Fairchild Republic A-10 Thunderbolt II: Difference between revisions

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FlightGear A-10 starts with all internal tanks full.
FlightGear A-10 starts with all internal tanks full.


2 wing tanks (left and right), 2 fuselage tanks (left main-afterward and right main-forward)
2 wing tanks (left and right), 2 fuselage tanks: main-aft linked to left system and main-forward, linked to right system, up to 3 external tanks (2 wings and 1 fuselage).
Up to 3 external tanks (2 wings and 1 fuselage).
Normally the left wing and left main tanks feeds the left engine and the APU,
the right wing and right main tanks feeds the right engine. The two feed lines could
be interconnected by opening the cross feed valve.
The wing boost pumps will supply the respective engine until the wing tanks are empty,
at which time the wing boost pumps will automatically shut off. The main boost pumps will
then supply the respective engine with the remainder of the fuel in the airplane.


In case of a wing tank boost pump failure, the wing tank fuel will gravity feed to its respective
Normally the left wing and left main tanks feed the left engine and the APU. The right wing and right main tanks feed the right engine. The two feed lines can be interconnected by opening the cross feed valve ('''E''' switch).
main tank fuel when its fuel level will be below 600 lbs. Check valves prevent reverse fuel
flow from the main tank to the wing tank.


In the event of a main tank boost pump failure, the affected engine will suction-feed from the
The wing boost pumps ('''G''' switch) supply the respective engines until the wing tanks are empty, then the wing boost pumps automatically shut off. The main boost pumps then supply the respective engines with the remainder fuel in main tanks.
affected tank for all power setting up to an altitude of nearly 10,000 feet.


Unequal fuel level between right main and left main tank (imbalance superior 750 lbs) will cause
In case of a wing tank boost pump failure, the wing tank fuel will gravity feed its respective main tank if the main tank fuel level is below 600 lbs. Check valves prevent reverse fuel flow from the main tank to the wing tank.
center of gravity shift that may exceed allowable limits. In this case, a valve named "tank gate"
could link the two main tanks.


Fuel from the external tanks is transfered to the main or wing tanks by pressure from
In case of a main tank boost pump failure, the affected engine will suction-feed from the affected tank for all power setting up to an altitude of nearly 10,000 feet.
the bleed air system. Wing tanks can be topped when the fuel level is below 1590 lbs.
 
Unequal fuel level between right main and left main tank (imbalance superior 750 lbs) will cause a longitudinal CG shift that may exceed allowable limits. In this case, a valve named "tank gate" could link the two main tanks.
 
Fuel from the external tanks is transfered to the wing or main tanks by pressure from the bleed air system. Wing tanks can be topped when the fuel level is below 1590 lbs.
Main tanks can be topped when the fuel level is below 3034 lbs.
Main tanks can be topped when the fuel level is below 3034 lbs.
The cycling is repeated until fuel is depleted from the external wing tanks first, and
The cycling is repeated until fuel is depleted from the external wing tanks first, and
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(<b>C</b>) Refuel Receiver Door lever.
(<b>C</b>) Refuel Receiver Door lever.


(<b>D</b>) Horizon Line
(<b>D</b>) External Tanks switches, Wings and Fuselage. Set to OFF to depressurize external tanks
 
(<b>E</b>) Primary Aiming Reticle Digital index.
 
(<b>F</b>) Magnetic Heading Tape.  


(<b>G</b>) Indicated Altitude in feet (ASL).  
(<b>E</b>) Cross Feed switch, allow any operating boost pump to feed both engines.


(<b>H</b>) Radar Altitude in feet (AGL) followed by letter "R".  
(<b>F</b>) Tank Gate switch, open a valve linking the left and right main fuel tanks.  


(<b>G</b>) .


(<b>H</b>) .


=== HUD ===
=== HUD ===
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