# Service difficulty reports: GE CF6-80C2A8

A list on [GE CF6-80C2A8](https://openairdocs.org/engine/ge-cf6-80c2a8.md).

Newest first. General aviation reporting is voluntary.

- [SDR P5CA2021011000011](https://openairdocs.org/sdr/P5CA2021011000011.md): Bleed Valve · malfunctioned · Jan 9, 2021 · N452PA · Boeing 74746NF · Compressor Bleed Valve
  > BLEED 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.
- [SDR CA190722001](https://openairdocs.org/sdr/CA190722001.md): Line · leaking · Jul 20, 2019 · Airbus A310 · Hydraulic System, Main
  > (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. H
- [SDR CA190708001](https://openairdocs.org/sdr/CA190708001.md): Actuator · faulted · Jul 5, 2019 · Airbus A310 · Landing Gear Position and Warning
  > (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 (T
- [SDR CA190401010](https://openairdocs.org/sdr/CA190401010.md): Control Lever · faulted · Mar 31, 2019 · Airbus A310 · Landing Gear Selector
  > (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-VALVE
- [SDR CA190327021](https://openairdocs.org/sdr/CA190327021.md): Switch · faulted · Mar 26, 2019 · Airbus A310300 · Elevator Control System
  > (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
- [SDR CA160108004](https://openairdocs.org/sdr/CA160108004.md): Wire · damaged · Jan 6, 2016 · Airbus A310300 · Electrical Power System Wiring
  > (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.
- [SDR CA151223004](https://openairdocs.org/sdr/CA151223004.md): Water Heater · sparks · Dec 22, 2015 · Airbus A310300 · Wash Water System
  > (CAN) WATER HEATER WAS PRODUCING SPARKS WHEN F/A DID RESET THE UNIT IN FLIGHT.
- [SDR CA151223003](https://openairdocs.org/sdr/CA151223003.md): Tube · broken · Dec 21, 2015 · Airbus A310 · Engine Thrust Reverser
  > (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.
- [SDR CA151203006](https://openairdocs.org/sdr/CA151203006.md): Valve · failed · Nov 20, 2015 · Airbus A310300 · Landing Gear Brake System
  > (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.
- [SDR CA150930003](https://openairdocs.org/sdr/CA150930003.md): Cdu · cracked · Sep 25, 2015 · Airbus A310300 · Engine Thrust Reverser
  > (CAN) CDU HOUSING CRACKED DURING TESTING OF THRUST REVERSER. OPERATED OK FOR 1 CYCLE AND THEN CRACKED AND SEPARATED ON CYCLE 2.
- [SDR CA150426001](https://openairdocs.org/sdr/CA150426001.md): Indicator · overheated · Apr 25, 2015 · Airbus A310300 · Independent Instruments
  > (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.
- [SDR CA140812009](https://openairdocs.org/sdr/CA140812009.md): Bolt · missing · Aug 10, 2014 · Airbus A310300 · Landing Gear Door Retract Section
  > (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 SHOW
- [SDR CA140124007](https://openairdocs.org/sdr/CA140124007.md): Fairing · ruptured · Jan 23, 2014 · Airbus A310300 · Aerodynamic Fairings
  > (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.
- [SDR CA140124006](https://openairdocs.org/sdr/CA140124006.md): Wire · shorted · Jan 22, 2014 · Airbus A310300 · Hydraulic Power System Wiring
  > (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 O
- [SDR CA131219016](https://openairdocs.org/sdr/CA131219016.md): Pin · cracked · Dec 14, 2013 · Airbus A310300 · Main Landing Gear Attach Section
  > (CAN) PIN IS CRACKED. REPORTED TO MFG AND WAITING FOR MFG INSTRUCTIONS.
- [SDR CA131213008](https://openairdocs.org/sdr/CA131213008.md): Hinge Pin · cracked · Dec 12, 2013 · Airbus A310300 · Main Landing Gear Strut/Axle/Truck
  > (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 A
- [SDR CA130826003](https://openairdocs.org/sdr/CA130826003.md): Line · cracked · Aug 24, 2013 · Airbus A310300 · Hydraulic System, Main
  > (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 ENGI
- [SDR CA130822012](https://openairdocs.org/sdr/CA130822012.md): Manifold · leaking · Aug 22, 2013 · Airbus A310300 · Hydraulic System, Main
  > (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.
- [SDR CA130610006](https://openairdocs.org/sdr/CA130610006.md): Eec · malfunctioned · Jun 4, 2013 · Airbus A310300 · Fuel Controlling System
  > (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,
- [SDR CA130417001](https://openairdocs.org/sdr/CA130417001.md): Cdu · damaged · Apr 12, 2013 · Airbus A310300 · Engine Controls
  > (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 FOUN
- [SDR CA130318011](https://openairdocs.org/sdr/CA130318011.md): Skin · cracked · Mar 11, 2013 · Airbus A310300 · Cargo/Baggage Doors
  > (CAN) DURING VISUAL INSPECTION, FOUND AFT CARGO DOOR ACTUATOR FITTING AT FRAME 61A AND INNER SKIN CRACKED BETWEEN LONGERON 1 AND 1A.
- [SDR CA130318014](https://openairdocs.org/sdr/CA130318014.md): Bearing · corroded · Mar 11, 2013 · Airbus A310300 · Emergency Exits
  > (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.
- [SDR CA130204003](https://openairdocs.org/sdr/CA130204003.md): Actuator · failed · Feb 2, 2013 · Airbus A310300 · Landing Gear Door Actuator
  > (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 I
- [SDR CA121203005](https://openairdocs.org/sdr/CA121203005.md): Control Panel · overheated · Nov 30, 2012 · Airbus A310300 · VHF Communications System
  > (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 CIR
- [SDR CA121127002](https://openairdocs.org/sdr/CA121127002.md): Bolt · worn · Nov 23, 2012 · Airbus A310300 · Trailing Edge Flap Control System
  > (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 APPROA
- [SDR CA120914010](https://openairdocs.org/sdr/CA120914010.md): Duct · fractured · Sep 10, 2012 · Airbus A310300 · Air Distribution System
  > (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 W
- [SDR CA120224005](https://openairdocs.org/sdr/CA120224005.md): Control Panel · smoke · Feb 7, 2012 · Airbus A310300 · Rudder Tab Control System
  > (CAN) FOUND SMOKE EMANATING FROM RUDDER AND AILERON TRIM CONTROL PANEL DURING COCKPIT PRE-DISPATCH CHECK. PART WAS REPLACED.
- [SDR CA111026013](https://openairdocs.org/sdr/CA111026013.md): Oven · burned · Oct 25, 2011 · Airbus A310300 · Buffet/Galleys
  > (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.
- [SDR CA110719003](https://openairdocs.org/sdr/CA110719003.md): Bearing · seized · Jul 18, 2011 · Airbus A310 · Trailing Edge Flap Control System
  > ON 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. S
- [SDR CA101223007](https://openairdocs.org/sdr/CA101223007.md): Seal · leaking · Dec 21, 2010 · Airbus A300* · Hydraulic System, Main
  > (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 STATION
- [SDR 2011F00121](https://openairdocs.org/sdr/2011F00121.md): Blade · broken · Mar 6, 2010 · Airbus A310300 · Turbine Section
  > HPT 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.
- [SDR CA091203003](https://openairdocs.org/sdr/CA091203003.md): Duct · cracked · Dec 2, 2009 · Airbus A310300 · APU Engine Fuel and Control
  > (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)

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/engine/ge-cf6-80c2a8/reports

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