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AFS-640

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AFS-640 ( afs-640 )

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AC 43.13-1B CHG 1 9/27/01 FIGURE 10-7. Operating center of gravity range. scales under the landing gear tires, a vertical line passing through the centerline of the axle will locate the point on the scale at which the weight is concentrated. This point is called the “weighing point.” Other structural locations capable of supporting the aircraft, such as jack pads on the main spar, may also be used if the aircraft weight is resting on the jack pads. In- dicate these points clearly in the weight and balance report when used instead of the land- ing gear. Typical locations of the weighing points are shown in figure 10-8. o. Zero Fuel Weight. The maximum permissible weight of a loaded aircraft (pas- sengers, crew, cargo, etc.) less its fuel is zero fuel weight. All weights in excess of maxi- mum zero fuel weight must consist of usable fuel. p. Minimum Fuel. The minimum fuel for balance purposes is 1/12 gallon per maximum- except-take-off horsepower (METO). Mini- mum fuel is the maximum amount of fuel which can be used in weight and balance com- putations when low fuel might adversely affect the most critical balance conditions. To de- termine the weight of fuel in pounds divide the METO horsepower by two. q. Full Oil. The full oil is the quantity of oil shown in the Aircraft Specifications or TCDS as oil capacity. Use full oil as the quantity of oil when making the loaded weight and balance computations. r. Tare. The weight of chocks, blocks, stands, etc., used when weighing aircraft is called tare and is included in the scale read- ings. Tare is deducted from the scale reading at each respective weighing point when tare is involved, to obtain the actual aircraft weight. Page 10-8 Par 10-2

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