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SU0000077_SSC RPT
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SU0000077_SSC RPT
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Last modified
4/8/2022 5:23:23 PM
Creation date
3/29/2022 1:34:31 PM
Metadata
Fields
Template:
EHD - Public
ProgramCode
2600 - Land Use Program
FileName_PostFix
SSC RPT
RECORD_ID
SU0000077
PE
2622
FACILITY_NAME
MS-00-14
STREET_NUMBER
23755
Direction
N
STREET_NAME
DE VRIES
STREET_TYPE
RD
City
LODI
Zip
95240
ENTERED_DATE
8/8/2001 12:00:00 AM
SITE_LOCATION
23755 N DEVRIES RD
RECEIVED_DATE
6/13/2000 12:00:00 AM
P_LOCATION
99
P_DISTRICT
004
QC Status
Approved
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EHD - Public
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RESTRICTED MATERIALS PERMIT cont . Page 5 <br /> 30EHRING FARMS Permit #: 59-98-1904187 <br /> CONDITION - U <br /> ENDOSULFAN <br /> GENERAL <br /> I . Do not apply endosulfan to fields under irrigation . <br /> 2. Do not irrigate fields treated with endosulfan for 72 hours following <br /> application. <br /> _ . Do not apply more than 1 . 5 lbs. a. i . /acre/application . Orchard crops and <br /> strawberries are exempted . <br /> 4 . A minimum .300 foot buffer zone shall exist between the treated area and a <br /> drain or canal to contain irrigation/rain runoff before it is discharged <br /> into surface waters. The buffer zone may be a fallow field , pasture land <br /> or an untreated portion of the field . <br /> AERIAL APPLICATION <br /> 5. Endosulfan shall not be discharged at a height of more than 10 feet above <br /> the crap or target. Discharge shall be shutoff whenever it is necessary <br /> to raise the equipment over obstacles such as trees or poles. <br /> 6 . Do not apply endosulfan when the wind velocity exceeds 10 miles per hour <br /> (m. p. h. ) . <br /> 7 . The flaw of liquid to aircraft nozzles shall be controlled by a positive <br /> shutoff system as follows; ( 1 ) each individual nozzle shall be equipped <br /> with a cheep: valve and the flow controlled by a suck back:. device or a <br /> boom pressure release devicep or (2) each individual nozzle shall be <br /> equipped with a positive action valve. <br /> 3. Aircraft nozzles shall not be equipped with any device or mechanism which <br /> would cause a sheet, cone, fan , or similar type dispersion of the dis- <br /> charged material , except as otherwise provided . <br /> 9. Aircraft boom pressure shall not exceed 40 psi . <br /> 10. Aircraft nozzles shall be equipped with orifices directed backwards, <br /> parallel to the horizontal axis of the aircraft in flight. <br /> 11 . Fixed wing aircraft and helicopters operating in excess of 60 m. p. h. shall <br /> be equipped with jet nozzles having an orifice of not less than 1/6 inch <br /> in diameter. <br /> 12. Helicopters operating at 60 m. p.h. or less shall be equipped as follows: <br /> ( 1 ) nozzles having an orifice not less than 1/16 inch in diameter, a <br /> number 46 (or equivalent ) or larger whirlplate may be used or (2) fan <br /> nozzles with a fan angle number not larger- than 80 degrees and a flow <br /> rate not less than one gallon per minute at 40 psi (or equivalent) ; or <br /> (T) the Microfoil (R) boom (a coordinanted spray system including airfoil <br /> shaped nozzles, with each orifice not less than 0.01i inches in diameter ) . <br /> 15. The working boom length on fixed wing aircraft shall not exceed 1/4 of the <br /> wing spam. The working boom length on helicopters shall not exceed 6/7 of <br /> the total rotor length or 3/4/ of the total rotor length where the rotor <br /> length exceeds forty (40) feet . <br /> T Last Page ��� <br />
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