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COMMERCE BUSINESS DAILY ISSUE OF MARCH 3,2000 PSA#2549Naval Air Warfare Center Aircraft Division, Contracts Department,
Building 129-2, Highway 547, Lakehurst, NJ 08733-5083 16 -- HYDRAULIC CARTS SOL N68335-00-RFI-002 DUE 031700 POC Kathlrrn
Kiley-DiPietro, Contract Specialist, 732-323-5197 N68335-00-RFI-002 --
Portable Hydraulic Power Supply (PHPS) THIS IS A REQUEST FOR
INFORMATION (RFI) ONLY. THERE IS NO SOLICITATION PACKAGE AVAILABLE. The
Naval Air Warfare Center Aircraft Division Lakehurst (NAWCADLKE) is
evaluating the availability of a Commercial Off The Shelf (COTS)
Portable Hydraulic Power Supply (PHPS), electric and diesel powered,
for US Navy shipboard and shore base aircraft support. Any system to be
considered for use must meet the following technical requirements. The
following requirements delineate the absolute minimum technical
requirements that a shipboard and shore based production PHPS unit
shall meet. FLOW: The PHPS unit shall be capable of delivering flows of
32 Gallons per minute (GPM) at 5000 pounds per square inch (PSI) and 50
GPM at 3000 PSI for continuous duty operation. FLOW RESPONSE: Pressure
compensation response time for instantaneous flow demand of 32 GPM @
5000 PSI 75 Milliseconds. STOWAGE AND TRANSPORTATION: Transportable
within the V-22 cargo hold, a gross weight not to exceed 4200 pounds
dry. While in transport the PHPS unit shall be capable of sustaining a
12G force side load and a 16G force forward and aft load or better.
FLUID PURIFICATION: Rate shall meet a minimum of 55 Gallons per 5
hours, water Removal shall be better than 200 PPM, chlorinated solvents
shall not exceed 100 PPM, complete removal of free air shall be no less
than 98% (by volume) desolved air and shall meet or exceed particulate
NAS 1638 Class 2. DEISEL ENGINE EMISSIONS: Nox shall not exceed 6.9
grams per brake horsepower-hour (g/bhp-hr), hydrocarbons shall not
exceed 1.0 g/bhp-hr and particulates shall not exceed 0.4 g/bhp-hr. In
addition Smoke Opacity shall not exceed, 20% on acceleration mode, 15%
on lug mode and 50% peak opacity on either the acceleration or lug
mode. The engine shall be certified by the California Air Resources
Board in accordance with the California Code of Regulations (Chapter
11, Title 13, Section 2420-2427). The PHPS units shall possess a
emission compliance certification, be labeled with an unconditional
statement of compliance with the California regulations for heavy-duty
off-road diesel cycle engines and meet Environmental Protection Agency
and California requirements while operating. OPERATING ENVIROMENT: PHPS
units shall operate between the temperatures of -40 F to +120 F. FLUID
COMPATIBILTY: PHPS units will conform to MIL-PRF-83282D
specifications. POSITION OF OPERATION: During shipboard utilization the
PHPS units shall maintain operations up to 8 1/2 from horizontal on any
axis. AMBIENT NOISE shall not exceed 85db. PAINT: PHPS units shall be
painted in accordance with the following: Primer: Epoxy Polymide per
Mil-P-23377F Type I Class II Top Coat: Polyurethane per Mil-C-85285
Type II Color: per FED-STD-595 Green No. 24052. It is requested that
information be submitted NO LATER THAN 17 MARCH 2000 to Mrs. Kathleen
Kiley-DiPietro, Naval Air Warfare Center Aircraft Division Code
25211B129-2, Highway 547, Lakehurst, NJ 08733-5082. Mrs. Kiley-DiPietro
can be reached at (732) 323-5197. Respondents are notified that a
formal solicitation MAY NOT necessarily result from this RFI. Any
comments provided may or may not be included in a formal solicitation.
The US Navy WILL NOT PAY for any information received in response to
this RFI nor will the US Navy compensate any respondent for any costs
incurred in developing the information provided to the US Navy. The US
Navy will not release any information marked with a Proprietary
legend, received in response to this RFI to any firms, agencies, or
individuals outside the US Navy without written permission in
accordance with the legend. Any and all responses shall be appreciated.
Posted 03/01/00 (W-SN430087). (0061) Loren Data Corp. http://www.ld.com (SYN# 0175 20000303\16-0021.SOL)
16 - Aircraft Components and Accessories Index Page
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