N381HA
Service difficulty reports · 251
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 = 'N381HA' 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 = 'N381HA' 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 HALA2021021600020Fcu · defectiveETOPS - DUE TO FCU FAULT IN OGG- MOC REQUEST TO REPLACE FCU. // INSTALLED NEW FCU PER AMM 22-81-12, OPS TEST AND "LAND TEST" PASSED PER AMM 22-97-00. OK FOR SERVICE. UNIT, FLIGHT CO OFF 43-2281-9-0002 02025 ON 33-2281-9-0001 01281SDR HALA2020122304240Bolt · shearedEMERGENCY EQUIPMENT, FOUND TWO BOLTS SHEARED ON 1L FORWARD LOWER STOP FITTING AND STOP SCREW FACE CRACKED. CORRECTIVE ACTION: R & R 2 SHEARED BOLTS ON STOP FITTING, PER AMM 52-11. REMOVED & REPLACED 1L BEAM 8 FWD END STOP FITTING, REF AMM 52-11. ADJ PER AMMSDR HALA2020110900198Accumulator · defectiveETOPS - BLUE HYD POWER ACCUMULATOR LEAKS INTERNALLY. REMOVED & REPLACED BLUE HYD ACCUMULATOR, PER AMM 29-12-42 UP TO STEP 4D(7). LEAK CHECK GOOD. PENDING STEP 4D(7). CHECK FOR AIR, 2158677. ACCOMPLISHED REMAINING STEPS. OK FOR SERVICE. ACCUMULATOR, PO SDR HALA2020050800108Plenum · delaminatedETOPS SIGNIFICANT SYSTEM - DIRECT Z190 NT: LH PACK PLENUM FOUND BADLY DE-LAMINATED AT MOUNTING BOLT AREAS AND CRACK LINES AT AFT EDGE. // ELECTRICAL CONNECTORS 521HH5 AND 521HH7 DISCONNECTED. 1)LH PACK PLENUM CHAMBER, PRIMARY HEAT EX-CHANGER, MAIN HEAT EX-CHANSDR HALA2020050600105Skin · corrodedFUSELAGE SKIN FOUND SUSPECTED CORROSION AT FRAME 76 - FRAME 77, STRINGER 41 LH - STRINGER 42 LH. (AFT CUTOUT HOLE OF WASTE
EXHAUST SYSTEM). // FUSELAGE SKIN CORROSION AT FRAME 76 - FRAME 77, STRINGER 41 LH - 42 LH REPAIRED AS PER REPAIR DESIGN APPROVAL SSDR HALA2020050300103Fitting · corrodedDURING CCK AND DURING INSPECTION PER EM 5753-01164, CORROSION WAS FOUND ON THE LH MLG RIB 6 FITTING. THE CORROSION WAS REWORKED PER SECT I OF ERA 586363-14AD. // THE REWORKED LH RIB 6 FITTING IS APPROVED FOR 30,033 TOTAL FLIGHT CYCLES OR 193,119 TOTAL FLIGHT SDR HALA2020042800098Glowstrip · damagedFOUND EEPL DAMAGED AT GALLEY DOOR 2. // REPLACED PHOTO-LUMINESCENT STRIP FLOOR EMERGENCY ESCAPE PATH
MARKING AS PER AMM 33-51-21-000-801 AND 33-51-21-400-801. OPS CHECK GOOD.SDR HALA2020042700096Axle · corrodedFOUND #5 AXLE SLEEVE WITH CORROSION ON SHOULDER. // #5 AXLE SLEEVE REPLACED AS PER AMM 32-41-14 REV 75.02SDR HALA2019122750301Light · unsecureMID GALLEY PATHWAY LIGHT STRIP CAME OUT, NEEDS TO BE RE-SECURED. SECURED LIGHT STRIP.SDR HALA2019102800233Warning Light · false activationAIRCRAFT 381 ATB-RETURNED TO HNL DUE TO THE FORWARD CARGO DOOR INTERMITTENT UNLOCKED ECAM MESSAGE APPEARED. PRESSURIZATION NOT AN ISSUE THE FLIGHT WAS AT 10000 FEET. DEFERRED PER MEL 52-70-1-HNL PERFORMED TSM TASK 52-31-00-810-803-A, NO FAULTS DETECTED. CLEANESDR HALA2019110600470Proximity Sensor · dirtyATB - ON CLIMB FWD CARGO INTERMITTENT UNLOCKED ECAM, PRESSURIZATION NOT AN ISSUE AT TIME AS WE WERE 10000 LEVELED OFF 11000 THEN DESCENDED. PERFORMED TSM TASK 52-31-00-810-803-A, NO FAULTS DETECTED. CLEANED AND INSPECTED FWD DOOR COMPARTMENT PROX SENSORS NSDR HALA2019093000392Valve · failedETOPS SIGNIFICANT SYSTEM - OUTER-TANK FUEL INLET VALVE FAILED. // REMOVED AND REPLACED OUTER-TANK FUEL INLET VALVE (RH) PER AMM 28-25-57-OPS CHECK GOOD. OK FOR SVC.
