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 CA120704005Engine · leaking(CAN) ACFT ARRIVED 10 TO 15 MIN AFTER RT ENGINE SHUTDOWN. THE RAMP CREW REPORTED A FIRE IN THE TAIL PIPE AND DISCOVERED A LEAK UNDER THE TAIL PIPE. THE ACFT HAS SINCE BEEN PULLED OFF LINE BY MAINTENANCE.SDR CA120628005Interface Unit · failed(CAN) THE FLIGHT CREW ENCOUNTERED A COMPLETE COMM FAILURE WHILE DESCENDING THROUGH 10,000 FT. THEY CONTINUED ON THE PLANNED ARRIVAL SQUAWKING 7700, EMERGENCY, THEN 7600 COMM FAILURE. THE FLIGHT LANDED. REPLACED NIM 1 AND 2 IAW AMM 34-02-04, CHECK SERVICEABSDR CA120628004Controller · failed(CAN) ACFT OPERATING ON A MAINTENANCE CHECK FLIGHT FOR PRESSURIZATION CHECK. THE ACFT FAILED THE MAINTENANCE CHECK AND A PAN PAN WAS DECLARED WITH ATC. CPCS CONTROLLER REPLACED IAW AMM 21-31-01, AC PACKS AND DUCTS INSPECTED AND LEAK CHECKED, CABIN PRESSURIZASDR CA120606005Oil System · leaking(CAN) FLIGHT TAXIED INTO GATE 1. WHEN ENGINES WERE SHUTDOWN, THE RAMP LEAD ADIVSED THAT NR 1 ENGINE WAS ON FIRE FROM THE ENGINE EXHAUST, CREW DEPLANED THE PASSENGER RAPIDLY LEAVING CARRY-ON BAGS BEHIND. MAIN ADVISED FOP`S TO SPIN, ROTATE, THE NR 1 ENGINE TSDR CA120529010Processor · failed(CAN) AFTER DEPARTURE, THE FLIGHT CREW RECEIVED MULTIPLE FLIGHT CONTROL FAIL MESSAGES, WHICH SENT CASCADING FURTHER MESSAGES. THE FLIGHT CREW ELECTED TO RETURN AS A PRECAUTION. THERE WAS NO ADVERSE PASSENGER REACTION. ON CLB ABOVE FL340, AVNX MAU 3A EICAS ASDR CA120611003Torque Tube · worn(CAN) DURING MAINTENENACE, THE LT NR 6 FLAP DRIVE TORQUE TUBE, PN 5912949-3 WAS FOUND WORN, AS WELL AS THE AFT SPAR BRACKET, PN 190-93293-001. AFTER POWER WAS RE-ESTABLISHED THE FLAPS WERE RETRACTED AND THE TORQUE TUBE WAS VERIFIED WEARING ON THE BRACKET. DUSDR CA120522016Control Panel · failed(CAN) CREW LOST THE STANDBY ACTUATOR FOR ELEVATOR CONTROL. INDICATOR WAS FLASHING ON AND OFF REVERSE YELLOW. ORIGINALLY LOST BOTH ELEVATOR SYS. NORMAL MODE WAS REESTABLISHED A SHORT TIME LATER. EICAS MSG ELEVATOR FAULT IN FLT. RESET C/O. SYSTEM RETURNED SDR CA120509007Turbine Blades · missing(CAN) PILOTS REPORTED VIBRATION DURING DESCENT. ON ARRIVAL AT GATE, ENGINES WERE INSPECTED. ENGINE 2 LP TURBINE WAS MISSING BLADES.SDR CA120509003Spda · failed(CAN) SPDA2 FAIL APPROXIMATELY. DIVERSION FOR MAINTENANCE. NORMAL DESCENT/APPROACH AND NO REQUIREMENT TO DECLARE PAN PAN OR EMERGENCY WITH ATC. ACFT LANDED BELOW MAXIMUM LANDING WEIGHT AT 41,500 KGS CMC INTEROGATED ACFT POWERED DOWN, FAULT REMOVED IAW FIM 2SDR CA120504007Valve · failed(CAN) PAN PAN DECLARED WITH ATC ACCOUNT OF AIR CONDITIONING PACK FAILURE AFTER DEPARTURE. 