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30 Cards in this Set

  • Front
  • Back

Static pressure

Altemeter


Vertical speed

Pitot pressure


يقيس في

Air speed


Machmeter

Air speed العملية

Pd=pt-ps

Machmeter العملية

Pd=pt-ps/ps

pfd

Electronic primary flight display

Fms

Flight management system

تكرار

Duplication

Aircraft speeds

Ias indicated air speed


Cas


Eas equivalent air speed


Tas

Density isa

1225gm m3

سرعة صوت على الارض

661.32knots

باش طلع Mach number متاع طيارة

Tas/lss

Total air temperature probe

لقياس


Temperature في الارض


Static air temperature

Engine instrument

N1 low pressure compressor


N2 high pressure compressor


Egt exhaust gas temperature


Engine pressure ratio


Fuel flow


Oil pressure

Gyroscope instrument

heading indicator


turn coordinator


attitude indicator (artificial horizon)

non gyro indicator

Air speed indicator


Machmeter


Vertical speed indicator


Altemeter indicator

مساعد او اضافي

auxiliary

مقياس

Gauge

Gyroscope spinning

25.000 rpm

صلابة

Rigidity

Gyroscope flight driven by :

Air ( suction gyro engine drevin vacum pump )


electric gyro ( ac motor)

Air data computer (adc) باش يخدم يحب

Pitot


static


Total temperature


Weight on wheel


modern aircraft, the ADC is typically integrated with other avionics systems, such as the Flight Management System (FMS) or the Autopilot,

AVGAS

Aviation gasoline

تفجير

detonation

Fuel strainer


شبيه ب filter

heading indicator


turn coordinator


Attitude indicator

One degree of freedom


One or two degree of freedom it shows roll and yaw


Three degree of freedom it shows pitch and roll

Fds

flight director system


Is integrated with the PFD .


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primary flight display provides real-time flight guidance system.


flight director system provides the guidance to specific flight path like autopilot .

متطلبات fds للعمل

Classification of electrical load

جيل جديد من csd

Integrated drive generator idg