GE CF34-8C5

Service difficulty reports · 772

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 = 'CF348C5'
  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 CA081007003Screw · loose(CAN) ALL SCREWS ON TOP OF WING UNDER THE SLATS WERE FOUND LOOSE. 2 SCREWS , 1 ON EACH SIDE, WERE FOUND PROTRUDING BEYOND THE WING SURFACE CAUSING MINOR DAMAGE TO THE UNDER SKING SURFACE OF THE SLAT. ALL SCREWS WERE TIGHTENED BACK.Oct 6, 2008 · Bombdr CL6002D15 · Leading Edge DevicesSDR CA080819005Window · cracked(CAN) DISC - IN CRUISE FLIGHT, F/O SIDE WINDSHIELD CRACKED AND WINDSHIELD HEAT ON RT SIDE FAILED.. ACFT RETURNED. NO PRESS PROBLEM. ALL OTHER SYS NORMAL. REMOVED AND REPLACED F/O SIDE WINDOW.Aug 16, 2008 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA080819004Windshield · cracked(CAN) "DISC - AFTER TAKEOFF CAPTAIN`S WINDSHIELD CRACKED. NO OTHER PROBLEMS NOTED. REMOVED AND REPLACED PILOTS WINDSHIELD.Aug 15, 2008 · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA200819936Light · inoperativeEMERGENCY CABIN LIGHT INOPERATIVE. (FLIGHT NR 4070) REPLACED EMERGENCY LIGHT IAW 33-51-21. OPS CHECK OK. Aug 3, 2008 · N804SK · Cndair CL6002D24 · Emergency LightingSDR SWIA200819918None · nonePOSSIBLE TAIL STIKE ON LANDING. (FLIGHT NR 4125) PERFORMED TAIL STRIKE INSPECTION IAW 32-71-00. NO DISCREPENCIES NOTED.Jul 31, 2008 · N800SK · Cndair CL6002D24 · Standard Practices/StructuresSDR FDK2008F00004Warning Message · false activationPAX DOOR LATCH CAUTION MSG. MX OPS CHECKED GOOD. (K)Jul 16, 2008 · N606LR · Cndair CL6002D24 · Door Warning SystemSDR FDK2008F00001Hook · missingOVERWING ESCAPE HOOK MISSING. MX INSTALLED MISSING HOOK. (K)Jul 10, 2008 · N601LR · Cndair CL6002D24 · Emergency EquipmentSDR FDK2008F00002Switch · dirtyPAX DOOR CAUTION MESSAGE IN FLIGHT. MX RE-REPACKED PSCU AND CLEANED SWITCHES. (K)Jul 2, 2008 · N606LR · Cndair CL6002D24 · Door Warning SystemSDR FDK2008F00003Warning Message · illuminatedPASSENGER DOOR LATCH, CAUTION MESSAGE AND PROX SYS FAULT 2. OPS CHECK GOOD. (K)Jun 30, 2008 · N606LR · Cndair CL6002D24 · Door Warning SystemSDR CA080618010Windshield · failed(CAN) RT COCKPIT SIDE WINDOW SHATTERED WHILE SITTING AT THE GATE. REMOVED AND REPLACED THE RT COCKPIT SIDE WINDOW.Jun 2, 2008 · Cndair CL6002C10 · Flight Compartment WindowsSDR REXA200800014Engine · contaminatedDURING CLIMB-OUT FROM KMEM, THE COCKPIT AND CABIN FILLED WITH SMOKE. THE FLIGHT CREW DONNED O2 MASKS, COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY WITH ATC. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE. THE AIRCRAFT WAS STOPPED ON THE TAXIWAY AND CFMay 22, 2008 · N153PQ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA080408002Control Unit · failedPRIOR TO DEPARTURE FLIGHT CREW COMPLETED A STAB TRIM RESET. SHORTLY AFTER FLAP RETRACTION ON TAKEOFF, FLIGHT CREW RECEIVED AN AP TRIM IS ND ASSOCIATED WITH AN AP PITCH TRIM ‘CAUTION MESSAGE. SUBSEQUENTLY CREW RECEIVED A ELEVATOR SPLIT’ CAUTION MESSAGE. CREWMar 29, 2008 · Cndair CL600* · Trailing Edge Flap Control SystemSDR MASA200800178Rod · defectiveNR 1 ENGINE, S/N 194271, EXPERIENCED ITT EXCEEDANCE OF 1031C FOR 2.7 SECONDS DURING START. BORESCOPE C/W WITH