ACTUATOR, SINGLE OFF 43-2826-9-0002 58020 ON 43-2826-9-0001 4612SDR HALA2019053000265Access Panel · openTFOA - LT FUEL PANEL FOUND OPEN ON ARRIVAL TO LAX. FUEL CAPS MISSING & HOLD OPEN ROD DAMAGED. REPLACED FUEL COUPLING CAPS PER AMM 28-25 REPLACED STRUT PER AMM 57-42. DOOR OPS CHK GOOD. OK FOR SVC.SDR HALA2019042350458Lens · brokenDOOR 3L EXIT LIGHT COVER BROKEN. REPLACED EXIT MARKING SIGN AT DOOR 3L.SDR HALA2019032100091Not Reported · missingFLOOR LIGHT STRIP IN AFT GALLEY IS MISSING PARTS. REPLACED EMERGENCY LIGHT STRIP IN AFT GALLEY. LP 5847373SDR HALA2019021900048Generator · failedAIRCRAFT 381, DIVERTED TO HNL DUE TO THE NBR 1 GENERATOR FAILED IN FLIGHT. CORRECTIVE ACTION: REPLACED NBR 1 IDG AND GENERATOR CONTROL UNIT. LP 4966279, 4966281.SDR HALA2019010700007Warning System · false activationETOPS SIGNIFICANT SYSTEM - DURING CLIMB ECAM A.ICE L OUTR WING HI PR - CREW AWARENESS. PERFORMED TSM 30.11.00.810.805A. A-ICE VALVES OPERATED NORMALLY. NO MSG'S, OK TO CONT.SDR HALA2019010200001Warning System · false activationETOPS SIGNIFICANT SYSTEM - AFTER PARKING ON ENGINE SHUTDOWN, ENG 1 OIL CHIP DETECTED.// PERFORMED A330 TSM 79-20-00-810-823 FOUND NO DEBRIS ON ENG 1 EMCD. PERFORMED EMCD CLEANING FUNCTIONAL TEST AND EMCD TEST, GIVEN TEST OK. ENG RUN-UP TEST AND NO ECAM MESSAGESDR HALA2018123100682Fault Message · false activationETOPS SIGNIFICANT SYSTEM - ELEC IDG 1 OIL SYS FAULT.// RESET ACFT ELEC SYS PER TSM 24-20-00. OPS NORMAL.SDR HALA2018121700661Fairing · puncturedLEFT WING NR 4 CANOE FAIRING HAS A PUNCTURE ON BOTTOM. INSTALLED PERMANENT REPAIR IAW SRM 57-56-00-300. A/C OK FOR SERVICE.SDR HALA2018102200279Valve · openAIRCRAFT 381, ATB TO HNL DUE TO THE CABIN ALT ECAM VENT EXTRACT VALVE FULL OPEN AT FL110. CORRECTIVE ACTION: FOUND VENT EXTRACT VALVE IN OPEN POSITION PER ME 21-26-2 (LP 4964629). VALVE NEED TO BE IN NOT FULLY OPEN POSITION PRIOR TO PUSHBACK. RE-POSITIONED VALSDR HALA2018101100490Valve · openOPEN - ATB, AT FL370 CABIN ALT CLIMBED TO 11,000'. CABIN ALT ECAM VENT EXTRACT VALVE FULL OPEN. FOUND VENT EXTRACT VALVE IN OPEN POSITION, VALVE NEEDS TO BE IN NOT FULLY OPEN POSITION PRIOR TO PUSH BACK REF MPM 21-18-21-20.SDR HALA2018101000489Pressure Switch · malfunctionedSUP - ETOPS SIGNIFICANT SYSTEM - ON LANDING ENG 1 MINOR FAULT ECAM.