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 CA111024007Duct · burned(CAN) DURING THE INSTALLATION OF CEILING PANEL 227CLC, THE EXPOSED WIRING CONTACTS ON THE PANEL ORDINANCE LIGHT CONTACTED THE WIRE REINFORCING ON THE AIR CONDITIONING DUCT IMMEDIATELY ABOVE THE PANEL. WHEN THE PANEL WAS ELECTRICALLY CONNECTED THE WIRING SHORTSDR CA111018008Cartridge · leaking(CAN) UPON DISCONNECTING THE CONNECTOR PLUG OF THE NR 1 AC AUX BOOST PUMP, THE AVIONICS TECH NOTICED THAT FUEL WAS EVIDENT IN THE FEMALE CONNECTOR AND ON THE MALE CONNECTOR. THE TECH CLEANED OFF BOTH CONNECTORS OF ALL FUEL UNTIL DRY, AND THEN RE-CONNECTED THE SDR CA111026012Bonding Strap · interference(CAN) ON TAXI OUT, INITIAL TEST OF AILERONS WAS UNUSALLY STIFF IN BOTH DIRECTIONS. NO BINDING FELT. SUBSEQUENT MOVEMENTS FELT NORMAL AND ACFT DEPARTED WITH NO FURTHER ISSUES. THIS BINDING FAULT OCCURRED ON 3 SEPARATE LOGS. ON ALL 3 NO FAULT REALLY FOUND. SDR CA111003005Sensor · failed(CAN) SLAT FAIL EICAS MESSAGE WHEN FLAP 1 SELECTED FOR LANDING. FLAPS SELECTED UP AND BACK TO POSSITION 1 IAW QRH PROCEDURE, NO FIX. EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. REPLACED OTBD SKEW AT SLAT 3-4 IAW AMM 27-83-01, CHECK SERV.SDR CA110930008Autopilot Sys · failed(CAN) FLIGHT CREW REPORTED AN AUTO-PILOT FAILURE ON DESCENT. AFTER ATTEMPTING TO RECYCLE THE AP THE FLIGHT EXPERIENCED SOME PITCH OSCILLATION WHICH NECESSITATED TURNING OFF THE AP. IAW SNL-22-0009 INTERIM SOLUTION COMPLETED FIM TASK 22-11-00-810-91T-A AND 22SDR CA110908006Landing Gear · failed(CAN) ON APPROACH, WHEN LANDING GEAR WAS SELECTED DOWN, RT MAIN GEAR DID NOT SHOW A GREEN INDICATION. YELLOW X IN RT MAIN INDICATION. CYAN"BRAKE FAULT" MESSAGE. RED "LG LEVER DISAG" MESSAGE. PERFORMED A GO-AROUND. ALL GEAR INDICATIONS WENT GREEN.LANDING NSDR CA111118012Skin · cracked(CAN) DURING ACFT STRUCTURE FULL-SCALE FATIGUE TESTS, CRACKS HAVE BEEN DETECTED IN THE REAR FUSELAGE UPPER SKIN NEAR FRAME 94 AND FRAME 97 IN STR 3LT/RT. REPAIRS DONE IAW AVAILABLE SBS.SDR CA110908004Blade · damaged(CAN) DURING NR 1 ENG INSPECTION DUE FMR/CMR FOUND 1 LPT BLADE MISSING AND SEVERAL DAMAGED.SDR CA110922004Sign · shorted(CAN) PAX SIGN, CB E13 POPPED BEFORE DEPARTURE. (PASSENGER SIGNS - OPTION 2) THE WIRE REINFORCEMENT THAT IS PART OF THE DUCTING HAS BECOME EXPOSED AND SHORTED THE ORDINANCE SIGN TERMINALS LOCATED ABOVE IT. THE ORDINANCE SIGN CONTACTS ARE NORMALLY EXPOSED. FSDR CA110822001Control Module · failed(CAN) DURING CRUISE THE CREW REPORTED A SPOILER FAULT WHICH THEY COULD NOT RESET USING QRH PROCEDURE. CREW DECLARED AN EMERGENCY ON LANDING. FOLLOWING FIM`S 45-45-00-810-899-A00, 