GE CF6-80C2A8

Service difficulty reports · 32

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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 = 'CF680C2A8'
  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 P5CA2021011000011Bleed Valve · malfunctionedBLEED NR 3 EICAS MESSAGE ON TAKE OFF ROLL. FWD TO MEL 36-11-03, MDDR 140670, CAT C. DEACT NR 3 HP BLEED. REMOVED AND REPLACED HPC (OFF PART: PN 773289-18, SN 200002037) AND HPV, IAW B747 AMM 36-11-00. OPERATIONS CHECK GOOD. THIS CLEARS MDDR 140670.Jan 9, 2021 · N452PA · Boeing 74746NF · Compressor Bleed ValveSDR CA190722001Line · leaking(CAN) PILOT REPORTS GREEN SYSTEM LOW QUANTITY MESSAGE ON ECAM, QRH HAS BEEN PERFORMED, QUANTITY LEVEL IS AT THE RED DOT, SAME. DISPATCH FOUND THAT THE AIRCRAFT CAN CONTINUE IN A NON-ETOPS ROUTE AND MAKE IT. SMALL POSSIBILITY OF DIVERTING MAINTENANCE ADVISED. HJul 20, 2019 · Airbus A310 · Hydraulic System, MainSDR CA190708001Actuator · faulted(CAN) AT TAKEOFF PHASE, MESSAGE ON ECAM, LDG DOOR NOT CLOSE. AIRCRAFT DIVERT. AS PER INVESTIGATION, FOUND L/H NOSE DOOR UPLOCK FAULT WITH MICROSWITCHES. MICROSWITCHES REPLACED AND LH NLG DOOR UPLOCK REPLACED IAW AMM 32-31-14 PB 401 AIRCRAFT BACK IN SERVICE (TJul 5, 2019 · Airbus A310 · Landing Gear Position and WarningSDR CA190401010Control Lever · faulted(CAN) AFTER TAKEOFF L/G LEVER INTERLOCK ECAM UNABLE TO RAISE GEAR ON SYSTEM 1 AND 2 ACCOMPLISHED CB RESET #U52 AS PER QRH SYSTEM RESET AND WAS UNSUCCESSFUL ON SYSTEM 1 LDG NORMAL CTRL MICRO SW UNIT 2GA REPLACED IAW AMM 32-31-11 PB401 LANDING GEAR ELECTRO-VALVEMar 31, 2019 · Airbus A310 · Landing Gear SelectorSDR CA190327021Switch · faulted(CAN) EN ROUTE ECAM YELLOW SERVO JAM. ECAM ACTIONS HAD ALREADY BEEN PERFORMED. YELLOW SERVO CTL SWITCHED OFF. SUSPECT AN INDICATION PROBLEM. CREW IS CHECKING THEIR ETOPS AND FUEL REQUIREMENTS. DUE TO FAULT AND RELATED INOP HYD SYSTEM FLIGHT UNABLE TO CONTINUE Mar 26, 2019 · Airbus A310300 · Elevator Control SystemSDR CA160108004Wire · damaged(CAN) WIRES LOCATED IN THE WHEEL WELL NEAR A CANISTER. THE WIRE ROUTING WAS TOO SLACK AND WITH TIME THE LOOSE PROTECTED WIRES GOT WORN OUT.Jan 6, 2016 · Airbus A310300 · Electrical Power System WiringSDR CA151223004Water Heater · sparks(CAN) WATER HEATER WAS PRODUCING SPARKS WHEN F/A DID RESET THE UNIT IN FLIGHT.Dec 22, 2015 · Airbus A310300 · Wash Water SystemSDR CA151223003Tube · broken(CAN) ENGINE NR 2 THROTTLE JAMMED DUE TO A RUPTURE THRUST REVERSER AIR TUBE. THE SAME TUBE WAS INSTALLED ON SEPT 02, 2015 IN THE EXACT LOCATION FOR THE SAME REASON.Dec 21, 2015 · Airbus A310 · Engine Thrust ReverserSDR CA151203006Valve · failed(CAN) ECAM YELLOW SYS LOW PRESSURE IN FLIGHT. 