// ACCOMPLISHED TSM 73-25-81-801-934-A FOUND LO OIL PRESS FAULT #1 ENG, REMOVED AND REPLACED #1 ENGINE LO OIL PRESSURE SWITCH PER AMM 79-34-15-000-804-A/400-804-A OPS/LEAK CK GOOD NO FAULTS ONSDR HALA2018100800481Actuator · faultyETOPS SIGNIFICANT SYSTEM - FUELERS ADVICE AIRCRAFT IS NOT ACCEPTING FUEL. REPLACED INR TK INLET VLV 1 ACTUATOR (603QL1) PER AMM 28-26-53-400-801-A. OPS TEST OK, AIRCRAFT FUELED OK.SDR HALA201809050417Unknown · odorFUMES PRESENT IN THE FLIGHT DECK ONLY ON DECENT THROUGH LANDING. WET SOCK ODOR. FLT ATTENDS STATED NO ODOR NOTED IN CABIN. . PERFORMED DUCT BURNOUT IAW A330 AMM 36-11 AND HIGH POWER RUNS IAW AMM 71-00. NO ABNORMAL ODORS NOTED. PERFORMED GVI OF APU BLEED FLESDR HALA2018090500414Unknown · odorFUMES AFTER TAKEOFF AT 30,000 FT, ODOR OF BURNING PLASTIC THEN SWEET ODOR IN THE FLIGHT DECK & R3 DOOR AREA. FLT ATTENDANTS STATED NO ODOR NOTED IN CABIN. PERFORMED DUCT BURNOUT IAW IAW AMM 36-11 AND HIGH POWER RUNS IAW AMM 71-00. NO ABNORMAL ODORS NOTED. SDR HALA2018081400370Oil System · lowAPU LOW OIL LEVEL ON STARTING. SERVICED THE APU OIL SYSTEM TO FULL. INSPECTED FOR LEAKS AND GENERAL SECURITY OF APU COMPARTMENT. NO DEFECTS NOTED. OK FOR SERVICE.SDR HALA2018060600282Lug · crackedWHILE ACCOMPLISHING WC 5753-01164-02B, FOUND A CRACK ON THE FWD LUG OF THE RT MLG RIB 6.SDR HALA2018060700192Lug · crackedDURING LINE MAINTENANCE IN SEA, THE RT MLG SUPPORT RIB NR 6 AFT PINTLE FORWARD LUG WAS FOUND CRACKED WHILE ACCOMPLISHING EM 5753-01164-02B DETAILED VISUAL INSPECTION. REPLACED RIB 6 AND REAR PINTLE PIN ASSEMBLY.SDR HALA2018052300240Rib · crackedDURING AFT TRUNNION AD INSPECTION, FOUND THE RT WING MLG RIB 6 AFT BEARING LUG CRACKED. REMOVED AND REPLACED THE NR 6 RIB IAW ENGINEERING REPAIR AUTHORIZATION 570123-14AD. PERFORMED ALL SYSTEM AND OPERATIONAL CHECKS. AIRCRAFT OK FOR SERVICE IAW ERA 570123-14SDR HALA2018041800177Chip Detector · false indicationNR 1 ENGINE OIL CHIP DETECTED AFTER LANDING. IAW AMM 79-20-00-810-823-A, INSPECTED THE CHIP DETECTOR. NO DEBRIS FOUND. CLEANED AND REINSTALLED THE CHIP DETECTOR. PERFORMED EMCD TEST. TESTED OK.SDR HALA2018030500067Fcu · faultedAUTO FLT FCU FAULT, STATUS PAGE INDICATES PART FCU. ILLUMINATED WHEN CHANGING ALTITUDE FROM FL 400 TO FL 410. FAULT NOT CONFIRMED ON ARRIVAL. TROUBLESHOT IAW TSM 22-81-00-810-859A. NO FAULTS. NO 30 DAY