WorksheetsBlock 1- Unit 2a Practice Quiz
Total questions: 12
Worksheet time: 12mins
The ___________: the main structural assembly to which other assemblies are directly or indirectly attached.
Fuselage
Empennage
Wings
Engines
Which major structural area of an aircraft is used to create lift for the aircraft and also provide stability/support during flight?
Engines
Vertical Stabilizer
Wings
Landing Gear
Which aircraft structure is designed to reduce the left/right swaying motion of the tail?
Horizontal Stabilizer
Vertical Stabilizer
Wings
Fuselage
A _______ engine uses a fan at the intake to increase thrust.
Turboshaft
Turbofan
Turboprop
Turboblade
Which main structural area of an aircraft provides a means to take-off and land while also supporting the aircraft when it is on the ground?
Wings
Fuselage
Engines
Landing Gear
A ________ engine uses a shaft & transmission to drive a helicopter rotor.
Turboprop
Turboshaft
Turbofan
Turboblade
A ________ engine combines a turbine engine, a reduction gearbox, and a propeller.
Turbofan
Turboshaft
Turbogear
Turboprop
Engines provide the power needed for the forward ________ of the aircraft.
Drag
Thrust
Lift
Gravity
What is the aft section of the aircraft that mounts to the fuselage?
Empanada
Empoleon
Empennage
Rearnage
Which aircraft structure is designed to reduce unwanted up and down movements of the tail?
Empennage
Fuselage
Vertical Stabilizer
Horizontal Stabilizer
What are streamlined enclosures used primarily to house and protect the engine and its components, the landing gear when retracted and stowed in the wheel well, and the external fuel tanks if installed?
Fuselages
Empennages
Nacelles
Wings
Where would the Vertical Stabilizer & Horizontal Stabilizer be located at?
On the fuselage
On the empennage
On the wings
On the landing gear