1 AIR CONDITIONING PACK WAS UNDER MEL AND INOPERATIVE. FLIGHT DESCENDED TO 10,000 FT ACFT WILL LAND APPROXIMATELY 1000 KGS OVER MLW NR 2 ENGINE FAN AIR VALVE REPLACED ISDR CA120503002Actuator · failed(CAN) ON APPROACH HAD A FLAP FAILURE, THE CREW CONDUCTED A MISSED APPROACH AND WENT THROUGH THE CHECKLIST. NO EMERGENCY WAS DECLARED. NO FURTHER ISSUES. FOUND NR 3 R FLAP ACTUATOR TRIPPED. REMOVED AND INSTALLED NR 3 RT FLAP TRANSMISSION IAW AMM 27-51-01.SDR CA120430007Pcu · failed(CAN) ON DESCENT AT APPROXIMATELY FL300, CREW SAW AN EICAS MESSAGE, AILERON LT FAIL. CREW FOLLOWED QRH AND CHECKED THE SYNOPSIS PAGE WHERE THE LT AILERON WAS STILL GREEN. LT OTBD PCU REPLACED IAW T/C E19-27-12-01-400-801A. PART REMOVED: LT AILERON OTBD PCUSDR CA120424007Module · failed(CAN) LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF, RETURNED, NO EMERGENCY DECLARED, ARFF CALLED TO STAND BY. NO FURTHER INCIDENT. NR 1 SPDA MOD 13 DC POWER MODULE REPLACED AND GEAR SWINGS CARRIED OUT. GROUND CHECKED SERVO AMM 24-61-13-400-801A,SDR CA120416001Plunger · sheared(CAN) DURING RAM AIR TURBINE MANUAL DEPLOYMENT INSPECTION, FOUND RAT DOWNLOCK PLUNGER SHEARED IN RAT STOW BAY.SDR CA120417002Wire Harness · failed(CAN) SLAT FAILURE ON DECENT YOW, PAN DECLARED WITH ATC. NO FURTHER INCIDENT. SLAT FAIL EICAS MESSAGE ON DESCENT. QRH ACTIONS CARRIED OUT SLATS DID NOT EXTEND PAST 0 ZERO INDICATION. CMC INTERROGATED FAULT CODE RECORDED 27831005AC3. SLAT HARNESSES AT POS SLSDR CA120405003Spoiler Sys · malfunctioned(CAN) ON ARRIVAL, THE FLIGHT CREW REPORTED HAVING A SPEED BRAKE DISAGREE ON APPROACH. FLIGHT LANDED NORMALLY T/S SYS. PERFORMED MULTIFUNCTION SPOILER PCU RIGGING IAW AMM 27-65-01. SYS CHECK GOOD. PERFORMED FLT CONTROLS RETURN-TO-SERVICE TEST. NO FAULTS NOTESDR CA120403007Carrier Assy · failed(CAN) MOC REQUESTED TO INSPECT BRAKE DISCKS DUE TO POSSIBLE BRAKE DISK KEEPER FAILURE DUE TO EARLY FINDING IN PREVIOUS AIRPORT OF CARBON BRAKE PARTS ON APRON BY AIRPORT ATHOURITY. MAINTENANCE FOUND 1 MAIN BRAKE FIRST DISK KEY KEEPERS MISSING COMPLETELY FROM TSDR CA120326001Valve · failed(CAN) FLIGHT WAS DISPATCHED UNDER MEL RELIEF WITH THE NR 2 ENGINE BLEED INOPERATIVE. SHORTLY AFTER TAKEOFF THE NR 1 ENGINE BLEED FAILED ALSO. AFTER A SUCCESSFUL AIRBORNE RESET OF NR 1 BLEED THE CREW ELECTED TO RETURN TO BASE AS A PRECAUTION AGAINST A REPEAT FASDR CA120312013Bolt · damaged(CAN) THE SEAL BACKUP RINGS WERE DAMAGED DURING INSTALLATION BUT SEALING INTEGRITY STILL ALLOWED THE SUCCESSFUL SERVICING OF THE GEAR WHILE IN CHECK. THE, IN SERVICE, OPERATION OF THE GEAR CAUSED DETERIORATION OF THE SEAL INTEGRITY TO THE POINT THE FLUID BYPASDR CA120312027Valve · failed(CAN) BLEED 2 FAILED DURING CLIMB, EMERGGENCY DESCENT TO 5000 FT, RETURNED TO STATION. RT PACK INLET