Using a normal climb under the given conditions, how much fuel would be used from engine start to a pressure altitude of 12,000 feet?

/in , /by

(Refer to figure 14.) GIVEN:

Aircraft weight 3,700 lb
Airport pressure altitude 4,000 ft
Temperature at 4,000 feet 21 °C

 

(Refer to figure 9.) Using a normal climb, how much fuel would be used from engine start to 12,000 feet pressure altitude?

/in , /by
Aircraft weight 3,800 lb
Airport pressure altitude 4,000 ft
Temperature 26 °C

Using a maximum rate of climb under the given conditions, how much fuel would be used from engine start to a pressure altitude of 16,000 feet?

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(Refer to figure 13.) GIVEN:

Aircraft weight 3,400 lb
Airport pressure altitude 6,000 ft
Temperature at 6,000 feet 10 °C

Determine the approximate ground roll.

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(Refer to figure 35.) GIVEN:

Temperature 85 °F
Pressure altitude 6,000 ft
Weight 2,800 lb
Headwind 14 kts

What is the maximum available flight time under the conditions stated?

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(Refer to figure 34.) GIVEN:

Pressure altitude 6,000 ft
Temperature +3 °C
Power 2,200 RPM – 22″ MP
Usable fuel available 465 lb