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 CA991103077Adc · failed(CAN) FLAP FAIL WHEN SELECTING FLAPS TO 45 DEGREES. FLAPS STOPPED AT 40 DEGREES AT 168 IAS.Oct 23, 1999 · Cndair CL6002B19 · Air Data ComputerSDR CA991210028Skin · lightning strike(CAN) LIGHTNING STRIKE ON LEFT SIDE OF FUSLAGE. FOUND LEFT ICE DETECTOR TRAILING EDGE DAMAGE AND EVERY 9-10 INCHES RIVET HEAD BURNT ALL THE WAY BACK TO LEFT WING. BURNS WITHIN LIMITS EXCEPT UNDER WINSHIELD. RIVETS REPLACED.Oct 23, 1999 · Cndair CL6002B19 · Wing, Plate/SkinSDR CA991103076Sensor · failed(CAN) FLAP FAIL IN-FLIGHT AT 8 DEGREES. INDICATION ZERO. CHANGE BPSU.Oct 20, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA991103075Flex Shaft · damaged(CAN) FLAP FAIL ON APPROACH AT 190 KNOTS. ZERO DEGREES FLAP LANDING. POWER DRIVE UNIT CHANGED DUE TO HIGH CURRENT DRAW. RIGHT NR 4 FLEXSHAFT DAMAGED. REPLACED. LEFT NR 5 CONDUIT ASSY REPLACED. AD 98-14R1 C/W.Oct 12, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA971582Bpsu · failedCLIMBING THROUGH 22,000 FEET, FLAPS FAIL MESSAGE ON EICAS. CYCLED CIRCUIT BREAKERS PER MAINTENANCE CONTROL WITH NO CHANGE. RETURNED TO SLC AND LANDED O FLAPS, (FLAPS FAILED AT 0 DID NOT OPERATE FLAP SELECTOR). REMOVED AND REPLACED LEFT BRAKE POSITION SENSOROct 12, 1999 · N407SW · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR CA991103073Ecu · failed(CAN) DURING TAXI FLAPS FAIL MESSAGE CAME ON. UNABLE TO RESET. FECU REPLACED AND BPSU.Oct 7, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA991028046Actuator · failed(CAN) FLAPS FAILED ON APPROACH. NR 3 ACTUATOR AND NR 5 LEFT ACTUATOR REPLACED.Oct 5, 1999 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA991103074Te Flap · failed(CAN) FLAP FAIL ON APPROACH. RESET CARRIED OUT SERV.Oct 5, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA030417004Bushing · loose(CAN) MIGRATING BUSHINGS ON WING ATTACHMENT FITTINGS.Oct 4, 1999 · Cndair CL6002B19 · Wing, Attach FittingsSDR AU991028042Valve · failed(AU) LEFT COWL ANT-I ICE FAILED. COWL ANTI-ICE VALVE REPLACED.Oct 2, 1999 · Cndair CL6002B19 · Air Intake Anti/De-Ice SystemSDR CA991028043Sensing Unit · failed(CAN) FLAPS FAIL ON APPROACH AT ZERO DEGREES. NR 5 FLEX SHAFT AND RIGHT BRAKE SENSOR REPLACED.Oct 1, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA9960532Engine · vibrationRIGHT HAND ENGINE N1 VIB 2.7 ABOVE LIMITS. BALANCED ENGINE TO ACCEPTABLE LIMITS.Sep 20, 1999 · N956CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA9960534Engine · failedRIGHT HAND ENGINE FAILED AFTER TAKEOFF (IFSD). REPLACED THE RIGHT HAND ENGINE.Sep 18, 1999 · N949CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA9960537Engine · failedIDG NR 2 CAUTION MESSAGE, FOLLOWED BY GEN NR 2 CAUTION MESSAGE ON TAKEOFF. IDG NR 2 CAUTION MESSAGE WENT OUT DURING ABORT. NR 2 GEN WAS RESET. FOUND SKYDROL IN ACCESSORY GEARBOX OF RIGHT ENGINE. REMOVED