viserfly

Questions for PRESSURE FUEL AND TEMPERATURE GAUGE( 1428-1487)

Answer the following questions

1.

A synchroscope is used on aircraft to

2.

The quantity of fuel in the tanks is measured by capacitor type contents gauges. The working principle of these sensors is to measure the

3.

If the tanks of your airplane only contain water, the capacitor gauges indicate

4.

The RPM indicator (or tachometer) of a piston engine can include a small red arc within the arc normally used (green arc)In the RPM range corresponding to this small red arc the

5.

A vibration indicator receives a signal from different sensors (accelerometers). It indicates the

6.

In transport airplanes, the temperatures are generally measured with :1- resistance thermometers2- thermocouple thermometers3- reactance thermometers4- capacitance thermometers5- mercury thermometersThe combination regrouping all the correct statements is

7.

The red pointer which is normally on the red line on the EGT (Exhaust Gas Temperature) indicators

8.

A millivoltmeter measuring the electromotive force between the ""hot junction"" and the ""cold junction"" of a thermocouple can be directly graduated in temperature values provided that the temperature of the

9.

The advantages of an electric float gauge are:1- ease of manufacture2- independence of the indication relative to the variations of the aircraft power system if the measurement is made by a ratiometer3- independence of the indication relative to the variations of the aircraft power system if the measurement is made by a galvanometer4- independence of the indication relative to temperature variationsThe combination regrouping all the correct statements is

10.

The sensors used to measure the exhaust gas temperature on an aircraft equipped with turbojets are

11.

The airplane outside air temperature ""probe"" measures the

12.

Torque can be determined by measuring the

13.

A thermocouple can be made of

14.

The electromotive force of a thermocouple is not modified if one or several intermediate metals are inserted in the circuit provided that

15.

The electronic tachometer sensor is composed of

16.

To permit turbine exit temperatures to be measured, gas turbines are equipped with thermometers which work on the following principle

17.

The static air temperature (SAT) is

18.

A manifold pressure gauge of a piston engine measures

19.

When compared with the volumetric fuel flowmeter, the mass fuel flowmeter takes into account the fuel

20.

The basic principle used for measuring a quantity of fuel in a transport airplane equipped with ""capacitor"" gauges is that the

21.

A ""Bourdon Tube"" is used in

22.

The signal supplied by a transmitter fitted with a 3-phase AC generator, connected to RPM indicator, is

23.

The probe used to measure the air intake pressure of a gas turbine engined powerplant

24.

The operating principle of Flowmeters, or ""unit flow meters,"" the most commonly used at the present time, is to measure across their system the

25.

The capacity fuel gauges provide information

26.

The pressure probe used to measure the pressure of a low pressure fuel pump is

27.

In a 3-phase synchronous motor type tachometer indicator :1- the transmitter is a direct current generator2- the voltage is proportional to the transmitter drive speed 3- the frequency is proportional to the transmitter drive speed4- the speed indicating element is a galvanometer5. the speed indicating element is an asynchronous motor driving a magnetic tachometerThe combination regrouping all the correct statements is

28.

In an engine vibration monitoring system for a turbojet any vibration produced by the engine is

29.

Different pressure sensors are used according to the intensity of the pressure measured (low, medium or high)Classify the following sensors by order of increasing pressure for which they are suitable :1- bellows type2- Bourdon tube type3- aneroid capsule type

30.

The main advantage of a ratiometer-type temperature indicator is that it

31.

In order to measure temperature the cylinder head temperature (CHT) gauge utilises a

32.

The operating principle of an ""electronic"" tachometer is to measure the

33.

The disadvantage of an electronic rpm indicator is the

34.

The gauge indicating the quantity of fuel measured by a capacity gauging system can be graduated directly in weight units because the dielectric constant of fuel is

35.

Among the following engine instruments, the one operating with an aneroid pressure diaphragm is the

36.

On an aeroplane equipped with a constant speed propeller, the RPM indicator enables

37.

The operating principle of the ""induction"" type of tachometer is to measure the

38.

The principle of capacitor gauges is based on

39.

The transmitter of RPM indicator may consist of :1- a magnetic sensor supplying an induced AC voltage2- a DC generator supplying a DC voltage3- a single-phase AC generator supplying an AC voltage4- a three-phase AC generator supplying a three-phase voltageThe combination of correct statements is

40.

The disadvantages of a single-phase A.C. generator tachometer are:1- the presence of spurious signals due to a D.C. generator commutator2- the importance of line resistance on the information value3- the influence of temperature on the tachometer informationThe combination regrouping all the correct statements is

41.

The yellow sector of the temperature gauge corresponds to

42.

A thermocouple type thermometer consists of

43.

The total air temperature (TAT) is always

44.

The principle of detection of a vibration monitoring system is based on the use of

45.

The indication of a fuel float gauge varies with :1- aircraft attitude2- accelerations3- atmospheric pressure4- temperatureThe combination of correct statements is

46.

The measurement of the turbine temperature or of the EGT (Exhaust Gas Temperature) is carried out at the

47.

Given :M is the Mach numberTs is the static temperatureTt is the total temperature

48.

The white sector of the arc of a temperature gauge corresponds to

49.

The float type fuel gauges provide information on

50.

The disavantages of an ""electric"" fuel (float) gauge are :1- the design is complex2- the indications are influenced by the airplane attitude variations3- the indications are influenced by the accelerations 4- the indications are influenced by temperature variations5- that an alternative current supply is necessaryThe combination regrouping all the correct statements is