WB com ASA

GIVEN: 689 feet. 716 feet. 1,275 feet.

GIVEN. 742 feet. 1,280 feet. 1,480 feet.

GIVEN. 425 feet. 636 feet. 836 feet.

GIVEN. 1,125 feet. 1,250 feet. 1,325 feet.

GIVEN: Fuel quantity ...................................................... 47 gal Power-cruise (lean) .................................... 55 percent Approximately how much flight time would be available with a night VFR fuel reserve remaining?. 3 hours 8 minutes. 3 hours 22 minutes. 3 hours 43 minutes.

(Refer to Figure 8.) GIVEN: Fuel quantity ...................................................... 65 gal Best power (level flight) .............................. 55 percent Approximately how much flight time would be available with a day VFR fuel reserve remaining?. 4 hours 17 minutes. 4 hours 30 minutes. 5 hours 4 minutes.

(Refer to Figure 8.) Approximately how much fuel would be consumed when climbing at 75 percent power for 7 minutes?. 1.82 gallons. 1.97 gallons. 2.15 gallons.

(Refer to Figure 8.) Determine the amount of fuel consumed during takeoff and climb at 70 percent power for 10 minutes. 2.66 gallons. 2.88 gallons. 3.2 gallons.

(Refer to Figure 8.) With 38 gallons of fuel aboard at cruise power (55 percent), how much flight time is available with night VFR fuel reserve still remaining?. 2 hours 34 minutes. 2 hours 49 minutes. 3 hours 18 minutes.

(Refer to Figure 9.) Using a normal climb, how much fuel would be used from engine start to 12,000 feet pressure altitude? Aircraft weight ................................................. 3,800 lb Airport pressure altitude .................................. 4,000 ft. 46 pounds. 51 pounds. 58 pounds.

(Refer to Figure 9.) Using a normal climb, how much fuel would be used from engine start to 10,000 feet pressure altitude? Aircraft weight ................................................. 3,500 lb Airport pressure altitude .................................. 4,000 ft Temperature ........................................................ 21°C. 23 pounds. 31 pounds. 35 pounds.

(Refer to Figure 10.) Using a maximum rate of climb, how much fuel would be used from engine start to 6,000 feet pressure altitude? Aircraft weight ................................................. 3,200 lb Airport pressure altitude .................................. 2,000 ft Temperature ........................................................ 27°C. 10 pounds. 14 pounds. 24 pounds.

Using a maximum rate of climb, how much fuel would be used from engine start to 10,000 feet pressure altitude? Aircraft weight ................................................. 3,800 lb Airport pressure altitude .................................. 4,000 ft Temperature ........................................................ 30°C. 28 pounds. 35 pounds. 40 pounds.

5482. (Refer to Figure 13.) GIVEN: Aircraft weight ................................................. 3,400 lb Airport pressure altitude .................................. 6,000 ft Temperature at 6,000 feet ................................... 10°C Using a maximum rate of climb under the given condi tions, how much fuel would be used from engine start to a pressure altitude of 16,000 feet?. 43 pounds. 45 pounds. 49 pounds.

GIVEN: Aircraft weight ................................................. 4,000 lb Airport pressure altitude .................................. 2,000 ft Temperature at 2,000 feet ................................... 32°C Using a maximum rate of climb under the given condi tions, how much time would be required to climb to a pressure altitude of 8,000 feet?. 7 minutes. 8.4 minutes. 11.2 minutes.

(Refer to Figure 14.) GIVEN: Aircraft weight ................................................. 3,700 lb Airport pressure altitude .................................. 4,000 ft Temperature at 4,000 feet ................................... 21°C 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?. 30 pounds. 37 pounds. 46 pounds.