AND REPLACED RIGHT ENGINE.Sep 18, 1999 · N945CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA991008023Wire · failed(CAN) FLAP FAILED ON DESCENT. BROKEN WIRE ON BPSU IN WHEELWELL. REPAIRED.Sep 14, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA9960511Engine · failedDURING CRUISE FLIGHT AFTER DEPARTING FROM IAD, THE HOT WARNING ACTIVATED FOR THE RIGHT ENGINE, THE RIGHT ENGINE WAS SHUTDOWN INFLIGHT AND AIRCRAFT CONTINUED DESTINATION FLIGHT TO CVG WHERE AN EMERGENCY WAS DECLARED. FOUND THE RIGHT ENGINE CONTAMINATED WITH MSep 10, 1999 · N967CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA9960497Spring · brokenWHILE PERFORMING A MAINTENANCE SERVICE CHECK 50 HOUR INSPECTION MECHANIC FOUND A BROKEN BLOCKER DOOR (P/N 228-50219-111) ON THE LEFT ENGINE THRUST REVERSER, VISIBLE FROM THE GROUND. FURTHER INVESTIGATION FOUND PROBABLE CAUSE TO BE TWO BROKEN RETURN SPRINGS (PSep 8, 1999 · N915CA · Cndair CL6002B19 · Engine Thrust ReverserSDR COMA9960493Engine · failedOILY SMELL FROM LEFT HAND ENGINE BLEED AIR. REPLACED ENGINE.Sep 7, 1999 · N933CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA9960484Engine · failedLEFT ENGINE ITT 880 DEGREES, VIB 4.0 IFSD. REPLACED LEFT HAND ENGINE.Sep 4, 1999 · N991CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA9960485Engine · failedTHICK OILY SMOKE IN COCKPIT FROM THE AIRCRAFT SYSTEM. REPLACED THE LEFT ENGINE.Sep 2, 1999 · N947CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA991104009Transmitter · failed(CAN) AILERON POSITION TRANSMITTER ARM INCORRECTLY INSTALLED WHICH CAUSED THE ARM TO RUB ON AILERON CABLE.Sep 1, 1999 · Cndair CL6002B16 · Aileron Control SystemSDR COMA9960479Exhaust Frame · crackedRIGHT HAND LOW OIL PRESSURE. REPLACED CRACKED EXHAUST FRAME.Aug 29, 1999 · N946CA · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR COMA9960466Seal · failedCREW REPORTED OIL SMELL FROM LEFT PACK WITH 10TH STAGE BLEED OPEN. CHANGED NR 3 CARBON SEAL ON LEFT ENGINE, PERFORMED COMPRESSOR WASHES. NO SMELL NOTED.Aug 23, 1999 · N947CA · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR COMA9960459Engine · leakingAFTER ENGINE WAS CHANGED, AN OIL SMELL WAS NOTED IN COCKPIT WITH LEFT 10TH STAGE BLEED OPEN DURING GROUND RUNS. REMOVED ENGINE (LEFT) (S/N 807070) AND INSTALLED (S/N 807255).Aug 21, 1999 · N947CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA990927081Actuator · failed(CAN) FLAP FAIL MESSAGE ON FINAL AFTER FLAPS APPEARED TO REACH 45 DEGREES. FLAP FLEX SHAFTS INSPECTED, LUBRUCATED. NR 3 RT ACTUATOR REPLACED AND SYSTEM RIGGED.Aug 14, 1999 · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR CA990927076Ecu · failed(CAN) ON APPROACH, FLAPS SELECTED FROM 8-20, LT FLAP STOPPED AT 13 AND RT AT 14. REPLACED FLAP SYSTEM ELECTRONIC UNIT AND RT BRAKE.Aug 13, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA990916005Engine · failed(CAN) HIGH VIBRATIONS.Aug 10, 