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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With the fuel transfer pump Defuel system fuel hoses. Fuel Delivery Equipment Figure 6.
There aqfars no damage and this item was abandoned by the original owner. 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.
Periodically monitor condition of the fuel transfer pump discharge hose. Clamp, Grounding Figure 2. Refer to figure 4.
Defueling System Fuel Hoses Remove condensation from fuel lines. Accessory Module Decals Figure 6.
NSN: (aafars) –
Operator Troubleshooting Continued Table 1. Rm System Components Removal Figure Manual Engine Start Verify that pump outlet hose pressurizes hose expands. Front Crankshaft Bearing Installation Figure 3.
Cylinder Head Installation Figure All fuel delivery components hoses, pump, filter, wyes, tees, elbows, etc. This allows components to be separated without spilling fuel. To see active listings click here.
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 hm couplings. The adapters also allow connection of AAFARS components to any other fuel system components that use standard two-inch, three-inch, aafas four-inch camlock couplings.
This unit can be used on the ground for refueling and also can be mounted in Helicopters. Particulate Aafarw Contamination Test Perform particulate contamination fuel test. Fuel Contamination Test Kit Position fuel drums figure 1, 2 on spill containment unit 1.
Tube, Outlet, Filter-Separator Figure 4. Thermal expansion of trapped fuel may damage a nozzle. Fuel recirculation also helps prevent pump overheating due to staticpressure aafar. Refer to figure Fuel Contamination Test Kit Figure 8. A twenty-four vdc auxiliary pump is provided to defuel the system after a mission or operation. Components of End Item List Table 2.
Privacy Statement Press Release Contact. Position one nozzle kit at each fueling point. Refer to figure 9.
My location click to change: Rotable Spare Parts for the Boeing Boeing Valved unisex couplings are dry break fittings. Pump-Engine Emplacement Figure 5. Equipment Data Table 1. Nozzles are equipped with non-valved unisex couplings to prevent trapping fuel ina disconnected nozzle.
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