(Refer to CAP698 figure 3.7)
Given:
Pressure Altitude: 4000 ft
Temperature: ISA +17° C
Take-off mass: 4000 lbs
Determine the rate of climb with both engines operating:
325 ft/min
1350 ft/min
1550 ft/min
1900 ft/min
(Refer to CAP698 figure 3.7)
Given:
Pressure Altitude: 4000 ft
Temperature: ISA +17° C
Take-off mass: 4000 lbs
Determine the rate of climb with both engines operating: