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 CA130614007Unknown · odor(CAN) SIGNIFICANT FUME EVENT REPORTED BY FLIGHT CREW IN CLIMB. MOST NOTICEABLE IN FLIGHT DECK. LASTED APPROXIMATELY 2-3 MINUTES. ASR AND OHS FORMS WILL BE COMPLETED BY CREW. IAW FIM TASK 21-20-00-810-803A, ENGINES RAN AT HIGH POWER ON INDIVIDUAL BLEED SOURSDR CA130614008Control Panel · failed(CAN) CREW RECEIVED A FORWARD CARGO COMPARTMENT SMOKE DETECTED WARNING. THE C1 CARGO COMPARTMENT WAS EMPTY DUE TO A MEL ITEM FOR AN INOPERATIVE FIRE EXTINGUISHING SYSTEM. THE FLIGHT DECLARED A MAYDAY WITH ATC AND LANDED. RT ENGINE WAS SHUTDOWN AND THE TRUCKSDR CA130604006Seal · failed(CAN) ON CLIMB OUT RECEIVED BLEED 2 MESSAGE,BLEED 1 ALREADY ON MEL,DESCENDED FROM FL250, CABIN PRESSURE RETURNED TO NORMAL.AIR RETURN, NO EMERGENCY DESCENT,NO EMERGENCY DECLARED WITH ATC,NOT OVERWEIGHT FOR LANDING. DUE TO CAS MSG BLEED 2 LEAK AT LOCATION 14.7SDR CA130603010Flap System · failed(CAN) AT APPROX 10, 000FT CREW GOT AN EICAS MSG FOR FLAP/SLAT FAILURE. DECLARED A PAN PAN WITH ATC. ATC CHANGED ARRIVAL RWY TO 08R FOR AN INTO WIND APPROACH ON THE LONG RWY. EMERG TRUCKS WERE CALLED OUT AND WERE WAITING FOR AC565`S ARRIVAL. FLAPLESS LANDING WASDR CA130603009Deflector · failed(CAN) FLIGHT WAS IN CLIMB THRU A120 WHEN THE CREW HEARD A LOUD POP FROM THE L1 DOOR AND WERE UNABLE TO PRESSURIZE AFTER. CREW ELECTED TO DIVERT BACK TO STATION. REPLACED L1 DOOR DEFLECTOR AS PER AMM 52-11-28 PB401.SDR CA130531001Control Cable · mislocated(CAN) DURING B CHECK THE AILERON CABLE SYSTEM WAS MODIFIED AS PER REF/A/. FOLLOWING THE AIRFRAME VISIT, CABLE CONTACT WAS NOTED ON THE GROMMET AT THE WHEEL WELL, THE CABLE ORIENTATION WAS ALSO FOUND ROTATED APPROXIMATELY 90DEGREES FROM THE SB ILLUSTRATION. FOLSDR CA130507008Precooler · failed(CAN) FLIGHT DEPARTED UNDER MEL 36-00-00-A1, BLEED NR 1 INOPERATIVE. IN THE CLIMB AT FL240, THE CREW BEGAN EXPERIENCING TROUBLE WITH THE NR 2 BLEED. THE FLIGHT BEGAN DESCENDING AND THE QRH WAS FOLLOWED. THE CREW FELT THAT THE BLEED HAD STABILIZED AND BEGAN SDR CA130429006Acm · failed(CAN) APPLIED T/O POWER DEPARTING AT APPROXIMATELY 60KTS-70KTS THERE WAS VISIBLE WHITE SMOKE FROM FROM GASPERS, CREW REJECTED T/O. SMOKE CLEARED AFTER THE REJECT. ACFT WAS MET AND ESCORTED BACK TO GATE WITHOUT FURTHER INCIDENT. LT PACK REMOVED INSPECTED HSDR CA130429007Wire Harness · failed(CAN) SLAT FAIL AT 3000 FT ON APPROACH. PAN PAN DECLARED WITH ATC. LANDED WITHOUT INCIDENT. MAINTENANCE DUTY PILOT AND FLIGHT SAFETY HAVE BEEN ADVISED. IAW FIM 27-83-00-810-814 FOUND RT & LT OTBD SLAT SKEW HARNESSES INTERMITTENT. BOTH HARNESSES REPLACED ASDR CA130429009Vhf Comm · failed(CAN) ON CLIMBOUT, NR 1 COMM WAS LOST, AS WERE CAPTAIN`S ACP AND OVERHEAD SPEAKERS. CREW PULLED A CB FOR