GE CF-34-1A

Service difficulty reports · 115

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 = 'CF341A'
  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 CA980512019Potentiometer · out of adjust(CAN) CREW SELECTED 20 FLAPS THEN THE FLAPS FAILED, LIGHT CAME ON. AIRCRAFT LANDED WITH 20 DEGREE FLAP. MAINTENANCE ADJUSTED FLAP ELECTRONIC CONTROL UNIT POTENTIOMENTERS NUMBERS 5 TO 8. PART TC: 6,891.Apr 15, 1998 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA980331013Current Limiter · failed(CAN) FOLLOWING INCIDENT ON ANOTHER AIRCRAFT VISUAL INSPECTION OF CURRENT LIMITER TO BUS BAR FOUND THAT THE ALUMINUM WASHERS UNDER THE HEAD OF THE BOLT WERE STARTING TO BURN AWAY. CANADAIR INFORMED. IPC WILL BE UPDATED AND OPERATORS WILL BE INFORMED OF DIFFIMar 27, 1998 · Cndair CL6002A12 · DC Power Distribution SystemSDR CA980318040Current Limiter · burned(CAN) DURING APU START A FLASHING WAS NOTED IN JB4. INVESTIGATION FOUND END OF CURRENT LIMITER F1KD OF 500 AMPS HAD BURNT AND MELTED. ALSO SECURING NUT AND BUSS BAR WERE DAMAGED. SECURING BOLT COULD NOT BE REMOVED NORMALLY. SUBMITTER SUGGESTS THAT PROBLEM HAD Mar 16, 1998 · Cndair CL6012A12 · DC Power Distribution SystemSDR CA980318043Ballscrew · broken(CAN) THE RIGHT THRUST REVERSER 4 O''CLOCK BALL SCREW ACTUATOR ANTI-ROTATION TANG FOUND BROKEN.Mar 13, 1998 · Cndair CL6012A12 · Engine Thrust ReverserSDR CA971222010Check Valve · failed(CAN) WITH AIRCRAFT FLAPS AT 20 DEGREES, NR 1 ELECTRIC PUMP NOT ON. MASTER CAUTION ON, AND CONTINUOUSLY COMING ON IF ELECTRIC PUMP NOT SELECTED ON. MAINTENANCE FOUND THAT THE ENGINE PRESSURE CHECK VALVE AND THE ELECTRIC PUMP PRESSUE HYDRAULIC SYSTEM CHECK VADec 18, 1997 · Cndair CL6002A12 · Hydraulic System, MainSDR CA970915002Apu · seized(CAN) WHILE TAXING, APU WAS STARTED AND RAN FOR APPROXIMATELY 15 MINUTES THEN AUTO SHUT DOWN. APU FAULT PANEL INDICATED APU ENGINE LOW OIL PRESSURE. OIL FILTER CONTAMINATED. TURBINE WHEEL VERY HARD TO ROTATE. APU REPLACED.Sep 5, 1997 · Cndair CL6002A12 · APU Core EngineSDR 97ZZZX3408Hose · rupturedTHE MOTIVE FLOW FUEL LINE THAT RUNS FROM THE LEFT WHEELWELL TO THE LEFT PYLON RUPTURED CAUSING FUEL TO VENT OVERBOARD. THE FUEL THAT VENTED OVERBOARD THEN MIGRATED AFT INTO THE TAIL CONE AREA CREATING A POTENTIAL HAZARD.Jul 17, 1997 · N601TX · Cndair CL6002A12 · Engine Fuel DistributionSDR CA970219013Generator · contaminated(CAN) INTEGRATED DRIVE GENERATOR OIL LEVEL FOUND LOW ON DAILY INSPECTION. CHIP DETECTOR PULLED AND FOUND METAL CONTAMINATED.Feb 13, 1997 · Cndair CL6002A12 · AC Generator-AlternatorSDR CA970128006Pneumatic Dr Uni · mis adjusted(CAN) LEFT THRUST REVERSER PDU UNLOCKED, LIGHT REMAINED ON WHEN THRUST REVERSER STOWED. FLEX LOCK FOUND DISENGAGED. INTERNAL TIMING FOUND OUT OF LIMITS. REPLACED PNEUMATIC DRIVE UNIT.Jan 24, 1997 · Cndair CL6012A12 · Engine Thrust ReverserSDR CA961007022Elbow Fitting · cracked(CAN) #3 SYSTEM HYDRAULIC BULKHEAD FITTING REAR OF VERTICAL STABILIZER REAR SPAR, BOTTOM PCV FOUND CRACKED ELBOW FITTING. REPLACED WITH STAINLESS FITTING.Sep 27, 1996 · Cndair CL6002A12 · Hydraulic System, AuxiliarySDR CA960827010Pdu · failed(CAN) PDU WOULD NOT MAINTAIN INITIAL RIGGING AS PER MM 1 1/3 TURNS ON DIRECTIONAL CONTROL VALVE GAP (0.315 +/- 0.015). FAILED RESET OF DIRECTIONAL CONTROL VALVE (SHOP AIR).Aug 25, 1996 · Cndair CL6002A12 · Engine Thrust ReverserSDR CA960826073Generator · failed(CAN) AFTER ENGINE START, GENERATOR ON LINE AND THEN FAILED. IDG (INTEGRATED DRIVE GENERATOR) REPLACED.Aug 13, 1996 · Cndair CL6002A12 · AC Generator-AlternatorSDR CA960620010Idg · oil loss(CAN) OIL LOSS RESULTED IN FAILURE OF CONSTANT SPEED DRIVE PORTION OF INTEGRATED DRIVE GENERATOR.May 27, 1996 · Cndair CL6002A12 · AC Generator-AlternatorSDR CA960304009Pneumatic Drive · failure(CAN) FAILURE OF INTERNAL LOCK MECHANISM OF THE FLEX SHAFT LOCK ON PNEUMATIC DRIVE UNIT. FAILURE OCCURRED DURING THRUST REVERSER STOW CYCLE. THRUST REVERSER ANNUNCIATOR REMAINED ON. FURTHER INVESTIGATION REVEALED THE PDU FLEX SHAFT LOCK FAULTY WITHIN THE UNIT.Feb 8, 1996 · Cndair CL6002A12 · Engine Thrust ReverserSDR CA960214019Flexshaft Lock · not engaging(CAN)FLEXSHAFT LOCK NOT ENGAGING CAM. FOUND UNSECURED AND FAILED ON SHAFT.Feb 5, 1996 · Cndair CL6002A12 · Engine Thrust Reverser
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