuel and ControlSDR HALA2021121300228Light · inoperativeSHIP 392 SECTION OF EMERGENCY PATH LIGHTING IN FRONT OF 1ST CLASS HAS COME LOOSE. CORRECTIVE ACTION: RESECURED EMERGENCY PATH LIGHTING STRIP AS REQUIRED. (7744044)Dec 11, 2021 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2021091600138Warning Message · false activationSHIP 392 MESSAGE INFLIGHT "DOOR R AFT CABIN". CORRECTIVE ACTION: FOUND NO POST FLT REPORT AND ALSO NO CLASS 3 FAULT ON PSCU. OPERATED RT AFT DOOR SEVERAL TIMES. INDICATION FOUND NORMAL. PERFORMED PSCU BITE TEST IAW AMM 52-71-00 TEST PASSED. (7722769)Sep 15, 2021 · N392HA · Airbus A330243 · Door Warning SystemSDR HALA2021061000067Fire Loop · faultedETOPS-APU FIRE LOOP A FAULT// TSM 45-13-51-810-976-A,,ACTIONED. FAULT 261334 FDU APU (13WG).REMOVD AND REPLACED APU FDU PER A330 AMM 26-13-34, FAULT CLEARED AND TEST PASSED. AC OK FOR SVC. P/N OFF 3711-00, S/N OFF ZL1594; P/N ON 3710-00-00, S/N ON HW1530, FTJun 9, 2021 · N392HA · Airbus A330243 · Fire DetectionSDR HALA2021050500055Support Rod · shearedETOPS - DURING NBR 1 ENG INPECTION FOUND ANI ICE VALVE DUCT SUPPORT ROD SHEARED // INSTALLED DUCT SUPPORT ROD END. REF A3330 IPC 30-21-48-60 ITEM 300. OK FOR SVCMay 4, 2021 · N392HA · Airbus A330243 · Engine Anti-Icing SystemSDR HALA2021020800011Seal · leakingSHIP 0392 LOUD PRESSURE SQUEAL AT 1R DOOR DURING MOST OF DESCENT UNTIL FINAL APPROACH. CORRECTIVE ACTION: DOOR SEAL INSPECTED CLEANED AND LUBED SEAL CHKS NML. (7268157)Feb 8, 2021 · N392HA · Airbus A330243 · Service DoorsSDR HALA2020122900227Blade · damagedETOPS-ON WALK AROUND, FOUND POSSIBLE DAMAGE ON FAN BLADE NR 17 ON NR 1 ENGINE, 25" FROM TIP OF BLADE. PERFORMED DYE PENETRANT TEST, PER EM 72-31-11-200-801 CRACK FOUND 2 LOCATIONS 386502. REMOVED NR 17 FAN BLADE S/N 48872, REF AMM 72-31-41. INSTALLED NR 17 FDec 25, 2020 · N392HA · Airbus A330243 · Turbine Engine Compressor SectionSDR HALA2020122404256Sign · detachedTHE EXIT SIGN AT THE 3R DOOR WAS BUMPED BY A PAX AND NEED TO BE RE INSTALLED. CORRECTIVE ACTION: RESINTALLED 3R EXIT SIGN.Dec 24, 2020 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2020101303351Skin · dentedC-CHECK, LT WING LEADING EDGE NR 6 LEADING EDGE HAS LARGE LEADING EDGE DENT. CORRECTIVE ACTION: REPAIRED PER A330 SRM 57-40-00-300-009.Oct 10, 2020 · N392HA · Airbus A330243 · Wing, Plate/SkinSDR HALA2020100803313Release Mech · out of adjustEMERGENCY EQUIPMENT, PASSENGER/CREW DOOR EVACUATION SLIDE ARMING LEVER SAFETY PIN CAN BE INSERTED WITH THE LEVER IN THE ARMED POSITION. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0282:5200-2012-HAL /008 00046. CLEANED AND ADJUSTED EMERGOct 6, 2020 · N392HA · Airbus A330243 · Passenger/Crew DoorsSDR HALA2020100500099Floor Panel · delaminatedFWD CARGO, FLOOR PANEL 132EG (ON PARTS RACK), HAS CORNER DELAMINATED. CORRECTIVE ACTION: SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0221:2000-1001-HAL /006 00123. REPAIRED PANEL WITH REFERENCE TO HAL A330 SRM 53-02-00.Oct 3, 2020 · N392HA · Airbus A330243 · Fuselage Floor PanelSDR HALA2020091000179Blade · defectiveBLADE, LP COMPR OFF 43-7231-9-0003 49448 ON 43-7231-9-0003 44304, SECURITY CHECK GOOD. OK FOR SERVICE. REPLACED NR 1 ENG LP COMPRESSOR BLADE NR 5, PER AMM 72-31-41. CONCAVE SIDE. 130 MM FROM L/E, 316 MM FROM TIP, 90% DEFLECTION, PHASE ARRAY INSPECTION- NRSep 9, 2020 · N392HA · Airbus A330243 · Turbine Engine Air Inlet SectionSDR HALA2020072400156Bleed Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - AIR ENG 2 BLEED NOT CLOSED ON ECAM DURING ENGINE RUN. RESET NO HELP. // PHYSICALLY MOVED THE PRV BLEED VALVE AND SUSPECT THE SHAFT IN PRV IS SHEARED. NEED NEW PRV. REPLACED #2 ENG PRV PER AMM 36-11-52-400-804-A. OPS AND LEAK CHEJul 23, 2020 · N392HA · Airbus A330243 · Compressor Bleed ValveSDR HALA2020032600077Stud · lockedETOPS SIGNIFICANT SYSTEM - #2 ENG GREEN HYD PUMP HAS TWO KEY LOCKED STUDS (12 O CLOCK & 3 O CLOCK POSITION) THAT REQUIRES BEING REPLACED.// REPLACED BOTH KEY LOCKED STUDS ON #2 ENG GREEN SYS HYD PUMP GEARBOX HOUSING PER AMM 72-61-41-300-801-A. SECURITY CHK OK.Mar 25, 2020 · N392HA · Airbus A330243 · Turbine Engine Oil SystemSDR HALA2020100500098Skin · dentedUPON WALK AROUND FOUND LEFT INBOARD FLAP TRAILING EDGE DENT 4IN L, 3IN W, 1.5MM DEPTH. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR, PER A330 SRM 57-54-00. NO FURTHER INSPECTIONS REQUIRED.Mar 11, 2020 · N392HA · Airbus A330243 · Trailing Edge FlapsSDR HALA2020022700043Probe · burnedETOPS SIGNIFICANT SYSTEM- DURING LIGHTNING STRIKE INSPECTION FOUND LIGHTNING DAMAGE ON PITOT PROBE 3 (9DA3). // REMOVED AND REPLACED PITOT PROBE 3 (9DA3) PER AMM 34-11-15-000-801-A/400-801-A. NO BLOCKAGE NOTED. BITE OF THE PHC 3 OK - NO FAULTS NOTE. OK FOR SVCFeb 26, 2020 · N392HA · Airbus A330243 · Pitot/Static Anti-Ice SystemSDR HALA2019110306361Cids · malfunctionedEXIT SIGNS AT DOOR 3L AND 4L ARE NOT ILLUMINATED. CYCLED CIDS CIRCUIT BREAKERS AND EPSU TEST. LP 5880581.Nov 2, 2019 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2019102100432Sign · brokenDURING CABIN VISIT, FOUND 3R EXIT SIGN BROKEN. // REPLACED EXIT SIGN AT 3R PER A330 AMM 33-51-10.Oct 20, 2019 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2019072300365Seal · wornETOPS / ENG#2 REQUIRED 6QTS OF OIL. PERFORMED ENGINE RUN AND FOUND OIL LEAKING FROM BREATHER OUTLET. REMOVED BREATHER OUTLET/ELBOW DUCT AND BREATHER COVER PER AMM 72-61-0-0-801-A. FOUND BREATHER HOUSING AIR BLOWN SEAL WORN. REPLACED BREATHER COVER AND BREATHEJul 23, 2019 · N392HA · Airbus A330243 · Turbine Engine Oil SystemSDR HALA2019071900363Control Unit · faultedETOPS / ENG 1 CTL SYS FAULT ECAM AFTER ENG SHUTDOWN. REMOVED AND REPLACED #1 ENG VSV CONTROL UNIT PER AMM 75-33-51.Jul 19, 2019 · N392HA · Airbus A330243 · Turbine Engine Compressor SectionSDR HALA2019071500360Heat Shield · damagedETOPS SIGNIFICANT SYSTEM - #2 ENG VIEW FROM AFT AT 4:00 CLOCK POSITION TR HEAT SHIELD BLANKET HAS A HOLE 