WB Com ASA

Given. 89.11. 96.89. 106.92.

Given. 86. 116.8. 125.0.

Given. 100.2. 109.0. 121.7.

Given. 91.76. 111.67. 118.24.

Baggage weighing 90 pounds is placed in a nor mal category airplane’s baggage compartment which is placarded at 100 pounds. If this airplane is subjected to a positive load fac. 315 pounds and would be excessive. 315 pounds and would not be excessive. 350 pounds and would not be excessive.

GIVEN: Empty weight (oil is included) .........................1,271 lb Empty weight moment (in-lb/1,000) ..................102.04 Pilot and copilot .................................................400 lb Rear seat passenger .........................................140 lb Cargo .................................................................100 lb Fuel....................................................................37 gal Is the airplane loaded within limits?. Yes, the weight and CG is within limits. — No, the weight exceeds the maximum allowable. No, the weight is acceptable, but the CG is aft of the aft limit.

(Refer to Figure 38.) GIVEN: Empty weight (oil is included) .........................1,271 lb Empty weight moment (in-lb/1,000) ..................102.04 Pilot and copilot .................................................260 lb Rear seat passenger .........................................120 lb Cargo ...................................................................60 lb Fuel....................................................................37 gal Under these conditions, the CG is determined to be located. within the CG envelope. on the forward limit of the CG envelope. within the shaded area of the CG envelope.

(Refer to Figure 38.) GIVEN: Empty weight (oil is included) .........................1,271 lb Empty weight moment (in-lb/1,000) ..................102.04 Pilot and copilot .................................................360 lb Cargo .................................................................340 lb Fuel....................................................................37 gal Will the CG remain within limits after 30 gallons of fuel has been used in flight?. Yes, the CG will remain within limits. No, the CG will be located aft of the aft CG limit. Yes, but the CG will be located in the shaded area of the CG envelope.

Total weight.....................................................4,137 lb CG location station ...............................................67.8 Fuel consumption ........................................13.7 GPH Fuel CG station.....................................................68.0 After 1 hour 30 minutes of flight time, the CG would be located at station. 67.79. 68.79. 70.78.

Total weight..................................................... 3,037 lb CG location station ............................................... 68.8 Fuel consumption ........................................ 12.7 GPH Fuel CG station..................................................... 68.0 After 1 hour 45 minutes of flight time, the CG would be located at station. 68.77. 68.83. 69.77.

An aircraft is loaded with a ramp weight of 3,650 pounds and having a CG of 94.0, approximately how much baggage would have to be moved from the rear baggage area at station 180 to the forward baggage area at station 40 in order to move the CG to 92.0?. 52.14 pounds. 62.24 pounds. 78.14 pounds.

An airplane is loaded to a gross weight of 4,800 pounds, with three pieces of luggage in the rear baggage compartment. The CG is located 98 inches aft of datum, which is 1 inch aft of limits. If luggage which weighs 90 pounds is moved from the rear baggage compartment (145 inches aft of datum) to the front compartment (45 inches aft of datum), what is the new CG?. 96.13 inches aft of datum. 95.50 inches aft of datum. 99.87 inches aft of datum.

GIVEN: Temperature .........................................................75°F Pressure altitude.............................................. 6,000 ft Weight ............................................................ 2,900 lb Headwind............................................................20 kts To safely take off over a 50-foot obstacle in 1,000 feet, what weight reduction is necessary?. 50 pounds. 100 pounds. 300 pounds.

GIVEN: Temperature .........................................................50°F Pressure altitude..........................................2,000 feet Weight ............................................................2,700 lb Wind ....................................................................Calm What is the total takeoff distance over a 50-foot obstacle?. 800 feet. 650 feet. 1,050 feet.

Determine the approximate runway length necessary for takeoff. GIVEN: Temperature .........................................................40°F Pressure altitude..............................................4,000 ft Weight ...........................................................3,200 lbs Headwind............................................................15 kts. 1,300 feet. 850 feet. 950 feet.

Determine the approximate runway length necessary for takeoff. GIVEN: Temperature .........................................................40°F Pressure altitude..............................................4,000 ft Weight ...........................................................3,200 lbs Headwind............................................................15 kts. 1,300 feet. 850 feet. 950 feet.

GIVEN: Temperature .......................................................100°F Pressure altitude..............................................4,000 ft Weight ............................................................3,200 lb Wind ....................................................................Calm What is the ground roll required for takeoff over a 50-foot obstacle?. 1,180 feet. 1,350 feet. 1,850 feet.

GIVEN: Temperature .........................................................30°F Pressure altitude..............................................6,000 ft Weight ............................................................3,300 lb Headwind............................................................20 kts What is the total takeoff distance over a 50-foot obstacle?. 1,100 feet. 1,300 feet. 1,500 feet.