GE CF6-80C2A5

Service difficulty reports · 164

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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 = 'CF680C2A5'
  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.

SDR CA030214011Wire · burned(CAN) ENGINE NR 2, HYDRAULIC FIRE SHUTOFF VALVE, CIRCUIT BREAKER 558 POPPING AND WILL NOT RESET. INSPECTION FOUND WIRING DAMAGED (P/N'S: 2912-5006, 2912-5007 AND 29-5003)(BURNT OVER 12INCHES)FROMCONNECTOR OF THE NR 2 ENGINE FIRE SHUTOFF VALVE (YELLOW SYSTEM),Jan 30, 2003 · Airbus A310304 · Hydraulic Power System WiringSDR CA030112004Transmitter · reads low(CAN) THE YELLOW HYDRAULIC TRANSMITTER READING LOW ON ARRIVAL. DURING SERVICING OF THE YELLOW HYDRAULIC SYSTEM, FLUID EMERGED FROM THE AIR DEPRESSURIZATION RELIEF VALVE. THE ERRONEOUS READING (FROM THE DEFECTIVE 'HYDRAULIC TRANSMITTER,CAUSED MTCE TO OVERFILL TDec 1, 2002 · Airbus A310300 · Hydraulic Quantity IndicatorSDR CA030112002Clamp · broken(CAN) UPON A/C ARRIVAL, DURING WALK AROUND, MTCE NOTED THAT THE NR 5 MLG WHEEL BRAKE COOLING FAN SHROUD ATTACHMENT CLAMP WAS BROKEN. MTCE REPLACED THE CLAMP IAW AMM 12-37-32.Nov 28, 2002 · Airbus A310300 · Landing Gear Brake SystemSDR CA021117002Duct · cracked(CAN) BLEED DUCT ON AIRFRAME SIDE OF ENGINE BLEED VALVE ON TAKE TO REVERSER AIR MOTOR OF NR 1 ENGINE WAS FOUND CRACKED AND SEVERELY LEAKING. DUCT WAS REPLACED AND A LEAK CHECK WAS CARRIED OUT AND NONE WERE FOUND.Nov 10, 2002 · Airbus A310300 · Engine Bleed Air SystemSDR CA030106020Plate · bent(CAN) A/C WAS COMING OUT OF AC CHECK AND DURING FERRY FLT CREW REPORTED THAT THEY WERE UNABLE TO OBTAIN FULL REVERSE THRUST ON EITHER ENGINE ON LANDING. PILOT WAS UNABLE TO MOVE THRUST LEVERS TO FULL REVERSE POSITION AND MAXIMUN REVERSE THRUST ACHIEVED WAS 40 Nov 1, 2002 · Airbus A310300 · Engine Thrust ReverserSDR 02FDEA00700Hmu · faultyNR 2 ENGINE FF 2500-5000 LB FLUCTUATION- ON CLIMB OUT, NOTICED FLUCTUATING FUEL FLOW EFFECTING A SPIKE IN N1 (5-10 PERCENT) EGT TEMP VARY 3-5 DEGREES ALONG WITH A SLIGHT N2 SPIKE (2 PERCENT) NOTIFIED MECHANIC, RETURNED TO LANDING RWY 36R. TAXI IN, INSTRUMESep 27, 2002 · N661FE · Airbus A300F4605R · Fuel Controlling SystemSDR AALA20021300Joint · wornEN ROUTE SJU-MCO, NR 1 ENGINE N1 VIBRATION CYCLED BETWEEN 4.0 AND 9.8. WHEN ENGINE REDUCED TO IDLE, ENGINE VIBRATION STOPPED. CAPTAIN DECLARED EMERGENCY AND AIRCRAFT LANDED AT MIA WITHOUT INCIDENT. REPLACED LEFT ENGINE JOINT. SYSTEM GROUND CHECKED NORMAL OSep 17, 2002 · N59081 · Airbus A300B4605R · Engine (Turbine/Turboprop)SDR