GE CF34-10E5A1
Service difficulty reports · 476
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 = 'CF3410E5A1' 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.
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 = 'CF3410E5A1' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CA150622001Unknown · malfunctioned(CAN) ATC CLEARED FLIGHT TO CLIMB FROM FL 370 TO FL 380. DURING CLIMB, CREW HAD AN UN-COMMANDED SPEED CHANGE FROM .77 TO .64. SELECTED MANAGED SPEED & INPUT .77. RESOLUTION IAW COMMENTS IN TROUBLESHOOTING DVDR DATA & HISTORY DATA LOAD, NO FAULTS. DATA SENTSDR CA150615021Sign · failed(CAN) FLIGHT CREW REPORTED SMOKE IN CABIN & INITIATED A DIVERSION. RESOLUTION R & R FASTEN SEAT BELT SIGN AT 18AC. OPERATIONS CHECKED GOOD ALL WORK DONE IAW 33-20-00.SDR CA150615018Pump · failed(CAN) RETURNED DUE TO FUEL FEED FAULT. RESOLUTION MAIN EJECTOR PUMP REPLACED IAW AMM 28-21-13.SDR CA150525010Proximity Sensor · dirty(CAN) AFTER DEPARTURE, L1 DOOR INDICATION SHOWED OPEN, CREW DESCENDED TO 10,000 FEET. CONSULTED WITH MOC WHO CHECKED WITH ACFT & ALSO SHOWED L1 OPEN. FLIGHT CONTINUED, NO LOSS OF PRESSURIZATION OCCURRED. RESOLUTION L1 DOOR, CLOSE & LATCH PROX SENSOR & TARGESDR CA150525009Engine · overheated(CAN) ENGINE OVERHEAT FOR 1 SECOND DURING START UP. RETURNED TO GATE FOR MX INVESTIGATION. ENG IS RETURNED TO SERVICE WITH NO FURTHER TROUBLESHOOTING.SDR CA150514001Feel Unit · failed(CAN) UNUSUAL ACFT HANDLING DURING TAKEOFF. HEAVY ELEVATOR CONTROLS DURING ROTATION. COPILOT ELEVATOR FEEL UNIT REPLACED IAW 27-31-03 PB 401. OPERATIONS TESTED IAW 27-31-03-710-801-A. RTS CARRIED OUT IAW 27-00-00-070-801-A & PASSED.SDR CA150515004Panel · damaged(CAN) STATION OPS CALLED TO ADVISE THAT ACFT HAD HEAT RELATED DAMAGE FOUND ON GPU RECEPTACLE. ACFT IS CURRENTLY OUT OF SERVICE. REPLACED FWD RAMP INTERPHONE PANEL IAW AMM 23-52-01.SDR CA150427010Pump · leaking(CAN) WHILE IN CRUISE, CREW REPORTED A STEADY DECLINE IN HYDRAULIC FLUID QUANTITY. IN CONJUNCTION WITH DISPATCH, MOC, FLIGHT CREW IT WAS DECIDED THAT A DIVERSION WOULD BE PRUDENT. CREW DECLARED A PAN PAN WITH ATC. LANDING WAS UNEVENTFUL. HYDRAULIC QUANTITY SDR CA150427009Connector · shorted(CAN) ON APPROACH CONDITIONS DRY ON RUNWAY, CREW REPORTED A PAN PAN DUE SLAT FAIL. NO EMERGENCY WAS DECLARED, BUT EMERGENCY VEHICLES MET THE FLIGHT. NO NEGATIVE PAX AND/OR IFS REACTION TO INCIDENT. MOC ADVISED. CARRIED OUT FIM 27-83-00-810-814-A, FOUND PINSSDR CA150427006Windshield · cracked(CAN) ON DESCENT WHEN PASSING THROUGH 20,000 FT THE F/O SIDE WINDOW CRACKED. MAINTENANCE WAS ADVISED AND THE ACFT HAS BEEN REMOVED FROM SERVICE FOR REPAIRS. RESOLUTION REPLACED F/O WINDSHIELD IAW AMM 56-11-00.SDR CA150414002Flap System · failed(CAN) ON