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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Refer to figure 3. Pushrod Measurement Figure Accessory Module Decals Figure 6.

TM 4-48.18/To 13c7-1-19 Airdrop of Supplies and Equipment : Rigging Forward Area

This unit can be used on the ground for refueling and also can be mounted in Helicopters. Fuel recirculation also helps prevent pump overheating due to staticpressure build. Please see the pictures with this listing: Fuel System Components Removal Figure To change from use of a D-1 nozzle to a CCR nozzle during refueling operations: Particulate Fuel Contamination Test Perform particulate contamination fuel test.

Refer to figures 10 and The auxiliary t is also useful for pumping down a component before or after removal from the system due to operational reconfiguration or maintenance action. Crankshaft Assembly Installation Figure 2. Position one nozzle kit at each fueling point.

Ask a Question About This Listing: The core components aafarx 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 afaars. Clamp, Grounding Figure 2. My location click to change: Mandatory Replacement Parts List Table 1.

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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 feet Refer to figure 4.

Fuel Contamination Test Kit Position fuel drums figure 1, 2 on spill containment unit 1.

Advanced Aviation Forward Area Refueling System AAFARS Model M100A1

Refer to figure This sale is for the pump engine module as seen in the pictures. With the fuel transfer pump Defuel system fuel hoses. Mouse over to Zoom – Click to enlarge. Tube, Outlet, Filter-Separator Figure 4. Tube, Inlet, Filter-Separator Figure 3.

APPENDIX A REFERENCES – TMP_95

Recirculation Manifold Figure There is no damage and this item was abandoned by the original owner. Airport Ground Support Equipment. Operator Troubleshooting Continued Table 1. Nozzles are equipped with non-valved unisex couplings to prevent trapping fuel ina disconnected aaars.

When connected with valves openthe unisex couplings are locked together, preventing accidental separation. This allows components to be separated without spilling fuel.

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Pump-Engine Emplacement Figure 5. To see active listings click here.

Section Ill. BASIC ISSUE ITEMS

Privacy Statement Press Release Contact. Register As a Buyer. Boeing Spare Parts Package Boeing Equipment Data Table 1. The system will operate satisfactorily from F Glass Panels, Partitions, Frames Etc.

They can be connected or disconnected only when the valves are closed. 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. Valved unisex couplings are dry break fittings. Refer to figure 6.

Fuel Delivery Equipment Figure 6. A twenty-four vdc auxiliary pump is provided to defuel the system after a mission or operation. The system allows a choice of recirculation setups to filter the fuel during operation.

Periodically monitor condition of the fuel transfer pump discharge hose. Equipment Data Continued Table 1. Manual Aafasr Start Verify that pump outlet hose pressurizes hose expands.

Refer to figure 7. D-1 Nozzle Assembly Figure 8. Refer to figure 9. Front Crankshaft Bearing Installation Figure 3.