10 SECONDS AFTER, LOSS OF MOST OF THE YELLOW SYSTEM HYDRAULIC FLUID AND ASSOCIATED PITCH FEEL, SPOILER, YAW DAMPER 2 AFS.Nov 20, 2015 · Airbus A310300 · Landing Gear Brake SystemSDR CA150930003Cdu · cracked(CAN) CDU HOUSING CRACKED DURING TESTING OF THRUST REVERSER. OPERATED OK FOR 1 CYCLE AND THEN CRACKED AND SEPARATED ON CYCLE 2.Sep 25, 2015 · Airbus A310300 · Engine Thrust ReverserSDR CA150426001Indicator · overheated(CAN) APPROXIMATELY 5 MINUTES AFTER FULL ACFT ELECTRICAL POWER WAS APPLIED, THE RUDDER TRIM INDICATOR BEGAN EMMITING SMOKE AND PRODUCED A HEAVY ELECTRICAL BURNING ODOR.Apr 25, 2015 · Airbus A310300 · Independent InstrumentsSDR CA140812009Bolt · missing(CAN) A/C HAD INFLIGHT TURNBACK LT MLG DOOR NOT CLOSING. MAINTENANCE FOUND LH MLG UPLOCK (FIN 321212) ROD ASSY (REF A310 IPC 32-36-44-02 ITEM 100) ADRIFT FROM RETAINER BRACKET (REF A310 IPC 32-16-16-05 ITEM 100). THE RETAINER BOLT WAS MISSING. INSPECTION SHOWAug 10, 2014 · Airbus A310300 · Landing Gear Door Retract SectionSDR CA140124007Fairing · ruptured(CAN) DURING WALK AROUND INSPECTION, IT WAS FOUND THAT THE RT VERTICAL STABILIZER TO FUSELAGE FAIRING WAS DAMAGED, REFER IPC 53-19-69, ITEM 250. AFTER INSPECTION IT WAS NOTED THAT THE DAMAGE WAS DUE TO DELAMINATION OF THE PANEL. PANEL REPLACED AND INFORMED.Jan 23, 2014 · Airbus A310300 · Aerodynamic FairingsSDR CA140124006Wire · shorted(CAN) DURING FLIGHT LT INNER FUEL PUMP FAULT MESSAGE TRIGGERED. TROUBLESHOOTONG CARRIED OUT AND THE FOLLOWING FINDING WERE OBSERVED, GREEN HYD PUMP NR 2 WIRING AT SPECIFIED RAMP SUPPORT SHORTED TO GROUND, RESULTING IN 2 OF THE 3 PHASES TO SEVERE AND CAUSING OJan 22, 2014 · Airbus A310300 · Hydraulic Power System WiringSDR CA131219016Pin · cracked(CAN) PIN IS CRACKED. REPORTED TO MFG AND WAITING FOR MFG INSTRUCTIONS.Dec 14, 2013 · Airbus A310300 · Main Landing Gear Attach SectionSDR CA131213008Hinge Pin · cracked(CAN) DURING THE A-CHECK, WHILE PERFORMING LUBRICATION OF THE LT MLG, THE FWD ATTACHMENT PIN WAS FOUND WITH CRACKS AND A PORTION BROKEN OFF. THIS PIN IS PART OF THE GEAR AND IS REPLACED WITH THE GEAR ON OVERHAUL. THE GEAR WAS OVERHAULED IN OCT 2007 AND HAS ADec 12, 2013 · Airbus A310300 · Main Landing Gear Strut/Axle/TruckSDR CA130826003Line · cracked(CAN) DURING FLIGHT THE GREEN HYDRAULIC FLUID NOTICED TO BE DECREASING, FOLLOWED