N330PH
Service difficulty reports not matched to an aircraft · 18
They name N330PH, 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 = 'N330PH' 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 = 'N330PH' 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 A6WA200100049Outflow Valve · stuck**CLOSED**CABIN WILL NOT PRESSURIZE, CAN SEE DAYLIGHT THRU DOOR AT UPPER LEFT HAND CORNER. MAINTENANCE REMOVED AND REPLACED REAR OUTFLOW VALVE.SDR A6WA200100028Gearbox · defectiveDESCENT OUT OF FL240, LT ENGINE SURGED FROM 0 PERCENT TO 30 PERCENT TORQUE AND LT PROP IMMEDIATELY WENT TO 103 PERCENT NP. FLEW FOR 4 MINUTES WITH ENGINE AT FLT IDLE AND NP AT 103 PERCENT. ENGINE SURGED 2ND TIME CAUSING ACFT TO YAW. ELECTED TO SHUTDOWN ENGISDR A6WA9900124Stick Shaker · failedFLT 7127 - DEN-BIS - AOA FAIL/STICK PUSHER FAIL ON TAKEOFF ROLL. MESSAGES WENT AWAY AFTER 30 SECONDS. RESET STICK PUSHER SYSTEM. OPS CHECKS GOOD. (M)SDR A6WA9900007Air Distribution · smokeDEN - FLT 7131 - CABIN FILLED WITH SMOKE AT ENGINE SHUT-DOWN. INSPECTED PACKS, FOUND NO DISCREPANCIES. GROUND RAN AIRCRAFT 15 MINUTES, COULD NOT DUPLICATE. NO CAS MESSAGE, SYSTEM OPS CHECK NORMAL. (X)SDR M8XA9800014Dau · defectiveSHORTLY AFTER TAKEOFF, THE FLIGHT CREW REPORTED A PROBLEM WITH THE NR 1 ALTERNATOR. THEY WERE ALERTED BY AC VOLT FAIL MESSAGE ON THE EICAS SCREEN. AIRCRAFT RETURNED TO DEN, LANDED WITHOUT FURTHER INCIDENT. DENVER MAINTENANCE REPLACED THE NR 1 DAU IAW AMM 31SDR M8XA9800005Seal · failedDURING CLIMBOUT, THE CREW REPORTED A PROBLEM WITH AIR LEAKING AROUND THE DOCUMENT DOOR. CREW THEN ELECTED TO RETURN TO DEN. AIRCRAFT LANDED IN DEN WITH NO FURTHER INCIDENT. MAINTENANCE INSPECTED THE DOCUMENT DOOR AND FOUND NO DISCREPANCIES. ALSO, CONDUCTEDSDR QXEA9700220Pseu · malfunctionAFTER TAKEOFF ON CLIMBOUT, THE LANDING GEAR LEVER WILL NOT SELECT UP. LEVER MOVED TO THE UP POSITION WHEN THE DOWNLOCK RELEASE BUTTON WAS DEPRESSED. REPLACED THE PROXIMITY SWITCH ELECTRONIC UNIT, OPERATIONAL CHECKS GOOD.SDR QXEA9700171Fan · failedSEA- ACRID SMELL IN COCKPIT AND CABIN. ISOLATED TO AFT AVIONICS FAN, PLACED ON MEL, REF 21-6. AIRCRAFT RETURNED TO SERVICE. MEL CLEARED BY REPLACING REAR AVIONICS FAN AND RECIRIC FILTER, OPERATIONAL CHECKS GOOD.SDR QXEA9700147Connector · dirtyDURING TEST OF THE FIRE EXTINGUISHING SYSTEM, THE NR 1 LT SQUIB LIGHT WAS INOP. CLEANED THE SQUIB CANNON PLUG CONNECTION ON THE NR 1 FIRE BOTTLE IN THE ENGINE COMPARTMENT, OPERATIONAL CHECKS GOOD.SDR QXEA9600282Sensor · malfunctioningLEFT REAR EMERGENCY EXIT DOOR WARNING CAS MESSAGE INFLIGHT AT 17,000 FT. LIGHT WENT OUT AT 4.50 CABIN PSID. PROXIMITY SENSOR REPLACED AND ADJUSTED IAW MAINT MANUAL, WARNING SYSTEM OPS CHECKED GOOD.SDR QXEA9600280Sensor · req. adjustmentDOOR WARNING CAS MESSAGE IN FLIGHT, SYSTEM INDICATED LEFT REAR UNDERWING EXIT. NO AIR LEAKS OR SOUND COMING FROM EXIT, NO LOSS OF CABIN PRESSURE. AIRCRAFT ALTITUDE WAS 14,000 FT, LIGHT EXTINGUISHED AT 5,000 FT. EXIT PROXIMITY SENSOR ADJUSTED IAW MAINT MANUASDR QXEA9600278Sensor · out of adjustINTERMITTENT DOOR WARNING CAS MESSAGE AFTER TAKEOFF, LEFT SIDE UNDER WING EMERGENCY EXIT. EMERGENCY EXIT PROXIMITY SENSOR ADJUSTED IAW MAINT MANUAL, DOOR INDICATION OPS CHECKED GOOD.SDR QXEA9600275Rib · crackLEFT WING LEADING EDGE SECTION 511AL .5 INCH CRACK NOTED IN OUTBOARD RIB UPPER FLANGE AT THE LAST FASTENER LOCATION. CRACK FOUND DURING C-CHECK. CRACK STOP DRILLED AND DOUBLER INSTALLED PER EA 7-57-49.SDR QXEA9600234Np Probe · malfunctioningNR 1 ENGINE BEGAN SURGING 20 TO 80 PERCENT ON APPROCH TO SEA. ALL ENGINE INSTRUMENTS INDICATED THE SURGING ALONG WITH AIRCRAFT YAW. NR 1 ENGINE BROUGHT TO IDLE AND PROP WAS FEATHERED. AIRCRAFT LANDED IN SEA WITHOUT FURTHER PROBLEM. NR 1 NP PROBE REPLACED ASDR QXEA9600059Pwr Supply · inoperativePDX - AFT EXIT SIGN INOP 9 AND 10, FLOOR PROXIMITY LIGHTS INOP AFT RIGHT HAND EXIT LIGHT INOP. BATTERY AND POWER SUPPLY 7LK REPLACED. DAMAGED PIN FOUND ON REMOVED UNIT AND AIRCRAFT CONNECTOR. LIGHTS OPS CHECKED GOOD AND AIRCRAFT RETURNED TO SERVICE.SDR QXEA9600015Battery Pack · dischargedPDX - EXIT SIGN ABOVE SEAT 11A AND RIGHT SIDE AFT EXTERIOR INOP. REPLACED AND LIGHT OPS CHECKED GOOD.SDR QXEA9500417Battery · dischargedPDX - GALLEY DOOR EXTERIOR EMERGENCY LIGHT IS INOP. BATTERY PACK REPLACED AND LIGHT OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.SDR QXEA9600069Trim Actuators · malfunctioningPDX - AT FL 260 ON DESCENT, MESSAGE ELEVATOR MISTRIM NOSE ON. AFTER AUTOPILOT DISCONNECT THE ELEVATOR TRIM WOULD NOT FUNCTION, THE TRIM WAS STUCK. FLIGHT CREW SELECTED STANDBY TRIM, BUT TRIM DIDN'T FUNCTION WITH CONTINUED FORWARD PRESSURE TO MAINTAIN FLIGHT
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