THE NR 1 RADIO TO ELIMINATE THE STATIC. THE CREW HAD CONSULT WITH MOC AND WERE CONTINUING ON WITH THE REMAINING 2 RADIOS. MORE COMMUNICATION PROBLEMS AROSDR CA130422003Pitot Tube · failed(CAN) REJECTED TAKE OFF AT APPROXIMATELY 100 KTS DUE TO AUTO THROTTLE ANNUNCIATION (RED), FUEL INDICATION NOT NORMAL AND SPEED DIFFERENCE. DUTY PILOT/FLIGHT SAFETY ADVISED. INTEGRATED PITOT/STATIC/AOA SENSOR NR 3 REPLACED IAW AMM 34-13-01, PB 401. CRITICAL SSDR CA130416019Fairlead · broken(CAN) THE MRO FOUND A FAIRLEAD BROKEN ON THE AILERON SYS IN FWD CARGO AFTER INVESTIGATION. FOUND WRONG FLANGE BUSHINGS INSTALLED AT INBD SIDE. BUSHINGS REPLACED IAW AMM 20-10-08, GOUGES PERMANENTLY REWORKED IAW PP ERJ190-54-49951.SDR CA130410012Starter · failed(CAN) AFTER THE PASSENGERS HAD BOARDED THE ACFT, DURING THE STARTING OR SLIGHTLY AFTER THE STARTING OF THE APU, A STATION ATTENDANT NOTICED SMOKE/FLAME COMING FROM THE AREA OF THE APU. THE SMOKE/FLAME WAS REPORTED TO THE CAPTAIN BY A STATION ATTENDANT AND THESDR Q0MF20130409003Blade · damagedAIRCRAFT B-16822 EXPERIENCED ENG NR 1 UNABLE TO ACCELERATE ACCOMPANIED ENG SURGE ABOUT TAKEOFF, THE CREW DECIDED TO ABORT TAKEOFF. THEN "ENG 1 FAIL" AND "ENG EXCEEDENCE" EICAS MESSAGE APPEARED DURING TAXIING BACK. MECHANIC PERFORMED ENG NR 1 INSPECTION FOUNDSDR CA130327001Deflector · failed(CAN) ON DEPARTURE ACFT WAS CLIMBING THRU 11750 FT WHEN CREW HEARD A LOUD BANG AND RUMBLING, UNABLE TO PRESSURIZE. CREW DESCENDED BACK DOWN BELOW 10000 FT AND DIVERTED BACK TO STATION. LANDED 1000 KGS OVERWEIGHT. CHANGED L1 DOOR DEFLECTOR FOR VIBRATION IAW SDR CA130326003Windshield · failed(CAN) AFTER DEPARTURE, IN THE VICINITY OF WAY POINT, THE CAPTAIN`S WINDSCREEN SHATTERED. THE CREW DECLINED A PHONE PATCH TO CONSULT WITH MAINTENANCE CONTROL AND ELECTED TO RETURN. THERE ACFT WAS NOT OVERWEIGHT. AN EMERGENCY WAS NOT DECLARED. THE DUTY PILOTSDR Q0MF20130322002Fadec · intermittentAIRCRAFT B-16828 EXPERIENCED NR 1 ENGINE FLAMEOUT DURING CLIMB, AT ALTITUDE 3500 FT. CARRIED OUT ENGINE FAILURE PROCEDURE AND AIRSTART SUCCESSFULLY. ACFT LANDED SAFELY. IAW ESM 73-00-00 REPLACED NR 1 ENGINE FADEC, PERFORMED ENGINE IDLE SPEED RUN UP FIVE TIMESDR CA130312003Seal · leaking(CAN) CLIMBING THROUGH FL210, CREW DETECTED A LOUD NOISE DESCRIBED AS SIMILAR TO A FLUSHING LAV BUT MUCH LOUDER. LEVELED THE AIRCRAFT AND DECLARED INTENT TO RETURN. DURING AIRSPEED OR AIRCRAFT CONFIGURATION CHANGES, THE CREW NOTICED A DIFFERENT SOUND. SOUSDR CA130304013Line · gouged(CAN) LT MAIN FUEL LINE ON TOP OF NR 1 ENGINE WAS REMOVED FOR ACCESS. UPON REMOVAL OF THE LINE THE FLANGE ATTACHING THE LINE TO THE FRONT SPAR WAS FOUND TO BE GOUGED. WHILE REMOVING THE FITTING FRON THE FRONT SPAR IT WAS FOUND THAT THE MAIN FUEL LINE IN THE WSDR CA130226001Detector · failed(CAN) SHORTLY AFTER TAKEOFF THE CREW REPORTED A BLEED LEAK, RT ENG BLEED INOPERATIVE AND RETURNED TO LAND. NO EMERGENCY WAS DECLARED RT PYLON ODS DETECTORS CH 1 AND CH 2 REPLACED IAW AMM 36-21-02-04. CHECKS SERVICEABLE.SDR CA130225014Sensor · failed(CAN) AFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. RETURNED AND LANDED OVERWEIGHT BY 500KG, 44.5, NLG WOW 2 SENSOR REPLACED IAW AMM 32-62-01/401. HARNESS OF NLG WOW 2 & STEERING FEEDBACK REPLACED IAW WMM 32-62-50. ACFT JACKED IAW AMM 07-10-01. ACFT GESDR CA130905010Fairing · missing(CAN) ON ARRIVAL HAD THE "FWD PYLON FAIRING ASSY" MISSING ON THE NR 1 ENGINE. 5 OF THE 7 SCREWS WERE STILL IN THEIR PRESENT LOCATION. NO OTHER DAMAGE TO ACFT WAS FOUND. A NEW PANEL WAS INSTALLED. IN ORDER TO MAKE A COMPARISON, AN INSPECTION WAS CARRIED OUT SDR CA130206003Wire Harness · failed(CAN) THE FLIGHT CREW ENCOUNTERED A SLAT FAIL MESSAGE ON APPROACH. THIS RESULTED IN A FLAP 2, SLAT ZERO LANDING CONFIGURATION. A PAN PAN WAS DECLARED AS A PRECAUTION FOR PRIORITY AND POSSIBLE HOT BRAKES. ON ARRIVAL. AFTER LANDING RUNWAY 23, THE ACFT WAS MET SDR CA130204013Bolt · loose(CAN) RIGHT MLG SIDE STAY BOLT ASSY NUT, LOCK RING AND KNURLED RING LOOSE DUE TO LOSS OF TORQUE. REF CMM 32-11-14, FIGURE 6, ITEMS 320, 330, 300. SIDE STAY BOLT ASSY NUT TORQUED IAW CMM 32-11-14. LOCKING RING INSTALLED, SEALANT APPLIED.SDR R61A201301180061Spinner · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE RIGHT ENGINE SPINNER CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE SPINNER IAW GE 34-10E MM 72-00-00 AND SB 72-0201. THE AIRCRAFT IS OUT OF SERVICE IN HEAVY CHECK.SDR CA130204012Retaining Ring · missing(CAN) RIGHT MLG SIDE STAY BOLT ASSY LOCK RING, SPRING RING AND RETAINING RING MISSING. PN`S 2821-0059, 2000A0764K01, M27426-1147D, REQUIRED, REF CMM 32-11-14. SUBTASK 32-11-14-440-053-A01. RIGHT MLG SIDE STAY BOLT ASSY RETAINING RING INSTALLED IAW TASK 32-11-SDR CA130114011Windshield · failed(CAN) CAPTAIN`S WINDSHIELD OUTER PANE CRACKED DURING FLIGHT AFTER HEATER ELEMENT BURNED, DESCENDED TO FL 300 AND CONTINUE. MAINTENANCE ADVISED. R & R LT WINDSHIELD IAW AMM 56-11-00 PB401, CONF 1, REF PP ERJ190-56-49133 FOR PERMANENT DISPOSITION/APPROVAL TO USDR CA121214002Unknown · fumes(CAN) A STRONG SMELL OF RAW KEROSENE PERMEATED THROUGH THE FLIGHT DECK AND CABIN AFTER BOARDING FLIGHT. CAPTAIN DEPLANED PASSENGERS AS A PRECAUTION ALLOWING MAINTENANCE TIME TO INVESTIGATE THE ROOT SOURCE OF FUEL SMELL. THE F/O AND THE S/D COMPLAINED OF HEADSDR CA121210005Actuator · leaking(CAN) WHILE AT GATE WITH PASSENGER ONBOARD FUEL LEAK COMING FROM THE NR 1 ENGINE WAS DISCOVERED. SPILL SIZE AT CURRENT 3FT X 2FT. CRF WAS CALLED ALONG WITH GTAA. ALL PASSENGERS WERE DEPLANED. GROUND RUN CARRIED OUT. FOUND ZERO