N396HA
Service difficulty reports · 150
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 = 'N396HA' 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 = 'N396HA' 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 HALA2019102200434Seat Track · corrodedSEAT TRACK BETWEEN FRAME 62 AND 71+11" AT -Y1959 IS CORRODED AT LOCATIONS: FR63+10". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR63+10-Y1959 LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TSDR HALA2019101800427Seat Track · corrodedSEAT TRACK BETWEEN FRAME 58.8 AND 62 AT +Y1959 IS CORRODED AT LOCATIONS: FR59;FR60+9" & FR61+19". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103
PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR59;FR60+9" & FR61+19" LOCATED ON INNER VERTICSDR HALA2019101800426Seat Track · corrodedSEAT TRACK BETWEEN FRAME 62 AND 71+11" AT +Y1959 IS CORRODED AT LOCATIONS: FR62+12";FR63+10";FR64+3";FR65" & FR66+10". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B, CORROSION AT LOCATION FR62 +Y1959 LOCATED ON INNESDR HALA2019101800425Seat Track · corrodedSEAT TRACK BETWEEN FRAME 67+9" AND 71+9" AT -Y450 IS CORRODED AT LOCATIONS: FR68+4" TO +9";FR70 & FR69+14" TO +15". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR70 -Y450 LOCATED ON INNER VERSDR HALA2019101800424Seat Track · corrodedSEAT TRACK BETWEEN FRAME 58+12" AND 67+12" AT -Y450 IS CORRODED AT LOCATIONS: FR59+4" TO +7";FR59+17";FR63+18";FR65+5" \& FR66+16". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B CORROSION AT LOCATION FR63+18 -Y450 LOSDR HALA2019101800423Seat Track · corrodedSEAT TRACK BETWEEN FRAME 54+13 AND 58+8 AT +Y1959 IS CORRODED AT LOCATIONS: FR56+13/& FR57+10. // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103
PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR56+13 & FR57+10 LOCATED ON INNER VERTICAL SURFACSDR HALA2019101800422Seat Track · corrodedSEAT TRACK BETWEEN FRAME 40 AND 47 AT +Y1959 IS CORRODED AT LOCATIONS: FR40+12",FR40.1+6",FR40.1+10",FR40.2+9",FR41+1",FR42+18". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATIONS FR40+12", FR40.1+SDR HALA2019101800421Seat Track · corrodedSEAT TRACK BETWEEN FRAME 53.2 AND 54 AT +Y1959 IS CORRODED AT LOCATIONS: FR53.4. // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103 PARA 6.A THRU 6.B (3)B
CORROSION AT LOCATION FR53.4 +Y1959 LOCATED OSDR HALA2019101800420Seat Track · corrodedSEAT TRACK BETWEEN FRAME 26 AND 37.4 AT -Y450 IS CORRODED AT LOCATIONS: FR29+9",FR32,FR33+12",FR37.2+2",FR37.3. // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 10
PARA 6.A THRU 6.B (3)B. CORROSION AT LOCATION FR29+9",FR32,FR33+12",FR37.2+2",FRSDR HALA2019101800419Seat Track · corrodedSEAT TRACK BETWEEN FRAME 31 AND 35 AT -Y1552 IS CORRODED AT LOCATIONS: FR33 + 2". // CORROSION REMOVED FROM SEAT TRACK IAW A330 SRM 51-74-00 REV 103
