N964AM
Service difficulty reports · 19
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 = 'N964AM' 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 = 'N964AM' 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 2025FA0000261Windshield · brokenWINDSHIELD RH BROKEN DURING FLIGHTSDR M17F20230703005Motor · unserviceableCTR SYS HYD ELECT MOTOR C1 PUMP ON STATUSSDR 2022F00217None · abnormalMANIJA DE ASEGURAMIENTO Y LIBERACION DE TOBOGÁN DURA, DESPLIEGUE DE TOBOGAN PUERTA 1L , GUARDA (MICA) DE LA PALANCA DE ARMADOY DESARMADO DE TOBOGÁN DESAJUSTADA. SDR ASMF202106008Acoustic Panel · damagedDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED DAMAGES AT RIGHT ENGINE THRUST REVERSER INNER WALL ACOUSTIC PANEL. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING THE RIGHT ENGINE AT BOTH THRUST REVERSERS INNER WALL ACOUSTIC PANELS LEADING EDGE WISDR ASMF202104001Engine · making metalDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED THE MESSAGE IN EICAS AND STATUS OF ENG OIL DMS L. MAINTENANCE PERSONNEL PERFORMED A REVISION, CONFIRMING THE MESSAGE IN EICAS AND STATUS OF ENG OIL DMS; SO THE DEBRIS MONITORING SYSTEM SENSOR DETAILED INSPSDR ASMF20200603016Windshield · crackedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT LPLA DUE TO LEFT WINDSHIELD GOT CRACKED. MAINTENANCE PERSONNEL REPLACED THE LEFT FLIGHT COMPARTMENT NUMBER 1 WINDSHIELD IAW AMM DMC-B787-A-56-11-01-00A-520A-A/720A-A AND THE LEFT WINDSHIELD HEAT PROTECTION UNIT WASSDR ASMF20190614014Oxygen Bottle · low pressureAIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT JFK DUE TO CREW OXYGEN CYLINDER WITH LOW PRESSURE AND DURING CRUISE AT 37,000 FEET AND THE OXYGEN PRESS DROPS 250 PSI WITH 1 HR. MAINTENANCE PERSONNEL PERFORMED AN OXYGEN CREW INSPECTION IAW AMM 35-12-85, DETECTING SDR ASMF201904230003Screw · looseDURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN THE RIGHT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING FUEL LEAK IN THE MANIFOLD BY LOOSE SCREWS; SO MANIFOLD LOOSE SCREWS WERE TIGHTENED IAW AMM DMC-B787-A-G71-71-00-00A-280A-A, ALL CORRECT.SDR ASMF201901090008Fuel Cell · leakingAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXYING, A FUEL LEAK WAS DETECTED IN THE LEFT WING; MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING FUEL QUANTITY IMBALANCE IN EACH TANK WITH FOLLOWING VALUES: 17.3 LH TANK, 16.8 RH TANK AND 4.5 CENTRAL TANK; SOSDR ASMF20180821007Module · failedAFTER LANDING, DURING FLAPS RETRACTION, THE SLAT DRIVE NON NORMAL CONDITION OCCURRED. MAINTENANCE PERFORMED FAULT ISOLATION PROCEDURE IAW AMM DMC-B787-A-27-81-00-00B-320A-A, TESTED CORRECT. ADDITIONALLY FLIGHT CONTROL MODULE WAS REPLACED IAW DMC-B787-A-27-02SDR ASMF20180625010Blade · damagedDURING A TRANSIT CHECK, DETECTED FOD DAMAGE TO THE LOW PRESSURE TURBINE 7TH STAGE OF THE LEFT ENGINE. MAINTENANCE PERFORMED AN INSPECTION AND FOUND A NICK WITH TWO CRACKS ON THE LOW PRESSURE TURBINE BLADE. FOUND OUT OF LIMITS IAW AMM DMC-B787-A-G72-00-00-10B-SDR ASMF201802004Window · crackedCAPTAIN REPORTED THAT DURING DESCENT, THE RIGHT FORWARD WINDSHIELD CRACKED AT FL 230 FT. MAINTENANCE PERSONNEL REPLACED THE RIGHT FORWARD WINDSHIELD IAW DMC-B787-A-56-11-01-00A-520A-A AND DMC-B787-A-56-11-01-00A-720A-A AND RIGHT WINDOW HEAT PROTECTION UNIT WASSDR ASMF20180116002Unknown · leakingDURING TRANSIT CHECK, DETECTED A HYDRAULIC LEAK IN THE LEFT MAIN LANDING GEAR RETRACT ACTUATOR. MAINTENANCE PERFORM A PRESSURIZATION OF THE SYSTEM TO VERIFY THE LEAKS, DID NOT CONFIRM THE HYDRAULIC LEAK. AS A PRECAUTION, THE LEFT MAIN LANDING GEAR RETRACT ASDR ASMF201708006Rectifier · malfunctionedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING ENGINES START, THE MESSAGES IN EICAS AND STATUS WERE SHOWN OF CABIN AIR CPRSR L2, RAM FAN PRIMARY L, HYD PUMP DEM R WERE SHOWN WITH MESSAGE CORRELATIONED P700 SOFT START RELAY MODULE CLOSED. MAINTENANCE PERSONNEL PERSDR ASMF201707004Outflow Valve · unknownAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, THE MESSAGES IN EICAS AND STATUS OF CABIN ALTITUDE, MSG 21-34127 AND EQUIP OVBD VALVE AFT, MSG 21-29021. MAINTENANCE PERSONNEL PERFORMED REVISION IAW AMM 21-27-00, CONFIRMING FAILURE IN PRESSURIZATION SYSTEM WITSDR ASMF201704012Scavenge Pump · damagedAIRCRAFT RETURNED, DURING CLIMB LEFT ENGINE OIL LOW PRESSURE INDICATION, CAPTAIN REPORTED STATUS MESSAGES FOR LEFT ENGINE OIL FILTER SENSOR AND LEFT ENGINE OIL SYSTEM, WITH N2 OF LEFT ENGINE 92.7% PRESSURE WAS 33 PSI. MAINTENANCE REPLACED THE OIL FILTER SENSOSDR ASMF201503027Bpcu · failedAIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO SEVERAL MSGS IN EICAS & STATUS. DETECTED FAIL & REPLACED THE LT BPCU IAW DMC-B787-A-24-41-05-004-520A-A & DMC-B787-A-24-41-05-00A-720-A, TESTED CORRECT. THE OVERWEIGHT LANDING CONDITION INSPECTION WAS NOT NECESDR ASMF201503024Structure · damagedDURING TRANSIT CHECK, CAPTAIN REPORTED LIGHTNING STRIKE. ACFT WAS SENT TO THE HANGAR & LIGHTNING STRIKE INSPECTION WAS PERFORMED IAW DMC-B787-A-05-51-19-00C-280B-A. DETECTED DAMAGED AT STATION 1425 BETWEEN STRINGER 11 & 12. NON-ROUTINE CARD A0224971 WAS GENSDR ASMF201403002Warning System · false activationAIRCRAFT RETURNED TO PLATFORM DUE TO CONFIGURATION STABILIZER WARNING LIGHT TURNED ON. MX PERFORMED THE FIM DMC-B787-A-27-02-00-28A-110A-A PROCEDURE, NO FAILURE WAS DETECTED, TESTED CORRECT.
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