Honeywell TFE731-50R
Service difficulty reports · 22
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 = 'TFE73150R' 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 = 'TFE73150R' 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 2025FA0000730Hydraulic System · low pressure#1 AND #2 HYDRAULIC LOW PRESSURE LIGHT ON. HYDRAULIC @ 2300PSI. PERFORMED GEAR FREE LANDING PROCEDURE.SDR EXFA2025FA0000730Warning Message · false activationUPON REDUCING POWER FOR DESCENT FLIGHT CREW NOTICED HYDRAULIC LOW PRESSURE LIGHTS ON. COULD NOT DUPLICATE ON THE GROUND.SDR 2025FA0000728Hydraulic Line · leakingHYDRAULIC LOW PRESSURE LIGHTS #1 AND #2 FLIGHT LIGHTS IN HYDRAULIC PRESSURE INDICATOR READ 2300 PSI. CREW PERFORMED FREEFALLING LANDING GEAR PROCEDURE.SDR EXFA2025120800728Pipe · crackedWHILE IN CRUISE FLIGHT, CREW NOTED HYDRAULIC LOW PRESSURE LIGHTS ON, ENGINES 1 AND 2 WITH A HYDRAULIC PRESSURE OF 2300 PSI. CREW DIVERTED TO AN ALTERNATE AIRPORT EXTENDING LANDING GEAR MANUALLY PRIOR TO LANDING.SDR 2025FA0000729Instrument Panel · faultedSTANDBY INSTRUMENT INOPSDR DBCA202212200010Fuel Nozzle · failedPRIOR TO POWER APPLICATION ON TAKEOFF THE NR 2 ENGINE ROLLED BACK. CREW EXITED THE RUNWAY AND RETURNED TO RAMP. MTN REMOVED AND INSPECTED ENGINE. FOUND FUEL NOZZLES UNSERVICEABLE.SDR 2022FA0000521Compressor Blade · failedAIRCRAFT DEPARTED KHLN JULY 31 2022 AROUND 9:55 AM MDT CLIMBING THROUGH 25,000FT PILOT REPORTED LOUD BANG FROM #2 ENGINE AND THEN THE ENGINE ROLLED BACK AND SHUTDOWN. THEY THEN TURNED BACK AROUND AND LANDED AT KHLN.SDR 3SRA20220110001Fuel Control · inoperativePHYSICAL ROLLBACK OF #1 ENGINE FOLLOWED BY THE AMBER #1 ENGINE COMPUTER LIGHT ILLUMINATING. ENGINE CONTINUED TO OPERATE IN MANUAL MODE. AIRCRAFT RETURNED TO KSUSSDR E0YA2021072100003Unknown · odorCLIMBING AT FL300 AND HEARD A LOUD BANG, FOLLOWED BY A BURNING SMELL AND VIBRATION. DIVERTED TO NEAREST AIRPORTSDR 9JLA2020110929419Wire Harness · defectiveTHE FLIGHT CREW REPORTED THAT THE NR 1 ENGINE N2 INDICATIONS WERE ERRATIC IN FLIGHT. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THAT THE NR 1 ENGINE HARNESS WAS DEFECTIVE. THE MX VENDOR REPLACED THE WIRING HARNESS WITH A NEW HARNESS. OPERATIONS CHECKSDR MDGA202012045254Warning Message · false activationON ROLL OUT THE AIRCRAFT SHOWED THAT THE OIL PRESSURE WAS LOW THE PILOT ABORTED AND RETURNED TO THE RAMP. UPON FURTHER INVESTIGATION THE CREW DETERMINED THAT AFTER AN ENGINE RUN ON THE RAMP THAT THE OIL PRESSURE WAS READING WITH I LIMITS AND CONTINUED THE TRIPSDR 9PMA20191114001Landing Gear · malfunctionedAIRCRAFT COMPLETED ROTATION AND AFTER APPROXIMATELY 3-4 SECONDS GEAR SELECTED UP BUT GEAR DID NOT CYCLE. CREW CHECKED GEAR INDICATION ALL GREEN CIRCLED PATTERN AND PREFORMED NORMAL LANDING . INSPECTED GEAR AND CONSULTED TECH OPS TEXTRON AVIATION . DEPARTED 2NDSDR 3FPY201810078003Stator Vane · damagedDURING