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 CA110323003Controller · malfunctioned(CAN) EN-ROUTE, THE ACFT EXPERIENCED A NR 1 BLEED LEAK. THE ACFT DESENDED TO FL200. IN CONSULTATION WITH FLIGHT DISPATCH, THE FLIGHT PLAN WAS RECALCULATED WITH THE ACFT BEING ABLE TO CONTINUE ONTO ORIGINAL STATION. FAULT CODE 36215007AM1 FOUND. PERFORMED TSSDR CA110316001Sensor · malfunctioned(CAN) AFTER TAKEOFF, THE FLIGHT CREW WERE UNABLE TO RAISE THE LG. AFTER SEVERAL ATTEMPTS, WHILE RUNNING THROUGH THE CHECKLIST, THE FLIGHT CREW WERE CONSIDERING A RETURN TO POINT OF DEPARTURE. ANOTHER ATTEMPT WAS SUCCESSFUL & ALL INDICATIONS WERE NORMAL. THESDR CA110316002Sensor · failed(CAN) THE FLIGHT CREW ENCOUNTERED A SLAT FAIL EICAS MSG. AFTER FOLLOWING THE QRH & IN CONSULTATION WITH MX, THE FLIGHT CONTINUED TO DESTINATION & LANDED WITH NIL FLAPS. THE LANDING WAS OTHERWISE ROUTINE. AN EMER WAS DECLARED AS A PRECAUTION & CFR DID PERFORSDR CA110315001Sensor · failed(CAN) THE FLIGHT CREW ENCOUNTERED A SLAT FAILURE ON APPROACH. AN EMERGENCY WAS DECLARED AS A PRECAUTION. THE LANDING WAS OTHERWISE ROUTINE AND THERE WAS NIL ADVERSE PASSENGER REACTION. REPLACED RH 2-3 SLAT SKEW SENSOR AND RH 3-4 SLAT SKEW SENSOR AS PER AMM 27SDR CA110310005Sensor · failed(CAN) FLAP/SLAT FAIL ON APPROACH, UNABLE TO SELECT FLAPS FULL. PAN PAN DECLARED WITH ATC, RETRACTED FLAPS AND INITIATED GO-AROUND FOUND RT FAILURE OF SKEW SENSOR S2/3. RT SKEW SENSOR REPLACED. AMM 27-83-01/401, GROUND CHECKED SERVICEABLE.SDR CA110217004Unknown · odor(CAN) EN ROUTE, THE F/A NOTICED A STRONG ODOR OF SMOKE. FWD GALLEY POWER WAS SHUT OFF AND THE ODOR DISSIPATED. MX WAS ADVISED.SDR CA110207001Shutoff Valve · failed(CAN) AFTER TAKE OFF, THE AIRCRAFT EXPERIENCE A COMPLETE LOSS OF THE AIRCRAFT ANTI ICING SYSTEM. AN ATTEMPT TO RESET THE SYSTEM WAS UNSUCCESSFUL AND RESULTED IN THE AIRCRAFT RETURNING TO POINT OF DEPARTURE. PRSOV REPLACED PER 36-11-03-04 TESTED PER 36-00-SDR CA110118003Door · misriggedAIR RETURN DUE TO DOOR INDICATION, UNABLE TO CLEAR MSG OR CONFIRM DOOR CLOSED. DEFERRED IAW MEL. DOOR RIGGING CHECK CARRIED OUT IAW AMM 52-11-00, AFT DOOR STOPS ADJUSTED. ACFT PRESSURIZED TO 4.3 PSID ON GRD IND. NORMAL MEL REMOVED.SDR CA110103005Steering Sys · failedON GEAR EXTENSION DURING APPROACH, THE CREW RECEIVED A STEER FAIR MESSAGE. DIFFERENTIAL STEERING USED ON LANDING AND SUCCESSFULL RESET CARRIED OUT AFTER CLEARING THE ACTIVE RUNWAY.SDR CA110103003Wire Harness · failedON APPROACH, WHEN FLAPS WERE SELECTED, A SLAT FAILURE OCCURRED. THE FLIGHT CONTINUED DOWNWIND AND