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.
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
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 HALA2021120700219Rib · corrodedSHIP 385 Z670 RH MLG: RIB 6 FWD & AFT LUGS MODIFICATION AS PER 5753-01163 -08B. CORROSION REMOVAL AT FWD LUG FWD & AFT SPOTFACE FOUND BEYOND LIMIT. CORRECTIVE ACTION: CARRIED OUT AIRBUS REPAIR INSTRUCTION R575-58741 ISSUE E. ASSOCIATED ER/A 14-594565. (2043711SDR HALA2021120700218Rib · corrodedSHIP 385 WHILE PERFORMING EM 5753-01164 (A330 SB 57-3124 R3), CORROSION WAS FOUND ON THE RH RIB 6 FWD LUG BORE AND FWD AND AFT FACES. CORRECTIVE ACTION: RBUSHES REWORKED AS PER ER/A 594565-14AD. (2043706)SDR HALA2021121000224Fitting · corrodedSHIP 385 CORROSION WAS FOUND ON THE RH RIB 6 FITTING. CORRECITVA ACTION: REF ERA 594565-14. (2043088)SDR HALA2021121000223Fitting · corrodedSHIP 385 CORROSION WAS FOUND ON THE L/H RIB 6 FITTING. CORRECTIVE ACTION: REF ERA 594564-14AD. (2043034)SDR HALA2021100800151None · noneSHIP 385 EMERGENCY EXIT SIGNS IN THE CABIN WILL NOT TURN OFF USING COCKPIT OVERHEAD PANEL SWITCH. CORRECTIVE ACTION: PERFORMED OPS TEST OF EMERGENCY LIGHTS IN REFERENCE TO AMM 33-51 . NO DEFECTS NOTED. (7734202)SDR HALA2021100500134A/C Pack · odorDURING LANDING ROLLOUT BURNING SMELL IN COCKPIT AND CABIN. TAXI OFF AND AFTER 4 MINS - ECAM PACK #1 FAULT. TURNED #1 PACK OFF AND SMELL/SMOKE SUBSIDED. REMOVED AND REPLACED LEFT PACK ACM PER AMM 21-52-21. OPS AND LEAK CHECK OK. NO SMELLS NOTED. OK FOR SVC. SDR HALA2021090800130Sign · detachedSHIP 385 3R EXIT SIGN FELL OFF. CORRECTIVE ACTION: REPLACED EXIT SIGN AT 3R JUMPSEAT. (7233028)SDR HALA2021031100050Bottle · low pressureSHIP 385 CHECK 1R DOOR PRESSURE CAME ON DURING DECENT ON THE 1ST F/A PANEL. CORRECTIVE ACTION: SERVICED PER A330 AMM 52-11. (7260601)SDR HALA2021030800028Heat Exchanger · leakingETOPS - #2 ENG OIL LEAKING OUT OF AIR-OIL COOLER FINS // REMOVED ENG #2 AIR-OIL HEAT EXCHANGER PER A330 AMM 79-21-51. WIP 939166. INSTALLED AIR OIL HEAT EXCHANGER AND TEST PER A330 AMM 79-21-51 TEST OK NO LEAKS NOTED COOLER, OIL-AIR OFF 43-7921-9-0001 41588 ONSDR HALA2021030500036Bottle · low pressureSHIP 385 FIRST FLIGHT ATTENDANT PANEL DOOR WARNING. CORRECTIVE ACTION: SERVICED 1R DOOR ASSIST BOTTLE PRESSURE PER A330 AMM 25-62-41. (5868328)SDR HALA2021021800016Cover · missingSHIP 0385 EXIT SIGN COVER MISSING ADJACENT TO 3R JUMP SEAT. CORRECTIVE ACTION: INSTALLED LENS COVER AS REQUIRED. (7266951)SDR HALA2020122900229Cylinder · low pressureEMERGENCY EQUIPMENT R1 DOOR EMERGENCY OPERATION CYLINDER PRESSURE IN AMBER BAND. C/W CHARGING AIR FOR R1 DOOR EMERGENCY OPERATION CYLINDER, PER A330 AMM 52-10-00 VERIFIED SAFETY PIN REMOVED FROM BOTTLE. RII COMPLIED WITH QC 5180.SDR HALA2020122200224Actuator · defectiveETOPS, FUEL QTY STARTED FLASHING APPROXIMATELY 1 HOUR AND 20 MINS OUT AND AUTO FWD TRIM XFER LEFT ONLY CREATED INNER MAIN TANK IMBALANCE OF MORE THAN 6600LBS. PERFORMED T/S, AS