N386HA
Service difficulty reports · 155
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 = 'N386HA' 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 = 'N386HA' 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 ASAA2026101267374Autothrust Sys · malfunctionedAUTOTHRUST MODE CHANGED FROM "D2" DERATE TO THR CLB AUTOMATICALLY AT 10,000 FT. GROUNDED - YES. PERFORMED OPS TEST OF THE ATHRL PER AMM 22-30-00-710-801-A AND AN AFS RTS PER AMM 22-96-00. NO DEFECTS NOTED. OK FOR SERVICE.SDR ASAA2026051664795Light Sys · faultedEMERGENCY LIGHTS STAYED ON REGARDLESS OF SWITCH POSITION. GROUNDED - YES. PERFORMED EMERGENCY LIGHT TEST & BITE CHECK PER AMM 33-51-00. OPS CHECK & BITE TEST GOOD. NO FAULTS. OK FOR SVC.SDR ASAA2026030863716Girt Bar · disconnected1L DOOR SLIDE WILL NOT ARM. ( MAIN ENTRY DOOR / SLIDES ). GROUNDED - YES. FOUND 1L GIRT BAR FWD SIDE DISCONNECTED FROM SLIDE ASSY. RESECURED FWD SIDE OF GIRT BAR IN REF AMM 25-62-41-400-801-A. OPS & SECURITY CHK GOOD. PLACARD REMOVED. MIC SHEET UPDATED. OK FORSDR HALA20251027329Fmu · faultedETOPS - ENG 2 LP SHAFT PROT LOSS ECAM AFTER LANDING. REMOVED AND REPLACED NR 2 ENG FMU W/ REF TO AMM 73-21-52 UP TO AND INCLUDING STEP 5.E.PERFORMED REMAINING STEPS. NO LEAKS NOTED. OK FOR SVC.SDR HALA20251001296Filler · brokenETOPS - ON PDSC WALK AROUND HEARD LOOSE OBJECT IN NR 2 ENGINE SPINNER. FOUND NR 2 ANNULUS FILLER FRIONT ARM & LOCATION PIN BROKEN OFF. REMOVED NR 2 ANNULUS FILLER & BROKEN PART. INSTALLED NEW ANNULUS FILLER IN NR 2 POSITION PER AMM 72-31-41. OK FOR SVC. (NOTESDR HALA20250915279Pump · leakingETOPS - LEAKING COMING FROM #2 ENG DRAIN MAST. HAYDRAULIC PUMP#1. #2 ENG G HYD. EDP. REMOVED AND INSTALLED UP TO STEP 4. D. 19 OF AMM 29-11-51-400-805-A.REPLACED ENG 2 G HYD EDP MOUNTING NUTS PER AMM 29-11-51. PERFORMED LEAK CHECK AND ENGINE RUN PER AMM 29-11-SDR HALA20250915280Pump · leakingETOPS - LEAKING COMING FROM #2 ENG DRAIN MAST. HAYDRAULIC PUMP#1. #2 ENG G HYD. EDP. REMOVED AND INSTALLED UP TO STEP 4. D. 19 OF AMM 29-11-51-400-805-A.REPLACED ENG 2 G HYD EDP MOUNTING NUTS PER AMM 29-11-51. PERFORMED LEAK CHECK AND ENGINE RUN PER AMM 29-11-SDR HALA20250902267Transfer Sys · faultedETOPS - FUEL AFT XFR FAULT. ON PREFLIGHT. REPLACED RIGHT INNER TANK INLET VALVE PER AMM 28-26-53-000. OPS TEST OK. OK FOR SVC.SDR HALA20250717217Bmc · faultedETOPS - BTB DUE TO BLEED AIR RIGHT WING LEAK. REMOVED AND REPLACED THE BMC 2 PER AMM 36-11-34. SYS TEST OK. A/C OK FOR SVC.SDR