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    Advanced Aviation Forward Area Refueling System AAFARS Model M100A1

    Welcome to Salvex Marketplace, where you can buy surplus, salvage, and discounted aircraft parts as part of a commercial repurposing strategy.

  • Advanced Aviation Forward Area Refueling System AAFARS Model M100A1
  • 182968005_405414
  • 182968005_405415
  • 182968005_405416
  • 182968005_405417
  • Attention

    This item is no longer available.

    Advanced Aviation Forward Area Refueling System AAFARS Model M100A1 Share with Buyers


    Welcome to Salvex Marketplace, where you can buy surplus, salvage, and discounted aircraft parts as part of a commercial repurposing strategy.

    ID:182968005
    Seller:
    Seller Industry:
    Quantity:1 Item
    Condition:
    Excellent, new

    :
    Product Location:
    End Time:

    Item Description

    We are collecting bids for this AAFARS Advanced Aviation Forward Area Refueling System Model M100A1 PUMP ENGINE MODULE. This item is in its original shipping crate and is brand new / never used.  There is no damage and this item was abandoned by the original owner.   This unit can be used on the ground for refueling and also can be mounted in Helicopters.

    The crate measurement is 8' x 6' x 40" high

    Please see the pictures with this listing:  This sale is for the pump engine module as seen in the pictures.

    Any questions, please ask.

    System Information:

    To provide a day or night, soldier-portable, four-point refueling system capable of providing filtered fuel at a rat of fifty-five gallons per minute to each of four nozzles separated by a distance of 100 feet (30.5 m), and to operate satisfactorily from 120 F (48.9 C) to -25 F (-31.7 C)

    OPERATOR, UNIT, DIRECT SUPPORT AND GENERAL SUPPORT MAINTENANCE ADVANCED AVIATION FORWARD AREA REFUELING SYSTEM MODEL M100A1 EQUIPMENT DESCRIPTION AND DATA EQUIPMENT CHARACTERISTICS, CAPABILITIES AND FEATURES

    The AAFARS is a modular, four man portable, four-point refueling system. AAFARS provides filtered fuel at fifty-five gallons per minute to each of four nozzles 100 feet (30.5 meters) apart. The system will operate satisfactorily from 120 F(48.9 C) to 25 F (-31.7 C).The core components of the AAFARS are the pump-engine module; the liquid fuel filter-separator; the accessory module; and the hoses, nozzles and fittings that deliver fuel from the fuel drums to the fueling points.

    The system allows a choice of recirculation setups to filter the fuel during operation. Fuel recirculation also helps prevent pump overheating due to staticpressure build.  All fuel delivery components (hoses, pump, filter, wyes, tees, elbows, etc.) feature unisex dry-break couplings, with the exception of the valved camlock elbow couplings that connect the fuel hoses and pressure control to the fuel drums. Valved unisex couplings are dry break fittings. They can be connected or disconnected only when the valves are closed. This allows components to be separated without spilling fuel. When connected (with valves open), the unisex couplings are locked together, preventing accidental separation. Nozzles are equipped with non-valved unisex couplings to prevent trapping fuel ina disconnected nozzle. Thermal expansion of trapped fuel may damage a nozzle.The AAFARS is designed to operate normally from four 500-gallon fuel drums. The system includes an adapter kit thatallows the AAFARS to be connected to any source which can be accessed through two-inch, three-inch, or four-inch camlock couplings. The adapters also allow connection of AAFARS components to any other fuel system components that use standard two-inch, three-inch, or four-inch camlock couplings.A twenty-four vdc auxiliary pump is provided to defuel the system after a mission or operation. The auxiliary pump is also useful for pumping down a component before or after removal from the system due to operational reconfiguration or maintenance action.

    a. Characteristics

    • Modular construction
    • Man portable
    • Provides the capability to connect to any source that can be accessed through 2-inch, 3-inch, or 4-inch camlock couplings

    b. Capabilities

    • Provides filtered fuel at 55 gpm to each fueling point
    • Provides filtered fuel at 90 gpm to one fueling point
    • Operates in a temperature range of +120 F (+48.9 C) to 25 F (-31.7 C)

    c. Features

    • Uses a D-1, CCR or fuel/oil servicing (open port) nozzle
    • Closed circuit recirculation
    • Electrical power provided by a maintenance free 24 vdc battery
    • All fuel discharge components feature valved unisex couplings with the exception of the camlock couplings at the fuel drums and pressure control and non-valved unisex couplings on the nozzles
    • Prime mover is a 2 cylinder diesel engine
    • Valved unisex couplings provide fuel discharge component isolation
    • Electric or manual start

    This is military surplus - you can find addtional info on this item:

    http://aviationmiscmanuals.tpub.com/TM-10-4930-351-14/



    This seller also has a 1000 Gallon Jet Fuel Tank available as well and can be used with this system:

    Jet A Fuel Tank - 1000 Gallons Capacity

     http://www.salvex.com/listings/listing_detail.cfm?aucID=182955728

     

    Seller Terms

    • Salvex and the seller have the right to reject any and all offers.
    • This product is sold AS IS, WHERE IS.
    • Buyer is responsible for all taxes, duties, loading and freight charges.
    • Seller does not offer any warranties or manufacturer warranties.
    • Upon receipt of cleared funds, Seller will provide the Buyer a Release Order for item pick up. Title transfers from Seller to Buyer upon issuance of the Release Order.
    • It is Buyer's responsibility to verify quantities and condition at the time of pick up. Once the product has been removed from Seller's location, there will be no adjustments based on quantity or condition.

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