1999 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR COMA9960413Engine · failedOIL SMELL IN COCKPIT DURING FLIGHT. REPLACED LEFT ENGINE.Aug 4, 1999 · N933CA · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA971539Seal · leakingUPON DEPARTURE, NOSE GEAR INDICATION DOWN AND LOCKED AFTER SELECTING GEAR UP. COMPLIED WITH CHECK LIST AND LOWERED GEAR. RETURNED TO FAT, MEL 32-30-1. REMOVED AND REPLACED NOSE GEAR STRUT TEE SEAL AND SERVICED NOSE STRUT. LEAK CHECKS OK IAW 32-21-00. SWUAug 3, 1999 · N403SW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR CA990812032Window · cracked(CAN) TWO LARGE CRACKS NOTICED AFTER TAKEOFF IN LOWER CORNER OF LEFT WINDOW.Jul 27, 1999 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA990812030Apu · leaking(CAN) AFTER APU START, STRONG SMELL IN COCKPIT AND SMOKE SMELL IN CABIN. LAVATORY SMOKE DETECTOR WENT OFF ONCE. AIRCRAFT AT GATE. APU OIL LEAKING INTO BLEED AIR SYSTEM. APU CHANGED AND COALESCER BAGS CLEANED.Jul 22, 1999 · Cndair CL6002B19 · APU Oil SystemSDR CA990812031Bpsu · failed(CAN) FLAPS FAILED AT 20 DEGREES AFTER TAKE-OFF. BPSU CHANGED ON LEFT SYSTEM.Jul 22, 1999 · Cndair CL6002B19 · Trailing Flap Position Indicating SystemSDR CA990812029Ecu · failed(CAN) FLAP FAILED AT ZERO DEGREES. FLAP ELECTRONIC CONTROL UNIT POTENTIOMETER NR 1 AND NR 8 ADJUSTED.Jul 20, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA990812027Ecu · failed(CAN) FLAPS CAUTION LIGHT ON WITH FLAPS AT 30 DEGREES, BUT SELECTED TO 45. FLAP ELECTRONIC UNIT AND FLAP CONTROL LEVER REPLACED.Jul 14, 1999 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR JBXA9900091Priorty Valve · inoperativeGEAR DISAGREE, 2 NOSE OPEN DOOR MESSAGES ON GEAR RETRACTION. REMOVED AND REPLACED HYDRAULIC PRIORTY VALVE IAW CL-65 MM 32-33-15. PERFORMED FUNCTIONAL CHECK ON PRIORTY VALVE IAW CL-65 MM 32-30-00. OPERATIONAL CHECK GOOD.Jul 13, 1999 · N578ML · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR COMA9960393Pin · shearedCREW REPORTED MAIN CABIN DOOR IS VERY HARD TO OPEN AND THAT DOOR HANDLE SEEMS TO GET STUCK WHEN PULLING UPWARD ON HANDLE. WHILE TROUBLESHOOTING THE DOOR HANDLE (P/N 600-31887-11 ITEM NR 5 PAGE 1 FIG 1 RJ IPC CH 52-11-02) FOUND THE PIN (HSP 115BO94-900 ITEM NRJul 12, 1999 · N781CA · Cndair CL6002B19 · Passenger/Crew DoorsSDR COMA9960360Wire Harness · looseAFTER TAKEOFF, RIGHT ENGINE ROLLED BACK AND THEN SURGED 10 PERCENT. SECURED LOOSE WIRING HARNESS AT FUEL CONTROL UNIT.Jul 11, 1999 · N943CA · Cndair CL6002B19 · Engine Fuel System WiringSDR SWIA971514Seal · failedAFTER DEPARTURE AIRCRAFT MAIN DOOR HAD LOUD SQUEAL AND AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO SLC. REMOVED AND REPLACED CABIN DOOR SEAL IAW SB 601R-52-067. PRESSURIZED AIRCRAFT AND ALL CHECKS GOOD.Jul 9, 1999 · N408SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA971515Pin · not removedGEAR DISAGREE ON DEPARTURE FROM