N639MM
Service difficulty reports · 16
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 = 'N639MM' 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 = 'N639MM' 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 AC2A2023062213901Actuator · unserviceableROTOR BRAKE FAIL CAS ILLUMINATED ON SHUT DOWN WITH CALIPER INDICATING DOWN POSITION. REPLACED ROTOR BRAKE ACTUATOR.SDR AC2A2022103013901Tail Boom · unserviceableTAIL STRUCTURE HAS AREA OF DELAMINATION ON R/H SIDE.SDR AC2A2022031713901Plate · corrodedCORROSION DAMAGE CAUSING REPLACEMENT OF AFT RIGHT UPPER PLATE.SDR AC2A2022010913901Bleed Valve · crackedDURING TROUBLESHOOTING OF LOW POWER ON #1 ENGINE, #2 ENGINE BLEED VALVE WAS REMOVED TO SWAP WITH #1 ENGINE BLEED VALVE AND FOUND #2 BLEED VALVE SEALING DISC WAS CRACKED. BLEED VALVE WAS REPLACED.SDR AC2A2021082313901Actuator · faulted1 R AP FAIL CAS LIGHT ILLUMINATED DURING CHECK. REPLACED NO 1 ROLL ACTUATOR AND PERFORMED FUNCTIONAL CHECK.SDR AC2A2021081813901Chip Detector · damagedMGB L/H SUMP CHIP DETECTOR RETAINING GROOVES WORN BEYOND ACCEPTABLE PUBLISHED MANUFACTURE LIMITS AS RECEIVED FROM OVERHAUL CONDITION.SDR AC2A2020020713901Chip Detector · unbondedTHE INTERMEDIATE GEARBOX (IGB) CHIP DETECTOR HAS ROTATIONAL MOVEMENT AT THE PIN FOLLOWER RETAINING RING COLLAR.SDR AC2A2020050113919Filter · crackedIBF MAINTENANCE INDICATOR FOUND CRACKED. *SUPPLEMENTAL INFORMATION* PART NUMBER ENTERED ON ORIGINAL SDR IN SECTION 5 WAS IN ERROR. PART NUMBER WAS SUBMITTED AS 104440-201 AND SHOULD HAVE BEEN 104441-201. *SUPPLEMENTAL INFORMATION* THE UNIQUE CONTROL CODE WAS ASDR AC2R2018112901Handle · vibrationCOCKPIT DOOR OPENED IN FLIGHT. LANDED AT GC205 (NEAREST CHEVRON PLATFORM. AFTER LANDING, CREW INSPECTED AND SECURED DOOR. DETERMINED CAUSE OF DOOR OPENING WAS VIBRATION OF THE DOOR HANDLE.SDR AC2A2020050113909Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR AC2A2020050113908Filter · crackedIBF MAINTENANCE AID FOUND TO BE CRACKED.SDR AC2R2018040201Fan · overheatedPRIOR TO CRUISE CLEARANCE, PILOTS NOTICED A STRONG ELECTRICAL OVERHEAT ODOR WITH A SIMULTANEOUS FWD FAN CAS MESSAGE. NO SMOKE OR FLAMES WERE NOTED. CREW COMPLIED WITH QRH. REPLACED THE PILOT'S COCKPIT FAN.SDR AC2R2017073102Blade · crackedTAIL ROTOR BLADE CRACK AT INBOARD ROOT NEAR EROSION SHIELD.SDR AC2R2017073101Blade · crackedTAIL ROTOR BLADE CRACK AT INBOARD ROOT NEAR EROSION SHIELD.SDR AC2R2018042004Oil Cooler · vibrationOIL COOLER FAN HIGH VIBRATION READINGS.SDR AC2A201309170001Torque Sensor · damagedENGINE TORQUE MISCOMPARE CAS MESSAGE ILLUMINATED DURING GROUND RUN. FOUND TORQUE SENSORS DAMAGED FROM CONTACT WITH ROTATING COMPONENT.
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