COMPLETED THE QRH. THE LANDING WAS CARRIED OUT IN A FLAP 2/SLAT 3 CONFIGURATION. ERS VEHICLES WERE CALLED OUT BUT AN EMERGENCY WAS NOT DECLARED. THERE WAS NO SDR CA101224003Brake · seized(CAN) NR 3 BRAKE UNIT SEIZED CAUSING TIRE FAILURE ON ARRIVAL. MTC ADVISED. NR 3 BRAKE REPLACED NR 3 & 4 TIRES REPLACED PER AMM. REMOVED BRAKE, & MAIN WHEEL ASSY.SDR CA101224002Wire · burned(CAN) DURING CRUISE THE F/A REPORTED TO THE CAPTAIN A BURNING SMELL IN THE AFT GALLEY AREA. ELECTRICAL POWER WAS REMOVED FROM THE GALLEY AND THE SMELL DISSAPATED. CMC INTERROGATED REAR GALLEY POWER RESTORED BOTH COFFEE MAKERS TURNED ON OVEN TURNED ON BOTH PSDR CA101129002Door · unsecureTHE FLIGHT CREW RECEIVED AN OVERWING EXIT DOOR INDICATION MESSAGE AFTER GETTING AIRBORNE. THE AIRCRAFT WAS RETURNED TO POINT OF DEPARTURE AND MET BY MAINTENANCE. FOUND LT EMERGENCY EXIT DOOR NOT STOWED PROPERLY. EXIT DOOR HANDLE RE-STOWED. INDICATION MSG CSDR CA101129001Drive Shaft · disconnectedSHORTLY AFTER TAKEOFF THE CREW REPORTED A SLAT FAIL MESSAGE. DUE TO ALTITUDE AND SPEED LIMITATIONS WITH SLAT EXTENDED THE FLIGHT WAS UNABLE TO CONTINUE TO DESTINATION AND MADE A DIVERSION. FOUND DRIVE SHAFT DISCONNECTED AT NR 1 LT SLAT ACTUATOR. SHAFT RECONSDR CA101129005Bearing · deterioratedMAIN GEAR RETRACT ACTUATOR HAVE A DEFECT IN DESIGN OR CONSTRUCTION THAT OVER A SHORT TIME ALLOWS THE EYE END BEARING AND ATTACH BOLT TO HAVE INDICATIONS OF IMMINENT FAILURE. EYE END BEARING RACES ARE FOUND SPLIT, THE BEARINGS HAVE MIGRATED OUT OF THE EYE END,SDR CA101122011Check Valve · failed(CAN) AFTER DEPARTURE, THE LANDING GEAR FAILED TO RETRACT, FLIGHT RETURNED TO POINT OF DEPARTURE, LANDING WEIGHT 43,800 KGS. REPLACED CHECK VALVE IN RETURN LINE AT SELECTOR VALVE PER AMM 32-33-02-04, P/N 170-70900-401, MFR: EMBRAER. REPLACE NOSE UPLOCK BOX PSDR CA101122025Door · bindingR2-L2 DISARMING DOOR VERY DIFFICULT. C4678657 CHECKED OK ON GROUND.SDR CA101119006Wire Harness · failed(CAN) THE FLT EXPERIENCED SLAT 3 FLAP 2 SNAG DURING DESCENT. EMERGENCY VEHICLES DISPATCHED AS A PRECAUTION. TOW CREW ON STD BY. LANDED WITHOUT INCIDENT AND TAXIED UNDER ITS` OWN POWER TO GATE. ALL PAX AND CREW OK. PAX REACTION GOOD. AIRCRAFT REMOVED FROMSDR CA101122027Handle · frozenDOORS L2 AND R2 WERE DIFFICULT TO DISARM ON ARRIVAL. DOORS L2 AND R2 FUNCTIONED FOUND SERVICEABLE BY MAINTENANCE.SDR CA101122026Lever · frozenR1 DOOR COULD NOT DISARM AT ARRIVAL. DOOR FLAP FREED BY MAINTENANCE.SDR CA101116002Actuator · failed(CAN) ON APPROACH TO SFO THE NOSE GEAR FAILED TO EXTEND. SUCCESSFUL EXTENSION ON 2ND