HALA20250707206Gasket · leakingATB - ATB DUE TO LOSS OF ENGINE 2 OIL. ADC MESSAGE CAME ON AT 4 QTS. OIL GOT DOWN TO .9 ON APPROACH. FOUND OIL LEAKING FROM TWO HP/IP TURBINE VENT OVERHEAT THERMOCOUPLES. REMOVED AND REPLACED GASKETS PER SB RB.211-72-AE302. OIL FOUND LEAKING. CLEANED AREA, PERSDR HALA20250701203Controller · faultedETOPS - IN FLIGHT, COCKPIT TEMP 56F WITH CONTROLLER AT 12:00 POSITION PERFORMED ZONE CONTROL RESET, NO HELP COCKPIT TEMP 52F WITH CONTROLLER FULL HOT. REMOVED & REPLACED ZONE CONTROLLER PE AMM 21-63-34/400. ECS SYSTEM TEST PASSED. OK FOR SVC.SDR HALA20250609170Handset · faultedETOPS - DOOR 1L INTERPHONE STATIC WHILE IN USE. REMOVED AND REPLACED 1L INTERPHONE HANDSET PER AMM 23-73-44, OPS TEST GOOD.SDR HALA20250430118Hydraulic Line · leakingETOPS - PER T/C NEEDED TO INSPECT NO.1 ENGINE GREEN SYSTEM . UPON INSPECTION OF NO.1 ENGINE GREEN SYSTEM , FOUND PRESSURE HOSE CHAFING AGAINST SUCTION HOSE. NEED TO REPLACE PRESSURE HOSE ON NO. 1 ENGINE. REMOVED & REPLACED NO. 1 ENGINE GREEN SYSTEM PRESSURE HOSDR HALA20250205051Fire Detector · faultedETOPS - ON LANDING RECEIVED ECAM ENG1 FIRE LOOP-A. FOUND ENG #1 LOOP A FIRE DETECOTR 4011WD OPEN REMOVED & REPLACED 4011WD ON ENG #1 PER AMM 26-12-15. OPS CHECK OK FOR SERVICE.SDR HALA20241230081Isolation Valve · faultedFUMES EVENT: DIRTY SOCKS OR CHEMICAL SMELL REPORTED THROUGHOUT THE ENTIRE CABIN. THE SMELL LASTED 7-10MINUTES THEN DISSIPATED COMPLETELY. PERFORMED ENG RUN OF #1 AND #2 ENGINE TO CONFIRM SMELL PER AMM 71-00-00-860-810-A. FAINT OIL SMELL OBSERVED. PERFORMED LEVSDR HALA20241216368Handset · faultedETOPS - 1L INTERPHONE CONNECTION BAD. REMOVED AND REPLACED 1L HANDSET ASSY PER AMM 23-73-44, OPS TEST GOOD. OK FOR SERVICESDR HALA20241112323Chip Detector · false indicationETOPS-REPEAT WRITE UP AFTER LANDING ECAM ENG 1 OIL CHIP DETECTED. PERFORMED TSM 79-20-00-810, FOUND DAMAGED PIN ON EMCD. REMOVED AND REPLACED SCAVANGE OIL FILTER [21195 DM]. NO DEBRIS FOUND ON EMCD. NO DEBRIS FOUND ON THE FILTER. PER AMM 79-22-45. PERFORMED LESDR HALA20241104066Switch · faultedBTB EMERGENCY LTS IN ARMED POSITION EMER LTS ON IN CABIN- RESETS UNSUCCESSFULL. REMOVED AND REPLACED EMER LIGHT SWITCH 4WL PER ESPM 20-45-21-01 AND OPS TEST PER AMM 33-51-00. OPS OK.SDR HALA20240930173Valve · faultedETOPS - PRIOR TO DEPARTURE UNABLE TO REFUEL. REMOVED & REPLACED FCMC 1 PER AMM 28-51-34, HIGH LEVEL SENSE TEST & SYSTEM TEST AND FUEL VALVES TEST GOOD. NO DEFECTS NOTED. A/C OK FOR SVC.SDR