N72649, cancelled Jan 4, 2012
Service difficulty reports · 17
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 = 'N72649' AND deregistration_id = 'N72649-2012-01-04' 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 = 'N72649' AND deregistration_id = 'N72649-2012-01-04' 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 AC2R64905232011Thermostat · malfunctionedPILOTS NOTICED NR 1 ENGINE OIL TEMP GAUGE ABOVE 110+. NO OTHER INDICATIONS WERE OBSERVED AT THIS TIME. REDUCED NR1 ENGINE TO FLIGHT IDLE AND INFORMED PAX OF SITUATION AND RETURNED TO BASE. REPLACED NR 1 ENGINE OIL THERMOSTAT.SDR AC2A649010711Gearbox · making metalON OUR INBOUND LEG ABOUT 10 MINS OUT OF LANDING, TRANSMISSION CHIP LIGHT ILLUMINATED. FOLLOWING THE EMERGENCY CHECKLIST, SLOWED DOWN AND PULLED THE MGB CHIP DET CB, RESET IT AND THE LIGHT STAYED ON. THERE WAS NO RISE OR FALL IN OIL PRESSURE. LANDED AS SOON AS SDR AC2A2009031781075Indicator · malfunctionedAFTER TAKEOFF, PLACED LANDING GEAR CONTROL LEVER UP, THE 3 GREEN LIGHTS EXTINGUISHED, BUT THE RED UNSAFE LIGHT REMAINED ON. WHILE THE ACFT WAS BEING SLOWED, IAW THE EMERGENCY PROCEDURES CHECKLIST.SDR AC2A116707Seat Back · crackedSEAT BACK FRAME CRACKED.SDR AC2A116734Bearing · roughGYRO REMOVED FOR ROUGH BEARINGS AND LOUD NOISE.SDR AC2A110829Starter Gen · malfunctionedNR 2 STARTER GENERATOR LIGHT COME ON IN FLIGHT. FOLLOWED EMERGENCY CHECK LIST. WHEN COMPLETING THE CHECKLIST THE NR 2 OIL PRESSURE GAGE WENT TO ZERO. NOTED THAT NO WARNING LIGHT WAS ON FOR THE NR 2 OIL PRESSURE SYSTEM. MAINTAINED A WATCH ON THE TEMPERATURE ASDR AC2A109592Hose · failedNR 2 SERVO SYSTEM CAUTION LIGHT ILLUMINATED APPX. 15 MINUTES INTO THE FIRST FLIGHT OF THE DAY, ACCOMPANIED BY NR 2 HYDRAULIC PRESSURE FLUCTUATING 2000 AND 3000 PSI. EMERGENCY PROCEDURE WAS COMPLETED PER THE EP CHECKLIST. ENROUTE TO LEEVILLE WITH SYSTEM NR 2 SSDR AC2A0000096Rod End · crackedWHILE PERFORMING THE REQUIREMENTS OF ASB 76-32-26, CORROSION INSPECTION OF THE THREADED JOINT, FOUND BEARING CRACKED. REPLACED POSITIONING ROD END. (X)SDR AC2A0000066Hose · bindingWHILE INSPECTING M/R DAMPERS, THE BLACK DAMPER HOSE WAS FOUND BINDING WHEN THE DAMPER WAS ROTATED. THE INBOARD FERREL WAS ALSO FOUND TURNING WHEN HOSE WAS ROTATED. REPLACED HOSE, THE BAD NOSE WAS FOUND TO BE .50 INCH SOFTER THAN THE NEW HOSE. (X)SDR AC2A0000013Brushes · wornPART IS PITTED, BRUSHES REPLACED. (X)SDR 20000622SH037Potentiometer · failedFEEDBACK POTENTIOMETER PREMATURE FAILURE, CAUSES ACTUATOR TO KICK IN-FLIGHT. (X)SDR 99ZZZX4405Potentiometer · failedSUBMITTER STATED POTS WEAR OUT LONG BEFORE THE OVERHAUL OF 3,000.00 HOURS. FEEDBACK POT PREMATURE FAILURE, SHOULD LAST UNTIL OVERHAUL TIME OF 3,000 HOURS. CAUSED ACTUATOR TO KICK IN-FLIGHT. COMPONENT P/N 7690001802106.SDR AC2A0000009Blade · delaminatedSKIN DELAMINATED ON TOP FROM STA 32 EXTENDING OUT TO STA 105, 6 INCHES BACK FROM LEADING EDGE ABOUT 5 INCHES. (X)SDR 97ZZZX5216Coupling · crackedCOUPLING WAS FOUND CRACKED IN 7 PLACES. IT WAS LOCATED AT THE INTERMEDIATE GEARBOX OUTPUT FLANGE. THE PREVIOUS COUPLING WAS ALSO CRACKED. THE RUN-OUT WAS CHECKED AND FOUND WITHIN MANUFACTURER'S LIMITS. THE NR 5 T/R DRIVESHAFT AND INTERMEDIATE GEARBOX WERESDR 97ZZZX3457Lens · splitBRAND NEW PART OUT OF STOCK, SPLIT ALONG GLUE LINE. LENS HALVES NOT BONDED TOGETHER PROPERLY. THIS WAS TO REPLACE THE LENS INSTALLED THAT WAS REMOVED FOR THE SAME REASON.SDR 97ZZZX3459Blade · disbondTWO AREAS OF DISBOND ON MAIN ROTOR BLADE. (TOP SURFACE STARTS AT BLADE STA 232 AND EXTENDS SPANWISE APPROXIMATELY 4 INCHES ALONG LEADING EDGE STRIP, EXTENDING AFT APPROXIMATELY 4 INCHES CHORDWISE). LOWER SURFACE STARTING AT BLADE STA 237, APPROXIMATELY EXTENSDR 97ZZZX3458Lens · splitSTROBE LIGHT LENS SPLIT IN HALF, GLUE DOES NOT HOLD HALVES TOGETHER ALONG BOND LINE.
Back to N72649, cancelled Jan 4, 2012