N965AM
Service difficulty reports · 24
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 = 'N965AM' 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 = 'N965AM' 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 ASMF202512090324Brake · faultedTHE PARKING BRAKE SET MSG DOES NOT SHOW IN THE EICAS WHEN THE PARKING BRAKE IS SET. REPLACED PARKING SER BULB AND CONFIRMED MAINT PAGE ATA 32. PARKING BRAKE OPERATION IAW MEL 32-45-01.SDR 2025FA0000412Satcom · faultedSATVOICE LOST MESSAGE, WAS CARRY OUT PROCEDURE FIM DMC-B787-A-23-10-F5-01A-421A-ASDR 2025F00144Satcom · faultedSATVOICE LOST MESSAGE AND WAS CARRY OUT PROCEDURE IAW DMC-B787-A-23-10-F5-01A-421A-ASDR M17F202307030007Control Unit · failedTRIM AIR RIGHT INOP BEFORE TAKEOFF. 216 103 42.
TRIM AIR LEFT IN FLIGHT FL380 RESET OK. 216 103 41.
PACK L FL380. 215 101 41 / CAB ALT ALERT WARNING FL380. 213 101 00.SDR 2022F00211None · failedACTUADOR FRENO 3 EN ESTATUS, AUTOBRAKE NO PUEDE SER SELECCIONADO / FALLA DE UNIDAD DE CONTROL DEL SITEMA DE FRENOS (BSCU)SDR ASMF202110000023None · noneDURING TRANSIT CHECK, IT WAS DETECTED SEVERAL LIGHTNING STRIKE ON FUSELAGE SKIN. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION PHASE 1A, LEVEL EXAMINATION AND PHASE 1B AND II, GENERAL VISUAL INSPECTION AND SYSTEM COMPONENTS IAW AMM SDR ASMF202110016None · noneDURING TRANSIT CHECK, IT WAS DETECTED AN EXPOSED MATERIAL ON LH ENGINE INBOARD THRUST REVERSER. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING EXPOSED MATERIAL ON LH ENGINE INBOARD THRUST REVERSER SLEEVE INNER BARREL SURFACE ON AREA OF 0.625" BY 1.5", LOCSDR 2021F00196Sleeve · damagedEXPOSED MATERIAL ON LH ENGINE INBOARD THRUST REVERSER SLEEVE. MAINTENANCE PERSONNEL PERFORMEDREVISION, DETECTING EXPOSED MATERIAL ON LH ENGINE INBOARD THRUST REVERSER SLEEVE INNER BARREL SURFACE ON AREA OF 0.625" BY 1.5", LOCATED ON TRANSIENT BLEED AIR DUCT AFSDR ASMF201904230013Brake Assy · damagedCAPTAIN REPORTED THAT AFTER LANDING, “AUTO BRAKE”, “BRAKE CONTROLS” AND “ELEC BRAKE PWR UNIT L1” MESSAGES WERE SHOWED ON EICAS; MAINTENANCE PERSONNEL PERFORMED TEST VIA AHM SHOWING FOLLOWING CODES: 24-43611 AND 32-49511;SO THE WO´S 5256177, 5256163 AND 5256176SDR ASMF2019042309Warning Message · false activationAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, THE MESSAGE IN EICAS AND STATUS ELEC WERE SHOWN. MAINTENANCE PERSONNEL PERFORMED FIM DMC-B787-A-24-20-F8-64A-421A-A PROCEDURE, SHOWING FAILURE CODE 24-13412; SO THE FIM DMC-B787-A-24-20-F8-64A-421A-A PROCEDURSDR ASMF20190109003Fan · failedDURING TRANSIT CHECK, THE MESSAGE IN EICAS AND STATUS PACK MODE L WAS SHOWN. MAINTENANCE PERSONNEL PERFORMED FIM DMC-B787-A-21-50-F2-78A-421A PROCEDURE, SHOWING FAILURE CODE 21-65421, DETECTING THE RAM AIR FAN WITH FAILURE; SO THE RAM AIR FAN WAS REPLACED IAW SDR ASMF2018101509023Line · leakingRIGHT ENGINE HYDRAULIC LEAK