TEMP SENSOR REPLACED IAW AMM 21-51-17. RT FAN AIR VALVE AND BELLOW REPLACED IAW AMM 36-11-09 PB401.SDR CA120305002Flap System · inoperative(CAN) AIR TURN BACK DUE FLAPS DID NOT RETRACT.SDR CA120306006Sensor · failed(CAN) FLIGHT DEPARTED UNDER MEL FOR ONE BLEED INOPERATIVE. AFTER DEPARTURE THE FLIGHT CREW REPORTED BEING UNABLE TO PRESSURIZE THE ACFT. THE FLIGHT RETURNED. NO EMERGENCY DECLARED NR 2 BLEED REPLACED BLEED TEMP SENSOR IAW AMM 36-14-03. ENGINE PNUEMATIC BLEESDR CA120221009Torque Tube · disconnected(CAN) THE ACFT ENCOUNTERED A FLAP FAILURE AFTER DEPARTURE. THE FLIGHT CREW ELECTED TO RETURN AS A PRECAUTION. FOUND TORQUE TUBE AT OUTPUT OF RT INBD FLAP ACTUATOR IMPROPERLY INSTALLED. TORQUE TUBE REINSTALLED. DRIVE LINE INSPECTION CARRIED OUT IAW AMM 27-SDR CA120221006Windshield · cracked(CAN) PAN DECLARED DUE TO CRACKED WINDSHIELD. DESCENT TO 10000 INITIATED AND FLIGHT PROCEEDED TO DESTINATION REPLACED CAPT WINDSHIELD IAW 56-11-00.SDR CA120221007Wire Harness · failed(CAN) CREW HAD A SLAT FAILURE ON ARRIVAL. CREW CHECKED LANDING DISTANCE REQUIRED AND MADE NORMAL LANDING WITH FLAPS 2, NO EMERGENCY WAS DECLARED AS "FLAP 1" WAS SELECTED, WE RECEIVED A "SLAT FAIL" MESSAGE ON THE EICAS. "SHAKER ANTICIPATED" WAS ALSO LATER DISSDR CA120216002Sensor · failed(CAN) SLATS FAILED IN THE FULL POSITION. GO-AROUND INITIATED DUE UNSTABLE APPROACH. FLIGHT DECLARED EMERGENCY. SLAT FAIL CAUTION ON SHORT FINAL, SLAT FULL/FLAP 5 WHEN CAUTION, SLAT FULL/FLAP 2 FINAL LANDING CONFIG, DUE NO FLAP THREE AVAIL ON FINAL. REPLACED SDR CA120214001Turbine Blades · damaged(CAN) ENGINE 2 LP VIB STEADY +2.0 IN CRUISE AS WELL AS 4.0 SPIKE AND AMBER BOX AT TOP OF DESCENT. FOUND 2 BLADES, LPT STG 4 MISSING APPROXIMATELY 3-3.5" FROM BLADE TIPS. ALSO CHIP DETECTED ON ENGINE MAINTENANCE.SDR CA120210001Turbine Blades · missing(CAN) DURING CLIMBOUT THRU FL23, FELT AND HEARD VERY NOTICEABLE RUMBLE FROM NR 1 ENGINE LP VIBREATION DURING CLIMB WERE BETWEEN 3.7-3.9 AND IN CRUIZE BETWEEN 2.6-3.0. FOUND TURBINE BLADES MISSING AND BENT.SDR CA120130006Flap System · failed(CAN) ON APPROACH TO RWY 12 ON APPROACH AT 5000 FT THE CREW REPORTED A FLAP FAIL, THE APPROACH WAS ABORTED AND RECEIVED VECTORS FROM ATC. PERFORMED QRH PROCEDURES, AND RETURNED FOR ROUTINE APPROACH/LANDING. ON FINAL WHEN SELECTING FLAP 1 WE HAD FLAP FAIL ON SDR CA120130007Mau · failed(CAN) IN CRUISE, CREW HAD THE AVIONICS MAU 2B STATUS MESSAGE. CREW FOLLOWED QRH. NO RESOLVE. JUST SOUTH OF CREW HAS NOW DECLARED A PAN PAN. AS BRAKING WILL BE AFFECTED. TASK 45-45-00-810-942-A, SUBTASK 810-433-A, 833-799-A CARRIED OUT. OPS CKD SERV. NO SDR CA120125007Windshield · cracked(CAN) THE FLIGHT CREW REPORTED A MAJOR CRACK IN THE