|
| |
TM 10-4930-240-13
1-10. LOCATION AND DESCRIPTION OF MAJOR COMPONENTS -cont.
i.
Single Point Refueling Nozzle (Type D1) (9). D1 nozzles are supplied with AFARE for refueling
aircraft with pressurized fuel systems. The D1 nozzles are non-regulating, so fuel pressure must
controlled by the pressure reducing skid assembly. For location and description of major component
on the D1 nozzle, refer to TM 10-4930-242-13&P.
j.
Closed Circuit Refueling (CCR) Nozzle with Gravity Fill Adapter (10). The CCR nozzles and gravity
fill adapters supplied with the AFARE are used to connect the fuel system to the aircraft. The hand
operated CCR nozzle locks onto the aircraft refueling adapter and regulates fuel pressure to the
aircraft Nozzle are supplied with a ground clamp and plug for electrical bonding of the nozzle to the
aircraft. Refueling aircraft with gravity feed fuel tanks requires connection of the gravity fill adapter
to the CCR nozzle. For location and description of major components on the CCR nozzle and gravity
fill adapter, refer to applicable TM 10-4930-243-13&P.
k.
Valve Section (11). The valve section is comprised of a gate valve and straight pipe section. The
valve section is used to assemble the AFARE system and provide control of fuel flow. Both ends of
the valve section are equipped with quick disconnect couplings.
l.
Filter Separator 200GPM File Assembly (12). The filter separator is a skid mounted unit containing a
separator tank and various valves, gages and piping. The filter separator is installed downline of the
200 GPM pump to remove water and particle contaminants from the fuel. For location and
description of major components on the filter separator, refer to TM 10-4330-236-13.
m.
Air Duct (13). Three collapsible air ducts connect the deflector assembly to the filter separator Each
duct is 12 feet long when extended and 4-feet long when collapsed. The air ducts carry hot exhaust
from deflector on the 200 GPM pump to the filter separator defrost shroud.
n.
Deflector Assembly (14). The deflector is mounted on top of the 200 GPM pump. The deflector
serves as a plenum to collect heat generated by the operating turbine engine and directing it into the
attached air ducts.
o.
200 GPM Pump Assembly (15). The pump assembly is a self contained, skid mounted unit powered
by a turbine engine. The pump assembly provides the force required to distribute fuel from the 500
gallon drums to the fuel dispensing nozzles. For location and description of major components on
the 200 GPM pump assembly, refer to applicable TM 10-4320-342-10.
p.
3-inch Manifold (16). The three inch manifold contains a gate valve and tee. The manifold is used to
assemble the AFARE system and provide control of fuel flow. The manifold is equipped with quick
disconnect couplings.
q.
Ground Rods (17). Three ground rods provide grounding for the fueling points and the 200 GPM
pump.
1-6
|
