Performance and Weight and Balance

通報

問題一覧

The performance tables of an aircraft for takeoff and climb are based on

pressure/density altitude

To determine pressure altitude prior to takeoff, the altimeter should be set to

29.92" Hg and the altimeter indication noted

At higher elevation airports the pilot should know that indicated airspeed

will be unchanged, but groundspeed will be faster

What effect does an uphill runway slope have on takeoff performance?

Increases takeoff distance

Which maximum range factor decreases as weight decreases?

Airspeed

When computing weight and balance, the basic empty weight includes the weight of the airframe, engine(s), and all installed optional equipment. Basic empty weight also includes

the unusable fuel, full operating fluids, and full oil

The CG of an aircraft can be determined by which of the following methods?

Dividing total moments by total weight

The CG of an aircraft may be determined by

dividing total moments by total weight

If all index units are positive when computing weight and balance, the location of the datum would be at the

nose, or out in front of the airplane

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