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Permitee.ROZAT DAN <br />8. Aircraft noz les shall not be equipped with any device or mechanism which would <br />cause a sheet, cone, fan, or similar type dispersion of the discharged material, except <br />as otherwise provided. <br />9. Aircraft boon pressure shall riot exceed 40 psi. <br />10. Aircraft nozzles shall be equipped with orifices directed bac wards, parallel to the <br />horizontal axis of the aircraft in flight <br />11. Fixed wing aircraft and helicopters operating in excess of 60 m.p.h, shall be equipped <br />with}et nozzles having an orifice of not less than 1/6 inch in diameter. <br />12. Helicopters operating at 60 mp.h. or less Mall be quipped as fol Iovs: (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; cc (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); cc (3) the Mirrofoil (R) boom (a coordinated spray system including <br />airfoil shaped nozzles with each orifice not less than 0.013 inches in diameter). <br />13, The working boom length on fixed wing aircraft shall not exceed 3/4 of the wingspan, <br />The working boom length on helicopters shall not exceed 67 of the total rotor length <br />or 3/4 total rotes length where the rotor ler>gh exceeds forty (40) feet., <br />Revised 03/95 <br />Description of Custom Site Conditions <br />Cmditlm ID DSErintim <br />*** LAST PAGE *** <br />Permit Number: 39-06-3900396 <br />