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SU0005331 SSCRPT
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SU0005331 SSCRPT
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Last modified
5/7/2020 11:31:37 AM
Creation date
9/6/2019 10:01:03 AM
Metadata
Fields
Template:
EHD - Public
ProgramCode
2600 - Land Use Program
FileName_PostFix
SSCRPT
RECORD_ID
SU0005331
PE
2611
FACILITY_NAME
PA-0500543
STREET_NUMBER
5113
Direction
E
STREET_NAME
MAIN
STREET_TYPE
ST
City
STOCKTON
Zip
95215
APN
15910004 & 06
ENTERED_DATE
8/24/2005 12:00:00 AM
SITE_LOCATION
5113 E MAIN ST
RECEIVED_DATE
8/23/2005 12:00:00 AM
P_LOCATION
99
P_DISTRICT
002
QC Status
Approved
Scanner
SJGOV\rtan
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FilePath
\MIGRATIONS\M\MAIN\5113\PA-0500543\SU0005331\SSC RPT.PDF
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EHD - Public
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L <br /> RESTRICTED MATERIALS PERMIT continued . . . . . Page#: 5 <br /> LOLLERI VICTOR Permit#: 39-99-3900391 <br /> ------------------------------------------------------ <br /> L CONDITION - U <br /> ENDOSULFAN=====______________________________ <br /> GENERAL <br /> L1 . Do not apply endosulfan to fields under irrigation. <br /> 2 . Do not irrigate fields treated with endosulfan for 72 hours following <br /> application. <br /> L3 . 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 /> f drain or canal to contain irrigation/rain runoff before it is discharged <br /> 6 into surface waters . The buffer zone may be a fallow field, pasture land <br /> or an untreated portion of the field. <br /> I. <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 /> L (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 /> L boom pressure release device; or (2) each individual nozzle shall be <br /> equipped with a positive action valve. <br /> 8 . Aircraft nozzles shall not be equipped with any device or mechanism which <br /> Lwould 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 /> L 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 /> L 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 /> Lshaped 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 /> i wing span. The working boom length on helicopters shall not exceed 6/7 of <br /> L the total rotor length or 3/4/ of the total rotor length where the rotor <br /> length exceeds forty (40) feet . <br /> 1_ <br /> *** Last Page *** <br /> L <br /> r <br /> 6 <br />
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