HALA20240626173Sensor · faultedETOPS - CABIN TEMP IN ROWS 25-31 IS MUCH WARMER THAN REST OF THE AIRCRAFT. REMOVED AND REPLACED PACK 1 CPRSR DISCHARGE TEMP SENSOR. ECS SYSTEM TEST OK. REF. 21-53-11-000-801-A AND 21-53-11-400-801-A. OK TO CONTINUE SERVICE.SDR HALA20240507022Tire · low pressureCREW REPORTED VIA ACARS THAT THEY HAVE NLG WHEEL TIRE LO PRESS MSG, WILL BE DECALRING EMERGENCY ON LAX ARRIVAL. ASKING FOR MX TO MEET ACFT ON RWY TO INSP NLG TIRES FOR PROPER PRESSURE. WHEEL TIRE PRESS LOW. REMOVED AND REPLACED NLG #2 PER AMM 32-41-12-000-801SDR HALA20240329079Warning Message · illuminatedBTB: #5 HOT BRAKE OVERHEAT WHEEL TIRE LO PR. PERFORMED INSPECTION OF #5 MLG WHEELS BRAKE PER AMM 05-51-16-200-801-A. NEED TO REPLACE #1 MLG WHEEL ASSY AND BRAKE PRECAUTIONARY. REMOVED AND REPLACED #1 MLG WHEEL ASSY AND BRAKE REF AMM 32-41-11 AND 32-42-27. SPINSDR HALA20240116020Unknown · unknownATB - FYD G. RSVR LO IN FLIGHT. AFTER FLAP RETACTION. UPON INSPECTION OF HYD. SYSTEM PIPING AND COMPONENTS FOUND STEEL BRAIDED LINE AT L/H MLG UPLOCK (DOOR) LEAKING THROUGH PUNCTURE. REOVED AND REPLACED DAMAGED LINE REF. AMM 32-31-33-400-801-A. CONTINUED ON LOSDR HALA20231222283Unknown · unknownETOPS - BOTH HF1 AND HF2 FAIL CHANNELIZE REPEAT WRITE UP. INSTALLED NEW HF2 COUPLER AND OPS CHECKED HF1 AND HF2 PER AMM 23-11-36, OPS TEST PASSED.SDR HALA20231211273Unknown · unknownETOPS - ECAM: NAV BARO REF DISCREPANCY. CAPT "PULL STD" BARO REF KNOB INOP. THE PULL STD FUNCTION DOES NOT CHANGE BARO REF TO STD, AND BARO REF VALUE DOES NOT CHANGE UNLESS PULLING KNOB. REMOVED AND REPLACED FCU PER AMM 22-81-12. ALL TEST GOOD. OK FOR SVCSDR HALA20231207263Unknown · unknownATB - AIR TURN BACK FM VERIFICATION FAIL (FM2 FAULT). REMOVED AND REPLACED FMGEC 2 PER AMM 22-83-34. AFS TEST AND LAND III CAPABILITY TEST PASSED. OK TO CONT. SERVICE.SDR HALA2023072800160Filter · misinstalledETOPS - WHILE WORKING TASK CARD 330-361143-01-1-2 FOUND #2 ENGINE FAN AIR THERMOSTAT FILTER CROSS THREADED. REPLACED #2 ENGINE FAN AIR VALVE THERMOSTAT PER AMM 36-11-43. OPS CHK GOOD. OK FOR SVC.SDR HALA20240712190Controller · malfunctionedETOPS - COCKPIT TEMP CONTROL KNOB. DOES NOT MAINTAIN TEMP. +/- 70 DEGREES. FROM HOT AIR 2. PERFORMED TSM 21-63-00-810-908-A. REPLACED ZONE CONTROLLER PER 21-63-34-400-801-A. TEST PASSED. OK FOR SVCSDR HALA2023031700050Oil Cooler · faultyOTHER - APU AUTO SHUTDOWN AT GATE. REMOVED AND REPLACED APU OIL COOLER PER AMM 49-91-44. OPS CHECK/LEAK CHECK GOOD. OK