Page 89 - Planning and Design of Airports
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Air craft Characteristics Related to Airport Design    61















                   “2D/2D2”              “3D”               “2D/3D2”
               Double dual tandem     Triple tandem       Dual tandem plus
                  Boeing 747           Boeing 777          triple tandem
                                                           Airbus A-380
            FIGURE 2-4  Complex landing gear confi gurations (Federal Aviation Administration).


                 The complexity of landing configurations prompted the FAA to adopt
                 standard naming conventions for aircraft landing gear configurations
                 [60]. Examples of this naming convention are represented in quotes in
                 Figs. 2-3 and 2-4.
                    The landing gear configuration plays a critical role in distributing
                 the weight of an aircraft on the ground it sits on, and thus in turn has
                 a significant impact on the design of airfield pavements. Specifically,
                 the more wheels on a landing gear, the heavier an aircraft can be and
                 still be supported on a ramp, taxiway, or runway of a given pavement
                 strength.

            Aircraft Weight
                 While the concept of aircraft weight may be thought to be a simple
                 one, the measurement of the weight of a given aircraft is actually rel-
                 atively complex. An aircraft will in fact be measured with a certain
                 number of weight measurements, depending on its level of loading
                 with fuel, payload, and crew, and assigned maximum allowable
                 weight values for takeoff, landing, and at rest.
                    These various measurements of aircraft weight are important to
                 airport planning and design, in particular the facilities such as ramps,
                 taxiways, and runways that are designed to support the aircraft.
                    While it is rare that any two aircraft, even those of the same model
                 and configuration, have the same weight measurements (as there are
                 almost always variations between aircraft in equipment, seating con-
                 figurations, galleys, and other objects), most manufactures will assign
                 typical weights to their aircraft for planning and design purposes.
                 These weights are as follows.
                    The “lightest” measure of an aircraft’s weight is known as the oper-
                 ating empty weight (OEW), the basic weight of the aircraft including
                 crew and all the necessary gear required for flight but not including
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