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43 Cards in this Set

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Explain the fuselage sections: Forward, Midbody, and aft fuselage.
Forward - includes the flight station.
Midbody - The midsection of the aircraft.
Aft fuselage - Includes the tail cone.
Explain the wing center section.
Consists of a box type beam which is an assembly of the front and rear spars, top and bottom skin panel, and ribs.
Explain the left and right wing outer panel.
Consists of wing flaps, leading and trailing edges, wingtips, ailerons, and engine nacelles.
Explain the tail sections: horizontal and vertical stabilizers.
Horizontal - Up and down.
Vertical - Left and right.
Provides stability of the aircraft.
Explain the flight control/ surface section: flaps.
Take offs and landings.
Explain the flight control/ surface section: Ailerons.
Helps turn plane side to side. (moves opposite)
Explain the flight control/ surface section: Rudder.
Pedals used to move aircraft on a vertical axis. (moves same)
Explain the flight control/ surface section: Elevators.
Control stick forward - Aircraft climbs.
Control stick aft - Aircraft dives/ descends.
Explain the flight control/ surface section: Trim tabs.
Enables pilot to ease through any unbalanced condition.
Explain the landing gear: Strut.
Absorbs the shock during take off and landing.
Explain the landing gear: Brakes.
Stops the aircraft.
Explain the landing gear: Wheels.
Made from magnesium or aluminum alloys. 2 general types (divided and demountable)
Explain the hydraulic system: Pumps.
There are 3 electrically driven, variable displacement type hydraulic pumps.
Explain the hydraulic system: Reservoirs (2).
1) max - 5.6 US gallons
2) max - 1 gallon
Explain the hydraulic system: Booster assemblies.
Allows pilot to have a normal feel of controls without considerable force.
Explain the hydraulic system: Actuators.
Transforms hydraulic fluid pressure into mechanical force.
Explain the following airframe component: Forward radome.
Serves as support for the hinges, latches, and aligning pin receptacles.
Explain the following airframe component: Aft radome.
Used as housing for the aft radar antenna, the MAD equipmenr, and two sensors for the missle warning system.
Explain the following airframe component: Bombay.
Transports weapons and cargo.
Explain the following Cabin Pressurization system: Engine Driven Compressor (EDC).
One of the ways to get air conditioning.
Explain the following Cabin Pressurization system: Cabin exhaust fan.
Air is drawn through the aircraft by the cabin exhaust fan.
Explain the following Cabin Pressurization system: Outflow valve.
Depressurize - Open.
Pressurize - Closed.
Explain the following Air Conditioning system: Refrigeration turbine.
Cooled by rapid expansion.
Explain the following Air Conditioning system: Heat exchanger.
80% of the cooling.
2 heat exchanger fans (primary and secondary)
Explain the following High Rate of Discharge (HRD) bottles: engine.
Equipped with 2 indpendent fire extinguishing systems.
Explain the following High Rate of Discharge (HRD) bottles: APU.
At a temp of 400 degrees, warning light glows, warning horns sound, and APU shuts down.
Explain the one of the two types of oxygen bottles: walkaround.
7-22 minutes at its best. 5-10 if not.
Explain the one of the two types of oxygen bottles: Main.
3 (P, CP, FE) Supplies 3 ppl for 3-5 hours at an altitude of 25,000 feet.
State the purpose of the aircraft foul weather system.
Enables the aircraft to perform its mission under various weather conditions.
Describe the following foul weather system: ice detector.
Indicates if structural icing conditions exist.
Describe the following foul weather system: Angle of Attack (AOA) heat.
Prevents ice formation on the AOA probe..
Describe the following foul weather system: engine ice control.
Prevents ice formation on the engine air scoop, torque meter shroud, and compressor.
Describe the following foul weather system: propeller ice control (prop deice)
As long as the system is operating, continuous heat anti icing is appled to the front spinners.
Describe the following foul weather system: wing deice.
Removes ice from the wing leading edges.
Describe the following foul weather system: Empennage ice control (EMP deice)
The horizontal and vertical stabilizer leading edges are electrically heated.
Describe the following foul weather system: windshield heating.
Prevents icing.
Describe the following foul weather system: windshield wipers.
Controlled by the P or CP.
Describe the following foul weather system: pitot heat.
The two pitot tubes are anti iced by an integral heating element.
Explain the following component: Structure.
Composed of 3 major components: forward, center, aft.
Explain the following component: flight control/ surface.
Operated from the flight station through conventional cable systems.
Explain the following component: hydraulics.
Operated from independent 3000 psi hydraulic systems No.1 and No.2
Define the following terms: Anti icing, Deicing.
Anti icing - Prevents ice formation.
Deicing - Removes ice build up.
What are the 3 methods that generate air conditioning?
1 - EDCs.
2 - Air multiplier.
3 - Ambient air.