NO DEFECTS. MX REPLACED MASTER AND SLAVE VG TORQUE RODS.Feb 19, 2008 · N933LR · Cndair CL6002D24 · Fuel Controlling SystemSDR MASA200800159Rod · defectiveNR 1 ENGINE, S/N 194271, EXPERIENCED ITT EXCEEDANCE OF 1031C FOR 2.7 SECONDS DURING START. BORESCOPE C/W WITH NO DEFECTS. MX REPLACED MASTER AND SLAVE VG TORQUE RODS.Feb 19, 2008 · N933LR · Cndair CL6002D24 · Fuel Controlling SystemSDR CA080218001Control Unit · faulty(CAN) ON LANDING, CREW RECEIVED IB ANTI-SKID CAUTION MESSAGE. AFTER TAXIING CLEAR OF ACTIVE RUNWAY IT WAS DETERMINED BOTH LT MAIN TIRES FLAT. MAINT FOUND MDC FAULT CODES INDICATED FAULTY ASCU. ASCU REPLACED, AXLE INSP. FOR OVERTEMP AND TIRES REPLACED. FUNCTIONFeb 16, 2008 · Cndair CL600* · Brake Anti-Skid SectionSDR CA080126003Window · cracked(CAN) AC DIVERTED, FOS SIDE WINDOW CRACKED IN FLT, CREW DECLARED EMRG NO PRESS ISSUES. NOTED CREW USED MASKS. MASKS NOT DROPPED IN CABIN. SIDE WINDOW P/N:601R33033-20, S/N: 04023H4068: CO-PILOT SIDE WINDOW 9573 HRS / 6860 CYCLES (TC NR 20080126003)Jan 16, 2008 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA080110003Connector · failed(CAN) FLAP FAIL MESSAGE ON POWER UP. CODES READ AND BPSU NR 2 WIRING FAILED. MEL 27-51-02-1 APPLIED. WILL PROVIDE UPDATE WHEN MORE INFO BECOMES AVAILABLE (TC NR 20080110003)Jan 10, 2008 · Cndair CL6002C10 · Flight Control System WiringSDR CA080106004Proximity Sensor · malfunctioned(CAN) AFTER TAKEOFF, A LANDING GEAR DISAGREE WARNING MESSAGE WAS DISPLAYED. CREW CYCLED THE GEAR UNTIL SELECTED DOWN AND GEAR LOCKED DOWN INDICATION (3 GREEN LIGHTS). AC PERFORMED A TURNBACK AND LANDED UNEVENTFULLY (AFTER FUEL DUMPING FOR NOT LANDING OVERWEIGHJan 2, 2008 · Cndair CL6002C10 · Landing Gear Position and WarningSDR CA071227008Pseu · failed(CAN) A/C EXPERIENCED A PROX SYS FAULT DURING CLIMB OUT MESSAGE BECAME INTERMITTENT AFTER 8-10 MINUTES. FLIGHT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINT REPLACED THE PSEU AND CHECKED THE SYS THROUGH THE MFG SERVICEABLE. GEAR SWINGS C/O, NFF. A/C RETUDec 20, 2007 · Cndair CL600* · Landing Gear Position and WarningSDR CA071211003Adc · malfunctioned(CAN) THE FO REPORTED AN AIRSPEED OVER-SPEED TAPE ILLUMINATED AND COVERED THE ENTIRE SPEED TAPE ON THE AIRSPEED INDICATOR. AN AMBER (STALL FAIL) EICAS MESSAGE AND STICK SHAKER ENSUED. THE STALL PTCT SWITCH WAS SELECTED OFF HOWEVER THE STICK SHAKER CONTINUED. QDec 8, 2007 · Cndair CL6002B16 · Air Data ComputerSDR CA071126008Gcu · failed(CAN) ACCORDING TO THE CREW WRITE UP: NR1- HYD 3A FAILED ( HYP PUMP 3A CAUTION MSG POSTED) ELECTRICALLY POWERED BY AC BUS NR2 - (GEN2 FAILED) WE DID NOT GET A AMBER GEN FAIL INDICATION OR WARNING. AC BUS 2 FAILED AGAIN, NO WARNING. TRU 2 AND ESS TRU FAILED, NONov 22, 2007 · Cndair CL6002D24 · AC Generation SystemSDR CA071118001Rod End · broken(CAN) REPORT FROM AIR ONE: REF /A/ - AIPC 27-33-01, FIG 1 WHILE PERFORMING TASK CARD 000-27-220-010 - OPERATIONAL TEST OF THE ELEVATOR PCUS, AIR ONE FOUND THAT WITH HYD 1 ONLY, THE ELEVATOR WOULD NOT MOVE. AFTER INSPECTION, THEY FOUND THAT PCU 1 ROD END (ONNov 15, 2007 · Cndair CL6002D24 · Elevator Control System
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