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 N6WA2017081002Engine · failedLEFT ENGINE FAILED IN FLIGHT.Aug 10, 2017 · N354CA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SWIA201743443Engine · vibrationNR 1 ENGINE VIBRATION EXCESSIVE, N1 VIBRATION INDICATION APPROXIMATELY 2.1. VIBRATION REDUCED BY REDUCING THRUST. SHOOK BLADES OUT. RAN ENGINE, VIBRATION REMAINED AT .2 OR LESS.Jul 3, 2017 · N713SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA2016091000007Engine · bird ingestionAIRCRAFT HIT A FLOCK OF BIRDS DURING CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND ENGINE DAMAGE. REMOVED AND REPLACED LEFT ENGINE AND PERFORMED CHECKS IAW AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.Sep 10, 2016 · N720PS · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR N6WA2016082902Actuator · leakingNR 2 ENGINE FUEL LEAK. R & R PRIMARY VG ACTUATOR IAW AMM 75-30-01, LEAK AND OPS CHECK GOOD.Aug 29, 2016 · N354CA · Cndair CL6002C10 · Compressor Bleed ControlSDR ASOA2016081115239Engine · failedAFTER TAKE OFF, ACFT BEGAN TO SHAKE, RT ENGINE VIBRATION CAUTION UP TO 6.8. AND ITT WENT RED. SHUT RT ENGINE DOWN AND RETURNED TO DEPARTURE. REMOVED AND REPLACED THE RT ENGINE IAW AMM 71-00-00. INSTALLED RT ENGINE IDG IAW AMM 24-11-01.Aug 11, 2016 · N398CA · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR V0XD20160314058Latch · brokenRIGHT AFT THRUST REVERSER LATCH PIN BROKEN. R & R RT AFT THRUST REVERSER LATCH IAW AMM 78-33-03 & 20-21-00.Mar 14, 2016 · N658CA · Cndair CL6002C10 · Engine Thrust ReverserSDR CA160314007Sensor · failed(CAN) LEFT ENGINE HIGH OIL TEMP, TEMP SENSOR REPLACED.Mar 11, 2016 · Cndair CL6002C10 · Engine Oil TemperatureSDR CA160122007Connector · arced(CAN) ESS TRU FAIL MESSAGE WITH CB POPPED. UPON TROUBLESHOOTING FOUND CONNECTOR PL108P1/J1 BURNT. CONNECTOR REPLACED.Jan 21, 2016 · Cndair CL6002C10 · Electrical Power System WiringSDR CA151217003Frame · corroded(CAN) DURING CHECK CORROSION WAS FOUND IN AVIONICS BAY ON ATTACHED FLANGE OF 5EA FRAMES. REMOVAL OF CORROSION WAS PERFORMED IAW SRM 51-21-06, AFTER BLEND OUT NDT INSPECTION FOR CRACKS AND REMAINING THICKNESS WAS PERFORMED WITH NO FINDINGS. FOR DETAILS OF DAMAGDec 11, 2015 · Cndair CL6002C10 · Fuselage Main, FrameSDR SIMA20151012005Stand Off · crackedLEFT ENG, LOWER TRANS COWL, INBD STANDOFF ANGLE IS CRACKED, APPROX .500 INCHES. R & R LT LOWER TRANS COWL STANDOFF IAW SRM 51-42-06 & ETN CR-54-015R1.Oct 12, 2015 · N502AE · Cndair CL6002C10 · Engine Thrust ReverserSDR SIMA20151012004Stand Off · crackedLEFT ENG, UPPER TRANS COWL, INBD STANDOFF ANGLE IS CRACKED, APPROX .500 INCHES. R & R STANDOFF ANGLE IAW SRM CHAPTERS 51-42-20, 51-42-28 & ETN-CR-54-015R1.Oct 12, 2015 · N502AE · Cndair CL6002C10 · Engine Thrust ReverserSDR