GE CF34-3A1

Service difficulty reports · 1,372

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 = 'CF343A1'
  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 SWIA95687Clamp · failedLT 14TH STAGE DUCT WARNING, FOLLOWED BY LT JET PIPE OVERHEAT MESSAGE. REPLACED AFT CLAMP ON LT 14TH STAGE BLEED AIR SHUT-OFF VALVE. RAN LT 14TH STAGE BLEED AIR AND LEAK CHECK GOOD.Nov 29, 1995 · N406SW · Cndair CL6002B19 · Pneumatic Distribution SystemSDR SWIA95686Seal · failedMAIN CABIN DOOR SEAL LEAKS. VERY LOUD SQUEAL AND LOSS OF CABIN PRESSURE. REPLACED CABIN DOOR SEAL WITH A NEW UNIT. OPERATION AND LEAK CHECK GOOD.Nov 28, 1995 · N408SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA95683Windshield · crackedWHILE LEVEL AT FL 350, CAPTAIN'S WINDSHIELD CRACKED, DIVERTED TO RKS. DESCENT AND LANDING WERE UNEVENTFULL. CONTACTED SGU MX CONTROL REMOVED AND REPLACED CAPTAIN'S WINDSHIELD IAW MM 56-11-00 PAGES 401 TO 410. TORQUED ALL BOLTS AND REINSTALLED NEW SEAL.Nov 19, 1995 · N403SW · Cndair CL6002B19 · Flight Compartment WindowsSDR COMA9560587Borescope Plug · brokenLEFT ENGINE N2 VIBRATION WARNING ON EICAS. REMOVED AND REPLACED THE LT ENGINE DUE TO FOD CAUSED BY A DEFECTIVE BORESCOPE PLUG, WHICH SEPERATED AND ENTERED THE ENGINE.Oct 27, 1995 · N946CA · Cndair CL6002B19 · Turbine SectionSDR SWIA95647Fail Message · activatedFLAP FAIL MESSAGE AFTER TAKEOFF. ALSO, FLAP OVERSPEED AURAL WARNING AT 230 KTS. REVIEWED FLAP FAULTS AT FECU AND RESET FECU. OP CK FLAPS, OP CK GOOD.Oct 22, 1995 · N410SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR COMA9560578Uplock · defectiveTHE NOSE LANDING GEAR DID NOT EXTEND, MLG INDICATED DOWN AND LOCKED. REPLACED THE NLG UPLOCK ASSEMBLY.Oct 19, 1995 · N914CA · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA95635Retract Mech · malfunctionedNOSE GEAR FAILED TO RETRACT. REMOVED AND REPLACED TOW BRACKET AND REINSTALLED PROX SENSOR. ADJUSTED SWITCH TO 0.045 TO 0.055 BRACKET IAW MM 32-61-05-400-805.Oct 11, 1995 · N403SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA95626Start Vlv Light · illuminatedRT ENGINE START LIGHT ON AND RT ENGINE START EICAS MESSAGE ON, CLIMBING THROUGH 15,000 FT. PROBLEM INTERMITTENT ON ABOUT 60 PERCENT OF THE TIME. PROBLEM APPEARED THROTTLE SENSITIVE. RETARDING RT THROTTLE, LIGHT GOES OUT AND ADVANCING THROTTLE LIGHT COMES ONSep 14, 1995 · N406SW · Cndair CL6002B19 · Engine Start Valves/ControlsSDR SWIA95600Fecu · malfunctionedFLAP FAIL MESSAGE AT FLAP RETRACTION AFTER TAKEOFF, FLAPS INOP, COMPLETED FLAPS UP LANDING. RESET FECU ON FLAP CON CHAN 1 AND CHAN 2, OPS CKS NORMAL.Jul 15, 1995 · N410SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA95599Contl Mech · malfunctionedFLAPS FAIL MESSAGE, FLAP FAILED AT 18 DEGREES. CONTACTED SGU MAIN CONTROL. DIVERTED TO MSO. RESET FECU CIRCUIT BREAKER FLAPS FAIL MESSAGE, CLEANED FLAPS, OPS CKS NORMAL.Jul 14, 1995 · N410SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA95593De-Ice Tube · failedLT ANTI-ICE DUCT WARNING WING ANTI-ICE SWITCH NORMAL OR STANDBY POSITION. REMOVED LT OUTBD WING LEADING EDGE, REMOVED PICCALO TUBE, INSTALLED LEADING EDGE, IAW MM 57-41-01, GROUND RAN A/C OPS CKS GOOD, SEE F/L 2536.Jun 18, 1995 · N408SW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR SWIA95582Scavenge Line · looseRIGHT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED IN FLIGHT, 16000 FT. PRESSURE FLUCTUATION BETWEEN 27 TO 22 PSI. ALL OTHER INDICATIONS WERE NORMAL. ANTI-ICE WAS SELECTED ON PRIOR TO LOW OIL PRESSURE READ OUT. WHEN PRESSURE WAS STEADY AT 22 PSI, ENGINE WAS SMay 23, 1995 · N403SW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR COM60465Fuel Pump · leakingFUEL LEAKING FROM R/T ENGINE. REPLACED THE ENGINE DRIVEN FUEL PUMP.May 3, 1995 · N917CA · Cndair CL6002B19 · Engine Fuel PumpSDR SWIA95574Tube · crackedANTI-ICE DUCT MESSAGE ON EICAS WITH WING ANTI-ICE SWITCH IN NORMAL AND STANDBY POSITION. COULD NOT CLOSE THE RIGHT FOURTEENTH STAGE VALVE. SWITCH IN CLOSED POSITION DID NOT GIVE CLOSED LIGHT. NO INDICATION ON ANTI-ICE PAGE. REMOVED LEFT LEADING EDGE AND FOMay 2, 1995 · N407SW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR SWIA95573Anti-Ice Duct · splitANTI-ICE DUCT RED EICAS MESSAGE WITH WING ANTI-ICE SELECTED ON. FOUND LEFT WING OUTBOARD DUCT SPLIT AT OUTBOARD END. LEADING EDGE AND DUCT REMOVED. INSTALLED SERVICEABLE ANTI-ICE DUCT IN LEFT OUTBOARD LEADING EDGE. INSTALLED LEADING EDGE IAW MM 51-41-01. OMay 1, 1995 · N406SW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR SWIA95566Bpsu · failedFLAP FAIL CAUTION MESSAGE ILLUMINATED DURING LANDING. FLAPS WERE AT 45 DEGREES. REMOVED AND REPLACED RIGHT FLAP BPSU (BRAKE POSITION SENSING UNIT) IN ACCORDAMCE WITH MM 22-51-00. OPERATIONALLY CHECKS GOOD.Apr 27, 1995 · N408SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA95555Skin · dentedABORTED TAKEOFF IN FSD. AIRCRAFT RETURNED TO GATE. INSPECTED AIRCRAFT AND FOUND DENT IN LEFT INBOARD FLAP ACTUATOR PYLON. INSPECTED LEFT INBOARD FLAP ACTUATOR PYLON. POPPED OUT DENT. DETERMINED AIRCRAFT TO BE AIRWORTHY AND OK FOR RETURN TO SERVICE. REINSApr 9, 1995 · N405SW · Cndair CL6002B19 · Trailing Edge FlapsSDR COM60446Control Amp · defectiveLEFT ENGINE ROLLED BACK TO 60 PERCENT N1. REPLACED THE LEFT ENGINE N1 CONTROL AMPLIFIER.Mar 28, 1995 · N916CA · Cndair CL6002B19 · Fuel Controlling SystemSDR SWIA95541Sensor · malfunctionedWING ANTI-ICE SENSOR CAUTION MESSAGE COMES ON WITH WING ANTI-ICE ON IN NORMAL. IN STANDBY, CHECKS OK. REPLACED LEFT WING CONTROL SENSOR AND OVERHEAT SENSOR. OPS CHECKS GOOD. SEE FL 5073 FOR MECH SIGN OFF.Mar 6, 1995 · N403SW · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR SWIA95538Structure · vibrationDURING CLIMB AS AIRSPEED APPROACHED 280 KTS, AIRPLANE BEGAN TO VIBRATE (LIKE OUT OF BAL NOSEWHEEL). IT ALSO YAWED LEFT (ABOUT 1/2 BALL OUT OF TRIM) AIRSPEED CHANGES OF 100 PLUS KNOTS HAD NO EFFECT ON VIBRATION OR YAW. THE SAME RUDDER TRIM KEPT EVERYTHING CENTEMar 2, 1995 · N406SW · Cndair CL6002B19 · Aircraft StructuresSDR SWIA95534Fecu · failedFLAPS FAILED ON APPROACH. REMOVED AND REPLACED FECU. FLAP OPS CHECK OK. SEE FL 5129 FOR MECH SIGN OFF.Feb 19, 1995 · N409SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA95526Uplock · iced upUNABLE TO GET RIGHT MAIN GEAR TO GIVE AN UP AND LOCKED INDICATION. CYCLED GEAR SEVERAL TIME THEN GOT A GEAR DISAGREE WARNING IN RETRACT POSITION. AFTER DE-ICING MAIN ENG GEAR, INSPECTED GEAR AND PERFORMED A GEAR SWING. NO PROBLEMS FOUND. SUSPECT LARGE AMOUFeb 14, 1995 · N403SW · Cndair CL6002B19 · Landing Gear Position and Warning
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