PARA 6.A THRU 6.B (3)B CORROSION AT LOCATION FR33+2" LOCATED ON INNER VERTICAL SURFACE AREA. UNABLE TO SUFFICSDR HALA2019081320341Unknown · odorATB, STRONG FUMES IN ENTIRE AIRCRAFT DURING INITIAL CLIMB FOR UP TO 20 MINS. CLEARED WITH NO USAGE OF CHECKLIST. T/S PER A330 FIM 21-00-00-810-801-A. NO DEFECTS NOTED. INSPECTED BOTH ENG'S . NO DEFECTS . OPENED AND INSPECTED BOTH PACKS AND NO DEFECTS. RAN ESDR HALA2019080530380Generator · inoperativeETOPS - APU GENERATOR FAILED AND UNABLE TO RESET. COMPLETED REMOVAL AND INSTALLATION OF NEW GENERATOR PER AMM 24-23-51-000-801-A/400-801A OPS CHECK GOOD. OK FOR SERVICE.SDR HALA2019072000364Transfer Valve · inoperativeETOPS / FUEL AFT TRANSFER INOP STATUS AFTER START RESET FCMC #1. REMOVED AND REPLACED FUEL AFT XFR VALVE 1 (700QN1).SDR HALA2019071500361Unknown · malfunctionedETOPS SIGNIFICANT SYSTEM - #1 RADAR INOP. PERFORMED OPS CK OF WXR 1 PER A330 AMM 34-41. OK FOR SERVICE. TEST OK.SDR HALA2019061800305Chip Detector · faultedETOPS SIGNIFICANT SYSTEM - ON ENG SHUTDOWN AT GATE AFTER FLIGHT, ENG 2 OIL CHIP DETECTED FAULT. PERFORMED TSM 79-20-00-810-824-A AND BITE CHECK OF EEC 2 CHA+B,
NO FAULTS DETECTED, INSPECTED NR 2 ENG CHIP DETECTOR, NO DEFECTS NOTED. OK FOR SVC.SDR HALA2019040100160Generator · faultedETOPS SIGNIFICANT SYSTEM - APU GEN FAULT. // PERFORMED TSM 24-20-81-810-942-A. REMOVED AND REPLACED APU GEN
PER AMM 24-23-51. OPS NORMAL, NO DEFECTS NOTED. LEAK CHECK OK. OK FOR SVC.SDR HALA2019031800135Warning System · false activationETOPS SIGNIFICANT SYSTEM - AFTER STARTING NR 2 ENG ECAM ENG2 OVSP PROT FAULT, ENGINE PARAMETERS NORMAL. MAINT CONTROL TOLD US TO SHUT DOWN ENG 2 AND RESTART. AFTER RESTART NO ECAM OR FURTHER MESSAGE ALL INDICATIONS NORMAL. SYSTEM TEST OF EEC 2 OK NO FAULTS NOTSDR HALA2019013100034Smoke Warning · false activationRCVD 2 TEMPO LAV SMOKE ALARMS ENROUTE. PERFORMED BITE OF SDF, NO FAULTS. OK FOR SVC.SDR HALA2018123100680Oil System · lowETOPS SIGNIFICANT SYSTEM - APU LOW OIL LEVEL MSG.// PERFORMED TSM 49-00-00810-815A. FAULT APU OIL LVL LOW, SERVICE APU PER AMM 12-13-49. NO LEAKS NOTED, OK FOR SVC.SDR HALA2018122740678Warning Message · false activationOPEN - ATB - INTERMITTENT FWD CARGO VENT AND BULK VENT INOP SYS INDICATIONS. ATB DUE TO DOG IN BULK CARGO.// PERFORMED VC SYSTEM 21-28-00-710-802A. SYSTEM TEST PASSED. ON CONDITION PAGE UNABLE TO CONTROL BULK CARGO TEMP. DEACTIVATED BULK CARGO ISOL VALVES PER SDR HALA2018112760611Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ENG 1- AIR EXCHANGER FAULT MINOR FAULT.// PERFORMED ENG 1 EEC CHAN"A" AND CHAN"B" TEST PASSED TAW AMM 73-21-00-710-812 AND "AIR/OIL HEAT EXCHANGER"CONNECTORS CLEANED AND RESECURED.SDR HALA2018111900599Lens · loose3L DOOR EXIT LIGHT COVER LOOSE.// RE-SECURED 3L DR EXIT LIGHT COVER. SECURITY CK GOODSDR HALA2018111500586Fault Message · false activationETOPS SIGNIFICANT SYSTEM - "ENG. 1 MINOR FAULT". // PERFORMED BITE CHECK OF BOTH EEC'S. NO FAULTS DETECTED. COULD
