Advanced Aviation Forward Area Refueling System(AAFARS) -Normal .. For more detailed information refer to TM &P. 2. 3. TM AAFARS MA1 – Free ebook download as PDF File .pdf), Text File .txt) or read book online for free. DIRECT SUPPORT. REFUELING SYSTEM. MAINTENANCE PROCEDURES (AAFARS). NSN ALPHABETICAL INDEX.

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Fuel recirculation also helps prevent pump overheating due to staticpressure build. Refer to figure 3.

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. To change from use of a D-1 nozzle to a CCR nozzle during refueling operations: Recirculation Manifold Figure Register As aafara Buyer.

Advanced Aviation Forward Area Refueling System AAFARS Model MA1 | Salvex

To provide a day or night, soldier-portable, four-point aafars 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 feet Refer to figure 7.

When connected with valves openthe unisex couplings are locked together, preventing accidental separation. Front Crankshaft Bearing Installation Figure 3. This sale is for the pump engine module as t, in the pictures. Auxiliary Pump Decals Figure 7. They can be connected or disconnected only when the valves are closed.


Advanced Aviation Forward Area Refueling System AAFARS Model M100A1

Cylinder Head Installation Figure This allows components to be separated without spilling fuel. This unit can be used on the ground for refueling and also can be mounted in Helicopters. Pump-Engine Emplacement Figure 5. Clamp, Grounding Figure 2.

TM Advanced Aviation Forward Area Refueling System (AAFARS) Model MA1 Manual

Refer to Figure Refer to figure 6. Equipment Data Table 1.

Operator Troubleshooting Table 1. The system allows a choice of recirculation setups to filter the fuel during operation. Refer to figure Glass Panels, Partitions, Frames Etc.

Components of End Item List Table 2.

Accessory Module Decals Figure 6. Fuel Contamination Test Kit Figure 8. Thermal expansion of trapped fuel may damage a nozzle. Manual Engine Start Verify that pump outlet hose pressurizes hose expands. Cylinder Head Removal Figure Airport Ground Support Equipment. The core components of the AAFARS are the pump-engine module; the liquid fuel filter-separator; the accessory module; and the hoses, aafare and fittings that deliver fuel from the fuel drums to the fueling points.


A twenty-four vdc auxiliary pump is provided to defuel the system after a mission or operation. Fuel Contamination Test Kit Position fuel drums figure 1, 2 on spill containment unit 1. Ask a Question About This Listing: Particulate Fuel Contamination Test Perform particulate contamination fuel test. Rotable Spare Parts for the Boeing Boeing This seller also has a Gallon Jet Fuel Tank available as well and can be used with this system:.

NSN 4930-01-495-0024:

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. Tube, Outlet, Filter-Separator Figure 4. Operator Troubleshooting Continued Table 1. Fuel System Components Removal Figure My location click to change: Refer to figures 10 and Boeing Spare Parts Package Boeing To see active listings click here.