CA020829014Shutoff Valve · failed(CAN) IN YQB, HAD TO SHUT NR 1 ENGINE DOWN WITH FIRE HANDLE SINCE MOVING THE HP FUEL LEVER NR 1 TO THE OFF POSITION. CLOSE THE HP FUEL VALVE. MAINTENANCE IN YQB, CHECKED THE FUEL SYSTEM FOR PROPER FUNCTION, IN ACCORDANCE WITH THE AMM 71-00-00, P.534 AND CHEAug 26, 2002 · Airbus A310300 · Fuel Selector/Shut-Off ValveSDR CA020722003Connector · burned(CAN) DURING PREDEPARTURE CHECK, IT WAS NOTICED THAT THE NR 2 ENGINE GREEN HYDRAULIC PUMP LOW PRESSURE LIGHT ON THE OVERHEAD PANEL, WAS NOT ON. IT WAS FOUND THAT NR 2 GREEN HYDRAULIC PUMP CONNECTOR FIN DV213 WAS BADLY BURNED AND THAT THE PINS WERE HEAVILY CORJul 21, 2002 · Airbus A310300 · Hydraulic Power System WiringSDR CA020718006Transmitter · failed(CAN) ON TAKE OFF ROLL A "TAKE-OFF CONFIGURATION WARNING" WAS TRIGGERED. AIRCRAFT SPEED WAS BELOW 80 KTS, CREW PROCEEDED WITH AN ABORTED TAKE OFF.TROUBLESHOOTING REVEALLED A DISCREPANCY BETWEEN THE THS POSITION INDICATION ON ECAM AND THE PITCH TRIM WHEEL INDEXJul 11, 2002 · Airbus A310300 · Stabilizer Position IndicatingSDR CA020705003Panel · damaged(CAN) DURING WEEKLY CHECK, NR 2 RT SLAT ACTUATOR PANEL ASSY. FOUND DAMAGED. PART OF THE COMPOSITE PANEL WAS MISSING. AIRCRAFT WAS AOG. THE PANEL WAS FLOWN IN. MAINTENANCE REPLACED THE PANEL I.A.W. AMM 57-40-00.Jul 2, 2002 · Airbus A310300 · Leading Edge DevicesSDR CA020708009Water Heater · failed(CAN) DURING THE C-08 CHECK, IT WAS DISCOVERED DURING THE OPERATIONAL TEST, THAT THE POTABLE WATER HEATERS, IN LAVATORY F, WERE MAKING THE C/B TRIP. THE 3 UNITS WERE REMOVED AND SENT TO THE AVIONICS SHOP. WHEN REMOVING THE TOP COVER OF ONE UNIT, WE FOUND A SOJun 13, 2002 · Airbus A310300 · LavatoriesSDR CA020528007Shutoff Valve · corroded(CAN) FUEL SHUTOFF VALVE, DURING 8C CHECK RT ENGINE LOWERED TO ALLOW FOR MOUNT BOLT REPLACEMENT & CORROSION REPAIR. ON REINSTALLED ENGINE INTERNAL & EXTERNAL LEAK CHECK OF LP FUEL FIRE SHUTOFF VALVE REQUIRED PER J/C 71-400-001-2. FUNCTION CHECK REVEALED THATMay 27, 2002 · Airbus A310 · Fuel Selector/Shut-Off ValveSDR 02FDEA00202Thrust Reverser · malfunctionedDURING T/O N1 GOT NR 1 THRUST REVERSER PRESSURIZED ON LEFT ECAM REJECT AT LOW SPEED. PERFORMED FUNCTION CHECK CND.Mar 16, 2002 · N665FE · Airbus A300F4605R · Engine Thrust ReverserSDR CA020308003Valve · unserviceable(CAN) FLT 757, LOST OF BLUE HYDRAULIC SYSTEM FLUID IN FLIGHT. HYDRAULIC LEAK WAS FOUND COMING FROM NR 3 RT SPOILER VALVE GROUP AT THE FILTER HOUSING CAP PACKING. AFFECTED SPOILER VALVE GROUP WAS REPLACED AND A/C WAS RETURNED TO