Chapter 2 section A airplane systems Flashcards

section a (46 cards)

1
Q

Fuselage

A

houses the cabin and cockpit, controls for airplane, cargo, and occupants
also attaches other airplane components

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2
Q

wing

A

air flows around the wings of an airplane and generates lift.
attached to the top, middle or lower portion of the fuselage

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3
Q

monoplanes

A

airplanes with one set of wings

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4
Q

biplanes

A

two sets of wings

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5
Q

two types of control surfaces attached to the rear of the wing or trailing edges

A

ailerons and flaps

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6
Q

ailerons

A

connected to the outside portion of the wing, connected to the cockpit control,
ailerons move in opposite directions to roll the plane in and out of turns.

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7
Q

flaps

A

inner portion of the wing

extend downward to increase wing’s lift for takeoff and landing

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8
Q

empennage

A

consists of vertical stabilizer, horizontal stabilizer, and elevator
help maintain straight path through the air

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9
Q

rudder

A

attached to the back of the vertical stabilizer
for moving the plane left or right
operated by pedals
combination of ailerons and rudder to turn plane

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10
Q

elevator

A

attached to horizontal stabilizer

for increasing or decreasing altitude

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11
Q

stabilator

A

pivots up and down, replacement for elevator

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12
Q

trim tab

A

usually located on elevator,

help minimize workload on flight controls

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13
Q

anti-servo tab

A

provides a control feel, also functions as a trim tab

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14
Q

landing gear

A

supports plane while on ground, normally three wheels

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15
Q

conventional landing gear

A

tailwheel planes, two wheels in front one on tail

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16
Q

nose wheel/ tricycle gear

A

one wheel at the nose, two at the back

steer airplane using rudder pedal

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17
Q

fixed gear

A

always remains extended, low cost

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18
Q

retractable gear

A

stows the landing gear inside the airplane

for high performance aircraft

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19
Q

landing gear struts

A

act as a shock that are attached to the wheels

20
Q

oleo strut

A

uses a piston enclosed in a cylinder with oil and compressed air to absorb the bumps and jolts

21
Q

disc brakes

A

can apply brakes by pressing on each rudder pedal

for a straight line press down on both simultaneously

22
Q

differential braking

A

helps steer the plane while taxiing

23
Q

powerplant

A

includes the engine and the propeller

24
Q

engine

A

primary function is for power to the propeller, and heat to the cabin

25
firewall
located between the engine compartment and the cockpit serves as a mounting point protects occupants
26
cowling
increases engine cooling effectiveness by ducting air around the cylinder, encloses the engine compartment
27
propeller
mounted on front of the engine | translates the rotational force of the engine into thrust
28
pilot's operating handbook (POH)
contains make and model of plane
29
FAA approved airplane flight manual (AFM)
required to be in every current manufactured plane by the FAA must be accessible through flight
30
FAA approved airplane flight manual includes
1. general 2. limitations 3. emergency procedures 4. normal procedures 5. performance 6. weight and balance 7. airplane and systems descriptions 8. handling, service and maintenance 9. supplements 10. safety and operations tips
31
Pilot's information manual (PIM)
contains the same information as the flight manual except for exact weight and balance data not updated
32
12 month inspection (annual)
annual | emergency locator transmitter (ELT)
33
Every 24 months
Transponder | altimeter and static system
34
100 hour inspections
aircraft used for flight instruction for hire and provided by flight instructor aircraft that carry any person, other than a crew member, for hire may overfly by 10 hours inspection due before 100 hours of flight
35
Emergency Locator transmitter replacement
if operated for more than 1 hour or after 50 % of batter life has expired
36
aircraft maintenance records
consist of logbooks for airframe, engine, and propeller operator must have readily available examine to insure the required inspections
37
Preventive maintenance
allowed to be done by private pilots | ex, replacing spark plugs, servicing wheels, bearing and struts, replacing and servicing batteries
38
Airworthiness directive
FAA part 39, can be a mandated (legal) one time fix for a defect. Either an Emergency AD (immediate compliance before flown) or not an Emergency AD (time frame to get fixed)
39
Minimum Flight Instruments for VFR day and night
Airspeed indicator, altimeter, magnetic compass
40
Minimum Engine and System monitoring indicator for VFR DAy and Night
Tachometer manifold pressure gauge fuel gauge for each tank oil temperature gauge for air cooled engine oil pressure gauge temperature gauge for liquid cooled engine landing gear position indicator for retractable landing gear
41
minimum requirement list (mel)
indicates the equipment that is allowed to be inoperative for a particular flight if it is not required by the regulations for day or night VFR specified by FAR 91.205
42
VFR Day and NIGHT
``` standby airspeed indicator standby altimeter altimeter airspeed indicator magnetic compass pilot system static system normal ```
43
Kinds of operations equipment list (KOEL)
in the limitations section of the AFM | specifies required equipment for conditions such as DAY VFR, NIght VFR, or IFR
44
IFR day and NIght
``` standby airspeed indicator PFD altimeter Standby ALtimeter PFD Heading Altimeter Airspeed indication Magnetic COmpass Attitude Gyro HSI Turn Coordinator CLock Nav Radio Pitot System Static System norma ```
45
Special Flight Permit aka ferry permit
allows plane to be flown to location for repairs obtained through the FAA flight standards district office (FSDO) if not allowed due to AD, AMT may have to be transported to the aircraft to resolve AD
46
four requirements must be checked if the equipment must be operational for the flight
Airworthiness Directive kinds of operations equipment list VFR day type certificate requirements prescribed in airworthiness flight rules for kind of flight being conducted