FUEL LEAK FROM MAST BOTH RUNNSDR CA121210003Valve · leaking(CAN) ON ENGINE START DURING PUSHBACK NR 2 ENGINE BEGAN LEAKING FUEL, COVERING AN AREA 3FT X 5 FT. CFR ON SITE. FLIGHT RETURNED TO GATE FOR ACFT CHANGE. REMOVED BY AC 084275 AND INSTALLED BY AC 063344 IAW AMM 75-23-02.SDR CA121210004Tiller · failed(CAN) ON ARRIVAL, THE CREW REPORTED A NOSE GEAR STEERING FAIL AND WERE TOWED TO THE GATE. REPLACED STEERING HANDWHEEL IAW AMM 32-53-05, MR BY AC17719 I/C BY AC 17846 , AND REPLACED LT RUDDER PEDAL RVDT IAW AMM 32-53-03, MR BY AC18365 I/C BY AC17846.SDR CA121204007Anti-Ice System · failed(CAN) 1 & 2 ENGINE ANTI-ICE FAIL EICAS MESSAGE AFTER T/O 1500` AGL. ENGINE TAI SYSTEM TESTED IAW AMM 30-21-00-710-801A NIL FAULTS. ACFT RELEASED FOR SERVICE IAW TECH SUPPORT AND MOC CONCURANCE.SDR CA121105026Sink · smoke(CAN) FLIGHT ATTENDANTS NOTICED SMOKE COMING OUT OF THE SINK IN THE LAV, AFTER PUSH. FLIGHT RETURNED TO THE GATE FOR INSPECTION AND WAS CLEARED BY MTC. ON RETURN ACA303, FLIGHT ATTENDANTS FELT NAUSEOUS, AND COMPLAINED ABOUT CONDITIONS. ONE OF THE F/A`S BOOKED SDR CA121019010Mau · failed(CAN) ON DEPARTURE THE CREW RECEIVED A FUEL FEED FAULT EICAS MESSAGE. AFTER CONSULTATION WITH MOC THE ACFT RETURNED TO STATION AND LANDED UNEVENTFULLY. THIS WAS THE SECOND SUCH AIR TURNBACK FOR THIS INDICATION, THE PREVIOUS HAVING OCCURRED ON 14 OCT. CHECKSDR CA121012015Valve · failed(CAN) BLEED FAIL ON APPROACH , GO-AROUND INITIATED, PERFORMED QRH PROCEDURE AND SUBSEQUENT LANDING OK HP VALVE REPLACED IAW AMM 36-11-01 NR 1 BLEED CHECKS SERVICEABLE FAN COWLS CLOSED.SDR CA121005003Filter · contaminated(CAN) WHEN THE CREW APPLIED TAKEOFF THRUST THERE WAS A PUFF OF SMOKE IN THE COCKPIT AND THE CABIN. THRUST WAS REDUCED AT LESS THAN 10KTS AND THE SMOKE DISSIPATED. NO EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO THE GATE FOR INVESTIGATION. BOTH RECIRC SDR CA121005002Clamp · loose(CAN) FLT WAS OPERATING WITH BLEED 1 INOPERATIVE UNDER MEL. AT TOP OF CLIMB 27,000 FT CREW RECEIVED A BLEED 2 LEAK MESSAGE. DUE BLEED 2 LEAK MESSAGE CREW WAS REQUIRED TO SHUTDOWN BLEED 2. CREW DESCENDED TO 10,000 FT AND SHUTDOWN, BLEED 2. FLT CONTINUED TO SDR CA120925001Windshield · failed(CAN) AT 5000 FT ON APPROACH THE CAPTAIN`S FRONT WINDSCREEN SHATTERED. THE CAPTAIN DECLARED A PAN PAN AND THE FLT LANDED WITHOUT FURTHER INCIDENT, SAFETY VEHICLES MEET THE ACFT JUST OFF THE RWY AND AFTER A QUICK VISUAL INSPECTION THE FLT TAXIED TO THE GATE. TSDR CA120824002Deflector · damaged(CAN) AFTER FLIGHT WENT AIRBORNE, LOUD NOISE HEARD IN CABIN. FLIGHT DECLARED A PAN PAN AND RETURNED, WHERE THEY WERE MET BY ARFF. THE FLIGHT LANDED APPROXIMATELY 2400KG OVERWEIGHT. INITIAL INVESTIGATION INDICATES FLAP CONTOUR ON OUTSIDE L1 CABIN DOOR APPEARSDR CA120824006Bleed Air