ATTEMPT. NO GO AROUND AND NO EMERGENCY DECLARED. NLG RETRACTION ACTUATOR REPLACED AS PER MM 32-32-01. NLG UPLOCK AND 2 HYD SYS BLED AS PER MM 29-70-00. LANDING GEAR EXTENSDR CA101115009Gear · failed(CAN) ON APPROACH TO LAND, THE CREW RECEIVED A NOSE GEAR NOT EXTENDED INDICATION AND PERFORMED A GO AROUND. AFTER THREE ATTEMPTS THE NOSE GEAR EXTENDED PROPERLY AND THE FLIGHT LANDED WITHOUT FURTHER COMPLICATION. LANDING GEAR EXTENDED AND RETRACTED NUMEROUS TSDR CA101108002Switch · malfunctioned(CAN) ON DEPARTURE, THE FLIGHT EXPERIENCE A "WEIGHT ON WHEELS" PROBLEM AND THE NOSE GEAR DOOR DIDN`T CLOSE. THE QRH CHECKLIST WAS FOLLOWED, SUBSEQUENT LG LEVER DISAGREE MESSAGE. THE FLIGHT RETURNED TO POINT OF DEPARTURE WITHOUT FURTHER INCIDENT. NLG SERVICESDR CA101104009Torque Tube · disconnected(CAN) AFTER DEPARTURE HAD SLAT FAIL MESSAGE. WE RAN QRH CHECKLIST AND RETURNED TO YYC. FOUND RT SLAT DRIVELINE MECH DISCONNECTED AT RT NR 5 SLAT ACTUATOR. CARRIED OUT FIM 27-81-00-810-801-A AND RE-CONNECTED TORQUE TUBE AS PER AMM 27-81-03/401. SLAT CONTROLSDR CA101102002Starter · failed(CAN) AFTER PUSH BACK, THE RAMP CREW REPORTED SPARKS AND GRINDING DURING THE NUMBER ONE ENGINE START. THE ENGINE START WAS ABORTED AND MAINTENANCE WERE CALLED TO PERFORM AN INSPECTION. CFR WAS ALSO CALLED OUT AS A PRECAUTION. FOUND STARTER DAMAGED. NR 1 ENG SDR CA101027009Strut · flakingNLG STRUT HAS AN 2.5" X 1.5" AREA WHERE CHROME APPEARS TO BE COMING OFF IN NUMEROUS SMALL FLAKES ON LT SIDE OF STRUT AT GLAND NUT.SDR CA100927013Engine · failedFLIGHT CREW REPORTED ON TOP OF DESCENT NR 2 ENG LP VIBRATION WAS INDICATING 4.0 UNITS. THE REST OF THE ENGINE PARAMETERS WERE INDICATING NORMALLY. ON THE GROUND DURING VISUAL INSP THE LAST STAGE TURBINE FOUND SEVERALLY DAMAGED. FOD COULD BE THE CAUSE OF THE SDR CA100929005Screw · undertorquedDURING B02 CK, WHILE PERFORMING J/C SP3-024 FOR WINDSHIELD FASTENER TORQUE FOUND 13 LOOSE FASTENERS. SCREWS ALL RETORQUED IAW AMM 56-11-00-04.SDR CA100920006Oven · smokeSMOKE REPORTED FROM GALLEY OVEN AFTER DEPARTURE. OVEN TURNED OFF. SMOKE DISSIPATED CLEANED AFT GALLEY OVEN. RAN FOR 10 MINUTES NO SMOKE DETECTED. OPS OK.SDR CA100920003Sensor · failedINSIDE THE MARKER LANDING R26R, CREW RECEIVED EICAS MESSAGE STEERING FAIL, ATC WAS ADVISED AND CREW USED HIGH SPEED EXIT OFF RUNWAY AND WERE TOWED TO THE GATE. REPLACED NR 2 STEERING FEEDBACK SENSOR IAW AMM 32-53-09, PB 401. TESTS OK. IND CHECK.SDR CA100922007Screw · undertorquedDURING B01 CK WHILE PERFORMING J/C SP3-024 FOR TORQUE CHECK ON COCKPIT WINDSCREEN FASTENERS FOUND: LT