An aircraft is currently at 1000 ft. If it needs to climb to 3500 ft over a distance of 15 NM while maintaining a groundspeed of 88 knots, what rate of climb in ft/min is necessary?
First, calculate the altitude to gain:
- Altitude to gain = 3500 ft - 1000 ft = 2500 ft
Convert distance and speed to time:
We know:
- Time = Distance ÷ Groundspeed
Time = 15 NM ÷ 88 kt = 0.17045 h
Convert hours to minutes:
- 0.17045 h x 60 = 10.23 minutes
Calculate required rate of climb:
Rate of Climb (RoC) is:
- RoC = altitude gain ÷ time
RoC = 2500 ft ÷ 10.23 min = 244.4 ft/min
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