PER A330 TSM TASK28-25-00-810-827-A. FOUND R INNER INLET VALVE DOES NOT MOVE. RESDR HALA2020121600222Actuator · defectiveATB-ECAM FUEL OUTER TANK TRANSFER RT OUTER FAILED TO OPEN. 6100 LBS TRAPPED. DIVERTED TO KLAX. REMOVED & REPLACED OUTER TANK FUEL INLET ACTUATOR, PER A330 AMM 28-25-57 OK FOR SERVICE. TAGGED PART PER TOPP 40-28-85 ODI REQUIREMENT ACTUATOR, SINGLE OFF 43-28SDR HALA2020080310165Fcu · unknownETOPS SIGNIFICANT SYSTEM - "MAP NOT AVAIL" STAYED ON CAPT ND. REMOVED AND REPLACED FCU PER AMM 22-81-12. OPS TEST GOOD. NO FAULTS NOTED. PERFORMED LAND CAT III CAPABILITY TEST PER AMM 22-97-00. TEST PASSED. OK FOR SVC.SDR HALA2020073100161Pcu · malfunctionedETOPS SIGNIFICANT SYSTEM - DURING 14 DAY CHECK, FOUND ENG 2 REV FAULT ON THRUST REVERSER CYCLE. DURING TROUBLE SHOOTING, FOUND FAULT CODE 783751, T LOCK (E2-
4005EG1 1/2/3/4) PCU (EG4007EG) BLOCKER DOORS 1 & 2 UPPER RIGHT AND LOWER RIGHT. REMOVED AND SDR HALA2020022400042Module · unknownETOPS SIGNIFICANT SYSTEM - #2 ENGINE FAULT ON THRUST REVERS-ER - T LOCK / PCM. // TROUBLESHOT REF. A330 TSM 78-37-00-810-833-A. REPLACED POWER CONDITIONING MODULE PER A330 AMM 78-37-61 AND COMPLETED TEST OF THRUST REVERS-ER DEPLOYMENT AND STOWAGE. OPS NORMAL PSDR HALA2020021000032Insert · missingRIGHT WING NUT PLATE INSERT MISSING AT WING FWD SPAR OUTBOARD OF # 1 SLAT TRACK. // REMOVED AND REPLACED NUT PLATE, REF. A330 SRM 51-42-11.SDR HALA2020021000031Actuator · failedETOPS SIGNIFICANT SYSTEM - FUELER'S REPORT END LIGHT FLASHING ON FUEL PANEL. // FUEL VALVES TEST SHOWS JETTISON VALVE 2 FAIL UNKNOWN. REMOVED
AND REPLACED JETTISON VALVE 2 FUEL ACTUATOR (100QV2) PER AMM 28-31-51. CHK OK.SDR HALA2020020760061Cids · malfunctionedON PARKING CHECKLIST, WHEN TURNING OFF EMERGENCY EXIT LIGHT EMERGENCY LIGHT ILLUMINATED AND WOULD NOT CYCLE OFF. RESET CIDS NBR 1 AND 2. LP 7228076SDR HALA2020020300026Sensor · malfunctionedETOPS SIGNIFICANT SYSTEM - AIR BLEED LOW TEMP ON BLEED 2 LEFT ENGINE BLEED TEMP 165C/24PSI, RIGHT ENGINE BLEED TEMP 75C/20PSI. LEFT PACK 108C INPUT/10C
OUTPUT. RIGHT PACK 102C INPUT/10C OUTPUT. // REPLACED RIGHT ENGINE EX-CHANGER OUTPUT TEMP SENSOR PER ASDR HALA2020013110021Sensor · malfunctionedETOPS - 1. AIR BLEED LOW TEMP ON BLEED 2 LEFT ENG BLEED TEMP 165C/24PSI. 2. OPEN - ECAM MSG: "APU BLEED FAULT" // 1. REPLACED RIGHT HEAT EXCHANGER OUTPUT SENSOR PER AMM 36-11-17, OPS AND LEAK CHECKS GOOD. 2. DEFERED BLEED VALVE INOP. LOG PAGE 7228023SDR HALA2020013100020Warning Light · illuminatedETOPS - AIR BLEED LOW TEMP BLEED 2 LEFT ENGINE, ECAM MESSAGE. APU BLEED FAULT. OPENSDR HALA2020012760017Isolation Valve · inoperativeSUP - ECAM MSG FUEL TRIM LINE FAULT WHEN APU SHUTDOWN, APU ISOL VALVE INOP. // REMOVED AND REPLACED FUEL ISOLATION VALVE ACTUATOR PER TSM 28-29