NOT DUPLICATE FAULT. OK FOR SVC.SDR HALA2018111400585Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ECAM "ENG 1 AIR EXCHANGER FAULT".// TROUBLESHOT FAULT MESSAGE FOR FLIGHT REPORT PER A330 TSM 79-20-00-810-809-A. OPERATIONALLY CHECKED AIR EXCHANGER VALVE. NO FAULTS NOTED. VISUALLY CHECKED ALL CANNON PLUGS AND PINS ATTACHED TO AIRSDR HALA2018110500365Warning Message · false activationETOPS SIGNIFICANT SYSTEM - ON LANDING. ENG 1 AIR EXCHANGER FAULT. ENG 1 MINOR FAULT.// PERFORMED TROUBLE SHOOT PER TSM 79-20-00-810-809-A. VISUAL INSPECTED AIR OIL/HEAT EXCHANGER, NO DAMAGE FOUND. PERFORMED FADEC SYSTEM TEST PER AMM 73-21-00. SYSTEM TEST OK. SDR HALA2018110500366Oil System · lowETOPS SIGNIFICANT SYSTEM - APU LOW OIL LEVEL. SERVICED 3 QT OF APU OIL PER AMM 12-13-49. C/W VISUAL INSPECTION OF APU & NO LEAK NOTED, RAN APU & OPS CHK GOOD. OK FOR
SVC.SDR HALA0218082100392Filter · activatedAFTER STARTING APU. APU FAULT ECAM MESSAGE, SHUT DOWN THE APU IAW ECAM. ECAM MESSAGE, LUBE PUMP FILTER & GEN SCAV FILTER 5100KT9. INSPECTED
BOTH OIL LUBE FILTER AND GEN SCAV FILTERS IAW TSM 49-62-00-810-916-A. NO FINDINGS OF METAL. DPI ON LUBE FILTER TRIPSDR HALA2018070200321Light · missingAFT GALLEY EMERGENCY LIGHT STRIP MISSING A PORTION. REPLACED EMERGENCY LIGHT STRIP IAW AMM 33-52, OPS CHECKED NORMAL. OK FOR SERVICE.SDR HALA2018062600307O-Ring · damagedDIVERSION TO NEAREST AIRPORT DUE TO G HYD FAILURE, LANDED BELOW 400K WEIGHT. FOUND GREEN HYD SYS HP MANIFOLD 5102JM OUTBOARD BLEEDER PLUG ORING DAMAGED. REMOVED AND REPLACED ORING PER AMM 29-11-53, RE-SERVICED GREEN SYSTEM, RAN ALL ELEC AND ENGINE DRIVEN PUMPSSDR HALA2018062600199O-Ring · damagedDIVERTED DUE TO GREEN HYDRAULIC SYSTEM QUANTITY LIGHT ON. REPLACED A DAMAGED GREEN HYDRAULIC SYSTEM HP MANIFOLD 5102JM OUTBOARD BLEEDER PLUG O-RING.SDR HALA2018062100296Sign · detachedEXIT SIGN AT THE R3 DOOR FELL OFF INFLIGHT. ATTACHED THE EXIT SIGN. SECURITY CHECKED GOOD.SDR HALA2018041000160Warning Message · false activationNR 2 ENGINE LP VALVE FAULT ECAM MESSAGE. PERFORMED A BITE TEST OF FCMS IAW AMM 28-51-00, NO DEFECTS NOTED.SDR HALA2018031500105Indication Sys · malfunctionedETOPS SIGNIFICANT SYSTEM - FUEL FLOW INDICATIONS + TOTALIZER DO NOT INDICATE ON FUEL. PERFORMED RESET OF FCMC 1 & 2. INDICATIONS NORMAL. OK FOR SVC.SDR HALA2018022200048Seam · leakingPRIOR TO DEPARTURE GROUND CREW FOUND A FUEL LEAK FROM THE RIGHT WING. FUEL LEAK FROM RIGHT WING SEAM BETWEEN FWD SPAR AND UPPER WING SUFRACE 5 - 6 INCHES INBD FROM RIB 11. RIGHT WING SEAM REPAIRED. LEAK CHECKED GOOD.SDR HALA2017120400268Lens · missingOVERHEAD AISLE EMERGENCY LIGHT AT ROW 25 LEFT MISSING LENS. INSTALLED NEW LENS.SDR HALA2017101600248Sign · detachedR3 DOOR EXIT SIGN DETACHED. SECURED THE SIGN.SDR HALA2017062000193Sign · detachedL3 DOOR EXIT SIGN DETACHED FROM CEILING. REPLACED THE EXIT SIGN.SDR HALA2017053000130Actuator · malfunctionedNR 2 A/C