Q2. Any acceleration in climb, with a constant power setting:
A) decreases the rate of climb and the angle of climb
B) improves the rate of climb if the airspeed is below VY
C) improves the climb gradient if the airspeed is below VX
D) decreases rate of climb and increase angle of climb
The only way we can accelerate in the climb at a constant power setting is to lower the nose, lowering the nose will decrease both the ROC & Angle Of Climb.
Q3.For a single engine class B aeroplane, V2 may not be less than:
A) not applicable
(V2 is the Speed at which the a/c becomes airborne safely with 1 engine Inop)
B) 1.15Vs
C) 1.2Vs
D) 1.5Vs
Q4. Regarding take-off, the take-off decision speed V1:
A) Is always equal to VEF (Engine Failure speed)
B) Is an airspeed at which the aeroplane is airborne but below 35 ft and the pilot is assumed to have made a decision to continue or discontinue the take-off
C) Is the airspeed of the aeroplane upon reaching 35 feet above the take-off surface
D) Is the airspeed on the ground at which the pilot is assumed to have made a decision to continue or discontinue the take-off
Q5. Any acceleration in climb, with a constant power setting:
A) decreases the rate of climb and the angle of climb
B) improves the rate of climb if the airspeed is below VY
C) improves the climb gradient if the airspeed is below VX
D) decreases rate of climb and increase angle of climb
Q6.The stall speed of an aircraft will increase with:
(a) decrease in the load factor
(b) increase in the pitch attitude for straight and level
(c) increase in the all up weight of the aircraft
Q1.NH wind at 2000ft 210/60. Thermal wind 20 knots. Lowest Mean temp : NW. Find upper wind?
Help anyone?
Correct me if I am wrong!
AP