N385HA

Service difficulty reports · 172

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 = 'N385HA' 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 HALA201506100106Filter · dirtyAPU BLEED FAULT, ECAM MESSAGE. OPS CHECKED BAD, RESISTANCE CHECK OK IAW TSM 49-62-00-810-841-A. REMOVED, CLEANED AND REINSTALLED APU BLEED VALVE FILTER ELEMENT IAW AMM 49-51-51-960-801A. OPS CHECKED GOOD.Jun 9, 2015 · N385HA · Airbus A330243 · Pneumatic Distribution SystemSDR HALA2015060500103Blade · vibrationAIR TURNBACK, FLT 7 DIVERTED AS CREW PRECAUTION DUE TO VIBRATION IN CRUISE AT 1.7 THRU CLIMB FL 360-380 N1 VIBRATION LT ENGINE. CLIMBING TO 3.9 REDUCED POWER STABLE AT 1.5 IN TURN CLIMBED TO 1.7, TROUBLESHOT IAW TSM 77-00-00-810-814-A22. VIBRATION DUE TO FANJun 3, 2015 · N385HA · Airbus A330243 · Turbine Engine Compressor SectionSDR HALA2015060405015Engine · vibrationRETURNED TO DEPARTURE DUE TO NR 1 ENGINE, N1 VIBRATION CLIMBED TO 3.9 DURING CLIMB THRU FL 360-380, REDUCING POWER N1 STABILIZED AT 1.5 IN TURN CLIMBED TO 1.7. TROUBLESHOOT IAW TSM 77-00-00-810-814-A22. VIBRATION DUE TO FAN LUBE AND WITHIN LIMITS FOR QC MONIJun 3, 2015 · N385HA · Airbus A330243 · Engine (Turbine/Turboprop)SDR HALA2015052805014Pin · migratedLEFT EMERGENCY EXIT GIRT BAR AFT PIN MIGRATED OUT. MAINTENANCE RESECURED THE RELEASE PINS.May 27, 2015 · N385HA · Airbus A330243 · Emergency EquipmentSDR HALA2015052700099Pin · migratedLEFT EMERGENCY EXIT GIRT BAR AFT PIN MIGRATED OUT. RESECURED RELEASE PINS, PERFORMED CHECKOUT REF AMM 25-62-42. OPS CHECK GOOD.May 27, 2015 · N385HA · Airbus A330243 · Emergency EquipmentSDR HALA2015032200070Slide · faultedSLIDE FAULT ON FAP. R & R 4L DOOR SLIDE IAW AMM 25-62-41-000-801-A01 AND AMM 25-62-41-400-801-A AND WC 2561-4004-4L. OPS AND SECURITY, CHECK GOOD INSPECTION.Mar 22, 2015 · N385HA · Airbus A330243 · Escape SlideSDR HALA2015033105008Slide · failedSLIDE FAULT ON FAP. MAINTENANCE R & R 4L DOOR SLIDE. OPS AND SECURITY CHECK GOOD.Mar 22, 2015 · N385HA · Airbus A330243 · Escape SlideSDR HALA2015022005004Warning Message · activatedAIRCRAFT 385 ATB, RETURNED TO DEPARTURE DUE TO NR 1 ENGINE AIR EXCHANGER FAULT. TROUBLESHOT IAW TSM 79-20-00-810-809A, FADEC SYSTEM TEST OK, GROUND CHECK WITH NO ECAM MESSAGES, RAN NR 1 AND 2 ENGINES ON THE GROUND, ALSO NO ECAM MESSAGES APPEARED. ACFT RETURNFeb 19, 2015 · N385HA · Airbus A330243 · Engine Oil System (Airframe Furnished)SDR HALA2015021900021Warning Light · false activationETOPS SIGNIFICANT SYSTEM - ENGINE 1 AIR EXCHANGER FAULT. REF TSM 79-20-00 FADEC SYS TEST OK GROUND CHK, NO ECAM MSG BOTH ENGINE 1, 2 RUNNING ON GROUND ALSO NO ECAM MSG, OK FOR SERVICE, MAINTENANCE NOTIFIED.Feb 19, 2015 · N385HA · Airbus A330243 · Engine Oil System (Airframe Furnished)SDR HALA2014120200202Fmu · malfunctionedAT LANDING ENG 1 CONTROL SYS FAULT, ECAM CAUTION LOG-PAGE UPDATED AT 02DEC14 1206 UTC. REMOVED NR 1 FMU IAW AMM 73-21-52. INSTALLED NR 1 ENGINE FMU REF AMM 73-21-52-400-802-A UP TO AND INCLUDING STEP 5A. C/W REST OF AMM 73-21-52. OPS, LEAK CHECK GOOD OK FORDec 2, 2014 · N385HA · Airbus A330243 · Fuel Control/Turbine EnginesSDR HALA2014100500164Fcu · leakingFOUND FUEL LEAKING FROM APU FUEL CONTROL UNIT. R & R APU FUEL CONTROL UNIT IAW MM 49-32-51-000-8 01-A/-400-801-A, OPS CK/LEAK CK GOOD, OK FOR SVC.Oct 5, 2014 · N385HA · Airbus A330243 · APU Engine Fuel and ControlSDR HALA2014092200161Skin · damagedDURING PDC FOUND DAMAGE TO AFT CARGO DOOR INNER SKIN. REMOVED INNER CARGO DOOR LINING PANELS AND LOWER CARGO DOOR ACCESS PANELS IAW AMM 52-32. CUT OUT DAMAGED AREA 2 PLACES TO 1" DIA. PERFORMED HFEC IAW ERA 529302-14, NO INDICATIONS. FABRICATED DOUBLERS & FSep 22, 2014 · N385HA · Airbus A330243 · Cargo/Baggage DoorsSDR HALA2014083100127Pump · contaminatedFUEL ECAM FOR LT PUMP FAULT. TROUBLESHOT IAW TSM 28-21-00-810-852, PURGED LEFT PUMP BOOST PUMP. FOUND DIRT AND WATER WHILE PURGING BOOST PUMP. NOW OPS NORMAL, OK FOR SERVICE.Aug 31, 2014 · N385HA · Airbus A330243 · Fuel Boost PumpSDR HALA2014081500114Toilet · leakingF/A REPORT LAV G HAS UNSTOPPABLE SEWAGE LEAK, AIR TURN BACK. INSTALLED NEW TOILET ASSY AT LAV G IAW AMM 38-31-41, OPS CHECKED OK. OK FOR SERVICE.Aug 15, 2014 · N385HA · Airbus A330243 · Waste Disposal SystemSDR HALA2014060700079Radome · crackedBIRD STRIKE DURING TAKEOFF. BIRD HIT UNDER THE COCKPIT ON CAPTAIN'S SIDE. PERFORMED BIRD STRIKE INSPECTION IAW MM 05-51-14. FOUND DAMAGE TO RADOME ON CAPT'S SIDE. FOUND A 6" VERTICAL CRACK AND A 9" HORIZONTAL CRACK. ALSO, FOUND DELAMINATION. R & R RADOME Jun 7, 2014 · N385HA · Airbus A330243 · Aerodynamic FairingsSDR HALA2014052600070Pitot Tube · failedCIRCUIT BREAKER TRIPPED FOR STANDBY PITOT HEAT DURING CLIMBOUT. WIRING CHECKED BETWEEN PHC-3 TO 9DA3, FOUND OK IAW AWM 30-31-06. R & R STANDBY PITOT IAW 34-11-15. REPLACED PHC-3 IAW AMM 30-31-34. OPS CHECK OK. OK FOR SERVICE.May 26, 2014 · N385HA · Airbus A330243 · Pitot/Static SystemSDR HALA2014042100049Warning Message · false activationADVANCING THROTTLES DURING TAKE OFF, ECAM AUTO THRUST FAULT. RETURN TO GATE. RTO 10 KTS. PERFORMED AFS AND LAND TEST IAW AMM 22-96 AND 22-97. SYSTEM OPS NORMAL. OK FOR SERVICE.Apr 21, 2014 · N385HA · Airbus A330243 · Autopilot SystemSDR HALA2014011300005Pitot Line · obstructedCAPTAIN`S AIRSPEED FAILED AFTER TAKEOFF ABOVE 100KTS. F/O'S AIRSPEED INDICATED 20 KTS SLOWER THAN NR 3 ON ISIS. NR 3 SEEMED CORRECT COMPAIRED TO GROUND SPEED. LOST AUTOPILOT, AUTOTHROTTLES, FMA-FLT DISPLAYS WENT TO ALT LOW. ACCOMPLISHED TSM 34-10-00. FLUSJan 13, 2014 · N385HA · Airbus A330243 · Pitot/Static SystemSDR HALA2013051300059Transmitter · malfunctionedETOPS SIGNIFICANT SYSTEM - BTB - FF INDICATION RT ENGINE AMBER LINES THRU INDICATION. RESET L& R FCMC AS PER MMNT. INSTRUCTIONS, NO CHANGE IN RT FF INDICATION, RETURNED TO GATE. C/W TSM 73-30-00-810-806-A, PER TSM REMOVED AND REPLACED NR 2 ENG FUEL FLOW TRANMay 13, 2013 · N385HA · Airbus A330243 · Fuel Flow IndicatingSDR HALA2012091400210Altimeter · out of limitsON DECENT "NAV ALTI DISCREPANCY" ALTIMETERS SHOWED UP TO A 300' DIFFERENCE. PERFORMED AMM 34-13-00-740-803A, ADR SYS TEST, NO FAULT NOTED, ACFT IS OK FOR SVC.Sep 14, 2012 · N385HA · Airbus A330243 · Altimeter, Barometric/EncoderSDR HALA2012090200200Power Supply · inoperativeEPSU AT 4R DOOR WILL NOT TEST. R & R 4R EPSU BATTERY TEST. OPS CHECKED GOOD.Sep 2, 2012 · N385HA · Airbus A330243 · Emergency LightingSDR HALA2012051900142Blade · nickedON WALK AROUND FOUND A NICK ON NR 1 ENGINE, LPC BLADE NR 21. FOUND BLADE NR 21 TO BE WITHIN LIMITS IAW MM 72-31-41 PAR (6).May 19, 2012 · N385HA · Airbus A330243 · Turbine Engine Compressor Section
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