By Federal Aviation Administration (FAA)/Aviation Supplies & Academics (ASA)
Basic airplane weight and stability keep watch over ideas and methods for the coaching, and the particular weighing of an airplane commence the dialogue, together with the tools of choosing the site of the empty weight middle 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 middle of gravity adjustments attributable to upkeep and adjustments or elimination and install of kit. Chapters are devoted to light-sport airplane, single-engine plane, multi-engine airplane, and commuter and big plane, in addition to helicopter weight and stability keep watch over and picking lateral CG. additionally integrated are examples of fixing weight and stability difficulties utilizing a hand held digital calculator, E6-B flight computing device, and a committed digital flight computer.
This 2016 version displays the newest aviation tactics, apparatus, thoughts, laws, and is a key reference within the FAA Airman Certification criteria (ACS). Illustrated all through with specific, full-color drawings, and features a word list and index.
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Extra info for Aircraft Weight and Balance Handbook: FAA-H-8083-1A
47 inches aft of the datum. To determine that the weight and CG are within the allowable range, refer to the CG range chart of Figure 412. 47 inches from the datum and one horizontally from 5,064 pounds. These lines cross inside the envelope, showing that the airplane is properly loaded. Figure 4-10. Twin-engine airplane weight and balance diagram. indd 5 3/14/07 10:26:40 PM Consider the loading for this particular flight: Cruise fuel flow = 16 gallons per hour Estimated time en route = 2 hours 10 minutes.
4 Determining the Loaded Weight and CG An important part of preflight planning is to determine that the aircraft is loaded so its weight and CG location are within the allowable limits. [Figure 4-2] There are two ways of doing this: by the computational method using weight, arms, and moments; and by the loading graph method, using weight and moment indexes. Figure4-2. Airplane loading diagram. Computational Method The computational method uses weights, arms, and moments. It relates the total weight and CG location to a CG limits chart similar to those included in the TCDS and the POH/AFM.
Any major alteration or repair requires the work to be done by an appropriately-rated aircraft mechanic or facility. The work must be checked for conformity to FAA-approved data and signed off by an aircraft mechanic holding an Inspection Authorization, or by an authorized agent of an appropriately rated FAA-approved repair station. A repair station record or FAA Form 337, Major Repair and Alteration, must be completed which describes the work. A dated and signed revision to the weight and balance record is made and kept with the maintenance records, and the airplane’s new empty weight and empty weight arm or moment index are entered in the POH/AFM.
Aircraft Weight and Balance Handbook: FAA-H-8083-1A by Federal Aviation Administration (FAA)/Aviation Supplies & Academics (ASA)