Pitot Statis System Flashcards

1
Q

Plastic tubing which convey total air pressure to the air speed indicator and static air pressure to the airspeed, vertical speed indicator and the altimeter

A

Pitot static system

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2
Q

Design to measure operating parameters of the aircraft engine they usually quantity pressure and temperature also includes measuring engine speed

A

Engine instruments

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3
Q

Use in controlling aircraft flight attitude

A

Flight instruments

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4
Q

Indicates the position of the flaps extended downward through a flaps position transmitter operated through a low voltage regulator

A

Flaps indicator

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5
Q

Indicates and measures the alternator output voltage of the electrical system

A

Ammeter

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6
Q

Connected to the engine by a flexible drive shaft and geared to the engine so that when the engine turns so does the shaft

A

Tachometer indicator

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7
Q

Gyroscopic instrument operated by a vacuum system suction gauge reading at 5.3 in of mercury is desirable for cairo instrument like

A

Attitude indicator

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8
Q

Electronic flight instrument display capable of operating as a primary attitude indicator backup attitude indicator with primary rate of turn indicator it functions added air data information such as air speed altitude and vertical speed

A

G5

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9
Q

Panel mounted air data and fuel computer a wind indicator display for graphically showing winds aloft head tail wind and drift angle fuel flow sensors and an air temperature sensor

A

Tas 1000 or air data computer

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10
Q

The cockpit contains the blank this is similar to a car dashboard providing the pilot with information about the flight the engine and the circumstances of the aircraft

A

Instrument panel

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11
Q

Pertains to the development of electronic devices in communication and navigation as applied to aeronautics

A

Avionics

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12
Q

What is the meaning of ics

A

Intercommunication system

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13
Q

Serve as the communication one of t41 and sf 260 aircraft

A

Gtn 750 mfd

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14
Q

What is the frequency of fab tower during takeoff

A

133.00

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15
Q

G5 has an external lithium ion battery that provides up to how many hours

A

4 hours

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16
Q

Radio station that transmit vhf radio signal in all direction over a certain area at 360° is called

17
Q

Radio station that transmit vhf radio signal in all direction over a certain area at 360° is called

18
Q

The antenna should be mounted blank on a bottom surface of the aircraft

19
Q

Serve as the communication 2 of t41 and sf 260 aircraft

20
Q

Test equipment used to test the transponder system

21
Q

Used to test the vor

22
Q

Emergency source of electrical power

23
Q

Rating of t41d alternator

A

28 volts 38 amperes

24
Q

Supplies fuel flow for start priming and engine operation if the engine driven pump should fail

A

Electric auxiliary fuel pump

25
Resistance is measured in units called
Ohms
26
Electricity which flows steadily in the same direction such as electricity produced by battery is
Direct current
27
Comprise of an electric motor and transmission assembly drive pulleys push pull rods cables and a follow-up control
Wing flaps system
28
Lightning system is mounted on each wing tip and aft end of the tail cone
Navigation lights
29
Protect aircraft electrical system from damage and failures
Circuit breaker fuses circuit protector
30
Primary source of electrical power of t41
Alternator
31
Regulates the output voltage of the alternator
Voltage regulator
32
Indicates the amount of current flowing
Ammeter
33
It is mounted at the leading edge of the left wing both lights used for takeoff and landing
Landing and taxi lights
34
Power rating of sf 260h alternator is
28 volts dc 70 amperes
35
What magneto is being used during starting of sf 260 fh aircraft
Left magneto
36
Converts the output voltage of the alternator from ac to dc
Rectifier diode
37
What does the flaps indicator indicates while the flaps are traveling
Stripped
38
This components activate the three greens on the landing gear control panel when the landing gears are done and lock
Down locked switch
39
This component located on the left main landing gear prevents the landing gear to retract while the aircraft is on the ground
Anti retraction switch