BY ECAM LOW LEVEL WARNING. LANDING MANUALLY EXTENDED FOR LANDING. ACFT HAD TO BE TOWED OFF RUNWAY DUE TO LOSS OF STEERING FROM GREEN HYDRAULIC SYSTEM FLUID LOSS. FOUND NR 2 ENGIAug 24, 2013 · Airbus A310300 · Hydraulic System, MainSDR CA130822012Manifold · leaking(CAN) O-RING FAILURE BETWEEN MANIFOLD ASSY FIN 291112, PN A2901150800000 AND BOSS FITTING MS21902-10. CAUSING ACFT TURN BACK DUE HYDRAULIC LOSS. IPC REF 24-24-03-04 050, O-RING REPLACED ON MANIFOLD ASSY FIN 291112. DEFECT ITEM NR 1100188.Aug 22, 2013 · Airbus A310300 · Hydraulic System, MainSDR CA130610006Eec · malfunctioned(CAN) AT THE TOP OF DESCENT, UPON THRUST REDUCTION TO FLIGHT IDLE, BOTH THRUST LEVERS WENT TO IDLE BUT THE NR 2 ENGINE N1 STAYED AT 70 PERCENT N1. STARTING AROUND 12,000 FT, TAT ABOVE FREEZING, THE N1 STARTED REDUCING TOWARDS IDLE. IT REACHED IDLE AT AROUND 8,Jun 4, 2013 · Airbus A310300 · Fuel Controlling SystemSDR CA130417001Cdu · damaged(CAN) NR 1 ENGINE THRUST REVERSER FAULT ON LANDING. FOUND OTBD REVERSER SLEEVE NOT FULLY STOWED. THRUST REVERSER WAS DEACTIVATED IAW MEL. ON DEPARTURE, THE NR 1 POWER LEVER WOULD NOT MOVE OUT OF IDLE POSITION. CENTER DRIVE UNIT (CDU) FEEDBACK MECHANISM FOUNApr 12, 2013 · Airbus A310300 · Engine ControlsSDR CA130318011Skin · cracked(CAN) DURING VISUAL INSPECTION, FOUND AFT CARGO DOOR ACTUATOR FITTING AT FRAME 61A AND INNER SKIN CRACKED BETWEEN LONGERON 1 AND 1A.Mar 11, 2013 · Airbus A310300 · Cargo/Baggage DoorsSDR CA130318014Bearing · corroded(CAN) DURING INSPECTION UNABLE TO OPEN RT OVERWING EMERGENCY EXIT DOOR, FROM THE INSIDE NOR FROM THE OUTSIDE. DOOR HAD TO BE PRYED UP IN ORDER TO OPEN. FOUND SLIDING BEARING/BUSHING CORRODED ON LIFTING MECHANISM SHAFT, ITEM 220 OF IPC 52-23-11, FIG 14.Mar 11, 2013 · Airbus A310300 · Emergency ExitsSDR CA130204003Actuator · failed(CAN) ON APPROACH THE CREW OBSERVED AN UNSAFE INDICATION OF THE NOSE GEAR UPON SELECTING GEAR DOWN FOR LANDING. THE CREW DECLARED AN EMERGENCY AND FOLLOWED THE APPLICABLE ABNORMAL CHECKLIST AND PERFORMED A GRAVITY GEAR EXTENSION WHICH RESULTED IN A SAFE GEAR IFeb 2, 2013 · Airbus A310300 · Landing Gear Door ActuatorSDR CA121203005Control Panel · overheated(CAN) IN CRUISE AT FL 370, VHF 2 CONTROL PANEL GREEN LIGHT WAS INTERMITTENT, THEN BECAME EXTINGUISHED. CREW NOTICED AN ELECTRICAL SPARK FOLLOWED IMMEDIATELY BY A LIGHT WHITE SMOKE COMING FROM UNIT AT THE ACTIVE GREEN LIGHT. THE CREW PULLED THE ASSOCIATED CIRNov 30, 2012 · Airbus A310300 · VHF Communications SystemSDR