N703AM
Service difficulty reports not matched to an aircraft · 21
They name N703AM, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N703AM' AND registry_match IS NULL 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 = 'N703AM' AND registry_match IS NULL 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 ASMF20070506Fuel Control · failedAIRCRAFT AIR TURN BACK, APU FAILED DURING CLIMB AND RT GENERATOR WAS INOPERATIVE. AIRCRAFT LANDED WITH 84367 KG AND MAXIMUM LANDING WEIGHT IS 85811 KG IAW DISPATCH MANUAL 5-3-1/2 NOT REQUIRING OVERWEIGHT LANDING INSPECTION. MAINTENANCE PERSONNEL REPLACED RT SDR ASMF200701008Blade · bentDURING TRANSIT CHECK, A BLADE WAS DETECTED DAMAGED DUE TO A FOD IN RT ENGINE. 3 BENDS WERE DETECTED AT 2 INCHES FROM BLADE LEADING EDGE TO MIDSPAN SHROUD, ONE OF 1.2500 INCH, OTHER OF 1.1250 INCH AND THE LAST ONE OF .8750 INCH. (2) BLADES SETS OF FAN STAGE WSDR ASMF200605001Warning System · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING LEFT ENGINE START, THE -L GEN- AND -LOW OIL PRESSURE- LIGHTS TURNED ON AND EGT REACHED 430 DEGREES CELSIUS. THE MAINTENANCE PAGE WAS CHECKED VERIFING THE EXCEDENCIES PARAMETERS, BEING ALL CORRECT. LEFTSDR ASMF200604015Warning Light · illuminatedAFTER ENGINE STARTING, CAPTAIN REPORTED THAT THE SPOILER LIGHT TURNED ON IN EICAS. THE FIM PROCEDURE 27-09-00 WAS PERFORMED AND NON FAULT WAS REPRODUCED. AIRCRAFT WAS DISPATCHED AND RETURNED TO PLATFORM AS A CONSEQUENCE THAT THE SPOILER LIGHT TURNED ON IN THSDR ASMF200604003Wheel · damagedDURING THE AIRCRAFT TOWING THE BAR SHEAR PIN WAS BROKEN AND THE NOSE LANDING GEAR EXCEEDED ITS TOW ANGLE. THE AIRCRAFT WAS SENT TO THE HANGAR AND IT WAS ACCOMPLISHED AN INSPECTION TO VERIFIED THE NOSE LANDING GEAR IAW M/M 05-51-09, NO DAMAGES WERE FOUND AND TSDR ASMF200512005Starter · damagedAIRCRAFT RETURNED TO PLATFORM, DURING TAXING THE RT ENGINE WAS REJECTED WITH N1 FALLING AND EGT INCREASING. THE RT STARTER AND VALVE WERE REPLACED IAW MM 80-11-01 AND MM 80-11-02 RESPECTIVELY, TESTED CORRECT.SDR ASMF200510010Igniter Box · failedCAPTAIN REPORTED THAT DURING RIGHT ENGINE START WITH IGNITION SELECTOR IN POSITION ONE, THE RIGHT ENGINE EGT DID NOT INCREASE. AIRCRAFT WAS SENT TO THE HANGAR AND DURING MAINTENANCE REVISION WAS DETECTED THE CABLE OF THE SYSTEM TWO DAMAGED. THE EXCITER IGNITSDR ASMF200507006Combust Chamber · damagedDURING LT ENGINE BOROSCOPIC INSPECTION, DETECTED COMBUSTION CHAMBER DAMAGED WITH 2 AXIAL CRACKS INTERSECTED WITH CIRCUMFERENTIAL CRACK OUT LIMITS. LT ENGINE REPLACED AND TESTED IAW MM 71-00-02 AND MM 71-00-00, RESPECTIVELY. ALL CORRECT.SDR ASMF200506006Bleed Valve · failedCAPTAIN REPORTED THAT DURING TAKEOFF, THE LT ENGINE EGT REACHED 647 DEGREE C. AIRCRAFT WAS SENT TO THE HANGAR AND LT ENGINE 2.5 BLEED ACTUATOR WAS REPLACED IAW MM 75-32-01 AND TESTS WERE PERFORMED IAW MM 71-00-00, ALL CORRECT. DURING OVERNIGHT SERVICE, THE LT SDR ASMF200505010Idg · failedCAPTAIN REPORTED RIGHT IDG WAS DEACTIVATED AND LEFT IDG WITH HIGH TEMPERATURE. THE RIGHT IDG WAS REPLACED IAW MM 24-11-01, TESTED CORRECT. THE LEFT IDG HIGH TEMPERATURE REPORT WAS VERIFIED