N966AM
Service difficulty reports · 27
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 = 'N966AM' 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 = 'N966AM' 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 ASMF202607220157Warning Message · illuminatedAFTER ENGINE START ELEC C1 PUMP FAULT, WAS CARRY OUT PROCEDURE IAW FAULT CODE DMC-B787-A-24-10-F5-H1A-421A-ASDR 2026F00066Seal · leakingLOW OIL QTY INDICATION WITH LOW PRESSURE INDICATION, UNSCHEDULED LANDING, VFSG LH OF ENGINE NR 1 WAS REPLACED IAW AMM DMC B787-A-24-21-09-00B-520A-A/720A-A. ENGINE VENTS AND DRAINS INSPECTION WAS PERFORMED IAW DMC-B787-A-G71-00-00A-280A-A, REPLACEMENT OF SDR ASMF2025111100304Seal · leakingDURING WALKAROUND FOUND SIGNS OF OIL LEAKS COMING FROM HEATER DRAIN VFSG RIGHT PAD ON ENGINE 2. SIX DROPS PER MINUTE. RIGHT VFSG ACCESORY GEARBOX SEAL ENG # 2 WAS REPLACED IAW AMM DMC-787-A-G72-64 -01-00A-520A-A /SDR 2024F00076Brake · warning messageBRAKE MESSAGE ON EICAS BEFORE ENGINE START. CORRECTIVE ACTION TAKE: NLG 04 ELECTRICAL CARBON BRAKE ASSY B787-8 WAS REPLACED IAW AMM 32-42-04-00A-520ASDR ASMF202110022None · noneDURING TRANSIT CHECK, IT WAS DETECTED SEVERAL LIGHTNING STRIKE ON LH ELEVATOR LOWER SKIN. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION PHASE 1A, LEVEL EXAMINATION AND PHASE 1B AND II, GENERAL VISUAL INSPECTION AND SYSTEM COMPONENTSSDR ASMF202110013None · noneDURING TRANSIT CHECK, IT WAS DETECTED SEVERAL LIGHTNING STRIKE ON WINDOW EROSION PROTECTION. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION PHASE 1A, LEVEL EXAMINATION AND PHASE 1B AND II, GENERAL VISUAL INSPECTION AND SYSTEM COMPONESDR ASMF202110006None · noneDURING TRANSIT CHECK, IT WAS DETECTED A SEVERAL LIGHTNING STRIKES ON FWD CARGO DOOR AND FUSELAGE SKIN. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION PHASE 1A, LEVEL EXAMINATION AND PHASE 1B AND II, GENERAL VISUAL INSPECTION AND SYSTSDR ASMF202110004None · noneDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED A SEVERAL LIGHTNING STRIKES ON FUSELAGE SKIN. MAINTENANCE PERSONNEL PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION PHASE 1A, LEVEL EXAMINATION AND PHASE 1B AND II, GENERAL VISUAL INSPECTION AND SYSTEMSDR ASMF202106018Control Box · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING RIGHT ENGINE START, THE RIGHT ENGINE CONTROL LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO RIGHT EEC IAW FIM DMC-B787-A-G733-20-F1-51A-421-A-A, SHOWING FAILURE CODE 732 466 52; SO THE RIGHT ENGINE CONFIGURSDR 2021F00172Control Box · failedAFTER ENGINE START R ENG CONTROL MESSAGE ON STATUS. AIRCRAFT RETURNED TO PLATFORM DUE TO DURING RIGHT ENGINE START, THE RIGHT ENGINE CONTROL LIGHT TURNED ON. MAINTENANCE PERSONNEL PERFORMED BITE TO RIGHT EEC IAW FIM DMC-B787-A-G733-20-F1-51A-421-A-A, SHOWING FSDR ASMF202106014Ball Mat · damagedDURING 4MO-P CHECK IN TASK CARD J8750-030-00-01 (27) AT MEX STATION, IT WAS DETECTED THE ROLLER OF PDU IN BALL MAT 122HF AND BALL MAT 121GF AT FWD CARGO COMPARTMENT OUT OF LIMITS. THE WO’S 7487831 AND 7487833 WERE ISSUED TO PERFORM PERMANENT REPAIR. THE PDU ROSDR 2021F00161Roller · failed25.05.2021 18:42 SEVERAL ROLLER OF PDU AT FWD CARGO COMPARTMENT
DURING 4MO-P CHECK IN TASK CARD J8750-030-00-01 (27) AT MEX STATION, IT WAS DETECTED THE ROLLER OF PDU IN BALL MAT 122HF AND BALL MAT
121GF AT FWD CARGO COMPARTMENT OUT OF LIMITS. THE WO’S 7487SDR ASMF202101003Fairing · damagedDURING OVERNIGHT CHECK AT MEX STATION, IT WAS DETECTED A DENT WITH DAMAGE AND PEELING PAINT ON WING TO BODY FAIRING PANEL 196AR. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT OUT OF LIMITS WITH DAMAGE AND PEELING PAINT ON WING TO BODY FAIRING PSDR ASMF20200602011Skin · damagedDURING TRANSIT CHECK, IT WAS DETECTED EVIDENCE FUEL LEAK WITH 90 DROPS BY MINUTE IN THE CENTRAL MAIN TANK. MAINTENANCE PERSONNEL PERFORMED EMPTIED CENTRAL MAIN TANK PROCEDURE, CENTER MAIN TANK REFUEL VALVES HAVE BEEN DEFERRED BY MEL 28-21-01-02 WITH FLIGHT NOSDR ASMF20200602002Transducer · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAXING, IT WAS SHOWN MESSAGE 325 132. MAINTENANCE PERSONNEL PERFORMED TESTS SHOWING FAILURE CODE 32-63017. PERFORMED FIM DMC-B787-A-32-50-F1-24A-421A-A STILL CONTINUING FAILURE SO AIRCRAFT WAS SENT TO THE HANGAR ANSDR ASMF2019100910Ring · out of positionDURING OVERNIGHT CHECK, IN BORESCOPE INSPECTION OF THE LEFT ENGINE WAS DETECTED A THE PISTON RING OUT OF POSITION ON TWO DIFFERENT ZONES BETWEEN THE OGV`S AND BLADES OF 10TH STAGE OF HIGH PRESSURE COMPRESSOR, DUE TO THIS CONDITION THE ENGINE IS OUT OF LIMITS ISDR ASMF20190816004Blade · missingDURING TRANSIT CHECK, IT WAS DETECTED MISSING MATERIAL ON FAN BLADE OF ENGINE NO. 1S/N: 956321; AIRCRAFT WAS SENT TO THE HANGAR AND MAINTENANCE PERSONNEL ISSUED THE WO 5544667 TO PERFORM A CONDITIONAL INSPECTION; IT WAS FOUND FAN BLADE WITH MISSING MATERIAL WISDR ASMF20190614015Control Unit · failedCAPTAIN REPORTED THAT EMERGENCY LIGHTS WERE BLINKING DURING TAKEOFF; SO THE FLIGHT CREW TURNED ON THE SWITCH AND CONTINUING TO DESTINATION. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING THE ROWS 28 TO 33 LIGHTS TURNED OFF, DURING THE APPLICATION OF TROUBLSDR ASMF2019010900012Fuel Cell · leakingDURING TRANSIT CHECK IN NRT STATION, MAINTENANCE PERSONNEL DETECTED FUEL LEAK (2 DROPS/SEG.) OUT OF LIMITS AT CENTER TANK AT THE REAR SPAR IN RH WHEEL COMPARTMENT; AIRCRAFT RETURN TO MEXICO CITY IAW BOEING MESSAGE 4-4342867131 “AEROMEXICO WOULD LIKE TO FLY THESDR ASMF20180918016Window · crackedDURING TRANSIT CHECK, IT WAS DETECTED THE LEFT FLIGHT COMPARTMENT WINDOW NUMBER 1 CRACKED. MAINTENANCE PERSONNEL PERFORMED REVISION DETECTING CRACKS OUT OF LIMITS IAW AMM DMC-787-A-56-11-00-03A-663A-A. THE LEFT FLIGHT COMPARTMENT WINDOW NUMBER 1 WAS REPLACED ISDR ASMF201802005Bumper · missingDURING TRANSIT CHECK, IT WAS DETECTED A MISSING RIGHT FWD BUMPER UPPER INSIDE OF THE OUTBOARD THRUST REVERSER. MAINTENANCE PERSONNEL REPLACED THE THRUST REVERSER RIGHT FWD UPPER BUMPER P/N 721Z3330-409 IAW MESSAGE BOEING NUMBER AMX-AMX-18-0146-02B RECORD NUMBESDR ASMF201801015Motor · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING TAKEOFF ROLL, THE MESSAGE SLAT SECONDARY FAIL AND CONFIGURATION ALARM WERE SHOWED WITH A SLAT SPLIT INDICATION AND SHIP SPEED WAS ALMOST CERO. MAINTENANCE PERSONNEL PERFORMED THE FLAP / SLAT OPERATION CHECK IAW FIM 2SDR ASMF201703008Valve Guide · leakingDURING TRANSIT CHECK, A FUEL LEAK WAS DETECTED IN THE RIGHT ENGINE. MAINTENANCE PERSONNEL PERFORMED REVISION, DETECTING FUEL LEAK IN THE TOP CAT OF FOHX FROM VSFG IAW AMM DMC-B787-A-G71-71-00-00A-280A-A. THEREFORE FUEL VALVE GUIDE POPPET WAS REPLACED IAW GENX SDR ASMF20161216010Valve · failedAIRCRAFT RETURNED TO PLATFORM DUE TO DURING START ENGINES, THE LEFT ENGINE AUTO STAR SYSTEM FAILED. MAINTENANCE PERSONNEL PERFORMED REVISION TO AUTO STAR SYSTEM, DETECTING THE EICAS MESSAGE FAIL, MAINTENANCE CODE 28-19217 AND THE CIRCUIT BREAKER C2822803 POPPESDR ASMF201510017Oxygen Bottle · leakingAIRCRAFT PERFORMED AN UNSCHEDULED LANDING DUE TO DURING CRUISE AT 38,000 FEET, THE CREW OXYGEN LOW LIGHT TURNED ON. PERFORMED AN OXYGEN CREW INSPECTION IAW AMM 35-12-85, DETECTING OXYGEN BOTTLE MANOMETER WAS INDICATED 0 PSI. THE OXYGEN BOTTLE WAS REPLACED IASDR ASMF201509002Motor · failedDURING TRANSIT CHECK, IT WAS DETECTED MSG IN EICAS & STATUS OF FLIGHT CONTROLS & SPOILERS WERE NOT FOLLOWED THE COMMAND. PERFORMED REVISION AT FLIGHT CONTROLS SYS IAW DMC B787-A-27-61-18-00A-720A-A, DETECTING THE SPOILER ELEC MOTOR UNIT POSITIONS 4, 5, 10 & 1SDR ASMF2014061706011Cowling · dentedDURING TRANSIT CHECK, DETECTED A DENT IN LT ENG INLET COWL NOSE AT 2:30 HRS POSITION OF 3 INCH LENGTH, 0.031 INCHES IN DEPTH, 1 INCH WIDE WITH MISSING MATERIAL & THREE SCRATCHES OF 0.875 INCHES, 2 INCHES & 1.5 INCHES OUT OF LIMITS IAW AMM DMC-B787-A-54-11-01-0
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