C F E CFE-738-1-1B
Service difficulty reports · 158
Newest first. General aviation reporting is voluntary.
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 engine_model_key = 'CFE73811B' 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 engine_model_key = 'CFE73811B' 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 20000509SH001Rotor · misalignedIT WAS FOUND THAT THE SEAL ROTOR, PN 3120524-2, WAS INSTALLED BACKWARDS. (X)SDR 20000509SH002Pump · misinstalledIT WAS FOUND THAT THE SEAL ROTOR, PN 3120524-2,WAS INSTALLED BACKWARDS. (X)SDR 20000517SH001Sensor · looseFLIGHT CREW REPORTED ENCOUNTERING COMPRESSOR STALLS AND AIRCRAFT YAW TO LEFT CLIMBING THROUGH FL 230. LEFT ENGINE CONTROLS MOVED TO FLIGHT IDLE AND SHUT DOWN LT ENGINE. FLIGHT DIVERTED TO LIT DASSAULT SERVICE CENTER. INVESTIGATION REVEALED T2 SENSOR CONNECTSDR 97ZZZX4256Harness · chafedFADEC WIRING HARNESS CHAFED WHERE IT PASSES THROUGH CLAMP. SUBMITTER STATED CLAMP NEEDS CUSHION TO PREVENT WIRE FROM BEING DAMAGED.SDR 97ZZZX2681Inlet · bolts looseAFTER ENGINE FAILURE, MORE THAN HALF THE BOLTS SECURING THE ENGINE INLET HA D UNSCREWED THEMSELVES. THE REMAINING WERE LOOSE. SUBMITTER SUSPECTS UNUSUAL ENGINE VIBRATION CAUSED THE BOLTS TO BACK OUT. THE INLET COULD POSSIBLY FALL OFF THE AIRCRAFT IN-FLIGHT.SDR 97ZZZX2682Engine · failedRIGHT ENGINE COMPLETELY FAILED AFTER TAKEOFF AT APPROXIMATELY 200 FEET AGL. AFTER A SUCCESSFUL LANDING, ENGINE WAS EXAMINED AND FOUND THE FAN SEIZED; THE TURBINE BADLY DAMAGED. NO EVIDENCE OF FOD WAS FOUND. AWAITING EVALUATION FROM THE MANUFACTURER TO DETERSDR 97ZZZX2485Line · crackedMAINTENANCE PERSONNEL NOTICED FUEL ON BOTTOM OF ENGINE COWL. FURTHER INVESTIGATION REVEALED A CRACKED WELD IN THE MAIN FUEL SUPPLY LINE WHERE THE FUEL PRESSURE SENDER IS LOCATED. LOCATION OF THE SENDER MAY IMPOSE UNDUE STRESS ON THE WELD.SDR JZBR14001Hmu · malfunctionINSTALLED HMU ON ENG FOR TEST AFTER C/W CFE 7388001. PERFORMED 2 NORMAL STARTS SATISFACTORILY. THE 3RD START ATTEMPT AND SUBSEQUENT ATTEMPTS FAILED. RE-INSTALLED ORIG HMU AND STARTS WERE NORMAL.
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