DURING TRANSIT CHECK, A HYDRAULIC LEAK WAS DETECTED IN THE RIGHT ENGINE PYLON. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING HYDRAULIC LEAK AND LOOSE HYDRAULIC LINE AT RIGHT ENGINE PYLON; SO THE HYDRAULIC LINE WAS TIGHTENED ISDR ASMF201801020Control Unit · failedAIRCRAFT RETURNED TO PLATFORM DUE TO A MESSAGE IN EICAS AND STATUS OF AUTO BRAKES AND BRAKE CONTROL WERE SHOWN. MAINTENANCE PERFORMED THE FIM DMC-B787-A-32-40-F2-34A-421A-A PROCEDURE, SHOWING FAILURE CODE BRAKES 42-01863, AUTOBRAKE 32-30530 AND BRAKE CONTROLSSDR ASMF201709005Warning Message · false activationAIRCRAFT RETURNED TO PLATFORM DURING TAXI, AN EICAS MESSAGE AND STATUS FLAP/SLAT CONTROL WAS SHOWN AND CONTROL SURFACE WITHOUT MOVEMENT. MAINTENANCE PERFORMED FIM DMC-B787-A-27-50-F1-J9A-421A-A PROCEDURE, CONFIRMING THE FAILURE AND THE ENGINE START FLAP LEVESDR ASMF201708002Line · leakingDURING TRANSIT CHECK IT WAS DETECTED FUEL LEAK FROM ENGINE 2, THEREFORE MAINTENANCE PERSONNEL PERFORMED LEAK TRACED TO LOOSE TUBE CONNECTION IAW DMC-B787-A-G71-00-FA-41A-421A-A AND TUBE CONNECTION WAS TIGHTENED IAW DMC-B787-A-G71-71-00-00A-280A-A, NO FURTHER LSDR ASMF201704007Windshield · crackedAIRCRAFT RETURNED FROM FLIGHT DUE TO DURING CLIMB THE LEFT WINDSHIELD CRACKED. MAINTENANCE PERSONNEL REPLACED THE FLIGHT COMPARTMENT NO.1 WINDOW LEFT SIDE IAW DMC-B787-A-56-11-01-00A-720A-A AND THE WINDSHIELD HEAT PROTECT UNIT IAW AMM B787-30-41--03-00A-720A. SDR ASMF201611012Fairing · crackedDURING RIGHT ENGINE 2 DAY CHECK, A BIRD STRIKE EVIDENCE WAS DETECTED AT RIGHT ENGINE AIR COOLER / OIL COOLER (ACOL). MAINTENANCE PERSONNEL PERFORMED THE BIRD STRIKE CONDITIONAL INSPECTION IAW AMM DMC B787-A-05-51-18-00A-280A-A, DETECTING BENT AND MISSING OF FISDR ASMF201611011Line · leakingDURING TRANSIT CHECK, AFTER TO REPLACE OF RIGHT VARIABLE FREQUENCY STARTER GENERATOR, A HYDRAULIC LEAK WAS DETECTED AT TUBE. MAINTENANCE REPLACED THE TUBE IAW AMM A-24-21-09-00B-520A-A / -720A-A, TESTED CORRECT.SDR ASMF201610020Tube · leakingDURING TRANSIT CHECK, AFTER TO REPLACE OF RIGHT VARIABLE FREQUENCY STARTER GENERATOR (VFSG), A HYDRAULIC LEAK WAS DETECTED AT TUBE OF VFSG. AIRCRAFT WAS SENT TO THE HANGAR, MAINTENANCE PERSONNEL REPLACED THE TUBE OF VFSG IAW AMM DMC B787-A-24-21-09-00B-520A-A SDR ASMF201606001Sensor · burnedCAPTAIN REPORTED A LIGHTNING STRIKE IN THE FUSELAGE SKIN DURING APPROACH. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE INSPECTION IAW DMC-B787-A-05-51-19-00C-280B-A, DETECTING BURNED MARKS AT LT SIDE STA 201, WL 270 AND 345, WL275, RT SIDE AT STA 117, WSDR ASMF201511001Module · damagedAIRCRAFT RETURNED OF FLIGHT DUE TO DURING CLIMB, THERE WAS NOT POTABLE WATER IN THE LAVATORIES. PERFORMED REVISION TO LAVATORIES IAW FIM DMC-B787-A-38-10-F1-73A-421A-A PROCEDURE, SHOWING FAILURE CODE 38-12669, DETECTING THE POWER MODULE RPDU41 DAMAGED. THE PSDR ASMF201506001Thrust Reverser · damagedDURING TRANSIT CHECK, IT WAS DETECTED THREE LIGHTNING STRIKES IN LT ENG LOCATED AT 03:00 POSITION. PERSONNEL PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION IAW DMC-B787-A-05-51-19-00C-280B-A, DETECTING TWO DAMAGES ON LT ENG OTBD REVERSER AT 09:00 POSITIOSDR ASMF2014061706012Tube · leakingDURING TRANSIT CHECK, IT WAS DETECTED A FUEL LEAK IN THE RT ENG STRUT SUPPLY TUBE. THE STRUT SUPPLY TUBE WAS REPLACED IAW DMC B787-A-28-22-21-03B-520A-A 720A & THE ENG FUEL FEED MANIFOLD LEAK TEST WAS PERFORMED IAW DMC-B787-A-28-22-21-23B-364A-A & DMC-B787-A-SDR ASMF201406001Tube · leakingDURING TRANSIT CHECK, IT WAS DETECTED A FUEL LEAK IN THE RT ENG STRUT SUPPLY TUBE. THE STRUT SUPPLY TUBE WAS REPLACED IAW DMC B787-A-28-22-21-03B-520A-A 720A & THE ENG FUEL FEED MANIFOLD LEAK TEST WAS PERFORMED IAW DMC B-787-A-28-22-21-02B-364A-A, TESTED CORR
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