N997AM

Service difficulty reports · 61

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 = 'N997AM' 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.

SDR ASMF200704002Sensor · failedAIRCRAFT REJECTED TAKEOFF AT 65 KNOTS DUE TO BLEED TRIP OFF LIGHT TURNED ON, ABNORMAL PROCEDURE QRH 2-4 WAS PERFORMED, RETURNING TO PLATFORM. AFTER MAINTENANCE INSPECTION, REPORT WAS DEFERRED IAW MEL 36-8. DURING TRANSIT CHECK, 390 DEGREES PNEUMATIC TEMPERATURApr 8, 2007 · N997AM · Boeing 737* · Pneumatic Indicating SystemSDR ASMF200608022Heating Element · failedAIRCRAFT RETURNED TO PLATFORM, (AUX PITOT HEAT) LIGHT TURNED ON. LIGHT WAS DEFERRED IAW MEL 30-5, CATEGORY (B) AND RVSM WAS MODIFIED WITH A NEW FLIGHT PLAN AT 270 FEET. DURING TRANSIT CHECK, THE AUXILIARY PITOT HEAT WAS REPLACED IAW FIM 30-31, TASK 801, TESTEDAug 30, 2006 · N997AM · Boeing 737* · Pitot/Static Anti-Ice SystemSDR ASMF200608007Transceiver · failedAIRCRAFT RETURNED TO PLATFORM, RADAR FAILURE. RADAR TRANSCEIVER WAS REPLACED IAW MM 34-43-41, TESTED CORRECT. AIRCRAFT WAS REFUEL.Aug 12, 2006 · N997AM · Boeing 737* · Doppler SystemSDR ASMF200606018Thrust Reverser · failedAIRCRAFT RETURNED TO PLATFORM (R ENGINE REVERSE) LIGHT TURNED ON AT P5. CAPTAIN PERFORMED 4 REVERSE CYCLES BUT FAIL CONTINUED. BITE TO EAU MODULE WAS PERFORMED AND REVERSE FAIL CODE APPEARED, THEREFORE, REVERSE WAS DEFERRED IAW MEL 78-1. DURING OVERNIGHT CHECKJun 28, 2006 · N997AM · Boeing 737* · Engine (Turbine/Turboprop)SDR ASMF200606001Warning System · malfunctionedAFTER ENGINES STARTED, -SPCU- LIGHT TURNED ON IN ELECTRICAL PANEL. CAPTAIN SHUT DOWN LEFT ENGINE AND ELECTRICAL PANEL WAS ERASED BUT FAIL CONTINUED. B-1 AND B-2 BREAKERS WERE RESEATED IN P-6 PANEL AND FIM 24-34 PROCEDURE WAS PERFORMED, ALL CORRECT. DURING OJun 1, 2006 · N997AM · Boeing 737* · DC Indicating SystemSDR ASMF200509003Actuator · failedCAPTAIN REPORTED THAT AILERON TRIM FAILED AND THE SELECTED RATE WAS OVERSHOOT. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK, THE CONTROL PANEL SWITCH OPERATION AND CONNECTOR ACTUATOR VOLTAGE WERE VERIFIED, DETERMINING THAT THE ACTUATOR NEEDS TO Sep 6, 2005 · N997AM · Boeing 737* · Aileron Tab Control SystemSDR ASMF200506009Heater · failedAIRCRAFT RETURNED TO PLATFORM AS CONSEQUENCE OF AUXILIARY PITOT DID NOT GET HOT FRM 303 060 00. THE REPORT WAS DEFERRED BY MEL 30-5. MAINTENANCE PROCEDURE WAS PERFORMED IAW FIM 30-31 TASK PAGE 801. DEFERRED REPORT WAS CLOSED.Jun 6, 2005 · N997AM · Boeing 73776N · Pitot/Static Anti-Ice SystemSDR ASMF200503019Eec · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE, N2 AND OIL PRESS WARNINGS TURNED ON. DURING CHECK, THERE WERE DETECTED RECENT FAULTS IN CDU WITH LEGENDS EEC NR 2 SUPPLY AND 73-21282-FAIL CODE. ENGINE WAS RESTARTED, SHUTTING DOWN AUTOMATICALLYMar 26, 2005 · N997AM · Boeing 737724 · Fuel Controlling SystemSDR ASMF200502007Ignition Unit · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT IGNITION SYSTEM FAILED IN LEFT ENGINE. DURING MAINTENANCE REVISION, THE C485 BREAKER LOCATED AT THE P18-2 A1 PANEL WAS THROWN AWAY. THE C485 BREAKER WAS REPOSITIONED IAW MM 74-00-00, TESTED CORRECT.Feb 7, 2005 · N997AM · Boeing 73776N · Ignition SystemSDR ASMF200501007Control Unit · failedDURING APPROACH, ATS DID NOT MAINTAIN SPEED, SPEED BRAKES DID NOT ARM, LIGHT TURNED ON, CAPT FLT DIRECTOR TURNED OFF, ALL ALERTS SOUND TURNED OFF, ILS WAS IN PARALLEL TO THE LOCALIZER AND PWS LIGHT TURNED ON. VERIFICATION FLIGHT WAS PERFORMED CONFIRMING FJan 13, 2005 · N997AM · Boeing 73776N · Landing and Taxi AidsSDR ASMF200501003Controller · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF "AUTO FAIL" LIGHT TURNED ON. BITE IN PRESSURIZATION CONTROLLER NR 2 WAS PERFORMED AND FAIL CONTINUE. DURING MAINTENANCE REVISION, CIRCUIT BREAKER P6-4 F3 WAS DETECTED ACTIVATED, CIRCUIT BREAKER WAS RESEATED ANDJan 5, 2005 · N997AM · Boeing 737 · Cabin Pressure Controller
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