End of Book Questions Chapter 7 Aircraft Power Plants
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1 End of Book Questions Chapter 7 Aircraft Power Plants 7-1. What engine does NOT draw air from the outside to fuel the combustion process? A. Gas turbine B. Rocket C. Turboprop D. Turboshaft 7-2. How many types of jet propulsion engines are there? A. 2 B. 4 C. 6 D How many major components make up a turbojet engine? B. 3 C. 5 D How many types of gas turbine engine are there? B. 2 C. 3 D Which of Newton s laws of motion explains the operation of jet propulsion? A. First B. Third C. Fifth D. Seventh 7-6. What component is an opening in the front of the aircraft that allows outside air to enter the engine? D. Turbine
2 7-7. Which of the following types of aircraft uses a turbojet engine? A. H-57 B. F/A-18 C. T-6 D. C What component is attached to the rear of the turbine assembly and is a tapered, cylindershaped outlet for the gases? D. Exhaust cone 7-9. What component is made up of a series of rotating blades and a row of stationary stator vanes? D. Exhaust cone How many igniter plugs are usually on an engine? A. 2 B. 3 C. 4 D What section of a turbojet engine drives the compressor and accessories by extracting some of the energy and pressure from the combustion gases? D. Turbine What engine was developed to provide the power requirements for aircraft of greater size, carrying capacity, range, and speed? A. Rocket B. Turboprop C. Turborotor D. Turboshaft How many major sections make up a turboprop engine? B. 2 C. 3 D. 4
3 7-14. What section of a turboprop engine consists of an axial-flow compressor, a combustion chamber, a multi-stage turbine, and an exhaust? A. Power B. Reduction C. Torquemeter D. Tail What assembly on a turboprop engine lowers the engine rpm within the range of efficient propeller rpm? A. Power B. Reduction C. Torquemeter D. Tail What type of engine has a high power-to-weight ratio and is widely used in helicopters? A. Rocket B. Turbojet C. Turboprop D. Turboshaft What control system on a gas turbine engine assists in cooling the engine? A. Accessory B. Ignition C. Fuel control D. Lubrication What component on an engine is the heart of the gas fuel system? A. Accessory section B. Ignition system C. Fuel control D. Exhaust cone For what do gas turbine engines use high voltage and a spark of high heat intensity? A. Cooling B. Ignition C. Thrust D. Shutdown How many different types of ignition systems are used on gas turbine engines? B. 2 C. 3 D. 4
4 7-21. What type of lubricant is used in all gas turbine engine lubrication systems? A. AMS oil B. Synthetic oil C. Hydraulic fluid D. Synthetic hydraulic fluid What section on a gas turbine engine is usually mounted beneath the compressor? A. Fuel control B. Accessory C. Ignition D. Lubrication What cycle is used to describe the gas turbine engine s cycle? A. Amber B. Braxton C. Brayton D. Camber In the ANA Bulletin No. 306m Designation System, the number 30 is used for what branch of service? A. Army B. Coast guard C. Air Force D. Navy What symbol is used for a turbojet engine? A. A B. J C. K D. T What symbol is used for a turboprop engine? A. A B. J C. K D. T How many designation systems are used to identify aircraft power plants? A. 2 B. 4 C. 6 D. 8
5 7-28. What letter preceding the basic designation signifies a special designation? A. A B. B C. X D. Z What is the engine manufacturer symbol for United Aircraft of Canada Ltd.? A. AD B. BA C. CA D. CP What is the engine manufacturer symbol for AiResearch Division, Garrett Corp.? A. BA B. GA C. LD D. MD Without ear protection, persons exposed to sound intensities above what db may suffer hearing damage? 10 B. 120 C. 130 D What area on an aircraft produces the two most serious hazards, the high temperature and the high velocity of the tailpipe? A. Exhaust B. Intake C. Landing gear D. Main rotor What area on an aircraft develops enough suction to pull in an individual? A. Exhaust B. Intake C. Landing gear D. Main rotor Keeping aircraft and power plants in top operating condition is the principal function of what type of personnel? A. Admin B. Maintenance C. Medical D. Security
6 7-35. In the MIL-STD-1812 engine designation system, what number is used by the Navy? 00 B. 200 C. 300 D. 400
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