## Use of Computer for Weight and Balance Computations (Part Two)

Determining CG, Given Weights, and Arms Some weight and balance problems involve weights and arms to determine the moments. Divide the total moment by the total weight to determine the CG. Figure 10-6 contains the specifications for determining the CG using weights and arms. Determine the CG by using the data in Figure 10-6 and […]

## Use of Computer for Weight and Balance Computations (Part One)

Electronic Calculator Determining the CG of an airplane in inches for the main-wheel weighing points can be done with any simple electronic calculator that has addition (+), subtraction (–), multiplication (×), and division (÷) functions. [Figure 10-1] Scientific calculators with such additional functions as memory (M), parentheses (( )), plus or minus (+/–), exponential (yx), […]

## Determining CG Changes Caused by Modifying the Cargo (Part Three)

Determining the Changes in CG When Passengers Are Shifted Using the loaded weight and CG of the Beech 1900, calculate the change in CG when the passengers in rows 1 and 2 are moved to rows 8 and 9. [Figure 9-47] Note that there is no weight change, but the moment index has been increased […]

## Determining CG Changes Caused by Modifying the Cargo (Part Two)

Determining the Maximum Amount of Payload That Can Be Carried The primary function of a transport or cargo aircraft is to carry payload, which is the portion of the useful load, passengers, or cargo that produces revenue. To determine the maximum amount of payload that can be carried, both the maximum limits for the aircraft […]

## Determining CG Changes Caused by Modifying the Cargo (Part One)

Since large aircraft can carry substantial cargo, adding, subtracting, or moving any of the cargo from one hold to another can cause large shifts in the CG. Effects of Loading or Offloading Cargo Both the weight and CG of an aircraft are changed when cargo is loaded or offloaded.In the following example, the new weight […]

## Operational Empty Weight (OEW)

Operational empty weight (OEW) is the basic empty weight or flet empty weight plus operational items. The operator has two choices for maintaining OEW. The loading schedule may be utilized to compute the operational weight and balance of an individual aircraft, or the operator may choose to establish fleet empty weights for a fleet or […]

## Commuter Category and Large Aircraft

Establishing the Initial Weight of an Aircraft Prior to being placed into service, each aircraft is weighed and the empty weight and CG location established. New aircraft are normally weighed at the factory and are eligible to be placed into operation without reweighing if the weight and balance records were adjusted for alterations and modifications […]

## Helicopter Weight and Balance Control

Weight and balance considerations of a helicopter are similar to those of an airplane, except they are far more critical, and the center of gravity (CG) range is much more limited. [Figures 8-1 and 8-2] The engineers who design a helicopter determine the amount of cyclic control authority that is available, and establish both the […]

## Ballast

It is possible to load most modern airplanes so the CG shifts outside of the allowable limit. Placards and loading instructions in the weight and balance data inform the pilot of the restrictions that prevent such a shift from occurring. A typical placard in the baggage compartment of an airplane is shown in Figure 7-11. […]

## Empty Weight CG (EWCG) Range and Adverse-Load CG Checks

Empty Weight CG (EWCG) Range The fuel tanks, seats, and baggage compartments of some aircraft are so located that changes in the fuel or occupant load have a very limited effect on the balance of the aircraft. Aircraft of such a configuration show an empty weight CG (EWCG) range in the Type Certificate Data Sheet […]