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i� <br /> ��errm�tee:Zt?L 1W1 &R Permit Number: 39-08-3900506 <br /> a � i <br /> 8,Aircraft nozzles shall not be equipped with any device or mechanism which would <br /> t. cause a sheet,come,fan,or similar type dispersion of the dischaawd material,except <br /> as otherwise provided <br /> 9.Aircraft boom pressure shall not exceed 40 psi. <br /> 10.Aircraft nozzles shall be equipped with orifices directed backwards,parallel to the <br /> i <br /> horizontal axis of the aircraft in flight. <br /> F 11.Fixed wing aircraft and helicopters operating in excess of 60 m.p.h. shall be equipped <br /> } with jet nozzles having an orifice of not less than 1/6 inch in diameter. <br /> 12.Helicopters operating at 60 m.p.h or less shall be quipped as follows: (1)nozzles <br /> having an orifice not less than 1/16 inch in diameter,a number 46(or equivalent) <br /> or larger whirlplate may be used;or(2)fan nozzles with a fan angle number not <br /> larger than 80 degrees and a flow rate not less than one gallon per minute at 40 psi <br /> (or equivalent);or(3)the 1vtcrofoil(R)boom(a coordinated spray"ern including <br /> airfoil shaped nozzles with each OrTice not less than 0.013 inches in diameter). <br /> boom 1 on fixed w aircraft shall not exceed 314 of the wingspan. <br /> 13.�e working length wing <br /> The working boom length on helicopters shall not exceed 6/7 of the total rotor length <br /> or 3/4 total rotor length where the rotor length exceeds forty(40)feet. <br /> k <br /> Revised 03/95 <br /> Description of Custom Site Conditions <br /> Candt[on ID Dere tion <br /> *** LAST PAGE *�` <br /> 1 <br /> f <br /> i <br />