CHAPTER 4
A2. Overspeed switch mechanism.
A3. Converts energy from compressed air to
REVIEW SUBSET NUMBER 1
shaft power.
A1. To provide specialized exterior lighting and
A4. Removing the positive potential.
illuminating the interior.
REVIEW SUBSET NUMBER 2
A2. To prevent filament fatigue failure.
A1. Jet engines run on a continuous burning
A3. Single and double contact bayonet.
fire.
A4. Navigation lights.
A2. The ignition exciter.
A5. Right wing tip.
A3. Between 45 percent and 65 percent of the
A6. Tanker aircraft.
engine rated speed.
A7. Amber.
A4. 34 pulses.
REVIEW SUBSET NUMBER 2
A5. A flameout or during aircraft weapons fire.
A1. Hydraulics.
REVIEW SUBSET NUMBER 3
A2. Control the flow of the fluid.
A1. Feather, ground stop, run, and airstart.
A3. The pump.
A 2 . When the power lever is above 66F
coordinator and the temp datum switch is
A4. Useful work by linear/reciprocating-
in AUTO.
mechanical motion.
A5. To ensure the hook is up and locked before
A3. Below 94 percent RPM.
removing hydraulic pressure.
A4. Chromel and Alumel.
A6. Nose wheel steering.
A5. A variable potentiometer, discriminating
A7. The airstream pressure.
device, and a cam-operated switch.
A8. 2,750 PSI.
REVIEW SUBSET NUMBER 4
REVIEW SUBSET NUMBER 3
A1. 65 percent RPM.
A1. Ram air temperature.
A2. 16, 65, and 94 percent switches.
A2. Crew safety and comfort.
A3. 10 percent.
A3. On the inner surface of the outer pane of
A4. To accommodate the temperature datum
glass.
valve.
A4. Hot air from combustion heaters or engine
A5. Drain valves.
A5. Electrical heating elements.
REVIEW SUBSET NUMBER 5
A1. Friction of the air over the aircraft creates
CHAPTER 5
enough heat to prevent icing.
REVIEW SUBSET NUMBER 1
A2. Hot bleed air and electrical.
A1. Start, constant speed drive, and air turbine
A3. Air at the inlet guide vanes.
motor generator.
AIV-3