FOR SERVICE.SDR HALA2023031700049Electrical Box · faultyOTHER - APU AUTO SHUTDOWN AT GATE. REMOVED AND REPLACED APU ECB PER AMM 49-61-34. OPS CHECK GOOD.SDR HALA2023010500003Control Unit · faultedETOPS - ENG 1 CTL SYS FAULT AFTER ENGINES SHUT DOWN. BITE TEST FAULTED VSV CONTROL UNIT. REMOVED AND REPLACED #1 ENG VSV CONTROL UNIT PER AMM 75-33-51-400-801-Q. NO LEAKS NOTED. TEST #5 OPS CHK GOOD. AIRCRAFT OK FOR SVC.SDR HALA2022100300266None · noneAIR ENG 1 BLEED NOT CLOSED ECAM MESSAGE. REMOVED AND REPLACED #1 ENG PRV VALVE PER AMM 36-11-52. OPS AND LEAK CHECK GOOD. MESSAGE EXTINGUISHED. OK FOR SVC. VALVE, BLEED, P OFF 33-3611-9-0002 01401 ON 33-3611-9-0002 01373SDR HALA2022100100265None · none"BTB- #1 ENG ONLY 20 PSI. DOES NOT MEET THE MIN TO START ENG. FOUND AIR LEAK AT BRAIDED LINE P/N FK25637. REMOVED SENSE LINE.
EMP# 1724236. 30SEP22. REPLACED #1 ENG SENSE LINE P/N FK25637
FOR THE REGULATED PRESS. TRANSDUCER. BLEED PSI AT 40. NO LEAKS
NOTSDR HALA2022090600275None · noneSHIP 386 4L DOOR ARMING LEVER IS HARD TO MOVE WHEN ARMING DISARMING. CORRECTIVE ACTION: VISUAL CHECK OF GIRT BAR NO DEBRIS. CHECK OF ARM/DISARM NO DEFECT NOTED. (9336267)SDR HALA2022080400140None · noneETOPS - APU HARD TO START // PRECAUTIONARY CHANGE ECB PER AMM 49-61-34. BITE TEST PASS. ACCOMPLISHED MULTIPLE STARTS OF APU. NO FAULT NOTED. RAN APU SUCCESSFUL. OK FOR SERVICE. BOX, ELECTRONIC OFF 33-4963-9-0002 S/N 04690 ON 33-4963-9-0002 S/N 00120SDR HALA2022060700110None · noneETOPS - APU AUTOSHUT DOWN NO ROTATION // REMOVED APU STARTER PER A330 AMM49-42-51-000-801-A ( 831817), INSTALLED APU STARTER IAW HAL A330 AMM 49-42-51-400-801A APU BITE TEST OK APU START NORMAL MOTOR, STARTER, OFF 33-4941-9-0001 S/N 80083 ON 33-4941-9-0001 S/SDR HALA2022060300109None · noneETOPS - APU AUTO SHUT DOWN // REMOVED & REPLACED APU STARTER PER AMM 49-42-51. OPS CHK OK MOTOR, STARTER,
OFF 33-4941-9-0001 S/N 80007 ON 33-4941-9-0001 S/N 80083SDR HALA2022041800093None · noneETOPS - FUEL AFT XFR FAULT FUEL DOES NOT AUTO TRANSFER AFT IN CRUISE. IT TRANSFERRED ALL FUEL FORWARD NORMALLY BEFORE DESCENT // BITE TESTED FCMC 1+2 PER AMM 28-51-00. FAULTED AFT XFR VALVE 1 (700QN1). REMOVED AND REPLACED ACTUATOR 700QN1 PER AMM 28-27-54. OSDR HALA2022040100128None · noneSHIP 386 3L EXIT SIGN FELL OFF. CORRECTIVE ACTION: REINSTALLED 3L EXIT SIGN LENS. (8458058)SDR HALA2022030400076None · noneSHIP 386 LH LOWER LG RIB 6 FWD FOUND WITH HEAVY CORROSION ON LUG BORE, FWD & AFT SPOT FACE