27-03-00-810-92E-A00, FOUND FCM4 FAULTED, REPLACED FCM4 IAW AMM 27-03-02 CHECKSDR CA110822003Oven · odor(CAN) CABIN CREW REPORTED A BURNING ODOR IN THE AFT GALLEY. CIRCUIT BREAKER WAS PULLED. CSR REPORTED BURNING ODOR COMING FROM AFT GALLEY COFFEE MAKERS. SMELL DISSIPATED AFTER UNITS SHUTOFF. ALL GALLEY CBS PULLED PRECAUTIONARY. ODOR WAS EITHER PLASTIC OR ESDR CA110816003Deflector · failed(CAN) CREW ADVISED FLIGHT DISPATCH AND MOC VIA THE VHF THAT THEY HAS A VERY LOUD NOISE, AND VIBRATION COMING FROM TOP OF THE L-1 DOOR. ALL INDICATIONS WERE NORMAL, HOWEVER MOC AND DISPATCH REQUESTED THE ACFT RETURN BACK TO DEPARTURE FOR MX. THE ACFT TOUCHED SDR CA110816001Coffeemaker · overheated(CAN) DURING CLIMB SMOKE WAS SEEN COMING FROM FWD GALLEY COFFEEMAKER. COFFEEMAKERS TURNED OFF AND C/B PULLED. FOUND FWD GALLEY C/M 101B AT FAULT. TWO WIRES BURNED ON THE RESERVOIR ELEMENT. COFFEEMAKER REPLACED. CKD SERVICE.SDR CA110816002Pitot Head · obstructed(CAN) SPEED DISCREPANCY ON T/O OF 40KTS BETWEEN CAPTAIN AND F/O REJECTED T/O AT 80 KTS AS A RESULT. AS WE PULLED OFF RUNWAY , "AFCS FAULT" EICAS MESSAGE. BEE FOUND IN NR 4 ADSP UNABLE TO REMOVE ALL DEBRIS. NR 4 ADSP REPLACED IAW AMM TASK 34-13-01. CHECK SERSDR CA110815007Deflector · damaged(CAN) LOUD SOUND: VIBRATION IN FWD CABIN/FLT DECK AREA SOUND/NOISE REDUCED W SPEED REDUCTION NEAR L1 DOOR AREA ALL PANELS ON WING TO BODY FRG, MAIN NOSE WHEEL WELL AREA LANDING DOOR, DOOR SEALS, VENT FLAP SEAL, FIND EBAY AREA, GVI OF LANDING GEARS (MAIN AND NSDR CA110808001Indicator · failedTHE FLIGHT DEPARTED NORMALLY UNDER MEL FOR BLEED 1 INOP. AFTER DEPARTURE THE FLIGHT EXPERIENCED A FAILURE OF THE OTHER BLEED. THE CREW CALLED A PAN PAN AND DID A RAPID DESCENT TO 10,000 FT AND RETURNED WHERE THEY ARE EXPECTED TO LAND OVERWEIGHT . REPLACED LSDR CA110805001Interface Unit · unserviceableJUST AFTER REACHING TOC, CREW SENT ACARS MESSAGE ADVISING THEY LOST ALL COMMUNICATIONS, ALL AUTO THRUST, AND ALL SPEED REF COMMUNICATIONS CAME BACK INTERMITTENTLY AND THE FLIGHT RETURNED. FOLLOWED TSM TASK 23-12-00-810-865 FOR VHF 1, ANT & COM MODULE PREVIOUSSDR CA110805003Clamp · looseTHE FLIGHT WAS DISPATCHED UNDER MEL FOR BLEED NR2 INOP AT APPROX FL220 THE ACFT DEVELOPED A BLEED NR 1 LEAK. THE FLIGHT REDUCED THE FLIGHT LEVEL AND RETURNED AND LANDED APPROX 1500K OVERWEIGHT. SOON AFTER ENCOUNTERING ICE COND IN CLIMB THRU FL200 EICAS BLEED SDR CA110725004Gcu · failed(CAN) WHILE ENROUTE AT FL360 THE ACFT HAD AN IDG 1 FAILURE. THE FLIGHT CREW DECLARED A PAN PAN AND DESCENDED TO FL300 TO START THE APU. AFTER A SUCCESSFUL APU START, THE FLIGHT CLIMBED TO 330 AND CONTINUED NORMALLY REF FIM 