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.
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