Sys · failed(CAN) BLEED 1 WAS ON MEL AND INOPERATIVE, CLIMBING THROUGH 21,500 FT THE CREW RECEIVED EICAS MESSAGE BLEED NR 2 LEAK. QRH PROCEDURES CARRIED OUT. PAN PAN DECLARED WITH ATC REQUESTING IMMEDIATE DESCENT CLEARANCE AND INITIATED RAPID DESCENT TO 9000 FT. RETURNESDR CA120822012Controller · intermittent(CAN) FLIGHT WAS AT FL370 ENROUTE, FLIGHT-CREW RECOGNIZED RISE IN CABIN PRESSURE ALTITUDE, EMERGENCY DECENT PERFORMED.CREW DONNED O2 MASKS, MASKS DID NOT FALL IN THEN CABIN. PASSENGER REACTION WAS MINIMAL. LANDED WITH NO ISSUE. MAINTENANCE INVESTIGATING. MSDR CA120807002Brake · failed(CAN) ON ARRIVAL RAMP CREW ADVISED THAT THEY SAW PARTS FALL OFF AS ACFT WAS PULLING INTO GATE 24A. RIGHT OTBD TIRE BRAKE NR 4 SUPPORT BRACKET. FOUND 3 PIECES ON RAMP. FIXED. NR 4 BRAKE ASSY REPLACED IAW AMM 32-49-11. REMOVED PN 90002340-2PR, SN AUG07-08SDR CA120807004Valve · failed(CAN) FLIGHT WAS DISPATCHED WITH MEL 36-11-09A LT BLEED AIR FAN VALVE OPEN WHICH INCURS 36-00-00-A1 BLEED 1 INOPERATIVE. ENROUTE, FLIGHT EXPERIENCED A BLEED 2 LEAK WHICH RESULTED IN LOSS OF PRESSURIZATION. THE FLIGHT DECLARED AN EMERGENCY AND DESCENDED TO 90SDR CA120803002Actuator · defective(CAN) ON APPROACH EICAS, FLAP FAIL, MESSAGE WHEN FLAPS SELECTED FROM 1 TO 2. TOUCHDOWN SPEED 175 KTS RATE OF DESCENT APPROXIMATELY 300 FPM AT TOUCHDOWN. LT NR 3 FLAP ACTUATOR REPLACED IAW AMM 27-51-01.SDR CA120726005Tailpipe · fire(CAN) CREW REPORT FIRE IN TAIL PIPE ON ARRIVAL.SDR CA120726002Precooler · leaking(CAN) BLEED 1 WAS CURRENTLY UNDER MEL. ONCE AIRBORNE PACK 2 SHOWED LEAKING AND FAILED INTERMITTENTLY, CABIN ALTITUDE INCREASED. FLIGHT DESCENDED TO 10,000 FT, AND RETURNED. NO EMERGENCY WAS DECLARED. INSPECTED ENGINE BLEED DUCTS AND OVERHEAT LOOPS IN PYLONSDR CA120712003Indication Sys · malfunctioned(CAN) ON APPROACH HAD TO DO A GO AROUND DUE FLAP INDICATION PROBLEM, NO ISSUES ON SECOND APPROACH, ALL SYSTEMS NORMAL. ON LANDING AFTER SELECTING FLAP 3 TO 5, EICAS MESSAGE GROUND PROXIMITY FAIL + TERRAIN INHIBIT AMBER FLAP + AMBER 3, AFTER GO AROUND AND FLAPSDR CA120711002Pump · failed(CAN) THE FLIGHT CREW DECLARED AN EMERGENCY LANDING IN YOW, DUE TO A NUMBER 1 (ONE) HYDRAULIC SYSTEM FAILURE. THE FLIGHT LANDED WITHOUT INCIDENT AND WAS ABLE TO TAXI NORMALLY TO THE ARRIVAL GATE. LEVEL FL400 "HYD 1 LOW QTY" MSG. QUANTITY WAS "0". SYSTEM PRESSDR CA120704010Engine · shutdown(CAN) DURING TAXI THE CREW REPORTED THE RT ENGINE SHUTDOWN. THE FLIGHT RETURNED TO THE GATE.SDR CA120905014Line · chafed(CAN) ACFT RECEIVED A, HYD 1 LO QTY, EICAS MESSAGE WHILE APPROACHING GATE. A HYDRAULIC LEAK WAS DISCOVERED FLOWING FROM THE LT ENGINE UPPER PYLON. THE LEAK WAS INVESTIGATED AND FOUND A CHAFED HYDRAULIC LINE, STARTING MID PYLON
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