N389HA
Service difficulty reports · 128
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 = 'N389HA' 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.
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 = 'N389HA' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR HALA2020022000040Light · missingEMERGENCY EXIT LIGHTING STRIP MISSING AT 4L DOOR FLOOR AREA. // REPLACED MISSING LIGHTED EMERGENCY STRIP PER A330 AMM 33-51
OPS CHK GOOD OK FOR SVC.SDR HALA2020013110022Eec · failedDURING TAXI OUT, THE NR 1 ENG FADEC FAULT MESSAGE, ENGINE SHUTDOWN SHORTLY AFTER ON ITS OWN. FOUND FAULT 732134, REMOVED AND REPLACED EEC IAW AMM 73-21-34. ALL TESTS AND ENGINE RUNS GOOD. CAT 3 AUTOLAND COMPLETED.SDR HALA2019120500505Pump · malfunctionedETOPS SIGNIFICANT SYSTEM - PRE DEPARTURE CREW FOUND R STBY FUEL PUMP SWITCH FAULT LIGHT ON, WHEN PUMP SELECTED ON .SD PAGE DISPLAYS LO. // R STBY FUEL PUMP ASSY REPLACED AND OPERATIONAL TEST CARRIED OUT OK.REF AMM 28-21-51-000-802A AND AMM 28-21-51-400-802A.SDR HALA2019100919376Lock · malfunctionedETOPS SIGNIFICANT SYSTEM - ENG 2 REV FAULT. TECHS RECOMMEND REPLACING PRIMARY LOCK OF RIGHT LOWER DOOR. REMOVED AND REPLACED PRIMARY LOCK OF RIGHT LOWER DOOR PER AMM 78-32-43. REVERSED "M" PROCEDURES. OPS CHECK THRUST REVERSE PER A330 AMM 78-31-00-740-802-A. NSDR HALA201910091975Lock · malfunctionedETOPS SIGNIFICANT SYSTEM - ENG 2 REV FAULT. MCC TECHS RECOMMEND REPLACING PRIMARY LOCK OF RIGHT LOWER DOOR. REMOVED AND REPLACED PRIMARY LOCK OF RIGHT LOWER DOOR PER AMM 78-32-43. REVERSED "M" PROCEDURES. OPS CHECK THRUST REVERSE PER A330 AMM 78-31-00-740-802-SDR HALA2019091200376Warning System · activatedOPEN - ETOPS - ENG 2 REV FAULT.SDR HALA2019090300365Unknown · malfunctionedUPON LANDING RIGHT BRAKE PEDAL WENT ALL THE WAY TO FLOOR WITH NO BRAKING PRESSURE RETURNED AS WE TAXIED IN. PERFORMED BSCU SYSTEM TEST AND NORMAL SYSTEM BRAKING TEST PER TSM 32-42-00. SYSTEM TEST OK. NO DEFECTS NOTED.SDR HALA2019080650834Sensor · malfunctionedETOPS - AMBER XX DISPLAYED RIGHT PACK BLEED PAGE // PERFORMED FIM TASK 21-53-00-810-844-A. REPLACED COMPRESSOR DISCHARGE TEMPERATURE SENSOR PER 21-53-11-000-801-A. OPS CHECK
GOOD.SDR HALA2019080650383Bleed Valve · inoperativeETOPS - APU BLEED VALVE FAULT ON ECAM. REMOVED AND REPLACED APU BLEED VALVE PER AMM 49-51-51-000-801-A. OPS CHECK OK PLACARD REMOVED LIDS CLEARED
VALVE, LOAD ASS OFF 33-4950-9-0002 02913 ON 33-4950-9-0002 02267SDR HALA2019072000123Tire · defectiveAIRCRAFT 389, ATO, ABORTED TAKEOFF AT 80-100 KNOTS DUE TO NOSE WHEEL HAD EXCESSIVE SHIMMY. CORRECTIVE ACTION: REPLACED LEFT AND RIGHT NOSE WHEEL TIRES. LP 5856045SDR HALA2019061400295Actuator · malfunctionedETOPS SIGNIFICANT SYSTEM - FUELERS REPORTED UNABLE TO FUEL AIRCRAFT. ECAM MSG - "FUEL T TANK XFR FAULT". // BITE TEST FAULTED FUEL OUTER TANK INLET VALVE 1 (500QU1). REMOVED AND
