The a/c fuel system consists of how many tank systems and how does each system work?
The aux fuel system consists of an auxiliary tank which is located in the wingtip inboard of the engine nacelle.
-filled automatically through an overwing filler(fuel cap), this tank transfers fuel straight to the main system and when the aux tanks contain fuel it is used first and automatically transfers fuel into the nacelle tank.
The engine drives how many fuel pump systems?
A high pressure fuel pump an a low pressure boost pump.
What is the standby fuel boost pump driven by an what are its 3 functions
The standby by low pressure boost pump is electrically driven. It’s functions are:
1. Back up for engine driven boost pump
2. To pump aviation gas above FL200
3. To pump fuel during cross feed
Three sources of energy are used to prevent or to break up life formations on the airplanes surfaces what are they.
1.Bleed air (pneumatics)
2. Electrical power
3. Engine exhaust
Surfaces kept ice free by engine bleed-air (pneumatics) are?
1.Wing and horizontal stabilizer m leading edges with inflatable boots
2. Brakes
Surface kept ice and/or water free by electrical energy/power are?
Surfaces kept ice free by engine exhaust gases are?
The air inlets for both engines
What are the 3 sources of energy that parent or break up ice on surfaces
What surfaces are kept water an or ice free by electrical energy
Surfaces kept ice free by engine bleed air (pneumatics) are?
Surfaces kept ice free by engine exhaust gases are?
The air inlets for both engines
What serial number prefix do King Air B200 use
BB-
Eg: BB-2000
What is the a/c electrical system
28-VDC system (volts direct current)
Which recieves power from a 24 volt 42 ampere hour lead acid cell battery