BEYOND 5753-01164-08A FIG 1 SHEET 2 OF 4 SPECIFIED REWORK LIMIT. CORRECTIVE ACTION: TASK ACCOMPLISHED AS PER ER/A 594574-14. (2143382)SDR HALA2022030400074None · noneSHIP 386 RH LOWER LG RIB 6 FWD FOUND WITH HEAVY CORROSION ON FWD & AFT SPOT FACE BEYOND SPECIFIED DIMENSIONS UNDER TASK 5753-01164-08B. CORRECTIVE ACTION: TASK ACCOMPLISHED AS PER ER/A 594573-14. NIL FURTHER. (2143379)SDR HALA2022030700078None · noneSHIP 386 DURING CCK AND DURING INSPECTIONS PER EM 5716-01019, HO LE H260 LHS WAS FOUND CRACKED. CORRECTIVE ACTION: REF ER/A 594575-14. (2142758)SDR HALA2022030700077None · noneSHIP 386 DURING CCK AND INSPECTION PER EM 5716-01019, HOLE H260 RHS WAS FOUND CRACKED. CORRECTIVE ACTION: MAINTENANCE PERFORMED REF ER/A 594575-14AD. (2142760)SDR HALA2022020300033None · noneSHIP 386 - ATO - DUE TO FMA MALFUNCTION. CORRECTIVE ACTION: NO FAULTS FOUND IN PFR. PERFORMED AUTOLAND TEST. PERFORMED RTO INSPECTION. (8452195)SDR HALA2022011900018Meter · defectiveETOPS - ON PDC FOUND #1 ENG FMU DRIPPING FUEL // REMOVED + REPLACED #1 ENG FMU PER AMM 73-21-52-400-801-A OPS + LEAK CHECK OK. A/C OK TO CONT. METER, FUEL; PO OFF 43-7321-9-0012 13396 ON 43-7321-9-0012 11262SDR HALA2022010400006Light · defectiveSHIP 386 PATHWAY LIGHTING STRIP IN AFT GALLEY DETACHED. CORRECTIVE ACTION: REPLACED 3 FT SECTION OF PHOTOLUMINESCENT STRIP ON AFT GALLEY. (8450659)SDR HALA2021112400173None · noneBTB #1 ENG FUEL LEAK // PER TSM 73-21-52-100-801A PERFORMED FMU DUMP VALVE CLEANING, CONDITION STAYED THE SAME. ND 1864498. REMOVED AND REPLACED FUEL DRAINS TANK EJECTOR PER AMM 71-71-42-000-804-A AND 71-71-42-400-804-A. NO FUEL LEAK NOTED DURING ENGINE START,SDR HALA2021111900167Unknown · odorFA REPORT ELECT ODOR IN AFT GALLEY WHILE ON DOWNWIND VECTOR, NO VISIBLE OBSERVATION IN GALLEY OR CABIN. ODOR ELIMINATED ON BASE LEG SECTOR 5MIN DURATION // PERFORMED VISUAL INSPECTION OF AFT GALLEY COMPONENTS. NO CBS TRIPPED RAN ALL OVENS ,CHILLERS,COFFEE MAKESDR HALA2021111200157None · noneFA CONFIRMED DOOR AT 1L IS LEAKING IN FLIGHT AT TOP R CORNER. MAINT REPEAT WRITE UPS. SEAT IS OUT OF PLACE // RESECURED DOOR SEAL (FWD UPPER CORNER) PER A330 AMM 52-11-18 LEAK CHECK GOOD PER A330 AMM 05-53-00. HAL NO GO ODI PROC 5211 ALREADY C/W REF LP 774360SDR HALA2021110100188None · noneSHIP 386 LIGHT STRIP CRACKED & LIFTING IN AFT GALLEY. CORRECTIVE ACTION: CONDITION AND SECURITY CHECK GOOD ON AFT GALLEY LIGHT STRIP. (6784138)
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