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Avionics > Pitot Statis System > Flashcards

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

A

VOR

17
Q

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

A

VOR

18
Q

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

A

Vertical

19
Q

Serve as the communication 2 of t41 and sf 260 aircraft

A

Gnc 255

20
Q

Test equipment used to test the transponder system

A

Ifr 6,000

21
Q

Used to test the vor

A

Ifr 4000

22
Q

Emergency source of electrical power

A

Battery

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
Q

Resistance is measured in units called

A

Ohms

26
Q

Electricity which flows steadily in the same direction such as electricity produced by battery is

A

Direct current

27
Q

Comprise of an electric motor and transmission assembly drive pulleys push pull rods cables and a follow-up control

A

Wing flaps system

28
Q

Lightning system is mounted on each wing tip and aft end of the tail cone

A

Navigation lights

29
Q

Protect aircraft electrical system from damage and failures

A

Circuit breaker fuses circuit protector

30
Q

Primary source of electrical power of t41

A

Alternator

31
Q

Regulates the output voltage of the alternator

A

Voltage regulator

32
Q

Indicates the amount of current flowing

A

Ammeter

33
Q

It is mounted at the leading edge of the left wing both lights used for takeoff and landing

A

Landing and taxi lights

34
Q

Power rating of sf 260h alternator is

A

28 volts dc 70 amperes

35
Q

What magneto is being used during starting of sf 260 fh aircraft

A

Left magneto

36
Q

Converts the output voltage of the alternator from ac to dc

A

Rectifier diode

37
Q

What does the flaps indicator indicates while the flaps are traveling

A

Stripped

38
Q

This components activate the three greens on the landing gear control panel when the landing gears are done and lock

A

Down locked switch

39
Q

This component located on the left main landing gear prevents the landing gear to retract while the aircraft is on the ground

A

Anti retraction switch

Avionics (1 decks)

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