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SU0003918 SSCRPT
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SU0003918 SSCRPT
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Entry Properties
Last modified
5/7/2020 11:30:19 AM
Creation date
9/8/2019 12:45:59 PM
Metadata
Fields
Template:
EHD - Public
ProgramCode
2600 - Land Use Program
FileName_PostFix
SSCRPT
RECORD_ID
SU0003918
PE
2622
FACILITY_NAME
PA-0300098
STREET_NUMBER
7921
Direction
N
STREET_NAME
PODESTA
STREET_TYPE
LN
City
LINDEN
ENTERED_DATE
5/11/2004 12:00:00 AM
SITE_LOCATION
7921 N PODESTA LN
RECEIVED_DATE
3/20/2003 12:00:00 AM
QC Status
Approved
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SJGOV\rtan
Supplemental fields
FilePath
\MIGRATIONS\P\PODESTA\7921\PA-0300098\SU0003918\SSC RPT.PDF
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EHD - Public
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RESTRICTED MATERIALS PERMI'l-. 'continued Page# : 9 <br /> PODESTA FARMS, FRED Permit# : 39-99--3900351 <br /> ---------- <br /> CONDITION - U <br /> ENDOSULFAN <br /> -- GENERAL <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 /> y 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 /> F 6 . Do not apply endosulfan when the wind velocity exceeds 10 miles per hour <br /> I (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 /> 8 . 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 /> i 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 /> (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 *** <br />
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