CA150916014Windshield · cracked(CAN) LT WINDSHIELD CRACKED ON CLIMB AND PERFORMED AN AIR TURN BACK.Sep 14, 2015 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA150827001Boot · out of position(CAN) LEFT BLEED DUCT WARNING DURING FLIGHT. COMPLIED WITH QRH. RT BLEED CLOSED CAUSING ULTIMATE LOSS OF PRESSURE. CREW INITIATED AN EMERGENCY DESCENT DUE TO THE LOSS OF CABIN PRESSURE, THE PASSENGER OXYGEN MASKS WERE RELEASED. INSPECTED LT BLEED DUCTS, FOAug 20, 2015 · Cndair CL6002C10 · Pneumatic Distribution SystemSDR SIMA20150709001Unknown · odorUPON ROTATION NOTICED A BURNING SMELL FROM THE PACK SYS, A SMALL LIKE FEATHERS OR BIRD. POSSIBLE INJECT OF BIRD ON LT ENGINE. PERFORMED FIM TASK 21-22-00, NO ABNORMAL ODOR IN COCKPIT OR CABIN AREA. RAN LT ENGINE & PACK IAW AMM 7100-00, NO DEFECTS NOTED.Jul 9, 2015 · N501BG · Cndair CL6002C10 · Air Distribution SystemSDR CA150710007Cable · corroded(CAN) AIRCRAFT HAS A HISTORY OF AUTOPILOT DISENGAGING ON ITS OWN WHILE IN FLIGHT. MDC LOGGED PITCH SERVO CIRCUIT. WHILE TROUBLESHOOTING THE PITCH SERVO CIRCUIT ISSUE, MX NOTICED THAT THE CONTROL WHEEL WAS NOT MOVING DURING THE CHECK OF THE AUTOPILOT AND THAT TJul 8, 2015 · Cndair CL6002C10 · Aileron Control SystemSDR CA150710003Proximity Switch · failed(CAN) ON DESCENT CREW GOT A STRONG ELECTRICAL SMELL IN THE COCKPIT, DONNED O2 MASKES & DECLARED AN EMERGENCY. A/C LANDED WITHOUT INCIDENT. MX FOUND PAX DOOR SENSOR PX 107 SMOKED.Jul 8, 2015 · Cndair CL6002C10 · Door Warning SystemSDR N6WA2015060601Connector · dirtyLEFT FADEC CAUTION IN FLIGHT. CLEANED CONNECTORS ON THE FMU & MASTER VG ACTUATOR. PERFORMED GND ENG RUN IAW AMM 71-00-00. NO MSGS OR DEFECTS NOTED.Jun 6, 2015 · N655CA · Cndair CL6002C10 · Engine Fuel System WiringSDR ASOA2015060312972Bulb · burned out12 AB AND 12CD LOWER EXIT SIGN HAVE 2 LIGHT BULBS BURNED ON EACH SIGN. R & R LIGHT BULBS IAW AMM 33-51-11. OPS CHECKED GOOD.May 29, 2015 · N612QX · Cndair CL6002C10 · Emergency LightingSDR CA150605004Wire Harness · chafed(CAN) CHAFED NAV LIGHT HOUSING WITH WIRE HARNESS. IT WAS ONLY FOUND AFTER SEVERAL FAILURE OF THE LIGHT AND A MORE EXTENSIVE FAULT ISOLATION.Apr 15, 2015 · Cndair CL6002C10 · Light System WiringSDR SIMA20150303003Engine · vibrationNUMBER 2 ENG VIBRATION 1.8 - 1.9 IN CRUISE. AMBER VABS ABOVE 10,000 FT. INSPECTED NR 2 ENG FAN BLADES IAW AMM 72-21-02, NO DEFECTS NOTED. PERFORMED VI CHECK IAW PARAMETERS WITHIN LIMITS SEE PIREP NR 4 FOR FURTHER ACTION. DEFERRED IAW MM REF 72-00-00-810-01Mar 3, 2015 · N524AE · Cndair CL6002C10 · Engine Vibration AnalyzerSDR CA150303008Compressor · stalled(CAN) NR 1 ENGINE COMPRESSOR STALL.Feb 18, 2015 · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR MASA2015021612908Engine · power lossNR 2 ENGINE LOST THRUST WITH A HIGH ITT & VIBE