Aircraft Jacking Manifold- Item description.pdf
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- Attached to
- Aircraft Jacking Manifold Hydraulic Pumping Unit Federal contract opportunity
- Solicitation number
- FA812525Q0094
About this file
This document is an Item Description from the Department of the Air Force's Oklahoma City Air Logistics Complex at Tinker Air Force Base, detailing requirements for Aircraft Jacking Manifold (Item A25-077). The 76 AMXG is requesting three (3) Hydraulic Pump Units with specific technical specifications, including a stainless steel, diesel-powered hydraulic pump with a 12-volt DC capacity, 11-gallon fuel tank, JP-8 aircraft fuel system compatibility, and a towable trailer chassis.
The equipment must feature a diesel engine with 24.0 continuous horsepower, four pneumatic tires, a static reel with 50' of cable, a stainless steel manhole with a quick-opening cam latch, and a 12V gel-type battery. Additional requirements include a 15 HP electric motor, operation maintenance manuals, and automatic flow control valves rated at 4000 PSI with specific flow characteristics. The hose configuration includes a 40-foot total length, branching into one 15-foot and one 85-foot hose, with precise flow control and pressure compensation specifications.
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Solicitation Amendment FA812525Q00940001 SF1449.pdf | ||
| Aircraft Jacking Manifold- Item description_Rev.1.pdf | ||
| Solicitation Amendment FA812525Q00940001 SF 30.pdf | ||
| Solicitation - FA812525Q0094.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
A25-077
The 76 AMXG is requesting three (3) Aircraft Jacking Manifold. This requirement must have the following specifications:
Three (3) Hydraulic Pumping Unit, NSN: 4320-01-524-4611
Stainless steel, power driven, hydraulic pumping unit. Diesel powered with 1800 RPM speed operation. 12-volt direct current capacity. 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
• 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.
File details come from the government source that posted it. Updated .