-00-810-802-A. OPS CHECK GOOD. OK FOR SVC.SDR HALA20200127001Isolation Valve · inoperativeOPEN - ETOPS, ECAM MESSAGE FOR FUEL TRIM LINE FAULT WHEN APU SHUTDOWN, FOUND APU ISOLATION VALVE INOPERATIVE.SDR HALA2020010870005Bleed Valve · malfunctionedETOPS SIGNIFICANT SYSTEM - FOUND MAINT MSG "APU BLEED FAULT" ON UPPER ECAM, WHEN APU BLEED SW TURNED "ON". // REPLACED APU BLEED VALVE REF A330 AMM 49-51-51. OPS CK NML.SDR HALA2019111800489Actuator · malfunctionedETOPS SIGNIFICANT SYSTEM - FUEL - APU LP VALVE FAULT. // T/S PER A330 TSM 28-29-00-810-801-A. REPLACED LP SOV ACTUATOR PER A330 AMM 28-29. OPS NML. NO LEAKS FOUND. MSG ERASED. OK FOR SERVICE.SDR HALA2019111800490Starter · unknownETOPS SIGNIFICANT SYSTEM - APU FAULT ON START-UP UNABLE RESTART. // REMOVED AND REPLACED ECB PER AMM 49-61-34. CONDITION SAME. REPLACED APU FUSE 6KA1 PER AMM 49-42-00 AS PRECAUTIONARY. PERFORM ELECTRICAL INSPECTION OF APU STARTER TERMINALS AND RELAYS PER ESPM SDR HALA2019102900235Cover · missingDURING INSPECTION, RIGHT WING INBOARD FLAP TRACK FIXED FAIRING COVER MISSING. REPLACED NEW CAP ON WING FIXED FLAP TRACK. LP 6785353SDR HALA2019100200395Liner · damagedETOPS SIGNIFICANT SYSTEM - DURING ENG1 A1 CHECK, FOUND ATTRITION LINER DAMAGED @ 6'OCLOCK POSITION. FERRY FLIGHT REQUIRED. THIS AIRCRAFT HAS BEEN INSPECTED THIS DATE AND IS SAFE FOR INTENDED FLIGHT. // REMOVED #1 ENGINE S/N 42009 AND THRUST REVERSER PER TASK CSDR HALA2019053000266Unknown · odorSTRONG MUSTY- MOLDY WET ODOR THROUGHOUT A/C DURING TAKEOFF CLIMB TO 15,000 FEET AND DECENT FROM 15,000 TO TOUCHDOWN. INSPECTED APU COMPARTMENT NO EVIDENCE OF LEAK RAN APU WITH BOTH PACKS FOR A 2HR PERIOD AND NO UNUSUAL ODOR NOTED. PER TASK 49-16-00-100-801-A CSDR HALA2019052800255Oil System · leakingON DECENT STRONG SMELL OF DIRTY SOCKS COMING FROM VENTILATION SYSTEM. UPON INSPECTION FOUND EXCESSIVE OIL NEAR APU INLET DOOR. FOUND OIL LINE BACKED OFF. REPLACED PACKINGS AND REINSTALLED LINES. NO FURTHER LEAK NOTED FROM THAT LINE. AFTER RUNNING APU FOR SOME SDR HALA2019040412151Sign · brokenDOOR 3R EXIT SIGN TAB BROKEN. REPLACED DOOR 3R OVERHEAD EXIT SIGN LENS. LP 5849813SDR HALA2019022200061Wire · damagedATB - ETOPS SIGNIFICANT SYSTEM - ENG 2 FUEL FILTER CLOG ECAM IN FLIGHT. COMPLIED WITH MX PROCEDURE REMOVED AND REPLACED #2 ENG LP FUEL FILTER PER AMM73-11-41. LEAK CHECK PENDING. PERFORMED LEAK CHECK, OPS CHECK & LEAK CHECK GOOD, OK FOR SVC.FOUND WIRE 1P021BSDR HALA2019022100058Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ENG 2 FUEL FILTER CLOG ECAM AMBER CLOG ILLUMINATED UNDER F.USED. REMOVED INSPECTED AND REINSTALLED RT ENGINE FUEL FILTER ELEMENT PER AMM 73-11-41. NO DEBRIS NOTED ON FILTER. ACCOMPLISHED TSM 73-21-79 FOR FUEL FILTER CLOGGED MESSAGESDR HALA2019010200002Warning System · false activationETOPS SIGNIFICANT SYSTEM - ENG 2 REV FAULT. PERFORMED BITE PER A330 AMM 78-31. NO FAULTS PRESENT. OKAY FOR SVC.SDR HALA2018123100683Pump · leakingETOPS SIGNIFICANT SYSTEM - #1 ENG. LEAKING FROM EDP (GREEN SYS).// REMOVED AND REPLACED #1 ENG EDP FOR GREEN HYD SYS PER AMM 29-11-51. NO LEAKS NOTED AND OPS CHK GOOD. OK FOR SVC.SDR HALA2018123100688Warning Message · illuminatedETOPS SIGNIFICANT SYSTEM - ENG 1 REV FAULT ILLUMINATED AFTER STOWING REVERSER.