Aircraft Jacking Manifold- Item description_Rev.1.pdf

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Attached to
Aircraft Jacking Manifold Hydraulic Pumping Unit Federal contract opportunity
Solicitation number
FA812525Q0094
Issued by
Department of the Air Force Materiel Command Air Force Sustainment Center

About this file

This document is an Item Description from the Department of the Air Force's Oklahoma City Air Logistics Complex (OC-ALC) at Tinker Air Force Base, detailing specifications for three Aircraft Jacking Manifolds. The required equipment includes a Hydraulic Pumping Unit with specific technical characteristics such as a welded steel housing, diesel/electric power, 12-volt battery, and a 3-hose configuration. Key specifications include a JP-8 aircraft fuel system, 11-gallon fuel tank, stainless steel 56-gallon fluid reservoir, a 24.0 HP diesel engine, towable trailer chassis, and a static reel with 50' cable.

The document outlines strict item acceptance criteria, focusing on asset condition and system setup. Acceptance requires zero physical damage to components, with minor cosmetic blemishes potentially acceptable at the discretion of the accepting party. System setup must involve successful installation and configuration according to vendor instructions, with all software components correctly installed and licensed. The item description includes detailed technical specifications for each component, such as automatic flow control valves rated at 4000 PSI, specific hose lengths, and precise operational parameters for the hydraulic system.

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Other files for this federal contract opportunity

Other files attached to Aircraft Jacking Manifold Hydraulic Pumping Unit, newest first.
File Type Posted
Solicitation Amendment FA812525Q00940001 SF1449.pdf PDF
Solicitation Amendment FA812525Q00940001 SF 30.pdf PDF
Solicitation - FA812525Q0094.pdf PDF
Aircraft Jacking Manifold- Item description.pdf PDF

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Text version

DEPARTMENT OF THE AIR FORCE

OKLAHOMA CITY AIR LOGISTICS COMPLEX (OC-ALC)

TINKER AIR FORCE BASE OKLAHOMA

Item Description

Aircraft Jacking Manifold

The 76 AMXG is requesting three (3) Aircraft Jacking Manifold. This requirement must have the following specifications:

Three (3) Hydraulic Pumping Unit, NSN: 4320-01-562-6243, Master NSN:

4320-01-524-4611

Welded steel housing, power driven, stainless steel fluid reservoir, hydraulic pumping unit.

Diesel/electric powered with 1800 RPM speed operation. 12-volt direct current capacity battery. 3 hose set configuration, female connection, constructed of zinc plated steel: 2.49in, 3/8-18 (NPTF)

• JP-8 aircraft fuel system

• 11-gallon fuel tank capacity

• Housing: Metal enclosures with access panels, hinged doors, storage compartments, and weather resistant properties.

• Stainless steel, 56 U.S. Gallons Capacity, Fluid Specification MIL-PRF-5606, MIL-PRF-83282, MIL-PRF-85257

• Diesel engine 24.0 Horsepower (HP) (continuous); 27.0 HP (intermittent); 2 cylinders, 4 cycle, in-line type, air/oil cooled

• Towable Trailer Chassis

• Front Steer Knuckle type with towbar

• Parking brake, hand lever assembly parking type (rear wheels)

• Tires and Wheels, Four (4) pneumatic tires, 6-ply, 6 x 9, split wheel

• Static Reel(s), one (1) spring rewind with 50' of cable w/clamp and plug

• Manhole, one (1) stainless steel, quick opening, with a single cam latch

• Battery 12 Volts Direct Current (VDC), 60 Amperes (Amps)/hour, gel-type

• Electric Motor 15 HP, 380/460 Volts Alternating Current (VAC), 50/60 Hertz (Hz)

• Operation maintenance manuals

• Operating Speed 1500/1800 RPM

Revison 1

• 40 feet; branching to (1) 15-foot hose and (1) 85-foot hose Termination Automatic flow control valve: pressure compensated; 4000 PSI rated; unrestricted supply flow; restricted 1.0±0.100 return flow.

• Automatic flow control valve: pressure compensated; 4000 PSI rated; unrestricted supply flow; restricted 1.0±0.100 return flow.

• Automatic flow control valve: pressure compensated; 4000 PSI rated; unrestricted supply flow; restricted 1.0±0.100 return flow.

Item acceptance is dependent on the following criteria being met and verified:

Asset Condition:

• Criteria: Items crated for shipment.

• No physical damage to any system components (hardware, software media, documentation) as verified by visual inspection upon delivery.

• Verification Method: Visual inspection of all delivered items against the packing list.

• Acceptance Threshold: Zero damaged components. Minor cosmetic blemishes that do not affect functionality may be accepted at the discretion of [Accepting Party Name/ Role].

System Setup:

• Criteria: Successful installation and configuration of all system components according to the vendor's installation instructions and configuration guides. All software components are correctly installed and licensed.

Revison 1

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