24-21-00-810-865-A, FAULT CLEARED DUSDR CA110725003Gasket · failed(CAN) ENGINE 1 BLEED LEAK OCCURED IN CLIMB AFTER T/O. FLIGHT RETURNED. OVERWEIGHT LANDING AT APPROX 47.8. FOUND PRECOOLER EXHAUST DUCT SEAL ADRIFT. SEAL REPLACED. PRECOOLER REPLACED IAW AMM. FUNCTION CHECK CARRIED OUT. NO FAULTS. CONSIDERED SERVICEABLE.SDR CA110721003Bleed Air Sys · failedFLIGHT DECLARED A PAN-PAN DUE TO A BLEED 1 FAIL IN THE CLIMB THROUGH 25 000 FT. (PACK 2 WAS ON MEL/21-51-00-A0). CREW COMPLETED THE QRH AND DESCENDED TO 10,000 FT AND DIVERTED. NORMAL APPROACH AND LANDING APPROX 1000 KGS OVERWEIGHT. FROM DEFECT LOG: NR 1 BLSDR CA110721004Acm · failedSMOKE IN CABIN. 2 MIN LATER PACK 2 FAILED, SMOKE DISSIPATED (AIR CONDITIONING PACKS - 1 INOPERATIVE) NR 2 AIR CYCLE MACHINE REPLACED IAW AMM 21-51-05. TESTED SERVICEABLE.SDR CA110718009Flap System · failedON APPROACH THE CREW RECEIVED A FLAP FAIL MESSAGE. THE 2ND RESET ATTEMPT WAS SUCCESSFUL AND NORMAL LANDING COMPLETED. NO EMERGENCY DECLARED.SDR CA110718011Flap System · faultyON APPROACH, THE FLAPS WOULD NOT FULLY EXTEND SO THE CREW PERFORMED A GO AROUND AND RECYCLED THE FLAPS. ON THE SECOND ATTEMPT THE SYS WORKED NORMALLY.SDR CA110708014Windshield · crackedCREW ADVISED FLIGHT DISPATCH VIA THE ACARS THAT THEY HAD DECLARED AN EMERGENCY WITH ATC DUE TO A CRACKED F/O SIDE WINDSHIELD. THE ACFT WAS AT FL300 OVERHEAD SSM. THEY DESCENDED TO 10,000 FT, 250 KTS, AND RETURNED TO DEPARTURE. NEW WINDSHIELD INSTALLED, LEAK SDR CA110708015Slat System · failedON APPROACH, THE CREW DECLARED PANPAN DUE TO A SLAT FAIL. LANDING WAS SAFELY COMPLETED SLAT FAIL AND ASSOCIATED CAUTIONS ON ARRIVAL. SHAKER ANTICIPATED, AOA LIMIT FAIL AND SPOILER FAULT UPON INITIAL SELECTION OF FLAP NR 2 RT OTBD SLAT ACTUATOR FOUND TORQUE LISDR CA110705005Ram Air Turb · misinstalledDURING RAT SYS FUNCTION TEST (J/C 39-24-23-00-004C-01), RAT FOUND UNABLE TO DEPLOY. INVESTIGATION REVEALED THAT THE RAT WAS NOT STOWED CORRECTLY. THE BLADES WERE NOT IN THE LOCKED AT GATE POSITION DESPITE THE LOCKING PIN IN THE EXTENDED POSITION. AS THE RAT WSDR CA110708012Flap System · failedDURING THE INITIAL APPROACH, THE FLIGHT HAD A "FLAPS FAIL MESSAGE" AND LANDED WITH ONLY PARTIAL FLAPS. THE CREW DECLARED AN EMERGENCY FOR THE LANDING. FIM TASK 27-03-00-810-813-A CARRIED OUT FAULT CLEARED IAW FIM TRANSITORY CONDITION OF FLIGHT CONTROL SYS. SDR CA110627015Slat System · failedSLAT FAIL EICAS MSG UPON SELECTION OF FLAP 1. QRH ACTIONED AND RECTIFIED ISSUE. NO FURTHER PROBLEMS. RESET IAW CREW COMMENTS.SDR CA110621004Shutoff Valve · failedTHE FLIGHT DISPATCHED UNDER MEL WITH NR1 BLEED INOP, AS THE FLIGHT CLIMBED THRU FL200. THE NR 2 BLEED