4" LONG. WELDED TEXTURE PATCH PER SAFRAN CMM 78-30-20 FRSX066 REPAIR 1. REMOVED #2 ENG O/B CENTER HEAT SHIELD BLANKET REF MM 78-30-20. INSTALLED #2 ENG CENJul 11, 2019 · N392HA · Airbus A330243 · Engine Thrust ReverserSDR HALA2019062540331Generator · inoperativeETOPS: AFTER LANDING DURING APU START APU GEN FAULT- 2ND ATTEMPT SAME RESULT // REMOVED APU GENERATOR PER AMM 24-23-51-000-801-A. INSTALLED APU GENERATOR IAWAMM 24-23-51-400-801-A. OPS CHECK PENDING. 6/22/2019 2361689. APU GENERATOR OPS CHECK GOOD.Jun 21, 2019 · N392HA · Airbus A330243 · AC Generator-AlternatorSDR HALA2019041600192Hf Comm · malfunctionedETOPS - HF 2 WILL NOT TUNE. DEFER PER MEL 23-11-01B. TROUBLESHOOT SYSTEM LATER. ODI PREVENTION. MEL PLAC INSTALLED. OK FOR SERVICE. DMI # 511467Apr 16, 2019 · N392HA · Airbus A330243 · HF Communications SystemSDR HALA2019041800000Hf Comm · malfunctionedETOPS - HF 2 WILL NOT TUNE. DEFER PER MEL 23-11-01B. TROUBLESHOOT SYSTEM LATER. ODI PREVENTION. MEL PLAC INSTALLED. OK FOR SERVICE. DMI # 511467.Apr 16, 2019 · N392HA · Airbus A330243 · HF Communications SystemSDR 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 Mar 14, 2019 · N392HA · Airbus A330243 · Stabilizer Control SystemSDR 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 Mar 12, 2019 · N392HA · Airbus A330243 · Autopilot SystemSDR HALA2019020700041Light · brokenDOOR 3R EXIT LIGHT BROKEN, RE-INSTALLED LENS COVER.Feb 7, 2019 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2019020700043Cover · crackedDOOR 3R EMERGENCY EXIT SIGN ASSEMBLY CRACKED. REPLACED SIGN COVER.Feb 6, 2019 · N392HA · Airbus A330243 · Emergency EquipmentSDR HALA2019020700049Lens · brokenETOPS SIGNIFICANT SYSTEM - EMERGENCY EXIT LIGHT 3R DOOR CRACKED AND BROKEN. RE-INSTALLED LENS COVER, NO DAMAGE NOTED OK FOR SVC.Feb 6, 2019 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2019010400005Warning System · false activationETOPS SIGNIFICANT SYSTEM - ON LANDING ENG 2 REV FAULT. PERFORMED TEST OF THRUST REVERSER DEPLOYMENT & STOWAGE PER AMM 78-31-00-740-802-A NO FAULT NOTED, GRND SCANNING SHOWS NO FAULTS OK FOR SVC.Jan 2, 2019 · N392HA · Airbus A330243 · Engine Thrust ReverserSDR HALA2018122400670Gear · damagedETOPS SIGNIFICANT SYSTEM - APU DOOR SHOWS OPEN WITH APU IN OFF POSITION/ AUTO SHUT DOWN ON ECAM.// PERFORMED BITE TEST ON APU SHUTDOWN MSG OIL CONTAMINATION OIL CHIP DETECTION REMOVED AND REPLACED FILTERS, AND INSPECTED CHIP DETECTORS. MSG CLEARS DOOR ACTDec 21, 2018 · N392HA · Airbus A330243 · Airborne Auxiliary Power Unit (APU) SystemSDR HALA2018121900665Fault Message · false activationETOPS SIGNIFICANT SYSTEM - ENGINE 1 REV. FAULT. // OPS TEST #1 ENG REV PER A330 AMM 78-31-00-740-802-A, OPERATION NORMAL. A/C, OK FOR SERVICE.Dec 18, 2018 · N392HA · Airbus A330243 · Central WarningSDR HALA2018111200332Sign · unsecureDOOR 3R CEILING EXIT SIGN IS BROKEN. RE-SECURED 3R CEILING EXIT LIGHT.Nov 11, 2018 · N392HA · Airbus A330243 · Emergency LightingSDR HALA2018110500364Sensor · dirtyETOPS SIGNIFICANT SYSTEM - COCKPIT TEMP DIFFICULT TO CONTROL WITH A FIXED TEMP SETTING,SUPPLY AIR VARIES FROM VERY COLD TO VERY HOT.