AviationTire Performance - Aeroplanes Performance Class B - Multi Engine Use of performance graphs and tabulated data Q 5 / 5

(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 one engine inoperative:

View figure

175 ft/min
325 ft/min
350 ft/min
1550 ft/min