FAILED. DID THE QRH PROCEDURE MSG EXTINGUISHED. THE FLIGHT DESCENDED TO 14000 FT AND MAINTAINED PRESSURE WITH THE APU BLEED AND CONTINUED NORMALLY TO DESTINASDR CA111005001Dome Nut · damaged(CAN) DURING F/O WINDSHIELD REPLACEMENT DUE TO HIGH PITCH NOISE REPORTED DURING FLIGHT, FOUND 15 ANCHOR NUTS (PN NAS1473S4) DAMAGED. THESE WERE THE ORIGINAL NUTS THAT WERE USED BY THE MFG TO INSTALL THE RT SIDE WINDSHIELD.SDR CA110609007Computer · failedWHILE IN CRUISE, CREW RECEIVED NUMEROUS FAULTS MESSAGES. - AVIONICS SYS FAULT. NO RVSM . PAN PAN ISSUED WITH ATC. AVNX MAU 1A FAIL OCCURED IN FLT, ABS 1 FAIL & SPOILER FAULT. QRH PROCEDURE C/O. NIC & PROCESSOR MODULE 1 (MAU 1 - NIC 1) REPLACED AS PREVENTIVESDR CA110609002Restrictor Valve · crackedRESTRICTOR VALVE ON THE LANDING GEAR FREEFALL SELECTOR VALVE FOUND CRACKED AND LEAKING.SDR CA110526002Tee Fitting · crackedNR 1 & 2 PYLONS, ENGINE DRIVEN HYD PUMP PRESSURE LINE TEE FITTINGS, CRACKED. PRESSURE LINE TEE FITTINGS CRACKED IAW THE ATTACHED PICTURES. NR1 PYLON FITTING DISPLAYED CRACKS AND NR 2 PYLON FITTING DISPLAYED CRACKS AND EVIDENCE OF LEAKING.SDR CA110518006Warning Message · illuminatedWHILE CLIMBING TO ALTITUDE FL210 THE ACFT LOST ITS PRESSURIZATION, CARRIED OUT QRH PROCEDURE AND RETURNED TO STATION. THE CREW DECLARED AND EMERGENCY AND WAS MET BY EMERGENCY VEHICLES ON ARRIVAL. THE FLIGHT WAS BELIEVED TO BE NOT OVERWEIGHT WHEN IT LANDED. SDR CA110516005Steering Unit · failedON ARRIVAL, THE CREW RECEIVED A STEERING FAILED MESSAGE AND THE ACFT WAS TOWED TO THE GATE NO FAULTS IN CMC. A/C RESET, OPERATIONAL TEST OK.SDR CA110511001Connector · damaged(CAN) AFTER TAKE OFF, LANDING GEAR WOULD NOT RETRACT AND AUTOPILOT WOULD NOT ENGAGE. NO EICAS MESSAGES. FLIGHT RETURNED TO YVR REPLACED SOCKETS ON P34 (NOSE WOFW PROX SNS2) REF WDM 32-62-50. REPLACED NOSE WOFW SENSOR 1 PER AMM 32-62-01 PB 401. GEAR SWING CARRSDR CA110509005Fadec · failed(CAN) AFTER T/O, CLIMBING THROUGH 1500 FT, NR 1 ENGINE FAIL MESSAGE RECEIVED ALONG WITH SLIGHT YAW TO THE LT. CREW SECURED ACFT AND RETURNED TO BASE. EMERGENCY DECLARED. FADEC WAS CHANGED, AND THE ACFT IS BACK IN SERVICE.SDR CA110504007Actuator · leaking(CAN) FLIGHT EXPERIENCED A GRADUAL FAILURE OF HYD SYS 1 AND DETECTED HYD FLUID SMELL IN THE COCKPIT FLIGHT DIVERTED AND DECLARED AN EMERGENCY FOUND NR 3 MF, 12H, SPOILER ACTUATOR LEAKING, REPLACED RT NR 3MF SPOILER ACTUATOR IAW AMM 27-65-01-00801A CARRIED OUT SDR CA110428008Seal · leaking(CAN) AFTER DEPARTURE AND IN THE CLIMB, A LOUD WHISTLING SOUND BEGAN TO EMANATE FROM BOTH EMERGENCY OVER WING EXITS. AS THE CLIMB CONTINUED, THE NOISE FROM THE LT SIDE DECEASED BUT INCREASED ON