Chapter 2 Flashcards

Aircraft Systems

1
Q

Fuselage

A

Houses the cabin and cockpit

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2
Q

Open Truss

A

An airplane that is held together with struts and wire bracing

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3
Q

Stressed Skin

A

An airplane where the external skin is made of sheet metal, plywood, or composites such as fiberglass.

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4
Q

Monocoque

A

An airplane where its skin carries all of the flight loads. The structure can be very strong, but dents and deformation to the skin can be very hazardous.

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5
Q

Semi-Monocoque

A

An airplane where its skin only carries some of the flight loads. It has an increased strength to its skin because of a substructure that helps to keep the airplanes airframe intact.

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6
Q

Wings

A

The structures on the sides of the fuselage (either top, middle, or lower part of the airplane) that generates lift for the airplane to fly

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7
Q

Monoplane

A

An airplane with a single set of wings

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8
Q

Biplane

A

An airplane with two sets of wings on each side of the fuselage

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9
Q

Ailerons

A

Control surfaces located on the outside portion of the wings that produce a rolling motion, and are controlled via the yoke/control wheel

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10
Q

Flaps

A

Control surfaces that are located on the inner portion of the wings, and are extended downwards to produce more lift and drag.

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11
Q

Empennage

A

The back end of the airplane (tail) that consists of the vertical stabilizer, the rudder, the horizontal stabilizer, and the elevator.

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12
Q

Vertical Stabilizer

A

A vertical fin, typically referred to as the tail, that improves the overall stability for the airplane, and also houses the rudder.

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13
Q

Horizontal Stabilizer

A

A horizontal fin that, like the vertical fin, aids in stability for the airplane, and houses the elevator.

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14
Q

Rudder

A

A control surface located on the tail of the aircraft that produces a yaw motion. For many aircraft, the rudder is used to turn on the ground, and helps to keep a turn in the air stable. The rudder is controlled with the rudder pedals under the yoke.

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15
Q

Elevator

A

Two control surfaces located on the horizontal fin that aids in creating pitch for the aircraft. The elevator is controlled via the yoke by pulling it forward or by pushing it back.

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16
Q

Stabilator

A

Similar to the elevator, the stabilator is one singular control surface on the horizontal stabilizer.

17
Q

Trim Tab

A

A smaller control surface located on the elevator that is used to ease the pressure from moving the yoke. The trim tab causes a more aerodynamic flow over the elevator, that in turn makes it easier to control the airplane. The trim tab is controlled via the trim wheel in the cockpit.

18
Q

Anti-Servo Tab

A

A trim tab that is used on a stabilator to ease the aerodynamic pressure.

19
Q

Main Wheel

A

Two of three landing gear that make up a Cessna. The main wheels are positioned at the sides of the airplane and are responsible for differential breaking. The nose wheel is a smaller wheel positioned at the nose of the airplane and is used for turning on the ground.

20
Q

Conventional Landing Gear/Tailwheel

A

An airplane with a small wheel located on the tail of the aircraft instead of the nose. This is also known as a tailwheel aircraft.

21
Q

Nosewheel

A

An airplane that has a third wheel placed under the nose. This design is also referred to as a tricycle gear aircraft.

22
Q

Fixed Gear

A

An airplane’s landing gear that always remains extended and cannot be retracted into the fuselage.

23
Q

Retractable Gear

A

Landing gear that has the ability to retract into the fuselage. This is more expensive, but it reduces drag caused by the landing gear.

24
Q

Oleo Strut

A

A landing gear design where a piston is enclosed inside a metal cylinder with oil and compressed air to absorb the bumps and uneven terrain on the ground.

25
Q

Disc Brakes

A

Located on the main wheels, disc brakes are the mechanisms used to slow a Cessna down on the ground.

26
Q

Differential Braking

A

An individually controlled braking system, where you can slow the movement of the right main wheel but keep the left main wheel actively rotating. This can aid in aircraft ground maneuvering such as sharper turns (30 degree instead of 10.)

27
Q

Powerplant

A

All of the machinery that contributes to the generation of thrust (Engine and propeller)

28
Q

Engine

A

The part of the aircraft that generates power to spin the propeller, that in turn generates thrust. The engine is also responsible for other mechanisms such as generating electricity for the cockpit, air conditioning/heat, and engine-driven vacuum pump for the heading and attitude indicator.

29
Q

Firewall

A

Protects avionics and pilots from engine heat.

30
Q

Propeller

A

Two rotating blades that translates rotational force from the engine into forward-acting force based on Newton’s Third Law.

31
Q

Pilot’s Operating Handbook (POH)

A

A manual specific to each plane that can help inform pilots of information about that specific plane that may not apply to other planes. The POH also contains the weight and balance sheet and aircraft limitations which is critical to have located inside the airplane at all times.

32
Q

FAA Approved Airplane Flight Manual (AFM)

A

Contains the specific airplane’s serial number, registration number, and a tab that ensured the airplane is approved by the FAA.

33
Q

Pilot’s Information Manual (PIM)

A

Nearly identical to the POH, the PIM does not contain weight and balance, but can be used as a useful study tool.

34
Q

Annual Inspection

A

An inspection done every year by an aviation maintenance technician (AMT) to ensure an aircraft is still airworthy to fly.

35
Q

100-Hour Inspection

A

An inspection (done over the course of 100 hours) specific to flight instruction or any aircraft that carries people commercially.

36
Q

Preventive Maintenance

A

A type of maintenance that can be done by a private pilot. This includes, replacing and servicing batteries, spark plugs, and wheel bearings and struts.

37
Q

Airworthiness Directive (AD)

A

A legally enforceable rule that was assigned because of an unsafe condition that exists or one that can develop in an aircraft because of its design, maintenance, or another cause.

38
Q

Kinds of Operational Equipment List (KOEL)

A

Found in the limitations section of the AFM, the KOEL specifies the required equipment for conditions such as DAY VFR, NIGHT VFR, or IFR.

39
Q

Special Flight Permit/Ferry Permit

A

The event where the FAA permits an airplane that’s not typically airworthy to be flown to a location where the needed repairs can be made.