APPROACH WHEN SELECTING FLAP TO FULL, LEVER DISAGREE FOLLOWED BY SLAT LOW RATE MESSAGE APPEARED. FULL FLAP EVENTUALLY ACHIEVED AND NORMAL LANDING PERFORMED. RESET FLAP/SLAT SYSTEM IAW QRRG. OPS CHK NORMAL. NO FURTHER DEFECTS.SDR CA150326002Sensor · failed(CAN) ACFT HAS EXPERIENCED A SLAT FAILURE AND WILL BE DECLARING A PAN PAN WITH ATC. DUTY PILOT ADVISED. RESOLUTION REMOVED AND INSTALLED NEW OTBD SLAT SKEW SENSOR IAW AMM 27-83-01-000-801-A AND 27-83-01-400-801-A FUNCTION AND OPS CHECKED SERV IAW FIM 27-83-00SDR CA150318004Unknown · odor(CAN) ON DEPARTURE HAD DIRTY SOCK ODOR FROM ROTATION TILL A10000 APU WAS OFF AT THE TIME AND THE ODOR WAS ONLY IN THE FLIGHT DECK. RESOLUTION IAW TASK 72-00-00-800-822 NR 1 ENGINE BOROSCOPE CARRRIED OUT NO FAULTS, NO TRACE OF OIL LEAK, NO OIL STAIN, NO OIL PUSDR CA150318007B-Nut · loose(CAN) APPROXIMATELY 1H ENROUTE, CREW ADVSD THE HYDRAULICS WERE DOWN TO 36 PERCENT. AS A PRECAUTIONARY, FLIGHT RETURNED BACK. FLIGHT LANDED WITH NOT INCIDENT AND NOT CFR REQUIRED. FOUND LOOSE B-NUT ON HYD PRESSURE, MAIN LINE IN FWD PYLON. TIGHTEND B-NUT AND LSDR CA150310015Video Display · failed(CAN) AFTER T OFF FLIGHT, CREW WERE NOTIFIED OF A BURNING ODOR COMING FROM ROW 28. FLIGHT CREW TURNED OFF IFE SYS AS A SAFE GUARD. RESOLUTION COULD NOT CONFIRM HARD FAULT. IFE SYS RUN WITH EAR JACKS INSTALLED, READING LIGHTS ON & IN SEAT ROWER ON. SVDU`S 28SDR CA150309004Sensor · failed(CAN) SLAT FAILURE ON APPROACH, QRH COMPLETED. FLIGHT LANDED NO INCIDENT. IAW FIM 27-81-00-810-803A SLAT INHIBITS CLEARED ACFT SYS RESET, MESSAGE CLEARED SLATS/FLAPS FUNCTIONED SEVERAL TIMES NO FAULT MESSAGES NO HISTORY, ACFT SERVICEABLE.SDR CA150309008Brake Sys · failed(CAN) DUAL BRAKE FAULT ON SHORT FINAL. GO-AROUND PERFORMED, CHECK LIST COMPLETED, AND ACFT PERFORMED A NORMAL LANDING. ACFT POWERED DOWN. MESSAGE CLEARED, CMC CHKD, NO HISTORY, NO CORRELATIONS FOR FDE, BRAKE SYSTEM TESTED IAW AMM NO FAULTS CONSIDERED SERVICSDR CA150309010Brake Sys · faulted(CAN) DUAL BRAKE FAULT ON SHORT FINAL. GO-AROUND PERFORMED, CHECK LIST COMPLETED, AND ACFT PERFORMED A NORMAL LANDING. ACFT POWERED DOWN. MESSAGE CLEARED, CMC CHK/D NO HISTORY, NO CORRELATIONS FOR FDE, BRAKE SYSTEM TESTED IAW AMM NO FAULTS CONSIDERED SERVICSDR CA150309005Receptacle · damaged(CAN) ELECTRICAL ARCING AND BLACK BURN MARKS PRODUCED WHEN CONNECTING A MOBILE GROUND POWER UNIT TO ACFT. PASSENGERS WERE DEPLANED. CRASH FIRE RESCUE RESPONDED. NO INJURIES REPORTED. REMOVED AC POWER RECEPTACLE IAW AMM 24-42-03-000-801-A. FOUND COMPOSITE SDR CA150305001Processor · failed(CAN) DURING THE FLIGHT, THE FLIGHT CREW ENCOUNTERED AN EICAS MESSAGE MAU 1A FAIL. THIS RESULTED IN NO NOSE WHEEL STEERING AVAILABLE AFTER LANDING. AS