WINDSHIELD TO HAVE 62 OF 83 SCREWS UNDER MINIMUM TORQUE VALUE, AND RT WINDSHIELD TO HAVE 65 OF 83 SCREWS UNDER MINIMUM TORQUE VALUE. ALL SCREWS RETORQUED SDR CA100913006Shutoff Valve · failedWHILE IN THE CLIMB THE ACFT HAD A SECOND BLEED FAILURE WHILE THERE WAS ALREADY ANOTHER BLEED INOP AND UNDER MEL. MOC AND THE CREW DISCUSSED A POSSIBLE ENROUTE FIX WITHOUT ANY SUCCESS . THE FLIGHT RETURNED TO LAND AT POINT OF DEPARTURE. LT ENG HPSOV REPLACEDSDR CA100824001Slat System · failedAFTER DEPARTURE, THE FLIGHT CREW ENCOUNTERED A SLAT FAILURE AT 1000 FT AGL. THE SNAG WAS NOT RESOLVED, THEREFORE THE ACFT RETURNED TO POINT OF DEPARTURE. T/S IAW FIM 27-81-00-810-805-A, STEP 1, SF-ACE CLEAR INHIBITS PROCEDURE CARRIED OUT. RESET SUCCESSFUL. (SDR CA100914008Bearing · disintegratedRT OTBD BRAKE STICKING ON TAXI. TEMPS 17/16/16/386. RT BRAKE FAULT. FURTHER INVESIGATION FOUND THAT THE MAIN WHEEL INBD BRG HAD FAILED. THE AXLE WAS SEVERELY DAMAGED AND DISTORTED, REQUIRING SHOCK STRUT REPLACEMENT.SDR CA100820003Wire Harness · chafed(CAN) THE W7 (WHITE) HARNESS PART NUMBER 2043M27P02 LOCATED ON THE CORE AREA OF THE CF34-10E ENGINES OF THE ERJ-190 HAVE BEEN FOUND TO BE CHAFING ON FUEL LINES RUBBING THROUGH THE PEAK, METALIC BRAID AND WIRING ON MULTIPLE AIRCRAFT. SPECIFICALLY THE DAMAGE HASDR CA100812005Fastener · looseDURING A/C 315 N01 CHECK WHILE PERFORMING J/C SP3-024 FOR TORQUE CHECK ON COCKPIT WINDSCREEN FASTENERS FOUND: LT: 44 FASTENERS FOUND LOOSE, 6-ANCHOR NUTS SPINNING RT: 52 FASTENERS FOUND LOOSE: ALL 21 CENTER SCREWS 1/4 TO 3/4 TURN LOOSE.SDR CA100730005Actuator · leakingON INBOUND TAXI ALL HYD PRESSURE AND FLUID WAS LOST FROM SYS 2. INVESTIGATION FOUND THE LEAK AT THE LT OTBD MULTIFUNCTION SPOILER ACTUATOR. 2 OF THE 4 BOLTS AT THE FLANGE HAD SHEARED AND CAUSED THE LEAK. LT NR 5 MFS PCU REPLACED IAW AMM 27-65-01, PN 414800-SDR CA100730004Diffuser · leakingAPPROX 90MINUTES INTO THE FLIGHT THE CREW REPORTED A SUSPECTED FUEL LEAK AND DIVERTED. THE ACFT WAS APPROX 1500KG OVERWEIGHT AT LANDING. REPLACED RT WING DIFFUSER IAW AMM 20-10-13-04. REPLACED LT WING FLOAT VENT VALVE IAW AMM28-12-05. DIFFUSER PN 170-09961SDR CA100719003Slat System · failedTHE ACFT ENCOUNTERED A SLAT FAILURE ON APPROACH. MX HAS BEEN ADVISED.SDR CA100812011Fastener · loose(CAN) ACFT 311, DURING N01 CHECK WHILE PERFORMING J/C SP3-024: UPON INSP OF WINDSHIELD TORQUE VALUE 25 SCREWS FOUND LOOSE ON THE RT AND 1 ON THE LT SCREWS WERE RETORQUED. ACFT HAD A SIMILIAR OCCURRENCE IN 2008-02-13, FOUND 27 LOOSE SCREWS M1325184.SDR CA100713013Blade · damaged(CAN) ON