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tla peso y balance elite

COMENTARIOS ESTADÍSTICAS RÉCORDS
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Título del Test:
tla peso y balance elite

Descripción:
elite 48 preguntas

Fecha de Creación: 2024/02/28

Categoría: Otros

Número Preguntas: 13

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Temario:

If an aircraft CG is found to be at 24 percent of MAC, that 24 percent is an expression of the. distance from the TEMAC. distance from the LEMAC. average distance from the LEMAC to the wing center of lift. distance from the CMAC.

The maximum weight of an aircraft is the. empty weight plus crew, maximum fuel, cargo, and baggage. empty weight plus crew, passengers, and fixed equipment. empty weight plus useful l. empty weight only.

What should be clearly indicated on the aircraft weighing form?. Minimum allowable gross weight. . Weight of unusable fuel. Weighing points. Maximum allowable gross weight.

What type of measurement is used to designate the arm in weight and balance computation?. Distance. Weight. Weight x distance. . Long.

When dealing with weight and balance of an aircraft, the term 'maximum weight' is interpreted to mean the maximum. weight of the empty aircraft. weight of the useful load. authorized weight of the aircraft and its contents. maximum permissible weight of a loaded aircraft (passengers, crew, and cargo) without fuel.

Zero fuel weight is the ?. maximum permissible weight of a loaded aircraft (passengers, crew, and cargo) without fue. empty weight only. basic operating weight without crew, fuel, and cargo. dry weight plus the weight of full crew, passengers, and cargo.

If it is necessary to weigh an aircraft with full fuel tanks, all fuel weight must be subtracted from the scale reading(s). except minimum fuel. including unusable fuel. except unusable fuel. maximum permissible weight of a loaded aircraft (passengers, crew, and cargo) without fuel.

Most modern aircraft are designed so that if all seats are occupied, full baggage weight is carried, and all fuel tanks are full, what will be the weight condition of the aircraft?. It will be at maximum landing weight (BOW). It will be at maximum taxi or ramp weight. A It will be in excess of maximum takeoff weight. It will be at maximum basic operating weight (BOW).

The empty weight of an airplane is determined by B. maximum permissible weight of a loaded aircraft (passengers, crew, and cargo) without fuel. multiplying the measured distance from each weighing point to the datum times the sum of scale reading less the tare weight. subtracting the tare weight from the scale reading and adding the weight of each weighing point. adding the net weight of each weighing point and multiplying the measured distance to the datum.

The major source of weight change for most aircraft as they age is caused by. installation of hardware and safety wire, and added layers of primer and paint on the structure. Cleaness aerodynamyc. accumulation of grime and debris in hard-to-reach areas of the structure, and moisture absorption in cabin insulation. repairs and alterations.

The maximum weight as used in weight and balance control of a given aircraft can normally be found. Advisory circular UAEAC. by adding the empty weight and payload. in the Aircraft Specification or Type Certificate Data Sheet. by adding the weight of full fuel, pilot, passengers, and maximum allowable baggage to the empty weight.

The useful load of an aircraft is the difference between. the maximum takeoff weight and basic empty weight. Zero fuel weight minus basic weight. (1) the weight of an aircraft with all seats filled, full baggage/cargo, and full fuel, and (2) aircraft weight with all seats empty, no baggage/cargo, and minimum operating fuel. maximum ramp or takeoff weight as applicable, and zero fuel weight.

To obtain useful weight data for purposes of determining the CG, it is necessary that an aircraft be weighed A in a level flight attitude. with all items of useful load installed. with no more than minimum fuel (1/12-gallon per METO horsepower) in all fuel tanks. ,. ,. with pallets and cargo containers.

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