Class b aircraft climb

#1. For this question use Performance Manual CAP 698 SEP 1 Figure 2.3. Using the climb performance chart, for the single engine aeroplane, determine the rate of climb and the gradient of climb in the following conditions: Given:- O.A.T at Take-off: ISA , Airport pressure altitude: 3000 ft, Aeroplane mass: 3450 Ibs, Speed : 100 KIAS

• A1,310 ft/min and 11.3%
• B1,130 ft/min and 10.6%
• C1,030 ft/min and 8.4%
• D1,140 ft/min and 11.1%

#2. For this question use Performance Manual CAP 698 SEP 1 Figure 2.3. Using the climb performance chart, for the single engine aeroplane, determine the ground distance to reach a height of 1,500 ft in the following conditions: Given:- O.A.T at Take-off : ISA, Airport pressure altitude: 5,000 ft, Aeroplane mass: 3,300 Ibs, Speed: 100 KIAS, Wind component: 5 kts Tailwind.

• A19,250 ft.
• B14,275 ft
• C14,925 ft
• D15,625 ft

#3. For this question use Performance Manual CAP 698 SEP 1 Figure 2.3. With regard to the climb performance chart for the single engine aeroplane determine the climb speed (ft/min). Given O.A.T : ISA + 15°C, Pressure Altitude : 0 ft, Aeroplane Mass : 3,400 Ibs, Flaps : up, Speed: 100 KIAS.

• A1150 ft/min.
• B1290 ft/min.
• C1370 ft/min.
• D1210 ft/min.