// CONFIRMED FAULT. PERFORMED THRUST REVERSER DEPLOYMENT AND STOWAGE TEST. REF A330 AMM 78-31. CHANNEL A&B TEST OK. NO 60 DAY HISTORY. OK FOR SERVICE.SDR HALA2018121340652Apu · unknownETOPS SIGNIFICANT SYSTEM - UNABLE TO START APU.// PERFORMED TSM 49-62-00-810-836-A. NO FAULTS NOTED. OPS CHECK GOOD. OK FOR SVC.SDR HALA2018121000643Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ENG #2 THRUST REVERSER FAULT.// T/S PER HAL330 TSM 78-31-00-810-974A NO FAULTS NOTED CONTACTED MCC OK FOR SVC.SDR HALA2018091700217Landing Gear · vibrationABORTED TAKEOFF DUE TO EXCESSIVE NOSE SHIMMY ABOVE 100 KNOTS. INSPECTED THE NOSE GEAR, TIRE PRESSURE, JACKED THE NOSE AND PERFORMED SPIN CHECK, NO VIBRATION FELT THROUGH RUDDER PEDALS AND FLAPS EXTENDED. THE VIBRATION WAS FELT ON THE 2ND TAKEOFF BETWEEN 100-SDR HALA2018040600140Filter · not reportedNR 1 ENGINE OIL CHIP DETECTED ECAM DURING ENGINE SHUTDOWN. REMOVED AND REPLACED THE NR 1 ENGINE SCAVENGE OIL FILTER ELEMENT. TROUBLESHOT IAW TSM 79-20-00-810-823A. ENG RUN AND LEAK CHECK OK. NO DEFECTS NOTED. OK FOR SERVICE.SDR HALA2018031600107Heat Exchanger · leakingRIGHT ENGINE AIR OIL HEAT EXCHANGER, LEAK EVIDENT DURING IDLE RUN. THE RT ENGINE AIR/OIL HEAT EXCHANGER WAS REPLACED IAW AMM 79-21-51-400-803-A. LEAK TESTED IAW AMM 71-00-00-700-827-A. NO LEAKS EVIDENT.SDR HALA2018031500104Floor Support · corrodedFLOOR SUPPORT BETWEEN FRAMES 75, Y381 FOUND TO HAVE CORROSION. CORROSION REMOVED IAW SRM 51-74-00, REV 97. FOUND TO BE BEYOND LIMITS IAW SRM 53-41-14, REV 97. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-72-1, REV 97, AND DRAWING F53478040 ISSUE A.SDR HALA2018031100077Seat Track · corrodedDURING H CHECK, THE SEAT TRACK BETWEEN FRAMES 58 - 62, +Y1959 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53476200.SDR HALA2018031100076Seat Track · corrodedDURING H CHECK, THE SEAT TRACK BETWEEN FRAMES 55 - 58, +Y2462 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F534762202.SDR HALA2018031100073Seat Track · corrodedDURING H CHECK, THE SEAT TRACK BETWEEN FRAMES 62 - 72, -Y2462 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING10F53478650.SDR HALA2018031100071Seat Track · corrodedDURING H CHECK, THE SEAT TRACK BETWEEN FRAMES 38 - 39.2, -Y450 WAS FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-72-11, AND DRAWING F53311114.SDR HALA2018031300099Seat Track · corrodedSEAT TRACK BETWEEN FRAMES 55 AND 58, -Y1959 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15. SEAT TRACK REPLACED IAW SRM 51-72-11, REV 97, AND DWG F53476200, ISSUE D.SDR HALA2018031300098Seat Track · corrodedSEAT TRACK BETWEEN FRAMES 58 AND 62, -Y1959 FOUND CORRODED. CORROSION REMOVED IAW SRM 51-74-00, REV 97. FOUND OUT OF LIMITS IAW SRM 53-00-15, REV 97. THE SEAT TRACK WAS REPLACED IAW SRM 51-72-11, REV 97, DRAWINGS F5347704011, ISSUE F, F5347704015 ISSUE
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