A PRECAUTION,THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC AND LANDED RUNWAY 36. THE LANDING WAS OTHERWISESDR CA150220001Bleed Valve · failed(CAN) THE FLIGHT DEPARTED WITH 1 ENG. BLEED INOP UNDER MEL. AFTER DEPARTURE, THE REAMING ENGINE BLEED BECAME UNSERVICEABLE. THE FLIGHT LANDED BACK WITHOUT FURTHER INCIDENT. NR 1 NAPRSOV REPLACED 36-11-03 PB401. ENG RUN CARRIED OUT - CK`D SERV.SDR CA150123002Actuator · failed(CAN) SLAT FAIL ON APPROACH GO AROUND TO RECONFIGURE ,CREW REQUESTED EMERGENCY VEHICLES TO MEET ON LANDING. LANDED WITHOUT INCIDENT. RESOLUTION FOUND LTH SLAT NR 4 ACTUATOR AT FAULT , ACTUATOR REPLACED AS PER AMM 27-81-01-400 , SLAT MECHANICAL RIGGING C/OUT PSDR CA150109003Pump · loose(CAN) EJECTOR PUMP SCREEN SEPARATED (WAS LOOSE) AND COULD POTENTIALLY MOVE AROUND INSIDE FUEL TANK. THIS SCREEN WAS SUPPOSED TO BE HELD IN PLACE BY THE GROOVE AROUND THE PUMP INLET.SDR CA150107005Sensor · failed(CAN) SLAT FAIL 5 MIN. AFTER TAKE-OFF. FLAP LEVER NOT ACTUATED. RESOLUTION L/H BOTH O/B SKEW SENSORS S 2/3 S3/4 REPLACED & TESTED SERVICEABLE AS PER AMM 27-83-01 ALSO SF ACE NR 2 REPLACED & TESTED SERVICEABLE AS PER AMM 27-53-02 PB 401.SDR CA150105003Control Unit · failed(CAN) ON APPROACH, THE CREW CONDUCTED A GO AROUND DUE TO A SLAT FAIL. SLAT/FLAP ACTUATOR CONTROL ELECTRONIC UNIT NR 1 REPLACED IAW 27-53-02-000/400-801A. TASKS 27-50-00-710-801A/500 AND 27-80-00-710-801/500 CARRIED OUT 4 TIMES. NO FAULTS WITH SLAT CONTROL SYSSDR CA141210002Tube · failed(CAN) AFTER DEPARTING, CREW RETRACTED THE NOSE GEAR , THERE WAS A LOUD BRAKING NOISE AND CREW HAD 3 RED ON GEAR. THEY PUT THE GEAR DOWN AGAIN AND GOT 3 GREEN, CREW CONSULTED WITH MOC AND AGAIN TRIED TO RETRACT THE GEAR WHICH WOULD NOW NOT RETRACT AND WAS LOCKSDR CA141201001Connector · corroded(CAN) LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF, RETURNED. DECLARED EMERGENCY. FOUND ACTIVE MESSAGE (NLG WOFW 2 SNSE/WRG FAULT. FAULT CODE 32612303PSS. CARRIED OUT T/SING AS PER FIM 32-61-00-810-891-A.. RESET BREAKER MAU 3 PWR 1.RHCBP (DC ESS BUS 2) TRANSDR CA141127006Uplock · failed(CAN) NOSE GEAR ISSUE, EMERGENCY DECLARED. NLG UPLOCK ASSEMBLY REPLACED IAW AMM 32-32-03-401. FUNCTIONAL + LEAK TEST COMPLETED SERVICEABLE.SDR CA141128002Wire Harness · failed(CAN) SLAT FAIL EICAS ON APPROACH, THE FLAP LEVER WAS NOT SELECTED YET. PAN PAN DECLARED, LANDED WITHOUT INCIDENT. REPLACED THE W511 SLAT WIRE HARNESS IAW AMM 27-83-07. CHECKED GOOD.SDR CA141127004Pump · failed(CAN) SHORTLY AFTER DEPARTING, CREW HAD A MAINTENANCE ISSUE. UPON DISCUSSING THE NATURE OF THE FAILURE WITH MOC, THE DECISION TO RETURN WAS MADE. IN FLIGHT HYD 2 EDP FAIL EICAS ADVISORY MSG. NR 2 EDP PRESS SWITCH REPLACED AS PER AMM 29-31-03-000-801-A.NO