(Refer to CAP 698 figure 3.7)
Given:
Pressure Altitude: 14 000 ft
Temperature: ISA +15° C
Take-off mass: 4750 lbs
Determine the rate of climb with both engines operating:
625 ft/min
750 ft/min
800 ft/min
1550 ft/min
(Refer to CAP 698 figure 3.7)
Given:
Pressure Altitude: 14 000 ft
Temperature: ISA +15° C
Take-off mass: 4750 lbs
Determine the rate of climb with both engines operating: