Vayudoot Aviation

1. The two principal types of direct reading pressure gauge are

the Bourdon tube type and the capsule operated type

manifold pressure type and engine pressure type

capacitance type and bellows

2. An aircraft has a compensated capacitance fuel contents gauging system and is refueled so that the total fuel contents are 76,000kg at a temperature of 18 degrees C and an S.G. of 0.81. whilst the aircraft is parked and temperature increases to 26 degrees C and the S.G. becomes 0.80. the indicated fuel contents have

remained the same

increased by 10%

decreased by 5%

3. Which of the following are used to measure temperature? 1. Thermocouple 2. Resistance 3. Reactance 4. Mercury

1,2,3,4

1,2&4

1,3&4

4. The "Bourdon tube" is used to measure

pressure

vibrations

fuel flow

5. What type of sensor is used to measure the output of a low pressure booster pump

bourdon tube

aneroid capsule

bellows

Question Bank

Questions for R* BL POWER PLANT AND SYSTEM MONITORING

Question Bank

Questions for R* B*L* POWER PLANT AND SYSTEM MONITORING

Questions for R* BL POWER PLANT AND SYSTEM MONITORING