LEFT HAND WINDSHIELD (OUTER LAYER), APPROXIMATELY 30 MINUTES PRIOR TO TOUCHDOWN. R & R LT WINDSHIELD IAW AMM 56-11-00. AND WINDSHIELD TEMP COMNTROL IAW AMM 30-42-01. OPS CK GOOD.SDR CA120119005Outflow Valve · failed(CAN) FLIGHT DEPARTED WITH CPC CH 1 INOP. AFTER DEPARTURE, THE REMAINING CABIN PRESSURE CONTROLLER FAILED. MASKS DID NOT DROP. CA INITIATED EMERGENCY DESCNT. CABIN PRESSURE NEVER EXCEEDED 7500`. NO EMERGENCY DECLARED WITH ATC T/S CARRIED OUT, NO FAULT FOUND. CSDR CA120105008Sensor · failed(CAN) THE AIRCRAFT ENCOUNTERED A SLAT FAILURE ON APPROACH. NIL EMEREGENCY WAS DECLARED AND THE LANDING WAS ROUTINE WITH NIL ADVERSE PASSENGER REACTION. ON APPROACH, SLAT FAIL EICAS MESSAGE. SLAT INDICATION ON EICAS STUCK AT 3. REPLACED LT SLAT O/B SKEW SENSORSDR CA120105007Slat System · failed(CAN) SLAT 3 WITH FAIL AT 10 DME AND FLAP 5 USED CHECKLIST COMPLETED. FLT LANDED WITHOUT INCIDENT. PERFORM FIM PROC 27-81-00-810-805-A00 SF ACE CLEAR INHIBITS PROC CARRIED OUT,OPS TEST OF SLAT SYSTEM IAW AMM 27-80-00-710-801-A. ALL TEST GOOD TRANSITORY CONDITSDR CA120104012Vent Line · distorted(CAN) LEFT ENGINE CENTER VENT TUBE REPLACED ON SPV CHECK AND RELEASED FOR SERVICE ON DECEMBER 22, 2011. FLIGHT CREW DISCOVERED CVT DISTORTED ON WALK AROUND.SDR CA120103014Sensor · failed(CAN) THE FLIGHT CREW RECEIVED AN EICAS FLAP FAILURE MESSAGE AT F380, PRIOR TO DESCENT WITH FLAPS INDICATING AMBER AND SHOWING ZERO. AS A PRECAUTION, THE FLIGHT CREW DECLARED AN EMERGENCY WITH ATC FOR PRIORITY HANDLING. THE LANDING WAS OTHERWISE ROUTINE AND SDR CA111219016Line · leaking(CAN) LOSS OF HYDRAULIC PRESSURE, RETURNING TO STATION, EMERGENCY NOT DECLARED. WILL HAVE THE USE OF NOSE WHEEL STEERING AND HALF OF BRAKES. HYD 1, LO QUANTITY FOLLOWED BY SYSTEM LOSS, STARTED AT FL280 SHOWED 18 PERCENT, LOST PRESSURE AFTER ABOUT 15 MIN. SOLSDR CA111208003Actuator · failed(CAN) POST AIRBORNE, UNABLE TO CROSSFEED FUEL WITH POTENTIAL FUEL IMBALANCE IMPLICATIONS. AFTER CONSULT WITH MOC, ELECTED TO RETURN, RESULTING IN AN OVERWEIGHT LANDING, 44,120KG. NO EMERGENCY DECLARED. NEW FUEL CROSSFEED LOW FUEL PANEL INSTALLED IAW 28-21-2SDR CA111206015Flap System · binding(CAN) CREW ADVISED VIA VHF TO DXP, ON ARRIVAL, FLAPS STUCK IN CONFIG 3, ACFT LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. SF-ACE 1 & 2 RESET IAW FIM 27-81-00-810-803-A, PG 203, BLK 1 TRANSITORY COND FLAPS/SLATS CYCLED NO FAULTS SYSTEM OPERATES NORMALSDR CA111205002Sensor · out of rig(CAN) DURING THE APPROACH TO LAND THE CREW REPORTED A SLAT/FLAP FAIL IN THE NR 3 POSITION. NO PAN PAN WAS DECLARED AND ERS WAS NOT CALLED OUT SKEW SENSOR BETWEEN RT SLATS 2 & 3 ADJUSTED TO BE WITHIN LIMITS IAW AMM 27-83-01.SDR CA111205003Unknown · odor(CAN) F/A`S REPORTED A SMOKE ODOR IN THE AFT CABIN. AFT GALLEY POWER, THE POWER TO THE IFE AND PC POWER WAS SHUTDOWN. THE ODOR DISSIPATED AND THE FLT CONTINUED TO DESTINATION. IFE, IN SEAT POWER, COFFEEMAKERS, OVEN OPERATED FOR 3 HRS+ WITHOUT ANY ABNORMAL SSDR CA111202002Blade · damaged(CAN) WHILE INFLIGHT, AT APPROXIMATELY FL320, THE CREW REPORTED HIGH ENGINE VIBRATIONS ON THE NR 2 ENGINE. THEY REDUCED POWER ON THE ENGINE TO IDLE TO REDUCE/STOP THE ENGINE VIBRATIONS. THEY DECLARED A PAN PAN EMERGENCY AND RETURNED TO WHERE THEY LANDED OVERSDR CA111128007Compressor · damaged(CAN) SIGNIFICANT ENG VIBRATION ON DEPARTURE, NR 2 ENG SHUTDOWN. ACFT DIVERTED, EMER DECLARED WITH ATC, CFR ON STANDBY. FLIGHT DEPARTED & THE ENG SURGED MULTIPLE TIMES AT 13 000 FT, WITH AUDIBLE BANGS & SMOKE, & LOSS ABOUT 40% OF POWER. THERE WERE NO ENG PASDR CA111116001Wire Harness · failed(CAN) MAYDAY DECLARED WITH ATC. LANDED WITHOUT INCIDENT AT 170KTS. WING SLAT HARNESS W612 REPLACED AND TESTED SERVICEABLE IAW AMM 27-83-07-400-801A. DURING FAULT ISOLATION ALSO FOUND BOTH OTBD RT SLAT SKEW SENSORS OUT OF ADJUSTEMENT, REF AMM
27-83-01.SDR CA111115002Actuator · tripped(CAN) SLAT FLAP FAILURE ON APPROACH. INITIATED GO AROUND AT APPROX 1000` AGL. NO ADVERSE PAX REACTION. NO ABRUPT MANEUVERING REQUIRED. NO EMER DECLARED, FOUND RT NR 7 SLAT ACTUATOR TRIPPED, NEW ACTUATOR ASSEMBLY INSTALLED IAW AMM 27-81-01-400-801-A.SDR CA110420007Bolt · sheared(CAN) RT MLG ACTUATOR, OTBD ATTACH FITTING HAS SHEARED HILOCK. THIS FINDING IS PREVIOUS TO A SIMILAR FINDING ON ANOTHER ACFT. THIS IS BEING REPORTED AS REQUESTED FROM TC.SDR CA111103007Sensor · failed(CAN) CREW ADVISED FLIGHT DISPATCH OF A FLAP FAIL MSG, CREW ELECTED TO DIVERT. TROUBLESHOT IAW FIM 27-51-00-810-805-A. REPLACED BOTH RT WING FLAP OTBD SKEW SENSORS T3 AND T4 IAW AMM 27-53-06. ELECTRONICALLY RIGGED AND OPS TEST SERVICABLE. SKEW SENSOR PN: 5SDR CA111027001Actuator · leaking(CAN) HYD SYS 2 FAILURE. AS A PRECAUTION, CREW DECLARED EMERGENCY DUE LONG LANDING ROLL AND LIMITED STEERING ON INVESTIGATION FOUND NR 5 MFS BROKEN. LT NR 5 MFS REPLACED AMM 27-65-01.SDR CA111028002Flap System · failed(CAN) CREW ADVISED FLIGHT DISPATCH VIA THE ACARS OF A FLAP FAIL EICAS MESSAGE. DURING APPROACH, WHEN FLAPS WERE SELECTED THEY CONFIRMED A FLAP FAIL AND DECLARED AN EMERGENCY WITH ATC. QRH PROCEDURES CARRIED OUT. SF ACE 1 REPLACED IAW MM 27-53-02 FLAP OPERASDR CA111024001Actuator · malfunctioned(CAN) SLAT FAIL ON RETRACTION AFTER T/O QRH USED, NO FIX. CARRIED OUT INSPECTION OF SLAT ACTUATORS FOUND RT NR 2 TRIPPED. REPLACED ACTUATOR IAW AMM 27-81-01-04. RIGGING AND OPS CHECK SERV IAW AMM 27-81-01-05.
Back to GE CF34-10E5A1