CREW SHUTDOWN ENGINE IN FLIGHT, EMERGENCY WAS DECLARED. THERE WAS NO BRACING BY PASSENGERS, ACFT LANDED & TAXIED TO GATE WITHOUT INCIDENT. ENGINE REPLACEMENT WILL BE REQUIRED DUE TO HIGH ITT. THERE ARE NO VISUFeb 16, 2015 · N505MJ · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR CA150227007Check Valve · faulty(CAN) ENGINE NR 2 ITT OVERTEMP. ENGINE 2 SHUTDOWN IN FLIGHT IAW QRH. EMER DECLARED. WE WERE IN THE INITIAL DESCENT, ABOUT 25 MINUTES OUT. WE ELECTED TO CONTINUE TO DESTINATION. ALL PROCEDURES & CHECKLISTS WERE FOLLOWED. LANDED & TAXIED TO GATE WITHOUT INFeb 16, 2015 · Cndair CL6002C10 · Compressor Bleed ControlSDR CA150107006Control Panel · failed(CAN) - AFTER TAKE OFF RT RUDDER FULL SCALE DEFLECTION WE WERE ABLE TO CENTER USING RUDDER TRIM, FULL SCALE DEFECTION WAS UNCOMMANDED ATB REMOVED AND REPLACED RUDDER TRIM ACTUATOR IAW AMM 27-22-01 REMOVED AND REPLACED AITLERON/RUDDER TRIM PANEL IAW AMM 27-12-Jan 5, 2015 · Cndair CL6002C10 · Rudder Tab Control SystemSDR CA141217016Actuator · failed(CAN) CREW REPORTED UNCOMMANDED YAW OSCILLATIONS IN FLIGHT, QRH PROCEDURES FOLLOWED AND WAY DAMPERS DISENGAGED BUT OSCULLATIONS CONTINUED. ADJUSTING RUDDER TRIM TENDED TO INCREASE OSCILLATIONS. THE ACFT LANDED WITHOUT EVENT. MAINT. REPLACED THE FCP, BOTH YAW Dec 15, 2014 · Cndair CL6002C10 · Autopilot SystemSDR CA141208003Control Panel · failed(CAN) DUAL YAW DAMPER FAILURE. DIFFICULTY CONTROLLING THE A/C. EMERGENCY DECLARED. REPLACED RELAY K58, K59. REPLACED YAW DAMPER PANEL , REPLACED RELAYS IAW AMM 22-22-07, PANEL IAW AMM 22-22-04 OK FOR SERVICEDec 3, 2014 · Cndair CL6002C10 · Autopilot SystemSDR CA150911011Hose · failed(CAN) BOMBARDIER RECEIVED A DISCLOSURE LETTER REGARDING THE CAPABILITY OF HOSE ASSEMBLIES THAT ARE USED ON THE POWERPLANT HYDRAULIC SYSTEM INSTALLATIONS. BOMBARDIER ASSESSED THE POTENTIEL SAFETY CONCERNS THEN. A REVIEW OF THIS FORMER ASSESSMENT WILL BE CONDUCTNov 28, 2014 · Cndair CL6002C10 · Hydraulic System, MainSDR CA141031005Valve · failed(CAN) WHILE TAXING WITH ANTI-ICE FOR ICE CONDITIONS BOTH THE LT AND RT WING ANTI-ICE FAIL MESSAGE APPEARED. SUBSEQUENTLY THE LT WING ANTI-ICE FAIL MESSAGE CLEARED BUT THE RT WING ICE REMAINED FAILED. CONTINUOUS LT AND 5 WING AMBER INDICATION. THE FLIGHT CREOct 21, 2014 · Cndair CL6002C10 · Airfoil Anti/De-ice SystemSDR CA150123008Hose · cracked(CAN) DURING TAKE-OFF ROLL, ANOTHER A/C REPORTED WHITE SMOKE COMING FROM THE CUSTOMER AIRCRAFT. CAPTAIN DECIDED TO ABORT TAKE-OFF AT ABOUT 80 KTS. CAUTION MESSAGE HYD EDP 2 IS POSTED. ONCE THE RUNWAY WAS CLEARED, CREW NOTICED THAT THE QUANTITY OF HYDRAULIC IN Oct 19, 2014 · Cndair CL6002C10 · Hydraulic System, MainSDR ASOA2014102211471Skin · damagedRT ENGINE CORE COWL HAS CHAFE DAMAGE DUE TO CONTACT WITH GREEN HARNESS. REPAIRED