SERVICE.Mar 8, 2002 · Airbus A310 · Drag Control ActuatorSDR 02FDEA00071Hmu · faultyON TAKEOFF NR 2 FADEC FAULTED. R&R HMU.Jan 25, 2002 · N672FE · Airbus A300F4605R · Fuel Control/Turbine EnginesSDR CA020118001Control Unit · malfunctioned(CAN) MANY INDICATIONS (DEFECTS REPORTED) OF SLATS / FLAPS SYSTEM NR 1 & 2 FAULTS HAVE BEEN REPORTED ON AIRCRAFT, HAVING SEVERAL MAINTENANCE ACTION C/OUT FROM 2001-11-25 TO 2001-12-20 AND THE FINAL RECTIFICATION BEING THE REPLACEMENT OF THE LAT FLAP CONTROL Dec 20, 2001 · Airbus A310300 · Leading Edge Slat Control SystemSDR CA020117017Door · missing(CAN) FOUND REFUELING PANEL DOOR MISSING ON ARRIVAL TO "VRA". REFUELING DOOR AND AN AIR INLET PANEL WERE REPLACED.Dec 10, 2001 · Airbus A310 · Service DoorsSDR 01FDEA00898Compressor · stalledDURING CLIMBOUT, SEVERE COMPRESSOR STALL NR 2 ENG.Oct 21, 2001 · N676FE · Airbus A300F4605R · Turbine Engine Compressor SectionSDR CA020628004Blade · damaged(CAN) COMPRESSOR STALL ON TAKE OFF IN LRM, ON ENGINE NR 2 , MTCE FOUND AFTER VISUAL INSPECTION, 2 BLADES DAMAGED. FURTHER INSPECTION C/OUT IN ACCORDANCE WITH AMM 72-00-00 P.600, REVEALED DAMAGE ON HIGH PRESSURE COMPRESSOR. NUMEROUS BLADES NICKED, CURLED, TORN Aug 5, 2001 · Airbus A310300 · Engine (Turbine/Turboprop)SDR CA010723043Valve · failed(CAN) ETOP REQUIRED REPORTING. AIRCRAFT COULD NOT TRANSFER ALL THE FUEL FROM CENTER TANK. FQIS RESET AND BITE CHECKED SERVICEABLE. THIS IS A RECURRING DEFECT WHERE THE FQIS IS REST AND THE DEFECT RETURND A COUPLE OF FLIGHTS LATER ADDITIONAL TROUBLE SHOOTING REJul 16, 2001 · Airbus A310 · Fuel Transfer ValveSDR CA010815003Door · missing(CAN) 1. DURING THE TURNAROUND IT WAS OBSERVED THAT THE MID LAV SERVICING PANEL DOOR WAS MISSING. 2. DMI 35881 WAS RAISED UNDER CDL 52-4. AIRCRAFRT RELEASED FOR FLIGHT.3. NO FURTHER INCIDENT DURING SUBSEQUENT FLIGHT.Jul 13, 2001 · Airbus A310304 · Service DoorsSDR 01FDEA00518Compressor · stalledDURING CLIMBOUT NR 1 ENG HAD 2 COMPRESSOR STALLS WITH FLAMES REPORTED BY TOWER DURING 2ND ONE.Jul 6, 2001 · N671FE · Airbus A300F4605R · Turbine Engine Compressor SectionSDR 01FDEA00461Warning System · activatedON T/O ECAM WARN ENG FAIL NR 2 ABORTED TAKEOFF. RETURN FOR 2ND TRY AND RECEIVED ECAM WARN ENG SHUTDOWN.Jun 16, 2001 · N681FE · Airbus A300F4605R · Central ComputersSDR CA010320021Line · loose(CAN) PILOT OBSERVED GREEN SYSTEM HYDRAULICS WAS LOOSING FLUID. AIRCRAFT DIVERTED TO YYT. HYDRAULIC LINE IN NR 1 ENGINE PYLONFOUND LOOSE. LINE TIGHTENED AND LEAK CHECK CARRIED OUT SERVICEABLE.Feb 14, 2001 · Airbus A310304 · Hydraulic System, MainSDR CA010301027Bushing · rotated(CAN) AIRCRAFT RETURNED TO YTR AS GEAR WOULD NOT RETRACT. AIRCRAFT PUT ON JACKS AND FOUND THAT LT BOGIE WOULD NOT TILT. IT WAS DETERMINED THAT ONE BUSHING ON THE SHOCK ABSORBER HAD ROTATED CAUSING THE HINGE PIN TO SEIZE, THEREFORE BOGIE WOULD NOT TILT AND GEARFeb 11, 2001 · Airbus A310304 · Main Landing Gear Strut/Axle/TruckSDR CA010226013Duct · damaged(CAN) DURING CLIMB, NR 2 ENGINE FIRE INDICATION OBSERVED. ENGINE RETARDED TO IDLE. FIRE WARNING DISAPPEARED. AIRCRAFT LANDED WITHOUT INCIDENT. 14TH STAGE DUCT FOUND DAMAGED. REPLACED I.A.W. MM 36-00-00. SUSPECT CLAMP CAUSED PROBLEM. RELATED PARTS REPLACED INCLJan 27, 2001 · Airbus A310304 · Engine Bleed Air SystemSDR 00FDEA00873Bleed Valve · malfunctioned00-354 NR 2 HP BLEED VALVE ON ECAM, NR 1 HP ECAM NOT CLOSED WARNING. DUAL HP VLV FAULTS. ** S/D ** COMINGDec 13, 2000 · N668FE · Airbus A300F4605R · Compressor Bleed ValveSDR 00FDEA00732Sensor · inoperativeON T/O ROLL PHL, NO FUEL FLOW NR 1. RETURNED TO GATE. REJECT 100 KTS.Oct 24, 2000 · N657FE · Airbus A300F4605R · Fuel Flow SensorSDR 00FDEA00319Engine · vibration00-133 AT ROTATION SPD NR 1 ENG START VIB LOUDLY. VIEW BIRDS ON RUNWAY ON ROTATION. PERFORMED TRIM BALANCE AND VIBRATION SURVEY PER A300 MM 72-21-00-2. VIB LEVELS WELL WITHIN LIMITS AT THIS TIME.May 3, 2000 · N681FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR CA000322017Fcu · malfunctioned(CAN) NR 2 THROTTLE WARN ON ECAM DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RESET SYSTEM, NO FAULT PRESENT. FLIGHT CONTINUED WITH NO OTHER FAULTS.Feb 28, 2000 · Airbus A310304 · Fuel Control/Turbine EnginesSDR AALA20000350Engine · stalledMIA - FLT 882 - AFTER TAKEOFF, RIGHT ENGINE EXPERIENCED COMPRESSOR STALL. RETURNED AND LANDED MIA WITHOUT INCIDENT. REPLACED RIGHT ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION. ENGINE BOROSCOPE REVEALED NUMBER SEVEN STAGE BLADES DAMAGED. (M)Feb 25, 2000 · N59081 · Airbus A300B4605R · Engine (Turbine/Turboprop)SDR AALA20000196Engine · lack of lubeJFK - 106 - NR 2 ENGINE SHUTDOWN DUE TO LOW OIL QUANTITY. REPLACED NR 2 ENGINE. (M)Jan 31, 2000 · N8067A · Airbus A300B4605R · Engine (Turbine/Turboprop)SDR 00FDEA00005Engine · malfunctioned00-5 - NR 2 ENGINE COMPRESSOR STALLED AFT CLIMB PWR SEL FOLLOW FLEX PWR T/O ON A NON PROFILE T/O. ENG RETARD TO IDLE AND NO FURTHER ADVERSE CONDITION NOTED. AC LAND WITH NR 2 IDLE, ENG SHUTDOWN AFT LAND.Jan 4, 2000 · N661FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR 99FDEA00333Engine · failedAFTER