Technical General 01 2024
Technical General 01 2024
Technical General 01 2024
4) Electrons are
a. Positive charge
b. Negative charge
c. Neutral charge
24) How do large aircraft equipped with tricycle landing gear obtain steering
control on ground?
A) By use of nose wheel steering
B) By use of rudder
C) By use of differential braking
30) When responding to a TCAS 2 resolution advisory, the crew must respond
within:
A) 2.5 Seconds using g forces +-0.25g
B) 5 Seconds using g forces of +- 0.25g
C) 5 Seconds using g-forces of +-0.5g
32) How is the ice prevented from forming on the front wind shield of large
system:
A) Warm air is blown over the wind shield
B) De-icing fluids are sprayed
C) Electrically heated wind shields
33) In the event of an engine surging occurring, the correct action to be taken is :
A) Close throttle quickly
B) Close throttle slowly
C) To open throttle fully
34) Current is :
A) A magnetic field produce around the conductor
B) Potential difference across the conductor
C) The number of electrons passing any point in the conductor in one second
37) Viscosity?
Ans. Viscosity is defined as the measure of a fluid’s internal friction, or its
resistance to flow. A liquid that flows freely has a low viscosity (thin oil) and one
which is sluggish has a high viscosity (thick oil).
47) Operational rough air speed VRA/MRA should consist of the following
feature
A. Be maximum structural cruise speed is with ability to with gust loads
B. For utility category aircraft the positive load limit above is 4.4 and 1.76 the
negative limit load factor
C. Should be high enough to avoid staling and low enough to avoid damage
to the structure
52) The extreme right limitation a gust load diagram is the speed:
a. Vd
b. Vc
c. Vb
d. Vs
53) What’s the limit load factor for a nominal transport category aircraft?
a. 2.5g
b. 1.75g
c. 3.75g
d. 1.5g
58) The difference between anti icing and de-icing system is:
A) Anti icing system prevents the formation of ice while deicing system
removes the ice after it is formed
B) De-icing system prevents the formation of ice while anti icing system
removes the ice after it is formed
C) Anti icing is used in air while de-icing is used on ground
64) The altitude above which icing does not occur since the droplets are all frozen
and will not adhere to the aircrafts surface is:
A) 37,000 ft
B) 42,000 ft
C) 40,000 ft
Note:- 1. This questions are all compiled as received from other forums.
2. This questions and options are not exactly same as came in DGCA exams
and just for reference.
Regards
Easy Learning Aviation