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<br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br />I <br /> <br />TABLE 1.1 (eontinued) <br /> <br />D . . <br />, e-J.cJ.ng gear: <br />Hy~~u1ic boots on all leading edges <br />Al~ohol de-icers on prop~Uers <br />Avionics: <br />Radios <br />Dual very high frequency omnirange (VOR) <br />Distance measuring equipment (DME) <br />Sperry flight director <br />Transponder <br />Automatie direction finders (ADF) <br />Electrical power: <br />For aircraft operation: 8400 W, 2BV dC (300 A) <br />3000 W, 11SV, 400 Hz (rot~ inverter) <br />For research instruments. <br /> <br />Total available: B400 W, 2BV de (300 A) <br />May be distributed as follows: 1000 W, llSV, 60 Hz (t'Otary inverter) <br />1000 W, 115V, 60 Hz (It It ) <br />1500 W, 115V, 400 Hz ( " " ) <br />2600 W, 2BV de. <br /> <br />