power_unit_jacks.docx

1108th TASMG HYDRAULIC POWER UNITS & TRIPOD JACK

REQUIREMENTS AND SPECIFICATIONS

REQUIREMENT

HYDRAULIC POWER UNIT 1EA (ANY COLOR)

Hydraulic Power Unit (HPU) will provide the 1108th TASMG MSARNG a source of clean, pressurized hydraulic fluid for performing required aircraft maintenance. This will allow the aircraft to be powered off line.

SPECIFICATIONS

An electric motor drives a pressure compensated piston pump. Filters are provided on the pressure and return systems. A bypass (dump) valve allows starting and stopping of the unit under a no-load, safe condition. The unit may use either the aircraft or on-board HPU reservoir.

· SYSTEM REQUIREMENTS:

· Must include:

· Motor driven hydraulic pump flow rate display

· Reservoir fluid level visual indicator

· Working Pressure Range 500-5,000 psi

· 3 PHASE. 60 HZ 220/230 Voltage

· Paint color:

· BLUE

· 50 FT Hoses (2 sets)

· Split system Crossover

· Hand pump

· Hour Meter

· Pyrometer

· SAFETY FEATURES:

· Must include:

· Pump/Motor coupling guard

· Sheet metal panels

· Pressure and return system relief valves

· Control circuit fuses

· Motor overload protection

· Emergency shut off switch

· Calibration port shut off valve

· Floor lock

· Foot actuated and released

· Fluid sample shut off valve

· ELECTRICAL POWER REQUIREMENTS:

· Must include:

· Electrical power supply must include a fused disconnect

· Type J fuses

· Type R fuses

· Equivalent magnetic type circuit breakers

· VENDOR REQUIREMENTS

· Vendor must be ISO 9001:2015 Certified/Compliant

· Vendor will provide on-site training and assistance at no additional charge

REQUIREMENT

HYDRAULIC POWER UNIT 1EA (ANY COLOR THAT IS DIFFERENT FROM 1ST UNIT)

Hydraulic Power Unit (HPU) will provide the 1108th TASMG MSARNG a source of clean, pressurized hydraulic fluid for performing required aircraft maintenance. This will allow the aircraft to be powered off line.

SPECIFICATIONS

An electric motor drives a pressure compensated piston pump. Filters are provided on the pressure and return systems. A bypass (dump) valve allows starting and stopping of the unit under a no-load, safe condition. The unit may use either the aircraft or on-board HPU reservoir.

· SYSTEM REQUIREMENTS:

· Must include:

· Motor driven hydraulic pump flow rate display

· Reservoir fluid level visual indicator

· Working Pressure Range 500-5,000 psi

· 3 PHASE. 60 HZ 220/230 Voltage

· Paint color:

· RED

· 50 FT Hoses (2 sets)

· Split system Crossover

· Hand pump

· Hour Meter

· Pyrometer

· Electric Clog Indicator

· Electric Over Temperature Meter

· SAFETY FEATURES:

· Must include:

· Pump/Motor coupling guard

· Sheet metal panels

· Pressure and return system relief valves

· Control circuit fuses

· Motor overload protection

· Emergency shut off switch

· Calibration port shut off valve

· Floor lock

· Foot actuated and released

· Fluid sample shut off valve

· ELECTRICAL POWER REQUIREMENTS:

· Must include:

· Electrical power supply must include a fused disconnect

· Type J fuses

· Type R fuses

· Equivalent magnetic type circuit breakers

· VENDOR REQUIREMENTS

· Vendor must be ISO 9001:2015 Certified/Compliant

· Vendor will provide on-site training and assistance at no additional charge

REQUIREMENT

JACK TRIPOD 9EA

SPECIFICATIONS:

The device will be utilized to lift an aircraft by its fuselage and/or main wing with other hydraulic jacks arranged by position and quantity to provide proper balance in conjunction with the correct jack pad.

· SYSTEM REQUIREMENTS:

· Must include:

· Casters

· Capacity

· 10 Tons

· Stage: M

· Extension

· Mechanical Range from 8.4 - 8.7 In

· Hydraulic Range from 20 – 23 In

· AIRCRAFT APPLICATION:

· Sikorsky UH-60 Black Hawk, Silkorsky M-60M

· VENDOR REQUIREMENTS

· Vendor must be ISO 9001:2015 Certified/Compliant