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18 Cards in this Set

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

defueling -1-2 psi
State the maximum fuel capacity in pounds
12,400 lbs