By Federal Aviation Administration (FAA)/Aviation Supplies & Academics (ASA)
Basic airplane weight and stability keep an eye on rules and methods for the coaching, and the particular weighing of an airplane commence the dialogue, together with the equipment of opting for the positioning of the empty weight heart of gravity. Loading computations with loading graphs and tables of weight and second indexes keep on with, together with directions on picking the burden and heart of gravity alterations attributable to maintenance and adjustments or removing and deploy of kit. Chapters are devoted to light-sport airplane, single-engine plane, multi-engine plane, and commuter and massive airplane, in addition to helicopter weight and stability regulate and selecting lateral CG. additionally incorporated are examples of fixing weight and stability difficulties utilizing a handheld digital calculator, E6-B flight machine, and a devoted digital flight computer.
This 2016 variation displays the newest aviation strategies, gear, suggestions, laws, and is a key reference within the FAA Airman Certification criteria (ACS). Illustrated all through with targeted, full-color drawings, and incorporates a word list and index.
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Extra info for Aircraft Weight and Balance Handbook: FAA-H-8083-1A
Fluids not considered to be part of the empty weight of the aircraft are potable (drinkable) water, lavatory precharge water, and water for injection into the engines. Configuration of the Aircraft Consult the aircraft service manual regarding position of the landing gear shock struts and the control surfaces for weighing; when weighing a helicopter, the main rotor must be in its correct position. Jacking the Aircraft Aircraft are often weighed by rolling them onto ramps in which load cells are embedded.
Figure 3-27] Mechanical scales should be protected when they are not in use, and they must be periodically checked for accuracy by measuring a known weight. Electronic scales normally have a built-in calibration that allows them to be accurately zeroed before any load is applied. The weight and balance report must include an equipment list showing weights and moment arms of all required and optional items of equipment included in the certificated empty weight. When an aircraft has undergone extensive repair or major alteration, it should be reweighed and a new weight and balance record started.
Tail wheel airplanes with the datum forward of the main wheels. 8 inches aft of the datum. 2 inches forward of the main-wheel weighing points which proves the location of the datum has no effect on the location of the CG so long as all measurements are made from the same location. Datum Aft of the Main Wheels Nose Wheel Landing Gear The datum of some aircraft may be located aft of the main wheels. The airplane in this example is the same one just discussed, but the datum is at the intersection of the trailing edge of the wing with the fuselage.
Aircraft Weight and Balance Handbook: FAA-H-8083-1A by Federal Aviation Administration (FAA)/Aviation Supplies & Academics (ASA)