T/O AT GEAR RETRACT, LOUD BANG THOUGHT TO BE FAILURE OF NOSE GEAR COMPONENT. *S/D* REMOVED AND REPLACED NR 2 ENG IAW WORK CARDS 64T0100-2 & 64T0700-2, FUNCTIONAL CK PRETEST ENG MM 71-00-00 AND JRH ALL CK NORMAL.Aug 11, 1999 · N660FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR AU990552Sensor · faulty(AUS) RT ENGINE N1 HYDROMECHANICAL SENSORS (2OFF) FAULTY.Apr 22, 1999 · Fuel Control/Turbine EnginesSDR AU990710Lever · faulty(AUS) DOOR EMERGENCY POWER ASSIST BOTTLE TOGGLES ON DOORS 3L AND 4R WERE NOT CONNECTED TO THE ACTIVATION CABLE LINKAGE. THE CONNECTING BOLT WAS FITTED, BUT DID NOT CAPTURE THE TOGGLE LEVER.Apr 8, 1999 · Boeing 747438 · Passenger/Crew DoorsSDR CA990224017Engine · failed(CAN) NR 2 ENGINE FAILED ON ROTATION. NO THROTTLE RESPONSE. SOME METAL PARTICLES FOUND IN THE EXHAUST. ENGINE REMOVED. WAITING FOR SHOP REPORT. PART TC: 8,624.Feb 11, 1999 · Engine (Turbine/Turboprop)SDR AU981683Clip · sheared(AUS) ON REMOVAL OF THE LT 'OFF WING' ESCAPE SLIDE, THE RELEASE STRING TENSION BAR WAS FOUND ADRIFT WITHIN THE SLIDE COMPARTMENT. FURTHER INVESTIGATION FOUND THE ATTACHMENT BEARING P-CLIPS (7 OFF) SHEARED.Dec 3, 1998 · Boeing 767338 · Escape SlideSDR CA981116010Blade · damaged(CAN) FLIGHT CREW REPORTED POSSIBLE BIRD STRIKE DURING TAKEOFF. ALL PARAMETERS DURING FLIGHT OK. DURING BIRD STRIKE, CHECK FOUND THE FOLLOWING FAN BLADES DAMAGED 32, 33, 34, 35. DAMAGED BLADES REPLACED AND ENGINE GROUND RUN SERVICEABLE.Nov 2, 1998 · Turbine SectionSDR AALA981372Adapter · failedSJU - FLT 574 - DURING CRUISE NR 1 ENGINE WAS SHUT DOWN BY CREW DUE TO ENGINE FIRE. RETURNED AND LANDED SJU. REPLACED NR 1 ENGINE. SHOP FOUND THE AGB IDLER ADAPTER THREADED INSERTS WERE PULLED OUT CAUSING FUEL TO LEAK, FIRE AND ENGINE SHUTDOWN. GENERAL ELEJul 9, 1998 · N80057 · Airbus A300B4605R · Turbine Engine Accessory DriveSDR 98FDEA00256Ecu · malfunctionedAT ROTATION, NR 2 ENGINE AND THROTTLE BEGAN TO ROLL BACK. NOTICED FLUX BUT ON PUSHING NR 2 THROTTLE BACK UP, ENGINE RETURNED TO NORMAL. REMOVED AND REPLACED NR 2 ENGINE ECU PER M/M 73-21-01-4. RAN NR 2 ENGINE PER JRH AND M/M 71-00-00-5. POWER ASSURANCE CHEApr 8, 1998 · N667FE · Airbus A300F4605R · Fuel Control/Turbine EnginesSDR AALA980556Anti-Ice Valve · failedYQX - FLT 141 - NR 1 ENGINE ANTI-ICE NACELLE VALVE FAILED TO OPEN. ICING CONDITIONS ANTICIPATED AT JFK. DIVERTED TO GANDER. NR 1 ENGINE NACELLE ANTI-ICE VALVE LOCKED OPEN AND DEFERRED PER MEL 30-1B AUTH NO 3-55DC-C. REMOVED AND REPLACED NR 1 ANTI-ICE VALVEMar 21, 1998 · N8067A · Airbus A300B4605R · Engine