IAW REO 670-54-23-959. MAJOR REPAIR.Sep 15, 2014 · N709EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR SIMA20140908003Compressor Blade · lack of lubeAT INITIAL CRUISE FLIGHT, NR 2 ENG FAN REACHED APPROX 3.5 VIBRATION. AOM VOL 1 PROCEDURE FOLLOWED. REDUCTION IN THRUST EVENTUALLY HELPED A BIT. FOLLOWED PROCEDURE IN AMM 22-21-02 & PERFORMED THE VIBRATION CHECK IAW 71-00-00. PERFORM BLADE LUBE WITHIN 50 F Sep 8, 2014 · N523AE · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR SWIA201439213Battery Pack · inoperativeAFT F/A FLASHLIGHT NOT WORKING. REPLACED AFT F/A FLASHLIGHT BATTERY.Aug 23, 2014 · N743SK · Cndair CL6002C10 · Emergency EquipmentSDR WVER0815201450919Skin · damagedRT ENGINE AFT CORE COWL HAS TWO SCREWS LOOSE AND PULLING THROUGH OUTER SKIN AT UPPER 9 O'CLOCK POSITION.Aug 15, 2014 · N509MJ · Cndair CL6002C10 · Engine Thrust ReverserSDR CA140807015Mcu · failed(CAN) JUST AFTER TAKE-OFF, THE STAB TRIM AND MACH TRIM FAILED AND WOULD NOT RESET. THE AIRCRAFT RETURNED TO AIRPORT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL MCU. OK.Aug 4, 2014 · Cndair CL6002C10 · Stabilizer Control SystemSDR MASA2014062702193Engine · unknownNR 1 ENGINE PRODUCED A LOUD BANG DURING CLIMB AT 12000 FEET. OPENJun 27, 2014 · N504MJ · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SIMA20140620004Fmu · failedFUEL BURN MUCH HIGHER THAN PLANNED LT NR 1 ENG BURNED 300 LBS HIGHER THAN NR 2 ENG. R & R NR 1 FMU IAW AMM 73-21-00. LEAK CHECKED IAW AMM 73-10-00, NO LEAK FOUND.Jun 20, 2014 · N511AE · Cndair CL6002C10 · Fuel Control/Turbine EnginesSDR CA140428003Unknown · odor(CAN) RETURNED TO THE GATE, SMOKE ODOR IN THE CABIN. SIMULTANEOUSLY EICAS DISPLAYED RT PACK FAULT. RT PACK HAS BEEN PLACED UNDER MEL.Apr 26, 2014 · Cndair CL6002C10 · Air Distribution SystemSDR CA140420001Warning Message · activated(CAN) OTBD SPOILERON AND OTBD FLT SPOILER CAUTION MSG.Apr 10, 2014 · Cndair CL6002C10 · Drag Control SystemSDR N6WA20141330001Oil System · lowLEFT ENGINE OIL LOW. SERVICED ENGINE OIL IAW AMM 12-13-79, NO LEAKS NOTED AT THIS TIME.Mar 30, 2014 · N690CA · Cndair CL6002C10 · Turbine Engine Oil SystemSDR ASOA2014031910158Sensor · failedAT LT ENG OIL TEMP STARTED TO CLIMB RAPIDLY TO 249C. NEVER RECEIVED MASTER WARNING OR CAUTION, ONLY RED TEMPERATURE ON EICAS, FOLLOWED QRH & SHUTDOWN LT ENGINE, ENROUTE, ACFT DIVERTED DUE TO MAINTENANCE EMERGENCY ACTIONS. R & R OIL LEVEL/TEMP SENSOR IAW AMM Mar 14, 2014 · N608QX · Cndair CL6002C10 · Engine Oil Temperature RegulatorSDR CA140314013Coffeemaker · burned(CAN) F/A REPORTED SMOKE IN THE CABIN AND THAT THE FUMES WERE BAD ENOUGH TO BURN SOME PASSENGERS THROATS WHEN BREATHING. EMERGENCY WAS DECLARED AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND CHEWING GUM STUCK TO A COFFEE