GE CF34-8C1

Service difficulty reports · 1,415

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 = 'CF348C1'
  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.

SDR SIMA200227902Fuel Control · malfunctionedXNA - FLT 3837 - DURING CRUISE FLIGHT CREW REPORTED AN INTERMITTENT CAUTION MESSAGE ON EICAS WITH AN ENGINE ONE ITT SPIKE. CREW DECLARED AN EMERGENCY, REDUCED POWER AND CONTINUED TO XNA AND LANDED WITH NO FURTHER PROBLEMS. MAINTENANCE RESET FADECS, OPERATIONOct 4, 2002 · N501BG · Cndair CL6002C10 · Fuel Control/Turbine EnginesSDR CA020927005Fuel Nozzle · cracked(CAN) FUEL LEAK NOTED AT APU. FOUND CRACKED FUEL NOZZLE. APU INOP'D IAW MEL.FUEL NOZZLE AT 2 O'CLOCK POSITION REPLACED. APU OPERATIONAL.Sep 24, 2002 · Cndair CL6002C10 · APU Engine Fuel and ControlSDR CA020905002Window · cracked(CAN) IN CRUISE, THE COPILOT SIDE WINDOW CRACKED. AIRCRAFT COMPLETED THE FLIGHT AND LANDED TO THE DESTINATION AIRPORT. THE AIRCRAFT WAS THEN FERRIED WHERE THE WINDOW WAS REPLACED. THE AIRCRAFT HAD 663 FH AND 581 FC AT THE TIME OF THE EVENT.Aug 28, 2002 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA020828001Line · cracked(CAN) LOSS OF PRESSURE ON HYDRAULIC SYSTEM NR 2. HYDRAULIC LEAK LOCATED IN AFT EQUIPMENT BAY ONE DP NR 2 PRESSURE LINE TO PRESSURE MANIFOLD. FOUND LINE CRACKED.Aug 22, 2002 · Cndair CL6002C10 · Hydraulic System, MainSDR CA020826001Line · cracked(CAN) DURNING FLIGHT, PILOT REPORTED A HYD. SYSTEM NR 1 FAILURE. FLUID AND PRESSURE WENT TO ZERO. AFTER FURTHER INVESTIGATION IT WAS DISCOVERED THAT THE PRESSURE LINE FROM THE EDP WAS THE CAUSE OF THE LOSS OF FLUID. A/C TAT IS 2,110.6 AND TAC IS 1,809.HYAug 19, 2002 · Cndair CL6002C10 · Hydraulic System, MainSDR CA020822001Nozzle · cracked(CAN) DURING ROUTINE MAINTENANCE, APU WOULD NOT START. APU BAY DOORS OPENED AND FUEL LEAK NOTED. FOUND THE FUEL NOZZLE AT THE 6 O'CLOCK POSITION CRACKED. APU INOPERATIVE IAW MEL 49-10-01, AND FUEL NOZZLE ORDERED. FUEL NOZZLE REPLACED AND AIRCRAFT RETURNED INAug 17, 2002 · Cndair CL6002C10 · APU Engine Fuel and ControlSDR CA020819003Window · cracked(CAN) IN FLIGHT, THE RT SIDE WINDOW CRACKED. WINDOW WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.Jul 31, 2002 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA020819004Window · cracked(CAN) IN FLIGHT, THE RT SIDE WINDOW CRACKED. WINDOW WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.Jul 25, 2002 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA020731001Fuel Nozzle · cracked(CAN) THE INITIAL PROBLEM REPORTED WAS THAT, WITH APU BLEED ON & BOTH PACKS OPERATING, DUCT PRESSURE WOULD DROP TO APPROX 20 PSI & APU BLEED CAUTION MESSAGE WAS POSTED. APU RPM ALSO DROPPED AND, DURING ENGINE START, APU GEN DROPPED OFF LINE. 1ST ACTION TAKEN Jul 24, 2002 · Cndair CL6002C10 · APU Engine Fuel and ControlSDR CA020731004Control Panel · failed(CAN) DURING TRANSIT REFUELLING, SMOKE NOTICED FROM FLIGHT DECK REFUEL/DEFUEL PANEL. MAINTENANCE PERSONNEL WERE SENT AND THE PANEL WAS REPLACED.Jul 24, 2002 · Cndair CL6002C10 · Aircraft Fuel SystemSDR CA020715004Control Panel · failed(CAN) WHILE REFUELING USING THE COCKPIT REFUEL / DEFUEL PANEL, THE PANEL FAILED AND WAS FOLLOWED BY A STRONG ELECTRICAL SMELL. AIRPLANE DEPOWERED.COCKPIT REFUEL/DEFUEL PANEL REPLACED. AIRCRAFT RETURNED IN SERVICE.Jul 8, 2002 · Cndair CL6002C10 · Aircraft Fuel SystemSDR CA020620002Windshield · cracked(CAN) CREW REPORTED THAT PILOT'S WINDSHIELD CRACKED IN FLIGHT.THE AIRCRAFT WAS ENROUTE AND TURNED BACK TO LAND. MAINT REPLACED THE WINDSHIELD PER AMM.Jun 5, 2002 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA020823001Control Unit · failed(CAN) LT INBOARD GROUND SPOILER DEPLOYED WHILE CLIMBING THROUGH 29,000 FT. CLIMB DECREASED AND BUFFET NOTICED. LT INBOARD GROUND SPOILER SHOWED DEPLOYED AND LT OUTBOARD GROUND SPOILER SHOWED AMBER. MESSAGE CLEARED SHORTLY. MAINTENANCE REMOVED AND REPLACEDMay 19, 2002 · Cndair CL6002C10 · Drag Control ActuatorSDR QXEA0300120Turbine Blades · damagedPDX - NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO HPT 1 BLADES 2/3 MISSING. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GEJan 24, 2002 · N609QX · Cndair CL6002C10 · Turbine SectionSDR CA021208001Control Panel · shorted(CAN) BURNING ODOR FROM COCKPIT REFUEL/DEFUEL PANEL. REFUEL/DEFUEL CONTROL PANEL REPLACED.Dec 27, 2001 · Cndair CL6002C10 · Aircraft Fuel Distribution System
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