ROUTINE ENGINE INSPECTIONS, THE LT ENGINE FAN STATOR VANES - LEADING EDGE SCREENS WERE FOUND DAMAGED - QTY 13 NEW VANE FAN STATORS INSTALLED.SDR ZESA10280724001Sensor · faultyAIRCRAFT LEFT KLBE WITH NORMAL TAKE OFF AND CLIMB, AT CRUISE THE ENGINE WENT INTO MANUAL MODE, CHECK LIST WERE FOLLOWED AND PILOTS RETURNED TO BLOCK AT KLBE AND LANDED WITHOUT INCIDENT. A DOWNLOAD WAS PERFORMED ON THE DEECS AND THEY WERE SENT TO ENGINE AOG SERSDR XCGA201804160001Fuel Control · failedPILOT REPORTED THAT WHILE DESCENDING THROUGH 24,000 FEET ON APPROACH, THE LEFT ENGINE ROLLED BACK AND FAILED. NO RESTART WAS ATTEMPTED, THE AIRPLANE MADE AN UNEVENTFUL LANDING. MAINTENANCE VISUALLY INSPECTED THE FUEL FILTER, NO CONTAMINATION WAS NOTED. THE FUESDR DXTA2018012100499Transducer · inoperativeDURING CRUISE, THE RIGHT ENGINE N1 ROLLED BACK APPROX 5 TO 7 PERCENT. SIGNIFICANT YAWING WAS NOTICED AS THE ENGINE ROLLED BACK AND THEN RESUMED NORMAL POWER. FELT LIKE WHEN ONE ENGINE COMPUTER GOES OFFLINE AND THEN RESUMES. DEEC DOWNLOADS REVEALED FAULT CODESDR KKVA201611280001Control Module · faultyCREW REPORTS FIRE BAG COMP RED CAS MESSAGE ILLUMINATED IN FLIGHT ON APPROACH 30 MILES OR 10 MINUTES FORM KMDW. SMOKE IN THE BAGGAGE COMPARTMENT WAS VERIFIED BY THE PIC AND AN EMERGENCY WAS DECLARED. UPON INITIAL INSPECTION AND TROUBLESHOOTING BY MAINTENANCE AFSDR DXTA2016092106304Connector · dirtyAT 40,000 FT APPROXIMATELY 200 MILES FROM DESTINATION, -48C IS A+8. RIGHT ENGINE ROLLED BACK 2 TIMES IN APPROXIMATELY 30 SECONDS. FIRST ROLL BACK UNABLE TO RECORD PARAMETERS. SECOND ROLL BACK APPROXIMATELY 97.6 N1, 92.4 N2, CRUISE. ONLY ABLE TO CATCH N1 BESDR DXTA2016071606267Oil System · overservicedWHEN SWITCHING FROM APU BLEED AIR TO MAIN AIR VALVES, AFTER TAKEOFF NOTED STRONG ACRID ODOR COMING FROM AIR CONDITIONING DUCTS. WHEN TAXING IN, ODOR WOULD INCREASE WHEN CHANGING BLEED AIR SOURCE.
PERFORMED APU AND ENGINE RUN WHILE SWITCHING BLEED AIR SOURCSDR DBCA201512280008Fan · out of balanceENROUTE CREW NOTED A VIBRATION FROM LT ENG. CREW DIVERTED & LANDING WAS UNEVENTFUL. CONTACTED MFG FOR SUPPORT. MFG COMPLETED VIBRATION SURVEY & DETERMINED LT ENG FAN REQUIRED BALANCING. REMOVED FAN BLADES, LUBED DOVETAILS & REINSTALLED. BALANCED FAN. OPESDR DXTA2015012605968Engine · overspeedNR 2 ENGINE OVERSPEED 105.1 N1. FL400, ISA + 4, MACH.75 THROTTLE DID NOT CONTROL ENGINE. OVERSPEED SELECTED ON NR 2 ENGINE COMPUTER. PILOT MANUALLY SHUTDOWN ENGINE. PUNGENT OIL ODOR JUST PRIOR TO ENGINE SHUTDOWN. TROUBLESHOT CAUSE OF NR 2 ENGINE N1 OVERSPEESDR CA120914001Cable · lack of lube(CAN) ON DESCENT, NR 2 ENGINE UNABLE TO RETARD THRUST BELOW 51 PERCENT N1. ACFT WAS DIVERTED, LANDED WITHOUT INCIDENT, NR 2 ENGINE SHUTDOWN USING LP FUEL COCK. RT ENGINE CONTROL TELEFLEX INSPECTION, CHECK AND LUBRICATION CARRIED OUT IAW AMM. ENGINES GROUND R
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