REPLACED LEFT OUTER TANK FUEL INLET VALVE ACTUATOR PER AMM 28-25-57-000-801-A. OPSDR HALA2019061100288Radio · inoperativeETOPS SIGNIFICANT SYSTEM, NR 2 HF RADIO WILL NOT TUNE. OPENSDR HALA201904043169Oil System · lowETOPS SIGNIFICANT SYSTEM - APU LOW OIL INDICATED ON APU ECAM PAGE. SERVICED APU TO FULL PER AMM 12-13 NO EXTERNAL LEAKS NOTED.SDR HALA201904043170Oil System · lowETOPS SIGNIFICANT SYSTEM - AFTER STARTING APU OBSERVED LOW OIL LEVEL ECAM. SERVICED APU AS REQUIRED 4 QTS ADDED,APU LOW OIL LEVEL LIGHT EXTINGUISHED. AIRCRAFT OKAY TO CONTINUE.SDR HALA2019031800129Computer · malfunctionedATB - ETOPS SIGNIFICANT SYSTEM - AUTO FLT AUTO THRUST OFF DURING CLIMB OUT. AUTO THRUST WAS ACTUALLY WORKING THOUGHT FOLLOWED PROCEDURES - ALL MESSAGES (STATUS ETC) WENT AWAY. CONTINUED FLT, THEN AUTO THRUST QUIT, RETURNED TO AIRPORT. REMOVE AND REPLACE FMG ECSDR 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 COMMANDESDR HALA2019010700011Oil System · lowETOPS SIGNIFICANT SYSTEM - LOW OIL LEVEL APU. PERFORMED GENERAL INSP. NO LEAKS NOTED. SVC'D APU OIL TO FULL PER AMM 12-13-49. RAN APU PER AMM 49-00-00. NO LEAKS NOTED. OK FOR SVC.SDR HALA2018123100681Sense Line · contaminatedETOPS SIGNIFICANT SYSTEM - ENG 1 CTL SYS FAULT CAME ON AT TOP OF DESCENT.// C/W A330 TSM 73-21-78-810-815 CLEANED MOISTURE TRAP AND BLEW OUT
P30 SENSE LINE. RAN ENGINE, NO FURTHER FAULTS NOTEDSDR HALA2018111400582Unknown · odorON DESCENT 5000' PAINT THINNER SMELL FOR ABOUT 5 MINUTES ENTIRE CABIN.// PERFORMED ENGINE GROUND RUN @ IDLE FOR APPROX 10 MINS NO SMELLS THROUGH CABIN OR COCKPIT NOTED. ALL CHECKS NORMAL A/C OK TO CONTINUE, EACH PACK ISOLATED DURING RUN, NO SMELLS NOTED OK FORSDR HALA2018101800524Not Reported · faultedETOPS SIGNIFICANT SYSTEM. ENG 2 MINOR FAULT. T/S PER TSM 73-21-71-810-952-A. PERFORMED GROUND REPORT NO FAULTS NOTED. OK TO CONTINUE.SDR HALA2018101700511Hf Comm · malfunctionedETOPS SIGNIFICANT SYSTEM, NR 2 HF WON'T TUNE. RESET HF2 ON 722VU. OPS CHK OKAY.SDR HALA2018053100270Seat Track · corrodedSEAT TRACK WAS FOUND CORRODED AT FRAME 40. 2+7, .3, & 3+8, FRAME 41, & 41+3, FRAME 42, & 42+15, FRAME 43+10, 44+6, 45, 46, AND 46+5. FOUND OUT OF LIMITS IAW SRM 53-31-15, REV 97. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, REV 97, AND DRAWING F57112824SDR HALA2018053000266Seat Track · corrodedSEAT TRACK BETWEEN FRAME FR47 AND 53.2 AT +Y450 IS CORRODED AT LOCATIONS: FR48-3" TO 4";FR49-9";FR49+8 TO 11";FR51;FR53-10". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 97. DAMAGE DIMENSIONS: FR 48-3?- 0.5" X 0.5" MAX DEPTH REMOVED 0.020" CENTRAL ARESDR HALA2018053000269Seat Track · corrodedSEAT TRACK BETWEEN FRAME 47 AND 53.2 AT -Y1959 IS CORRODED AT LOCATIONS: FR47+6";FR48;FR48+15";FR49+5";FR50+4";FR50+16 "FR51+14"FR52+7";FR53;FR53+8";FR53+12";FR53+1 4";FR53.1+7";FR53.1+14". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 97. DAMAGE DIMENSDR HALA2018053000268Thrust Washer · missingLEFT WING FLAP TRACK 1 CARRIAGE "Y" ROLLER THRUST WASHERS FOUND MISSING FROM UPPER I/B POSITION. LT FLAP TRACK NR 1 CARRIAGE INBD UPPER "Y" ROLLER THRUST WASHER REPLACED IAW AMM 27-57-77.SDR HALA2018053000267Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 54 AT -Y1959 IS CORRODED AT LOCATIONS: FR53.5+11". CORROSION REMOVED BY GRINDING AS PER SRM 51-74-00 REV 97. DAMAGE DIMENSIONS: DAMAGE DIMENSIONS: 1. BLEND DIMENSIONS: 1. FR53.5+11" SUPERIOR L=1.500" W=0.800" DEPTH=0.032" CENTSDR HALA2018052500256Seat Track · corrodedSEAT TRACK CORRODED AT FRAME 57+16. THE CORROSION WAS REMOVED IAW SRM 51-74-00 REV 97. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15, REV 97. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, REV 97, AND DRAWING F53476200, ISSUE R.SDR HALA2018052500255Seat Track · corrodedSEAT TRACK FOUND CORRODED AT FRAMES 59+5, 60+16, 62+5, 63+16. THE CORROSION WAS REMOVED IAW SRM 51-74-00, REV 97. THE SEAT TRACK WAS REPAIRED IAW SRM 53-41-15, REV 97.SDR HALA2018052500254Seat Track · corrodedSEAT TRACK CORRODED AT FRAMES 53.3+3, 53.5+11, AND 53.5+16. THE CORROSION WAS REMOVED IAW SRM 51-74-00, REV 97. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15, REV 97. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, REV 97, AND DRAWING F53326941, ISSUE A.SDR HALA2018052500253Seat Track · corrodedSEAT TRACK CORRODED AT FRAMES 47+4 - 6, 48-2, 49-4 - 6, 50+4.5 - 6.6, 51-2, 52-3.5, 52+9.5, 53+3.5 - 5.5, 53.1-2.5, AND 53.2-4.5 - 7. THE CORROSION WAS REMOVED IAW SRM 51-74-00, REV 97. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-15, REV 97. THE SEAT TRACK WAS RSDR HALA2018052500252Seat Track · corrodedSEAT TRACK CORRODED AT FRAMES 33-3, AND FR 33+2. THE CORROSION WAS REMOVED IAW SRM 51-74-00, REV 97. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, REV 97, AND DRAWING F53275878
ISSUE E.SDR HALA2018052500251Seat Track · corrodedSEAT TRACK CORRODED AT FRAMES 29, 29+7, 29+9, 29+16, 32+3, 32+13, 36, AND 37+7. THE CORROSION WAS REMOVED IAW SRM 51-74-00, REV 97. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, REV 97, AND DRAWING F53276421, ISSUE G.SDR HALA2018052500250Seat Track · corrodedSEAT TRACK CORRODED AT FRAMES 29-2, 30+8, 33, 33+6, 36-4, AND 37+8. CORROSION REMOVED IAW SRM 51-74-00, REV 97. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15, REV 97. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, REV 97, AND DRAWING F53276421, ISSUE G.SDR HALA2018052500249Seat Track · corrodedSEAT TRACK CORRODED AT FRAMES 53.3+3, 53.3+13, AND 53.4. THE CORROSION WAS REMOVED IAW SRM 51-74-00 REV 97. FOUND TO BE OUT OF LIMISTS IAW SRM 53-00-15, REV 97. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, REV 97, AND DRAWING F53326931, ISSUE A.SDR HALA2018052500248Seat Track · corrodedSEAT TRACK CORRODED AT FRAMES 37.4+5, 39+7.5, 39.1+5, 39.1+11.5, AND 39.2-2. THE CORROSION WAS REMOVED IAW SRM 51-74-00, REV 97. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-15, REV 97. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, REV 97, AND DRAWING F533111SDR HALA2018052500247Seat Track · corrodedSEAT TRACK CORRODED AT FRAME 57+15. CORROSION REMOVED IAW SRM 51-74-00 REV 97. FOUND OUT OF LIMITS IAW SRM 53-00-15, REV 97. SEAT TRACK REPLACED IAW SRM 51-72-11, REV 97, AND DRAWING F53476200, ISSUE R.SDR HALA2018052500257Seat Track · corrodedSEAT TRACK, -Y450 FOUND CORRODED BETWEEN FRAMES 72, AND 74+6. THE CORROSION WAS REMOVED IAW SRM 51-74-00, REV 97. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15, REV 97. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, REV 97, AND DRAWING F53478040, ISSUE G.SDR HALA201805250177Seat Track · corrodedDURING AN H CHECK, THE SEAT TRACK BETWEEN FRAMES 72 - 75, -Y450 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53478040.SDR HALA2018041700148Light · detachedFLOOR EMERGENCY LIGHT STRIP IN THE FIRST CLASS GALLEY, FOUND LOOSE FROM THE FLOOR. SECURED THE LIGHT STRIP.SDR HALA2018041800178Light · unsecureEMERGENCY LIGHT STRIP AT THE FIRST CLASS GALLEY FLOOR. UNSECURE. SECURED THE LIGHT STRIP, CHECKED GOOD. OK TO CONTINUE.SDR HALA2018041600172Idg · low pressureAIR TURNBACK DUE TO AN ELECTRIAL NR 1 IDG OIL LOW PRESSURE. REMOVED AND REPLACED THE NR 1 IDG IAW AMM 24-24-51, OPS AND LEAK CHECKED GOOD. BITE TESTED GOOD.SDR HALA2018040900132Light · looseFLOOR EMERGENCY LIGHT STRIP BY JUMPSEAT 41R IS LOOSE. SECURED THE EMERGENCY LIGHTING STRIP.SDR HALA2018032700124Warning Message · false activationAUTO FLT FCU FAULT. PERFORMED AN AFS SYS TEST IAW AMM 22-96-00. MESSAGE CLEARED. TESTED OK. OK FOR SERVICE.SDR HALA2018031100081Light · detachedEMERGENCY LIGHT PEELING OFF THE FLOOR IN THE AFT GALLEY BETWEEN THE JUMP SEATS, SECTION MISSING. REPLACED THE EMERGENCY LIGHT STRIP IN AFT GALLEY.SDR HALA2018030500069Light · unsecureAFT GALLEY FLOOR LIGHT STRIP COMING UP FROM FLOOR. NEEDS TO BE SECURED. SECURED LIGHT STRIP AS REQUIRED. OK FOR SERVICE.SDR HALA2018021500043Sign · malfunctionedEXIT SIGN AT DOOR 3L WAS STROBING, NOW IT'S ORANGE. RESET CIDS AMM 23-35-00, OPS CHECK GOOD OK FOR SERVICE.SDR HALA2018021500030Sign · malfunctionedEXIT SIGN AT DOOR 3L WAS STROBING AND NOW IS ORANGE. RESET CIDS PER AMM 23-35-00.SDR HALA2018013000025Warning Message · false activationOIL ALERT FOR THE NR 1 ENGINE. INSPECTED THE NR 1 ENG FOR OIL LEAKS. NO ABNORMALITIES FOUND. ACFT OK FOR RETURN TO SERVICE.SDR HALA2017122700325A/C Pack · overheatedAFTER ENGINE START, THE NR 2 AIR PACK OVERHEAT. ACCOMPLISHED ECAM ACTIONS. ECAM ILLUMINATED FOR PACK TEMP AT 144 DEGREES. PACK TEMP COOLED WHEN SELECTED OFF, TURNED ON NORMAL.SDR HALA2017103100265Oil Cooler · faultedDIVERSION/ATB, APU FAILED/AUTO SHUTDOWN DURING TEST FLIGHT. HIGH OIL TEMP-OIL COOLER AND COOL FAN ASSY FAULTED. REPLACE OIL COOLER.
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