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18 Cards in this Set
- Front
- Back
State the funtion of the propeller on an E-2C/C-2A system
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convert power developed by engine into thrust
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What part of the propeller system has electrical anti/de-ice components
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front and rear spinners and leading edge of the blade
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Name the major subassemblies of the propeller
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front spinner, back spinner, propeller dome, propeller hub, blades, propeller control assembly
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State the function of the following major engine components:
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(blank)
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Reduction gear box
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reduces power section RPM to the range of efficient RPM
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Torquemeter
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transmits and measures torque produced by power section
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Compressor assembly
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compressor air inlet housing, compressor rotor, 2 piece compressor case, diffuser
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Accessory drive housing
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provides mounting pads for fuel pump, fuel control, external scavenge oil pump, and generator
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Combustion section
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six individual combustion liners evenly spaced in an annulus formed by outer and inner casings
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Turbine section
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consist of turbine inlet casings and front/rear bearing support, rotor vane casing, vane assemblies
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State the six major subassemblies of the propeller on a C-2A
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hub, dome, 4 blades, electrical contact ring assembly, low pitch stop assembly, pitch lock regulator assembly
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State the function of the following fuel system components:
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(blank)
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Boost pumps
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2 in each fuel tank provide uninterrupted fuel flow to both engines down to 1% fuel remaining
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Fuel tank vent
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maintain fuel tank pressure during all aircraft operating conditions
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Fuel quantity probes
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provides an indication of fuel quantity on indicator in cockpit
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Fuel jettison (dump)
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permits dumping of excess fuel for proper landing weight
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State the maximum pressures for pressure fueling and suction defueling
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fueling 60 psi
defueling -1-2 psi |
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State the maximum fuel capacity in pounds
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12,400 lbs
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