SLC. BURNED FUEL DOWN TO LANDING WEIGHT AND RETURNED TO SLC. FOUND GEAR PIN IN NOSE GEAR. REMOVED PIN.Jul 9, 1999 · N416SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA971516Sensing Element · looseON CLIMB-OUT RIGHT 14TH DUCT MSG ILLUMINATED. FOLLOWED QUICK REFERENCE HANDBOOK AND LIGHT EXTINGUISHED WHEN RIGHT 14TH BLEED VALVE WAS CLOSED. RETURNED TO SLC. TORQUED RIGHT 14TH STAGE DUCT SENSING ELEMENT IAW MM 36-21-00. OPS CHECKS GOOD AT THIS TIME.Jul 9, 1999 · N407SW · Cndair CL6002B19 · Air Intake Anti/De-Ice SystemSDR CA990707070Hose · cracked(CAN) IN-FLIGHT, NR 2 SYSTEM HYDRAULIC QUANTITY AND PRESSURE WENT TO ZERO. HOSE FOUND CRACKED.Jul 6, 1999 · Cndair CL6002B19 · Hydraulic System, MainSDR CA990715034Mfc · failed(CAN) ENGINE WOULD NOT DECELERATE TO IDLE, WITH THE THRUST LEVER AT THE IDLE STOP THE ENGINE PARAMETERS REMAINED AT N1 66, ITT 570, N2 82, FF 400. MFC REPLACED. AIRCRAFT RETURNED TO SERVICE.Jul 6, 1999 · Cndair CL6002B19 · Fuel Control/Reciprocating EnginesSDR CA990715039Trim Panel · failed(CAN) RUDDER TRIM RUNAWAY ON OPERATION OF RUDDER TRIM. DRILL COMPLETED/OPERATES NORMAL. TRIM PANEL REPLACED.Jun 28, 1999 · Cndair CL6002B19 · Rudder Tab Control SystemSDR CA990719018Frame · cracked(CAN) FUSELAGE STATION 718.0, STRINGERS 10-12 FOUND CRACKED ON BOTH SIDES OF FUSELAGE.Jun 25, 1999 · Cndair CL6002B19 · Fuselage Main, FrameSDR CA990719019Frame · cracked(CAN) FUSELAGE STATION 718.0, STRINGERS 10-12 FOUND CRACKED ON BOTH SIDES OF FUSELAGE.Jun 25, 1999 · Cndair CL6002B19 · Fuselage Main, FrameSDR CA990719017Torque Tube · out of rig(CAN) DOOR WARNING LIGHT ON IN-FLIGHT. TORQUE TUBE UPPER LATCH CAMS FOUND OUT OF RIG.Jun 15, 1999 · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA971502Service Panel · not closedON TAKEOFF, ADC NR 2 FAILED. SHORTLY THEREAFTER A LOUD VIBRATION COULD BE HEARD AND FELT IN THE COCKPIT. RETURNED TO SLC. FOUND OXYGEN SERVICE PANEL UNLATCHED CAUSING A DISTURBANCE IN AIRFLOW TO THE NR 2 PITOT TUBE. PERFORMED INSPECTION OF O2 SERVICE PANELJun 9, 1999 · N412SW · Cndair CL6002B19 · Service DoorsSDR SWIA971510Service Door · not closedAFTER TAKEOFF, A VERY LOUD SQUEAL WAS HEARD ALONG WITH IAS STALL FAIL, MACH TRIM AND EFIS COMP. RETURNED TO SLC. SECURED OXYGEN SERVICE DOOR IN FRONT OF RIGHT PITOT TUBE. ALL SYSTEMS FUNCTION NORMAL.Jun 6, 1999 · N405SW · Cndair CL6002B19 · Service DoorsSDR COMA9960250O Ring · cutRIGHT HAND ENGINE LOW OIL PRESSURE WARNING. REPLACED THE ENGINE DRIVER HYDRAULIC PUMP DRIVE PAD O-RING.Jun 5, 1999 · N962CA · Cndair CL6002B19 · Turbine Engine Accessory DriveSDR SWIA971497Indication · malfunctionedNOSE GEAR DISAGREE WARNING LIGHT AFTER GEAR RETRACTION. NOSE GEAR LIGHT STAYED GREEN. PERFORMED GEAR SWING IAW MM 32-30-00, NO PROBLEMS FOUND. COULD NOT DUPLICATE DISCREPANCY.Jun 1, 1999 · N411SW · Cndair CL6002B19 · Landing Gear Position and Warning
Back to GE CF34-3A1