ASSIGNMENT Chapter 4 AIRCRAFT ELECTRICAL SYSTEMS
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1 ASSIGNMENT Chapter 4 AIRCRAFT ELECTRICAL SYSTEMS 4-1. What are the two most common types of bulb bases? A. Single wire and single contact B. Doubled filament and index C. Single and double contact bayonet D. Clear and frosted 4-2. On which wing tip will the green navigation light be found? A. Left B. Right C. Both left and right D. Wing tips do not have navigation lights 4-3. The science of liquid pressure and flow is known as. A. Rotary-mechanical B. Hydraulics C. Fluid power D. Actuating pressure 4-4. What system provides the pilot with adequate directional control during ground operations? A. Push button switch B. Rudder pedal C. Hydraulic steer-damp D. Nose wheel steering 4-5. The pneumatic system compressor comes on when system pressure drops below what PSI value? A. 100 B. 1,500 C. 2,750 D. 3,150
2 4-6. Where is the resistance heating element installed in electrically heated windshields? A. Outer surface of windshield B. Current buss bars C. Inner surface of the outer pane of glass D. Lower surface of the inner pane of glass 4-7. What type of light provides the landing safety officer with a visual indication of a carrier aircraft s safe or unsafe landing configuration? A. Index B. Position C. Formation D. Approach 4-8. What is the landing configuration of an aircraft if the Landing Signal Officer (LSO) observes flashing approach lights? A. The landing gear only is up B. The landing and arresting gears are up C. The arresting gear is not fully extended D. Normal operation 4-9. The fuselage formation lights are connected in parallel with and controlled by the same switches as what other lights? A. The fuselage signal lights only B. The wingtip formation lights only C. The fuselage signal and wingtip formation lights only D. The fuselage signal, wingtip formation, and navigation lights What lighting feature is provided to aid a crew member who is reading a chart? A. Red floodlights B. White floodlights C. Extension lights D. Momentary contact switches to bypass the rheostats on floodlights
3 4-11. In aircraft hydraulic systems, the AE maintains circuits that control the fluid. A. viscosity B. flow C. shape D. pressure Which of the following components directs the fluid flow in a hydraulic system? A. Reservoir B. Pump C. Selector valve D. Actuating unit The catapulting system s launch bar warning light illuminates when which of the following conditions exist? A. The launch bar is up and locked with weight off the landing gear B. The launch bar is up and locked with weight on the landing gear C. Solenoid B is energized D. Solenoid A is energized Which of the following is a correct temperature equivalent? A. 100 C = 212 F B. 32 C = 212 F C. 32 F = 100 C D. 0 F = 32 C In an aircraft, cabin air pressure is controlled by the operation of which of the following components? A. A safety valve and a manual dump control B. A pressure regulator and a safety valve C. A manual dump control and a pressure regulator D. Bleed air shut off valve
4 4-16. Which knob controls warm, dry air used as muscle air for the Avionics flow control valve and the cabin flow valve? A. BLEED AIR B. TEMP CABIN C. CABIN PRESS D. ANTI ICE Windshield overheating is prevented by the combined actions of a shutoff valve and what other component? A. A thermostat B. A dump valve C. A thermistor D. An electronic temperature controller What method is used to deice the empennage of P-3 aircraft? A. A powered, controlled system provides constant heat to the empennage B. Hot engine bleed air is circulated under the surfaces C. Leading edges of the vertical and horizontal stabilizers are electrically heated D. Heat from the cabin routed through control valves heats the empennage How many components are in a basic hydraulic system? A. One B. Two C. Three D. Four Which component of the Wing Flap Asymmetry system will allow a confidence check of the Wing Flap Asymmetry Shutoff valve and Shutoff Valve Test light without tripping the system? A. Wing Flap Control Valve B. Wing Flap Asymmetry Relay C. Wing Flap Brake Relay D. Test/Reset Switch
5 4-21. The Wing Flap system is made up of the Wing Flap Asymmetry system and the Wing Flap Position indicator system. What do both systems combined detect for? A. Automatic arrest of asymmetry and unequal extension B. Unequal extension of the wing flaps and the amount of wing flap extension from 0 to 50 percent C. Automatic arrest of asymmetry of the wing flap and amount of wing flap extension D. Amount of wing flap extension from 0 to 50 percent The Landing Gear Warning System uses the landing gear control levers as a visual indication for the landing gear position? What is the other type of indication to visually check the landing gear is up or down? A. Digital display B. Flashing wheels indication C. Three down and locked lights D. Warning flags What mechanically prevents movement of the landing gear control lever from the wheels down position when the aircraft weight is on the gear? A. A solenoid B. Torque-link switch C. Armature pin D. Shock strut oleo To maintain cabin temperature, the Cabin Temperature Channel of the temperature controller uses how many bridge circuits? A. one B. two C. three D. four
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