HISTORY. PERFORMED LAND CAT 3 CAPABILITY TEST IAW AMSDR HALA0218022800057Scavenge Pump · malfunctionedAPU FAULT ECAM ILLUMINATED. APU LAST LEG SHOWS LUBE PUMP FILTER & GENERATOR SCAVANGE FILTER. PERFORMED TSM 49-62-00-810-916-A. LUBE AND GEN FILTERS SHOW NO METAL PARTICLES. BOTH DPIS NOT EXTENDED. APU WIRING CHECKED OK IAW TSM 49-62-00-810-916-A, STEP 4.D.(SDR HALA2018021200040Warning Message · false activationONE HOUR INTO FLT FUEL, A LOW FUEL PRESSURE L2 PUMP, RECYCLED PUMP OFF & ON, NO CHANGE, CLEARED ITSELF AFTER 5 MINUTES. PERFORMED AN OPS TEST OF THE MAIN & STANDBY PUMPS, AUTOMATIC AND MANUAL MODE IAW AMM 28-21-00-710-801A, NO DEFECTS NOTED, OK FOR SERVICESDR HALA2017122700327Fire Detector · shortedINTERMITTENT NR 2 ENGINE FIRE LOOP B FAULTED. REMOVED AND REPLACED FDU 2 IAW AMM 26-12-34, CONDITION SAME, ORIGINAL FDU REINSTALLED. FOUND PYLON DETECTOR 7WD2 READING 9.9 OHMS PIN C TO A OUT OF LIMITS AND SHORTED TO GROUND FROM STUD. REPLACED THE PYLON FIRESDR HALA201710230026Regulator Valve · inoperativeAIR ENGINE NR 1 BLEED FAULT. PERFORMED BITE TEST OF BMC. FAULTED NR 1 PRESSURE REG VALVE, REMOVED AND REPLACED NR 1 PRESSURE REG VALVE PER AMM 36-11-52. LEAK CHECK AND BITE TEST GOOD. OK FOR SERVICE. VALVE, BLEED, P OFF 33-3611-9-0002 01965 ON 33-3611-9-0002 0SDR HALA2017090100006Sign · detachedEXIT SIGN AT DOOR 3R DETACHED FROM THE DOOR. RE-SECURED EXIT SIGN COVER.SDR HALA2017080400218Actuator · failedLEFT INLET VALVE FAILED. OUTER TANK. REMOVED AND REPLACED THE OUTER TANK INLET VALVE ACTUATOR IAW AMM 28- 25-57. OPS CHECKED AND TESTED OK.SDR HALA2017062300165Warning Message · false activationNR 2 ENGINE HAD A MINOR FAULT AND NR 2 AIR EXCHANGER FAULT ILLUMINATED DURING ROLLOUT, AFTER MOVING THRUST REVERSER LEVER TO IDLE REVERSE POSITION. PERFORMED TSM 79-20-00-810-809-A, FADEC SYSTEM TESTED OK. AIR/OIL HEAT EXCHANGER VALVE OPERATES SMOOTHLY. OK SDR HALA2017061400157Control System · malfunctionedNR 2 ENGINE CONTROL SYS FAULT DURING SHUTDOWN. TROUBLESHOT THE NR 2 ENGINE CONTROL SYS IAW 71-00-00-810-924-A. ALL OPS NORMAL, UNABLE TO DUPLICATE FAULT. NO HISTORY. ACFT OK FOR SERVICE.SDR HALA2017053000129Manifold · leakingFUEL LEAKING FROM NR 2 ENGINE. REMOVED AND REPLACED THE NR 2 ENGINE INBOARD FUEL MANIFOLD ASSEMBLY IAW AMM 73-11-43-400-802-A. LEAK CHECKED OK. ACFT OK FOR