POT THAT WAS BURNING AND CREATING THEMar 12, 2014 · Cndair CL6002C10 · Buffet/GalleysSDR CA140317001Cascade · broken(CAN) AIRPORT AUTHORITY FOUND PARTS ON THE AIRFIELD ON MARCH 7TH AND PROVIDED THE PARTS TO OPERATOR FOR THEIR REVIEW. DURING A SCHEDULED VISIT ON MARCH 11TH, MAINTENANCE FOUND SECTIONS OF THE THRUST REVERSER CASCADES WERE FOUND MISSING.Mar 7, 2014 · Cndair CL6002C10 · Engine Thrust ReverserSDR CA140304004Safety Valve · failed(CAN) CABIN ALT CAUTION MESSAGE. AIRCRAFT DIVERTED. CONTROLLER PREVIOUSLY DEFERRED. FOLLOWED QRH, UNABLE TO CONTROL CABIN PRESSURE. EMERGENCY DECLARED AS A PRECAUTION.Mar 2, 2014 · Cndair CL6002C10 · Pressure Regulator/Outflow ValveSDR CA140306010Unknown · odor(CAN) STRONG ELECTRICAL BURNING ODOR IN COCKPIT THEY REPORT WATER DRIPPING FROM ESCAPE CATCH ON PEDESTAL. STRONG ELECTRICAL BURNED ODOR COMING FROM THE TRIM PANEL WITH A SLIGHT DISCOLORATION. AFTER REMOVING THE PANEL AND PUTTING BACK POWER ON THE ACFT, IT SEFeb 19, 2014 · Cndair CL6002C10 · Air Distribution SystemSDR SIMA20140204005Engine · vibrationON TAKEOFF TKO E1 VIB ON 1.4. VIBE CLIMBED DURING ACCENT AT 17,500 E2 VIB WENT AMBE AT 1.8. THRUST REDUCED TO CRUISE POWER TO LOWER VIB. GOT VIB REDUCED TO 1.6 THEN WITHOUT INPUT VIB RETURNED TO AMBER 1.8 BOTH REDUCED TO TAKE VIB TO GREEN RANGE AT 1.4 AT 22Feb 4, 2014 · N513AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SWIA201435966Engine · failedPERFORMED A REJECTED TAKE OFF AT APPROXIMATELY 105 KNOTS DUE TO LOSS OF DIRECTIONAL CONTROL & APPARENT LOSS OF POWER FROM THE NR 2 ENG. FLT 1301 REPLACED ENG ON CP 10385995.Jan 7, 2014 · N746SK · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR CA140106011Servo · locked(CAN) AT 1000 FT AGL FLIGHT CONTROLS LOCKED UP AND WERE FREE AND NORMAL THEN LOCKED UP AGAIN. HAPPENED A TOTAL OF 3 TIMES.Jan 1, 2014 · Cndair CL6002C10 · Aileron Control SystemSDR ASOA2014013109822Doubler · chafedRIGHT ENGINE LOWER CORE COWL, INNER SKIN DOUBLE REPAIR HAS CHAFE DAMAGE. REMOVED DOUBLER ON RT LOWER COWL DOOR IAW SRM 51-42-06-001-001. COMPLIED WITH REPAIR OF THE FWD CORE COWL IAW REO 670-54-23-959. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW ASA SOPDec 24, 2013 · N723EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR CA140106005Windshield · cracked(CAN) CRACKED RIGHT WINDSHIELD.Dec 22, 2013 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA131216015Wire · broken(CAN) PRIOR TO TAKEOFF WE HAD ACFT DEICED. JUST 15 MINUTES AFTER TO CLIMBING THROUGH 17000 FT AT 290 KTS. WE HEARD A LOUD BANG ON THE LT SIDE OF ACFT, THEN GEAR DISAGREE WARNING POSTED ON ED1. LT MAIN GEAR WAS INDICATING RED AND ALL HYDRAULIC PRESSURES NORDec 14, 2013 · Cndair CL6002C10 · Landing Gear System Wiring
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