Question: (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

(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 Airport temperature 26C. CPC Figure 9.png Group of answer choices 51 pounds. 58 pounds. 46 pounds.

NORMAL CLIMB-100 KIAS CONDITIONS: FLAPS UP MIXTURE SETTING GEAR UP PRESS ALT PPH 2,550 RPM 25 INCHES MP OR FULL THROTTLE S.L. to 4,000 108 COWL FLAPS OPEN 8,000 96 STANDARD TEMPERATURE 12,000 84 NOTES: 1. INCREASE TIME, FUEL, AND DISTANCE BY 10% FOR EACH 10 *C ABOVE STANDARD TEMPERATURE. 2. ADD 12 POUNDS OF FUEL FOR ENGINE START, TAXI, AND TAKEOFF ALLOWANCE. 3. DISTANCES SHOWN ARE BASED ON ZERO WIND. FROM SEA LEVEL WEIGHT PRESS ALT RATE OF CLIMB (LB) (FT) (FPM) TIME FUEL USED DISTANCE MIN (LB) (NM) 3,800 S.L. 580 0 0 0 2,000 580 3 6 6 4,000 570 7 12 12 6,000 470 11 19 19 3,000 365 16 27 28 10,000 265 22 37 40 12,000 165 32 51 59 3,50 S.L 585 0 0 0 2,000 685 3 5 000 575 6 11 10 5,000 565 9 16 16 3,000 155 13 23 23 0,000 350 18 31 33 2,000 240 25 41 46 3,200 S.L. 800 0 0 2,000 300 2 4 4,000 795 5 9 8 6,000 575 8 14 13 3,000 560 11 19 19 10,000 445 15 25 27 12,000 325 20 33 37 Figure 9. Fuel, Time, and Distance to Climb

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