FIX.SDR CA141117001Unknown · odor(CAN) ON TAXI OUT, A DEADHEADING ACFT EMPLOYEE NOTICED A BURNING ODOR IN THE AFT CABIN, THE F/A AGREED THAT WAS A STRONG BURNING RUBBER ODOR. THE CREW ELECTED TO CALL THE FIRE TRUCKS OUT AND RETURN TO THE GATE. NO SMOKE ODOR EVIDENT ON RTG. BOTH ENGINES RUSDR CA141103017Slat System · failed(CAN) DURING APPROACH, FLIGHT EXPERIENCED A SLAT FAILURE. NORMAL LANDING. RESET SLAT/FLAP AND OPS CHECKED OK. RETURN TO SERVICE COMPLETED SUCCESSFULLY.SDR CA141103019Fan · failed(CAN) DURING THE MORNING STARTUP OF THE AIRCRAFT AND THE GPU HOOKED UP, WHEN POWER WAS SELECTED ON THE AIRCRAFT IT BEGAN TO FILL WITH SMOKE AND FUMES. POWER WAS SHUTDOWN, THE FUMES AND SMOKE DISSIPATED. MTC IS CURRENTLY INVESTIGATING. RT RECIRCULATION FAN SDR CA141031009Actuator · failed(CAN) ON APPROACH FLIGHT EXPERIENCED A SPOILER CONTROL FAULT. A RESET WAS ATTEMPTED BUT WAS UNSUCCESSFUL. WITH WET RUNWAYS, THE CREW ELECTED TO DECLARE A PAN WITH ATC. THE LANDING WAS UNEVENTFUL AND THE ACFT TAXIED TO THE GATE. THE CREW REPORTED THAT THERE WASDR CA141031016Unknown · smoke(CAN) CREW REPORTED A POSSIBLE ODOUR EVENT ON DEPARTURE. IAW FIM 21-20-00-810-801A INVESTIGATED PROBABLE SOURCE OF SMOKE ODOR WITH NOTHING OBVIOUS OR TRACE OF SMOKE ODOR.SDR CA141023001Girt Bar · out of adjust(CAN) AIRCRAFT ARRIVED AND COULD NOT OPEN THE L1 DOOR. SUSPECT THE LOWER SEAL WAS FROZEN AND WAS IMPEDING DISARMING THE L1 DOOR. ESCAPE SLIDE GIRT BAR FOUND OUT OF ADJUSTMENT. GIRT BAR ADJUSTED IAW AMM 52-11-00-820-02A. DOOR FUNCTION TESTS SERVICEABLE.SDR CA141014018Control Lever · failed(CAN) ON DEPARTURE, AIRCRAFT WAS UNABLE TO RETRACT THE LANDING GEAR. THE CREW ELECTED TO RETURN BACK WHERE. AN EMERGENCY WAS NOT DECLARED. MTC CONTROL, THE DUTY PILOT AND CORPORATE SAFETY WERE ADVISED. LANDING GEAR CONTROL LEVER REPLACED AND GEAR SWINGS CARSDR Q0MF20141008006Hinge · brokenDUE TO ECM VBV DOOR POSITION TREND ABNORMALITY ON LT ENG SN 994295, OUR ENGINEER ISSUED EO NR TE1031003 TO PERFORM VISUAL INSPECTION TO THE VBV DOOR ASSEMBLY, ESPECIALLY ON THE HINGE IF ANY CRACK SIGN, & FOUND HINGES OF LT ENG VBV DOOR ASSEMBLY AT 8 O'CLOCK POSDR CA141003003Actuator · disconnected(CAN) THE ACFT ENCOUNTERED A FLAP FAILURE ON APPROACH TO RUNWAY. THERE WAS NIL EMERGENCY DECLARED, ALTHOUGH CFR WAS REQUESTED TO BE ON STANDBY. RESOLUTION FOUND TORQUE TUBE RT SIDE OF SLAT PDU DISCONNECTED. CARRIED OUT COMPLETE LT AND RT MECHANICAL AND ELECTSDR Q0MF20140929005Hinge · brokenDURING I NR 1 CHECK, FOUND HINGES OF RT ENG VBV DOOR AT 8 O'CLOCK POSITION WERE BROKEN. THE DOOR WAS HUNG BY THE BENT LINKAGE. NO EVIDENCE OF IOD WAS FOUND DURING BORESCOPE INSPECTION. THIS IS THE 7TH CASE IN OUR ERJ-190 FLEET DURING 7 YEARS