Specs.pdf

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Attached to
Diesel Hydraulic Power Unit Federal contract opportunity
Solicitation number
80NSSC21771577Q
Issued by
National Aeronautics and Space Administration Shared Services Center

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RFQ 80NSSC21771577Q.pdf PDF

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Text version

Meet Specifications Listed Hydraulic Test Stand Comments

Condition: New

Engine:

1) Diesel, Tier IV Final Jet A option desirable

2) Fuel Tank: Stainless Steel

3) Low Engine Oil Pressure Shutdown

4) Engine Coolant over Temp Shutdown

5) Run Time on Tank of Fuel: 8 hours Minimum

Frame/Chassis:

1) Fully enclosed Aluminum Cabinet Shell (Weather Proof)

2) Removable top panel for access to components

3) Towbar with brake

4) Pnuematic or solid tires

Pump System:

1) Hyd Fluid Mil-PRF- 87257,Single System

2) Reservoir Capacity: 50 gal minimum Stainless Steel

3) Minimum flow/pressure: 25 GPM @ 4000 PSI Fully Adjustable

4) By-Pass Dump Valve

5) Non-Bypass High Pressure Filter: 3 Micron Absolute

6) Return Filter: 6 Micron Absolute

7) Oil Cooler

8) Reservoir Selector Valve: To allow to use either unit's or aircraft's reservoir

9) Exterior Fluid Sampling Valve

Instumentation:

1) High Pressure Dual Scale Flow Meter (4% accuracy minimum) w/ Cert of Calibration

2) Liquid Filled Pressure Gauge (1% accuracy minimum) w/ Cert of Calibration

3) Hyd. Oil Temp Gauge

4) Reservoir Sight Glass

Misc.

1) 50' Supply and Return Hoses

2) Reservoir Hand Pump

3) Return Sight Glass

4) Forklift Tubes

Delivery:

1) FOB to Palmdale, CA

2) ETA ARO 180 Days

Sheet1

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