SERVICE.SDR HALA2017042100105Line · leakingNR 2 ENG OIL LEAK NOTED FROM UNDER THRUST REVERSER COWLS AND UPLIFTED 4.5 QTS. LEAK TRACED TO OIL RETURN PIPE FROM FWD BEARING COMPARTMENT TO SCAVANGE PUMP. PIPE REPLACED IAW MM 79-22-51-000-803-A. ENG RUN C/OUT. NIL LEAKS EVIDENT.SDR HALA2017042100158Warning Message · illuminatedABORTED TAKEOFF DUE TO RECEIVING A ECAM FOR BRAKES RELEASE AND BRAKE 1 RELEASED MESSAGE AT 90 KNOTS. FOUND NR 1 WHEEL HUB CAP MISSING.SDR HALA2017041500101Actuator · defectiveFUELERS REPORT HAVING TROUBLE FUELING. LT FUEL OUTER TANK, INLET VALVE ACTUATOR FAULT. RESET FCMC 1 & 2, NO HELP, DOWN POWER A/C, RESET POWER, FCMC 1 & 2 SYS TEST OK. NO FURTHER DEFECTS NOTED DURING CONTINUED FUELING. OK FOR SERVICE. REMOVED & REPLACED LT FUELSDR HALA2017031700070Warning System · false activationETOPS SIGNIFICANT SYSTEM - DURING CLIMB, STS PAGE DISPLAYED " INOP SYS FUEL AFT XFR" NO ASSOCIATED ECAM, NO FUEL XFR'D FROM INNERS TO TRIM TANK. MAN FWD XFR OK, AUTO FWD XFR OK. FUEL AFT XFR VLV 2 (700QN2),T/S'D PER TSM 28-27-00, PERFORMED FUEL VALVE TEST PER SDR HALA2017030700054Unknown · malfunctionedETOPS, AFTER LANDING ECAM ENG 2 REV UNLOCKED, CYCLED NR 2 ENG TR MULTIPLE TIMES ON GROUND. OPS CHECK NORMAL. OK TO CONTINUE PER AMM 78-31-00-740-802ASDR HALA2017030700053Connector · dirtyETOPS, ENG 2 REV UNLOCKED. FOUND LOWER OUTBOARD THRUST REVERSER HAD GAP. T/S PER TSM78-30. REMOVE AND REINSTALLED, CLEANED CONNECTOR PER AMM 78-31. CYCLED T/R MULTIPLE TIMES PER AMM 78-31. NO CURRENT FAULTS NOTED. OK TO CONTINUE SERVICE.SDR HALA2017013100019Unknown · odorON DESCENT BTW 7000' & 4000' FUMES WERE SMELT IN CABIN & COCKPIT ODOR WAS DESCRIBED AS OILY SOCK SMELL. ACCOMPLISHED GROUND ENGINE RUN NR 1 ENGINE, SHUTDOWN THEN RAN NR 2 ENGINE WITH PACKS ON ENGINE BLEED ONLY, NO ODOR OR SMELL IN COCKPIT OR CABIN NOTED, OK FSDR HALA2016121800552Outflow Valve · inoperativeCAB PRESS SYS 1 FAULT CAUTION. T/S PER TSM 21-31-00-810-803-A. FOUND FWD OUTFLOW VALVE INOP. REMOVED AND INSTALLED FWD OUTFLOW VALVE PER AMM 21-31-51-000-801-A AND 21-31-51-400-801-A. OPS CHECKS GOOD PER AMM 21-31-00-710-801-A AND AMM 21-31-00-710-802-A. A/C SDR HALA2016112300215Light · looseEMERGENCY LIGHT STRIP FLIGHT DECK ENTRY IS LOOSE. REPLACED FLIGHT DECK ENTRY AND FIRST CLASS GALLEY EMERGENCY LIGHT STRIP.
Back to N381HA