// CLEANED FLIGHT DECK TEMP SENSOR AND LINE PER A330 AMM 21-63-17 PERFORMED SYSTEM TEST PER A330 AMM 21-63-00 OP CHECK NORMAL ONov 4, 2018 · N392HA · Airbus A330243 · Cabin Temperature Control SystemSDR HALA2018101900532Seat Track · corrodedSEAT TRACK BETWEEN FRAME 26 AND 37.4 AT -Y1959 IS CORRODED AT LOCATIONS: FR26+14", FR32+0",FR32+16", FR33+4", 37.3+0". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98. UNABLE TO FULLY REMOVE CORROSION DAMAGE OR ACCURATELY MEASURE DEPTH. DAMAGE LOCATEDOct 18, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018101900531Track · not reportedAFT CARGO ROLLER TRAY -Y1470, C58 - 60 REQUIRES REMOVAL FOR ACCESS. ROLLER TRAY REMOVED, DAMAGED BLENDED AND ASSESSED. FOUND TO BE OUT OF LIMITS DUE TO DAMAGE LARGER THAN 25MM DIAMETER AT ZONE 1, DAMAGE ALSO WITHIN 150MM LIMIT BETWEEN BLENDS AND OUT OF LIMIT DOct 18, 2018 · N392HA · Airbus A330243 · Cargo CompartmentsSDR HALA2018101900530Seat Track · corrodedSEAT TRACK BETWEEN FRAME 40 AND 47 AT +Y1957 IS CORRODED AT LOCATIONS: FR41+5", FR42+17", FR44+6", FR45+18".// CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 98. DAMAGE DIMENSIONS: CENTRAL AREA FR41+5?= 1" X 1" X 0.005", CENTRAL AREA FR44+6? = 2" X 0.5Oct 18, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018101800528Seat Track · corrodedSEAT TRACK BETWEEN FRAME 47 AND 53.2 AT +Y1957 IS CORRODED AT LOCATIONS: FR47+6", FR50+3", FR53.1+13". CORROSION REMOVED IAW SRM 51-74-00 REV 97. DAMAGE DIMENSION: AT FR47 + 6" AND FR50 + 3" LOCATED ON SEAT TRACK INNER VERTICAL AREAS, UNABLE TO SUFFICIENTLY REOct 18, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018101800527Seat Track · corrodedSEAT TRACK BETWEEN FRAME 26 AND 37.4 AT +Y1959 IS CORRODED AT LOCATIONS: FR26+16", FR30+0", FR30+9", FR32+4". CORROSION REMOVED IAW SRM 51-74-00 REV 98. DAMAGE DIMENSION: AT FR26+16", FR30+0", FR30+9", FR32+4" LOCATED ON SEAT TRACK INNER VERTICAL AREAS, UNABLEOct 18, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach FittingsSDR HALA2018101800526Roller Tray · corrodedBULK CARGO ROLLER TRAY FR65 TO FR68 +Y301 HAS CORROSION EVIDENT. ROLLER TRAY REMOVED IAW MM 25-51-21 R61.05 IAW CMM 25-51-83 REV4. CORROSION ON FLANGE BLENDED AROUND FASTENER HOLES. BLEND EXCEEDS ALLOWABLE LIMITS. EVIDENCE OF (LEVEL 2) CORROSION STILL PRESENT Oct 18, 2018 · N392HA · Airbus A330243 · Cargo CompartmentsSDR HALA2018101800525Seat Track · corrodedSEAT TRACK BETWEEN FRAME 26 AND 37.4 AT -Y1959 IS CORRODED AT LOCATIONS: FR26+14", FR32+0",FR32+16", FR33+4", 37.3+0". CORROSION REMOVED PER SRM 51-74-00 REV 98. UNABLE TO FULLY REMOVE CORROSION DAMAGE OR ACCURATELY MEASURE DEPTH. DAMAGE LOCATED AT -Y1959 FR26Oct 18, 2018 · N392HA · Airbus A330243 · Fuselage, Seat/Cargo Attach Fittings
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