OPERATION. THE SDR CA140925001Sensor · out of adjust(CAN) INCIDENT DETAILS: AFTER TAKEOFF UNABLE TO RETRACT LANDING GEAR. RETURNED. PAN PAN DECLARED WITH ATC. RESOLUTION FIM 32-61-00-810-890-A C/OUT AND FOUND NLG WOW SENSOR 1 & 2 CLEARANCE AT 0.060" AND 0.090", BOTH SENSORS ADJUSTED IAW AMM 62-61-00 TO 0.044SDR Q0MF20141003004Engine · flamed outEXPERIENCED RUNWAY EXCURSION DURING LANDING PHASE, ACFT ROLLING INTO THE SOFT GRASS THEN BACK TO THE RUNWAY. PILOT FOUND LT ENG HAD FLAME OUT, THEN TAXIED TO THE GATE SAFELY. AFTER ACFT PARKED, THE MECHANIC INSPECTION FOUND EICAS SHOWS LT ENG FAIL MSG, RT ENSDR CA140922003Windshield · delaminated(CAN) F/O`S WINDSHIELD DELAMINATED WHILE IN FLIGHT. IT WAS NOT KNOWN WHAT ASPECT OF THE FLIGHT THIS ORIGINALLY OCCURRED. FLIGHT CONTINUING TO DESTINATION. REPLACED THE RT WINDSHIELD IAW AMM 56-11-00-PB401.SDR CA140915009Controller · failed(CAN) SLAT FAIL ON DECENT. DECLARED PAN PAN. LANDED 0 SLAT 2 FLAP. UNEVENTFUL LANDING. FAULT CODE 27833008ACE SLATS ACE2 LATCH FAULT, T/S CARRIED OUT AS PER FIM 27-83-00-810-819-A, REPLACED S/F ACE NR 2 AS PER AMM 27-53-02 PB401, OPS CHECK AS PER AMM 27-80-0SDR CA140828003Control Module · failed(CAN) DURING APPROCH, BRAKE FAULT INDICATION ON THE LEFT AND RIGHT SIDE. CREW INITIATED A GO AROUND. PAN DECLARED WITH ATC. FLIGHT LAND WITHOUT ANY OTHER PROBLEMS. BRAKING SEEMED TO BE NORMAL ON TAXI IN. CARRIED OUT FIM TASK 32-41-00-810-825-A & 824-A. FASDR CA140822004Oven · smoke(CAN) ON APPROACH, SMOKE WAS REPORTED IN THE AFT GALLEY. LOCAL MAINTENANCE WAS ADVISED ON ARRIVAL. FOUND OVEN CIRCUIT CREATING THE ODOR. REPLACED OVEN AND CONTROLLER IAW S.P.SDR CA140818014Sensor · failed(CAN) SPOILER FAULT AT ALTITUDE, FOLLOWED QRH PROCEDURE, NIL FIX. PAN PAN DECLARED WITH ATC. RESOLUTION CARRIED OUT FIM 27-03-00-810-813-A. REPLACED PILOT INBD CONTROL-YOKE POSITION SENSOR AS PER AMM 27-66-01/401. CONTROL YOKE RIGGING AND OPS CHECK CARRIED OUSDR CA140819002Flap System · malfunctioned(CAN) FLAP CONTROL ISSUE IN DESCENT. GO-AROUND INITIATED, PERFORMED QRH PROCEDURE, SUBSEQUENT LANDING WITHOUT ISSUE. NO CURRENT/ACTIVE CMC MESSAGES.SDR CA140818009Riser · leaking(CAN) FLIGHT CREW CONDUCTED AN AIRBORNE RETURN SHORTLY AFTER DEPARTURE DUE TO A LOUD HOWL COMING FROM THE LEFT OVER WING EXIT. THERE WERE NO ABNORMAL PRESSURIZING INDICATIONS. NO EMERGENCY WAS DECLARED. REPLACED RISER DUCT PER PP ERJ190-21-54875 AND AMM 21-2SDR CA140725002Slat System · failed(CAN) ON APPROACH AT 3000 FT THE CREW SELECTED FLAPS AND RECEIVED A SLAT FAIL AND SPOILER FAIL MESSAGES. THE QRH WAS CARRIED OUT AND THE SLAT AND FLAPS DEPLOYED NORMALLY AND THE LANDING WAS CONDUCTED WITHOUT FURTHER ISSUES. MAINTENANCE WILL INSPECT THE AIRCR
Back to GE CF34-10E5A1