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SU0004813 SSCRPT
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SU0004813 SSCRPT
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Last modified
5/7/2020 11:31:14 AM
Creation date
9/9/2019 11:00:47 AM
Metadata
Fields
Template:
EHD - Public
ProgramCode
2600 - Land Use Program
FileName_PostFix
SSCRPT
RECORD_ID
SU0004813
PE
2622
FACILITY_NAME
PA-0500017
STREET_NUMBER
715
Direction
S
STREET_NAME
WAGNER
STREET_TYPE
RD
City
STOCKTON
APN
15907016
ENTERED_DATE
2/8/2005 12:00:00 AM
SITE_LOCATION
715 S WAGNER RD
RECEIVED_DATE
2/1/2005 12:00:00 AM
P_LOCATION
99
P_DISTRICT
002
QC Status
Approved
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SJGOV\rtan
Supplemental fields
FilePath
\MIGRATIONS\W\WAGNER\715\PA-0500017\SU0004813\SSC RPT.PDF
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EHD - Public
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` Restricted Materials Pert Conditions ti,/ Pagett: 4 of 4 <br /> The Following Conditions Apply To . . . . . . . . . . . . . . . . . . . . . . Permit#: 39-03-3904309 <br /> ------------------------------------------------------------------------------- <br /> CONDITION - U <br /> ENDOSULFAN <br /> 1. Do not apply endosulfan to fields under irrigation. <br /> ` 2. Do not irrigate fields treated with endosulfan for 72 hours following <br /> application. <br /> 3. 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 crop 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 flow 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 check valve and the flow controlled by a suckback device or a <br /> boom pressure release device; or (2) each individual nozzle shall be <br /> equipped with a positive action valve. <br /> S. 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 ,het 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 /> (3) the Microfoil (R) boom (a coordinanted spray system including airfoil <br /> 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 <br /> wing span. 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 /> *** Last Page Of Conditions *** <br />
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