PACK REGULATOR FAULT. NR 2 PACK RAM AIR DOOR CLOSED ECAM MESSAGE. PERFORMED TROUBLESHOOTING IAW TASK 21-63-00-810-886-A. RESET THE CIRCUIT BREAKERS FOR PACKS 1 & 2, AND SYSTEM TESTED IAW AMM 21-63-00, FOUND CLASS 3 FAULT ON THE NR 2 PACK AIR INLETSDR HALA2017041700155Light · unsecureROW 17A EMERGENCY LIGHT NOT SECURE. SECURED THE EMERGENCY LIGHT.SDR HALA2017041700156Light · unsecureEMERGENCY LIGHT LOOSE ADJACENT TO 45HJ. EMERGENCY LIGHT SECURED.SDR HALA2017040900094Brake · lockedABORTED TAKEOFF DUE TO ACFT PULLED HARD LEFT AT BEGINNING OF T/O ROLL APPEARS NR 1 & NR 5 WHEEL BRAKES LOCKED UP ABORTED AT APPROXIMATELY 70-80 KNOTS. REF LOG 8115523 NR 1 BRAKE "GRABBING". REMOVED & REPLACED NR 5 BRAKE ASSY PER AMM 32-42-27. OPS NORMAL NO DESDR HALA2016121700551Controller · malfunctionedF/O SIDE STICK FCPC 1 FAULT. REMOVED AND REPLACED FLT CONTROL STICK CONTROLLER IAW AMM 27-92-41 UP TO STEP 4G,SDR HALA2016120600523Unknown · odorFA'S IN AFT GALLEY AREA REPORTED A TEMPORARY "ELECTRICAL BURNING" SMELL THEY COULD NOT LOCATE EXACT LOCATION BUT PWRD OFF ALL AFT OVENS AND SMELL WENT AWAY. OPERATED ALL 7 AFT GALLEY OVENS, COULD NOT DUPLICATE "ELECTRICAL BURNING" ODOR. NO DEFECTS NOTED, OK FSDR HALA2016111000206Cover · unsecureDOOR 3R EXIT SIGN COVER FELL OFF. RE-ATTACHED EXIT SIGN COVER.SDR HALA2015101200210Engine · making metalACFT RETURNED TO GATE, APU AUTO SHUTDOWN. OIL CHIP DETECTION MESSAGE 499111. TROUBLESHOT IAW TSM 49-62-00-810-915-A, REPLACED SCAVANGE/LUBE FILTERS IAW AMM 49-91-41, COLLECTED OIL SAMPLES, NO METAL NOTED. INSPECTED CHIP DETECTOR, AND FOUND SMALL METAL PARTISDR HALA2014122100214Warning Message · false activationFM MESSAGES ON MCDU NR 1. PERFORMED RESET OF BOTH FMGEC 1 & 2, AFS BITE IAW 22-96-00, TEST OK. OK FOR SERVICE.SDR HALA2014102900178Fuel Sys · malfunctionedEXCESSIVE FUEL FLOW ON NR 1 ENGINE DURING CLIMBOUT + 3-4000 LBS AN HOUR. THEN NORMAL DURING CRUISE/LEVEL OFF NR 1 FUEL USED 1200 LB > THAN NR 2 ENG (CONT) 3 + 20 HRS AFTER DEPARTURE NR 1 ENG FUEL FLOW CYCLING BETWEEN 5- 9000 LBS AN HOUR DURING CRUISE FUEL USESDR HALA2014091600138Warning Light · false activationAPU START SUCCESSFUL. APU FAULT AFTER INFLIGHT START. TROUBLESHOT IAW TSM 49-62-00. CHECKED LUBRICATION, OIL FILTER AND GENERATOR OIL FILTER DIFFERENTIAL PRESSURE INDICATORS. CHECK OK. PERFORMED APU TEST IAW AMM 49-62 TEST OK. INDICATION NORMAL. UNABLE SDR HALA2014062900092Computer · malfunctionedBLEED AIR LOW TEMP ECAM LT ENGINE DURING INITIAL CLIMB, PERFORMED ECAM ACTIONS, JETTISON FUEL FOR NORMAL LANDING. REMOVED AND REPLACED NR 1 BMC IAW AMM 36-11-34. BITE TEST OK PER AMM 36-11-00. ACCOMPLISHED TSM 36-21-00-810-914-A. NO FAULTS NOTED ON GROUND.SDR HALA2014053000073Adiru · out of alignmentAFTER ADIRS ALIGNMENT ECAM AUTO FLT FM1 FAULT. ALIGNED ADIRS. RESET FMGEC 1 & 2. GROUND OPS CHECKED OK, AMM 22-96-0.
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