THE RT. THIS WAS FOLLOWED BY AN INDICATION WARNING IN THE FLIGHTSDR CA110425009Sensor · corroded(CAN) LANDING GEAR FAILED TO RETRACT AFTER DEPARTURE, EMERGENCY DECLARED WITH ATC AND RETURNING TO DEPARTURE. FOUND WATER IN WOW SENSOR NR 1 AND CORROSION ON PINS ALSO CMC FAULTED NLG WOWNR 2 SENSOR . WOW SENSOR NR 1 AND SENSOR NR 2 REPLACED IAW AMM 32-62-0SDR CA110420005Manifold · leaking(CAN) NR 2 HYDRAULIC QUANTITY DROP TO 10 PERCENT, DECLARING EMERGENCY, MAY REQUIRE TOW OFF RUNWAY DURING REPLACEMENT OF NR 2 HYD SYS CASE DRAIL FILTER FOUND BOWL ASSY DAMAGED. REQS NR 2 HYD SYS MANIFOLD, PN 2346H000-006 TO BE REPLACED. REPLACED NR 2 HYD SYS SDR CA110415006Pump · leakingENROUTE AND IN CRUISE, CREW EXPERIENCED A NR 2 HYD FAILURE. QRH WAS FOLLOWED AND FLIGHT CONTINUED TO PLANNED STATION. AN EMERGENCY WAS NOT DECLARED. AN UNEVENTFUL LANDING WAS CARRIED OUT AND ACFT TOWED TO GATE. NR 2 EDP REPLACED IAW AMM 29-11-01-04. NR 2 SDR CA110418001Slat System · failed(CAN) DURING THE APPROACH TO LAND THE ACFT HAD A SLAT FAILURE. THE CREW EXECUTED A GO AROUND AND REQUESTED EMERGENCY VEHICLE TO STAND BY FOR THE NEXT APPROACH AND LANDING. SLAT FAIL EICAS MESSAGE ILLUMINATED WHEN SELECTING FLAP 1. SLAT POSITION INDICATED ASSDR CA110415007Acm · seized(CAN) COCKPIT, SMELLED LIKE ELECTRICAL FIRE, IN CHARGE DID EMERGENCY CALL REPORTING SMOKE IN CABIN. SOURCE COULD NOT BE IDENTIFIED. RETURNED TO LAND ASAP. WE NOTICED "PACK 1 FAIL" MESSAGE ONCE LANDED ON 06L. IAW AMM 05-50-27 AND DVDR INFO, NO FURTHER ACTIOSDR CA110411001Fastener · sheared(CAN) LT MLG BODY END ATTACHMENT FITTING FOUND 2 AFT LOWER LOCK FASTENERS SHEARED.SDR CA110330001Control Quadrant · failed(CAN) DURING THE LANDING AND TAXI THE CREW DISCOVERED ENGINE NR 2 THRUST LEVER WILL GO INTO REVERSE POSITION WHEN THRUST LEVER BROUGHT TO IDLE, WITHOUT SELECTING REVERSE. THE THRUST CONTROL QUADRANT, TCQ, WAS REPLACED. T/S A MECHANICAL FAULT WITHIN THE BOX,SDR CA110401003Compressor · seized(CAN) ON APPROACH THE CREW NOTICED SOME SMOKE IN THE COCKPIT AFTER FLAP SELECTION - FLIGHT DECLARED AN EMERGENCY WITH ATC - LANDED NORMALLY FOUND NR 2 ACM MISSING A TURBINE BLADE. REPLACED ACM & DUAL HEAT EXCHANGER AS PER AMM 21-51-004,21-51-04. LEAK CHECK CSDR CA110328004Deflector · missing(CAN) AFTER TAKEOFF THE CABIN CREW REPORTED A VERY LOUD SQUEAL FROM ONE OF THE CABIN DOORS, AND THE CREW RETURNED TO LAND. DOOR DEFLECTORS, PASSENGER AND SERVICE, MISSING. REPLACED L1 DOOR DEFLECTOR IAW AMM 52-11-28, OPS NORMAL.SDR CA110324002Brake · faulted(CAN) DECLARED EMERGENCY DUE TO BRAKE FAULT, INBD BRAKES WORKING ONLY. LANDED AND TAXIED TO GATE WITH OUT INCIDENT.
Back to GE CF34-10E5A1