AND DETECTING LEAK IN DRAIN SEAL. THE LEFT IDG REPORT WAS DEFERRED ISDR ASMF200505002Engine · failedAIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF DURING CLIMB AT 15000 FT THE RIGHT ENGINE OIL TEMPERATURE REACHED 177°C AND INCREASED IN IDLE TO 207°C, SHUTTING DOWN THE ENGINE PER OIL T RED MESSAGE AND RETURNING TO MEX. ENGINE GRAPHICS WERE CHECKED DETERMINISDR ASMF200502010Engine · lack of lubeDURING ENGINES STARTING, RT ENGINE DID NOT STABILIZED AND WAS SHUTDOWN. OIL QTY CHECKED & REFILLED TO THE CORRECT LEVEL. RT ENGINE RESTARTED & ACFT DISPATCHED BUT IT RETURNED TO PLATFORM DUE TO DURING TAXING OIL TEMP INDICATION 177 DEGREES. ACFT SENT TO HASDR ASMF200501016Fuel Control · malfunctionedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXING AND AFTER RIGHT ENGINE STARTING AUTO-SHUTDOWN WITHOUT ANY APPARENT CAUSE. CAPTAIN PERFORMED CLEANING PROCEDURE FOR ENGINE REVISION. ENTRANCE, EXHAUST AND MASTER CHIP DETECTOR OF RIGHT ENGINE WERSDR ASMF200407005Pump · failedDURING TRANSIT CHECK, CAPTAIN REPORTED HIGH TEMPERATURE ON ENGINE NR 2 REACHED 648 DEGREES (F) DURING TAKE OFF. THE MAXIMUM TEMPERATURE IAW MM 71-00-01 IS 645 DEGREES (F), SO AIRCRAFT WAS SENT TO THE HANGAR AND RT ENGINE FUEL PUMP AND PURGE VALVE WERE REPLACEDSDR ASMF20040603Static Wick · lightning strikeDURING DESCENT, A LIGHTING STRIKE AT RANDOM AND (WXR WEAK) LIGHT TURNED ON DURING WXR OPERATION. LIGHTING STRIKE VISUAL INSPECTION WAS PERFORMED IAW MM 05-51-09 AND NO DAMAGES WERE FOUND. THE LIGHTING STRIKE WAS DISCHARGED IN 3 STATIC DISCHARGERS, ONE IN LT ASDR MEX2004008Warning Light · illuminatedAIRCRAFT RETURNED TO PLATFORM DURING TAXING (ELEV FEEL AND RUDDER RATIO) EICAS MESSAGES APPEARS. THERE WAS BITE TEST PERFORMED IAW 27-31-00 AND BOTH CHANNELS WORKED CORRECT.SDR MEX2003444Adc · failedFLT 928 - MEX-MTY - AIRCRAFT RETURNED TO PLATFORM, DURING TAXI AFTER ENGINE STARTING EICAS OVERSPEED MESSAGE WENT ON. DURING REVISION CADC NR 2 WAS ALARMED, SO IT WAS REPLACED IAW MM 34-12-01, ALL TESTS CORRECT. (M)SDR MEX2003407Engine · malfunctionedAIRCRAFT RETURN TO PLATFORM DURING ENGINES STARTING, THEY DID NOT STABILIZE IN LOW RPM AND THEY WERE SHUT DOWN. DURING REVISION NO ERROR EICAS MESSAGES WERE DETECTED AND PNEUMATIC PRESSURE OF APU WAS CORRECT. BOTH ENGINES WERE STARTED IAW MM, ALL TESTS CORRESDR MEX2003303Control Panel · brokenAIRCRAFT RETURNED TO PLATFORM DUE TO CAPTAIN REPORT THAT DURING LANDING ALTIMETER SELECTION WAS STUCK AT 3200 AND ALTITUDE SELECT WAS BROKEN. REPORT WAS DEFFERED IAW MEL DURING TRANSIT CHECK, PANEL SELECTOR CABIN PRESSURE WAS REPLACED IAW 21-31-01, ALL TESTSSDR MEX2003276Regulator · failedAIRCRAFT AIR TURN BACK DUE TO (RT ENGINE BLEED OFF) AND (RT PACK OFF) MESSAGES AT 310 FT, LOOSING CABIN PRESSURE AND APPEARING MESSAGE OF CABIN ALTITUDE WITH AUDIBLE ALARM. AIRCRAFT WAS SENT TO THE HANGAR. PILOT PRESSURE REGULATOR AND TEMPERATURE SENSOR OFSDR MEX2003088Apu · failedMEX-ORD - AIRCRAFT RETURNED TO PLATFORM DUE TO AIRCRAFT POWER UNIT FAILED WITHOUT APPARENT CAUSE. PERFORMED BITE PROCEDURE IAW FIM 49-11-00. (M)
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