Page 311 - Planning and Design of Airports
P. 311

Structural Design of Airport Pavements      269


                 additional wheels and spacings, were created to distribute increased
                 gross weights, resulting in equivalent per wheel loads not exceeding
                 the 350,000 lb maximum.

                 Equivalent Aircraft Method
                 Historical airfield pavement design methods recommended by the
                 FAA beginning in 1975 took into account the varying weights and
                 landing gear configurations of the fleet of aircraft that may regularly
                 utilize a given airfield’s pavement. This historical method involved
                 determining the number of total annual aircraft departures by each
                 type of aircraft and group them into “equivalent annual departures”
                 of each aircraft in terms of the landing gear configuration of a given
                 design aircraft, that is, the aircraft in the fleet mix that requires the
                 greatest pavement strength. This grouping is based on converting the
                 number of annual departures of all aircraft other than the design air-
                 craft to an equivalent number of annual departures by using the mul-
                 tipliers given in Table 7-5.
                    The equivalent annual departures of the design aircraft were
                 determined by summing the equivalent annual departures of each
                 aircraft in the group, according to the formula given in Eq. (7-4).

                                                     /
                                                 ⎛ W ⎞ 12
                                  Log R =  log R × ⎜  2 ⎟              (7-4)
                                       1      2
                                                 ⎝ W 1 ⎠
                 where R  = equivalent annual departures by the design aircraft
                        1
                       R  =  annual number of departures by an aircraft in terms of
                        2
                          design aircraft landing gear configuration
                      W  = wheel load of the design aircraft
                        1
                      W  = wheel load of the aircraft being converted
                        2

                  To Convert From      To           Multiply Departures By
                  Single wheel         Dual wheel   0.8
                  Single wheel         Dual tandem  0.5
                  Dual wheel           Dual tandem  0.6
                  Double dual tandem   Dual tandem  1.0
                  Dual tandem          Single wheel  2.0
                  Dual tandem          Dual wheel   1.7
                  Dual wheel           Single wheel  1.3
                  Double dual tandem   Dual wheel   1.7

                 TABLE 7-5  Factors for Converting Annual Departures by Aircraft to
                 Equivalent Annual Departures by Design Aircraft
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