Pitot Statis System Flashcards
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
Pitot static system
Design to measure operating parameters of the aircraft engine they usually quantity pressure and temperature also includes measuring engine speed
Engine instruments
Use in controlling aircraft flight attitude
Flight instruments
Indicates the position of the flaps extended downward through a flaps position transmitter operated through a low voltage regulator
Flaps indicator
Indicates and measures the alternator output voltage of the electrical system
Ammeter
Connected to the engine by a flexible drive shaft and geared to the engine so that when the engine turns so does the shaft
Tachometer indicator
Gyroscopic instrument operated by a vacuum system suction gauge reading at 5.3 in of mercury is desirable for cairo instrument like
Attitude indicator
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
G5
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
Tas 1000 or air data computer
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
Instrument panel
Pertains to the development of electronic devices in communication and navigation as applied to aeronautics
Avionics
What is the meaning of ics
Intercommunication system
Serve as the communication one of t41 and sf 260 aircraft
Gtn 750 mfd
What is the frequency of fab tower during takeoff
133.00
G5 has an external lithium ion battery that provides up to how many hours
4 hours
Radio station that transmit vhf radio signal in all direction over a certain area at 360° is called
VOR
Radio station that transmit vhf radio signal in all direction over a certain area at 360° is called
VOR
The antenna should be mounted blank on a bottom surface of the aircraft
Vertical
Serve as the communication 2 of t41 and sf 260 aircraft
Gnc 255
Test equipment used to test the transponder system
Ifr 6,000
Used to test the vor
Ifr 4000
Emergency source of electrical power
Battery
Rating of t41d alternator
28 volts 38 amperes
Supplies fuel flow for start priming and engine operation if the engine driven pump should fail
Electric auxiliary fuel pump
Resistance is measured in units called
Ohms
Electricity which flows steadily in the same direction such as electricity produced by battery is
Direct current
Comprise of an electric motor and transmission assembly drive pulleys push pull rods cables and a follow-up control
Wing flaps system
Lightning system is mounted on each wing tip and aft end of the tail cone
Navigation lights
Protect aircraft electrical system from damage and failures
Circuit breaker fuses circuit protector
Primary source of electrical power of t41
Alternator
Regulates the output voltage of the alternator
Voltage regulator
Indicates the amount of current flowing
Ammeter
It is mounted at the leading edge of the left wing both lights used for takeoff and landing
Landing and taxi lights
Power rating of sf 260h alternator is
28 volts dc 70 amperes
What magneto is being used during starting of sf 260 fh aircraft
Left magneto
Converts the output voltage of the alternator from ac to dc
Rectifier diode
What does the flaps indicator indicates while the flaps are traveling
Stripped
This components activate the three greens on the landing gear control panel when the landing gears are done and lock
Down locked switch
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