ARRIVAL SERVICE CHECK FOUND NR 1 ENGINE LPT BLADE MISSING 3/4 OF A BLADE WITH CONSIDERABLE DAMAGE TO ADJACENT BLADES AND AFT SIDE OF GUIDE VANES.SDR CA100812008Screw · looseDURING NR 1 CHECK WHILE PERFORMING J/C SP3-024 FOR TORQUE CHECK ON COCKPIT WINDSHIELD FASTENERS FOUND: F/O`S WINSHIELD RETAINERS ARE BELOW MINIMUM TORQUE VALUES AT LOCATIONS 1,3,7,9,26,30,43,46,48,50,52,54,56,62,63,64,66,72,74,76, 77,78,81,83 CAPT`S WINDSHIELSDR CA100812010Screw · looseDURING NR 1 CHECK WHILE PERFORMING J/C SP3-024 FOR TORQUE CHECK ON COCKPIT WINSCREEN FASTENERS RT WINDSHIELD SCREWS FOUND BELOW RECOMMENDED TORQUE VALUES.SDR CA100614006Rod · gougedLT COCKPIT, SIDE DIRECT VISION SLIDING WINDOW, LWR ACTUATION ROD, PN B755410-104, WAS REMOVED FROM ACFT UNSERVICEABLE DUE TO DEEP GOUGING MARKS FOUND ON ROD BARREL. INSP OF LT AND RT WINDOW SHROUDS, LOWER AFT ATTACH BRACKETS (PN 170-12309-401) SHROUD ATTACH SSDR CA100601003Engine · power loss(CAN) AT FL 380, ENG NR 2 ROLLED BACK FOR 15 SECONDS, AND THEN AUTO RELIGHT. AT -55C. ANTI ICE WAS OFF FOR ROLLBACK. PILOT ACTION WAS ANTI ICE MODE SELECTOR ON. ACFT WAS CLOSE TO A THUNDER CELL IN IMC CONDITIONS. ENG NR 2 VIBS 0.1 LP, 0.2 HP BLEED AIR ALL SDR CA100812012Fastener · looseDURING NR 1 CHECK WHILE PERFORMING J/C SP3-024 FOR TORQUE CHECK ON COCKPIT WINDSHIELD FASTENERS, FOUND LOOSE (UNDERTORQUED) FASTENERS AT THE FOLLOWING LOCATIONS: LT: 0,41,75,78,80, RT: 60,74,78 REPEAT 2007-11-19 RETORQUED WINDSHIELD L4379049.SDR CA100812009Screw · looseDURING N01 CHECK WHILE PERFORMING J/C SP3-024 FOR TORQUE CHECK ON COCKPIT WINDSCREEN FASTENERS FOUND LOOSE SCREWS (UNDERTORQUED) IN THE FOLLOWING LOCATIONS: LT: 3,7,13,46,48,50,52,54,56,60,64,68,72,74,76,78,80. REPEAT FINDINGS. (SEE PREVIOUS SDRS 2010072219SDR CA100526003Hydraulic System · leakingACFT ENCOUNTERED A HYD SYS 1 FAILURE AFTER DEPARTURE. FLIGHT DID AN AIR TURNBACK. ATC HAD CFR ON STANDBY FOR ARRIVAL. FOUND THAT NR1 HYD QTY DROPPED TO ZERO, FOLLOWED BY PRESSURE DROP TO ZERO PSI. L3 MULTIFUNCTION SPOILER WAS LEAKING. REPLACED LT L3 MFS IASDR CA100812013Fastener · looseDURING NR 1 CHECK, WHILE PERFORMING J/C SP3-024 FOR TORQUE CHECK ON WINDSHIELD FASTENERS FOUND FASTENERS LOOSE (UNDERTORQUED).SDR CA100812007Screw · looseDURING NR 1 CHECK WHILE PERFORMING J/C SP3-024 FOR TORQUE CHECK ON COCKPIT WINDSCREEN FASTENERS FOUND SCREWS LOOSE (UNDERTORQUED) AT THE FOLLOWING LOCATIONS: LT: 76, 80, RT: 48,70,74,78,80. REPEAT FINDING, (SEE PREVIOUS SDRS FOR SAME ISSUE: 20100722003, 20100
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