W&B 2022

What is the new CG if the weight is removed from the FWD compartment under Loading Conditions WS-1. 27.1 percent MAC. 26.8 percent MAC. 30.0 percent MAC.

What is the new CG if the weight is shifted from FWD to the AFT compartment under Loading Conditions WS-1. 15.2 percent MAC. 29.8 percent MAC. 30.0 percent MAC.

What is the new CG if the weight is shifted from the AFT to the FWD compartment under Loading Conditions WS-2?. 26.1 percent MAC. 20.5 percent MAC. 22.8 percent MAC.

Where is the new CG if the weight is added to the AFT compartment under Loading Conditions WS-2?. +17.06 index arm. +14.82 index arm. +12.13 index arm.

What is the new CG if the weigh is added to the FWD compartment under loading conditions WS-3. 11.4 percent MAC. 14.3 percent MAC. 14.5 percent MAC.

What is the new CG if the weight is shifted from FWD to the AFT compartment under Loading Conditions WS-3. 29.2 percent MAC. 33.0 percent MAC. 28.6 percent MAC.

What is the new CG if the weight is shifted from AFT to the FWD compartment under Loading Conditions WS-4. 37.0 percent MAC. 23.5 percent MAC. 24.1 percent MAC.

Where is the new CG if the weight is removed from the AFT compartment under Loading Conditions WS-4?. +15.53 index arm. +8.50 index arm. -93.51 index arm.

What is the new CG if the weight is removed from the FWD compartment under Loading Conditions WS-5?. 31.9 percent MAC. 19.1 percent MAC. 35.2 percent MAC.

Where is the new CG if the listed weight is shifted from the FWD to the AFT compartment under loading conditions WS-5?. +19.15 index arm. +13.93 index arm. -97.92 index arm.

What is the STAB TRIM setting for Operating Conditions R-1?. 8 ANU. 7-5/8 ANU. 7-3/4 ANU.

What is the STAB TRIM setting for Operating Conditions R-2?. 5-3/4 ANU. 7 ANU. 6-3/4 ANU.

What is the STAB TRIM setting for Operating Conditions R-3?. 3 ANU. 4-1/2 ANU. 5 ANU.

What is the STAB TRIM setting for Operating Conditions R-4?. 4-1/4 ANU. 4-1/2 ANU. 5 ANU.

What is the STAB TRIM setting for Operating Conditions R-5?. 6-3/4 ANU. 8 ANU. 7-1/2 ANU.

What is the CG in inches from datum under the following loading conditions? Basic Empty Weight 5005 lbs Pilot 190 lbs Front Seat Passenger 200 bls Cargo Zone 1 180 lbs Cargo Zone 2 505 lbs Cargo Zone 3 198 lbs Cargo Zone 4 600 lbs Cargo Zone 5 0 lbs. 196.4 inches AFT of datum. 200.4 inches AFT of datum. 204.1 inches AFT of datum.

What is the old and new CG if 300 pounds of cargo is moved from Zone 2 to Zone 3 given the following conditions? Basic Empty Weight 5005 lbs Pilot 190 lbs Front Seat Passenger 200 bls Cargo Zone 1 180 lbs Cargo Zone 2 505 lbs Cargo Zone 3 198 lbs Cargo Zone 4 600 lbs Cargo Zone 5 0 lbs. 200.2 and 198.6. 196.4 and 199.2. 200.4 and 202.

What is the CG in inches from datum under the following Loading Conditions? Basic Empty Weight 5005 lbs Pilot 185 lbs Cargo Zone 1 200 lbs Cargo Zone 2 240 lbs Cargo Zone 3 500 lbs Cargo Zone 4 400 lbs Cargo Zone 5 200 lbs Cargo Zone 6 50 lbs. Station 202.6. Station 198.5. Station 205.6.

With the load weights shown in FIGURE 414, you fill the fuel tanks to the maximum fuel to remain under maximum gross weight and compute the center of gravity. Your computations indicate. At a CG of 200.1, your loading is satisfactory for flight operations. At a CG of 180.19, you need to redistribute your loads. At a CG of 190.27, you only need to change the CARGO POD LOADING.

With the following conditions, would the airplane be in the approved weight and CG envelope for landing? CG location: 25% MAC Aircraft Weight: 74,000 lbs. No, the airplane is over the maximum approved landing weight. Yes, the airplane is within the approved weight and CG envelope. No, the airplane is below the maximum landing weight, but the CG is AFT of limits.

You are preparing for a flight, with the following planned loading takeoff. Would the aircraft be within the approved weight limitations? Basic Operating Weight (including crew): 49,500 lbs Passengers, baggage and cargo: 20,850 lbs Fuel weight: 9,500 lbs. Yes, the weight would be within limits. No, max zero fuel weight would be exceeded. No, the max takeoff weight would be exceeded.

What adverse flight characteristics could result from operating an aircraft with the center of gravity (CG) beyond the published forward limitations?. The flight control forces may become very light. It could be difficult or impossible to flare for landing. It could be difficult or impossible to recover from a stall.

What adverse flight characteristics could result from operating an aircraft with the center of gravity (CG) beyond the published aft limitations?. The flight control forces may become very heavy. It could be difficult to flare for landing. It could be impossible to recover from a stall.