R11ChangePage130Apr2013.pdf

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Attached to
A/S32 R-11 Refueler Federal contract opportunity
Solicitation number
FA8533-12-R-35653
Issued by
Department of the Air Force Materiel Command Lifecycle Management Center Robins Air Force Base

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Performance Specification Change Page One (1)

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Text version

MIL-PRF-32080E Change Page 1 30 Apr 2013

1. In paragraph 3.8.2 Pumping system. Under item “e”, the following sentence “The HMS system shall control flow rates from 0 to a maximum of 700 gpm with a maximum hydrant inlet pressure of 130 psig when filling the cargo tank." shall be changed to read as follows: " When filling the cargo tank, the HMS system shall not allow the maximum flow rate to exceed 700 gpm."

2. In paragraph 3.10.8.1.2 Tachometer. The following sentence "The tachometer shall incorporate both a bargraph indication and numerical value readout and shall be readable from a distance of 15 feet, during daytime or nighttime operations." shall be changed to read as follows : "The tachometer shall incorporate a numerical value readout and shall be readable from a distance of 15 feet, during daytime or nighttime operations."

3. In paragraph 3.13 Hydrant service module (HSM). The following sentence “at (3) a flow rate up to and including a maximum of 700 gpm with a maximum hydrant inlet pressure of 130 psig.” shall be changed to read as follows: “and (3) the maximum flow rate shall not exceed 700 gpm.”

4. In paragraph 4.3 User operational test. The following sentence “The first production aircraft refueling truck shall be delivered to a Government designated site for a test period of 90 days for user operational testing.” shall be changed to read as follows: “The first production aircraft refueling truck shall be delivered to a Government designated site for a test period of 30 days for user operational testing.”

5. In paragraph 4.6.30 HSM test. The following sentence in item “b.”, “Testing shall verify that fuel can be issued from a simulated Type III hydrant system, through the HSM, into the cargo tank without passing through the pump, filtration system, or meter, at flow rates up to and including a maximum of 700 gpm at the maximum simulated hydrant inlet pressure of 130 psig.” shall be changed to read as follows” “Testing shall verify that fuel can be issued from a simulated Type III hydrant system, through the HSM, into the cargo tank without passing through the pump, filtration system, or meter, at flow rates up to 700 gpm maximum.”

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