时间：2011-10-20 00:58来源：蓝天飞行翻译 作者：航空 点击：次
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‘Fixed Pitch Propeller’ means a propeller, the pitch of which cannot be changed, except by processes constituting a workshop operation. ‘Flame resistant’ means not susceptible to combustion to the point of propagating a flame, beyond safe limits, after the ignition source is removed. ‘Flammable’, with respect to a fluid or gas, means susceptible to igniting readily or exploding. ‘Flap extended speed’ means the highest speed permissible with wing-flaps in a prescribed extended position. ‘Flash resistant’ means not susceptible to burning violently when ignited. ‘Full-up Configuration’ (Engine related definition) means an EECS that has no known Faults or Failures present. [Amdt. No.:Def/1] ‘Gyroplane’ means a rotorcraft the rotors of which are not engine driven except for initial starting, but are made to rotate by action of the air when the rotorcraft is moving, and the means of propulsion of which, consisting usually of conventional propellers, is independent of the rotor system. ‘Harness’ means the equipment, consisting of two shoulder straps and a lap belt, which is provided to restrain a member of the flight crew against inertia loads occurring in emergency conditions. ‘Helicopter’ means a rotorcraft that, for its horizontal motion, depends principally on its engine-driven rotors. ‘Heliport’ means an area of land, water, or structure used or intended to be used for the landing and take-off of helicopters. ‘Icing Atmospheric Conditions’. The definitions of atmospheric conditions are given in this sub- paragraph and Figures 2 to 7: a. ‘Continuous Maximum Icing’. The maximum continuous intensity of atmospheric icing conditions (continuous maximum icing) is defined by the variables of the cloud liquid water content, the mean effective diameter of the cloud droplets, the ambient air temperature, and the inter-relationship of these three variables as shown in Figure 2. The limiting icing envelope in terms of altitude and temperature is given in Figure 3. The inter-relationship of cloud liquid water content with droplet diameter and altitude is determined from Figure 2 and Figure 3. The cloud liquid water content for continuous maximum icing conditions of a horizontal extent, other than 17·4 n miles, is determined by the value of liquid water content of Figure 2, multiplied by the appropriate factor from Figure 4. |