Anti-Icing SystemSDR 98FDEA00202Compressor · burnedREJECTED T/O AT APPROX 120 KTS, (18R MEM) DUE TO FIRE ON NR 2 ENGINE. AFTER BOTH BOTTLES WERE FIRED THE FIRE WENT OUT. A/C NOT EVACUATED EMERGENCY CREW CONFIRMED NO FURTHER SMOKE. FOUND HOLE BURNED THROUGH REAR COMPRESSOR STAGE AT 8 O'CLOCK FUEL NOZZLE POSIMar 17, 1998 · N654FE · Airbus A300F4605R · Turbine Engine Compressor SectionSDR 98FDEA00165Engine · flamed outDURING IDLE DESCENT PASSING FL260, NR 1 ENGINE FLAMED OUT. NO APPARENT ENGINE DAMAGE. ALL FUEL PUMPS ON, 18000 LBS OF FOB. REMAINING, FUEL DISTRIBUTION NORMAL. FOLLOWING ECAM INSTRUCTIONS, ENGINE RE-LIT WITH APPLICATION OF CONTINUOUS IGNITION. ADVISED ATCMar 7, 1998 · N658FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR AALA980491Gasket · deterioratedLHR - FLT 105 - AIRCRAFT MADE AN UNSCHEDULED LANDING AT BOS DUE TO CREW NOTING RIGHT INNER, FUEL TANK QUANTITY FLUCTUATION. UPON LANDING BOS, AIRCRAFT BEHIND US ON TAXIWAY REPORTED 'FUEL POURING FROM NR 2 ENGINE' PULLED NR 2 FIRE HANDLE AND FIRED AGENT 1. TRFeb 27, 1998 · N70074 · Airbus A300B4605R · Engine Fuel PumpSDR 98FDEA00110Press Switch · failedFUEL PRESSURE LIGHT ILLUMINATED ON CLIMBOUT. NR 1 FUEL FILTER CLOGGED LIGHT ON. FOUND FUEL FILTER OK. FOUND PRESSURE DIFFERENTIAL SWITCH BAD. REMOVED AND REPLACED SWITCH, OPS NORMAL PER AML 73-34-11. ENGINE LEAK CHECK GOOD.Feb 17, 1998 · N650FE · Airbus A300F4605R · Fuel Indicating SystemSDR AALA980216Engine · failedJFK - FLT 141 - N2 ENGINE VIBRATION ECAM, NR 2 ENGINE INDICATION FLASHING. VARIED FROM 4.6 AT CRUISE POWER INCREASING TO 6.0 -6.4 WHEN THROTTLE REDUCED TO IDLE. POSSIBLE SLIGHT BUZZ LEFT IN NR 2 THROTTLE. N1 VIB AND ALL OTHER INDICATIONS NORMAL. NOTICEABLEJan 25, 1998 · N70072 · Airbus A300B4605R · Engine (Turbine/Turboprop)SDR AALA980195Engine · defectiveJFK - FLT 657 - WHEN CLIMB RATE WAS SELECTED, NR 1 ENGINE WOULD NOT DEVELOP CLIMB POWER. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE. ACCOMPLISHED ENGINE RUN AND LEAK CHECKED NORMAL. SYSTEM GROUND CHECKED NORMAL OPERATION. OPERATIONAJan 21, 1998 · N14056 · Airbus A300B4605R · Engine (Turbine/Turboprop)SDR AALA980130Oil Cap · leakingJFK - FLT 0106 - AT 33,000 FEET, NR 1 ENGINE OIL PRESSURE WAS 32-34 PSI (NR 2 WAS 56 PSI) NR 1 OIL QUANTITY WAS 17 QUARTS AT LEVEL OFF, BUT SLOWLY DROPPED TO 11 QUARTS BEFORE STABILIZING. FOUND OIL CAP LEAKING REPLACED CAP AND CHECK VALVE ASSY. LEAK CHECKS OJan 15, 1998 · N14068 · Airbus A300B4605R · Turbine Engine Oil System
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