CA121127002Bolt · worn(CAN) ON APPROACH, THE SLATS EXTENDED NORMALLY BUT NO FURTHER MOVEMENT OF THE FLAP LEVER WAS POSSIBLE AFTERWARDS. THE SLAT/FLAP LEVER WAS STUCK IN THE UP POSITION PREVENTING THE MOVEMENT THROUGH THE POSITION DETENTS. THE CREW ADVISED ATC THAT A HIGHER APPROANov 23, 2012 · Airbus A310300 · Trailing Edge Flap Control SystemSDR CA120914010Duct · fractured(CAN) ACFT ARRIVED WITH 2 SNAGS RELATED TO AIR CONDITIONNING. CABIN TEMP HARD TO COOL DOWN AND LOW FLOW PLUS BOTH PACKS SURGING ON THE GROUND. REF W/O 1089584. DURING TROUBLESHOOTING, FOUND NR 1 PACK OUTLET DUCT RUPTURED. MISSING AREA APPROX 6" X 3". DUCT WSep 10, 2012 · Airbus A310300 · Air Distribution SystemSDR CA120224005Control Panel · smoke(CAN) FOUND SMOKE EMANATING FROM RUDDER AND AILERON TRIM CONTROL PANEL DURING COCKPIT PRE-DISPATCH CHECK. PART WAS REPLACED.Feb 7, 2012 · Airbus A310300 · Rudder Tab Control SystemSDR CA111026013Oven · burned(CAN) FWD GALLEY NR 2 OVEN BURNING ODOR. MEL 25-20, CAT D RAISED BY KLM IN AMS. UPON INVESTIGATION, FOUND FAN SEIZED. REPLACED OVEN IAW AMM 25-34-00. OPS CHECKED SERVICEABLE.Oct 25, 2011 · Airbus A310300 · Buffet/GalleysSDR CA110719003Bearing · seizedON CLIMB OUT, ON FLAP RETRACTION, CREW RECEIVED A FLAP SYS 1 & 2 FAULT WITH FLAP JAM MESSAGE. ACFT RETURNED TO DEPARTURE AIRPORT AND LANDING WAS UNEVENTFUL. INVESTIGATION REVEALED THE LT WING FLAP DRIVE SYS STEADY BEARING AT POSITION FIN 275494 WAS SEIZED. SJul 18, 2011 · Airbus A310 · Trailing Edge Flap Control SystemSDR CA101223007Seal · leaking(CAN) ON DEPARTURE OUT DURING CLIMB AFTER SLECTING FLAPS UP ECAM WARNING "BLUE SYSTEM, LOW QTY" ACCOMPANIED BY "BLUE SYSTEM, LOW AIR PRESSURE". CREW FOLLOWED QRH AND SELECTED ENGINE DRIVEN HYDRAULIC PUMP TO OFF (DEPRESSURIZED CONDITION) AND RETURNED TO STATIONDec 21, 2010 · Airbus A300* · Hydraulic System, MainSDR 2011F00121Blade · brokenHPT STAGE 1 BLADE FOUND BROKEN AND MISSING DURING ROUTINE BSI, ON FOLLOWING CF6-80C2A8 ENGINES SN 659611, 659399, 659526, 659392, 659408, 659612, 659414. SECONDARY DAMAGE WAS ALSO OBSERVED ON NUMBER OF BLADES. ALL THE BLADES WAS NEW WHEN INSTALLED.Mar 6, 2010 · Airbus A310300 · Turbine SectionSDR CA091203003Duct · cracked(CAN) PIREP DEFECT 1037394 - FUEL MIGRATING FROM LT INNER TANK TO CTR TANK. MX FOUND THE APU BOOST PUMP CANNISTER DELIVERY DUCT CRACKED. REPLACED PER MM 49-32-14 AND SERVICEABLE. (TC NR 20091203003)Dec 2, 2009 · Airbus A310300 · APU Engine Fuel and Control
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