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Two in-line, multiple cartridge filters capable of
filtering out 5 micron absolute particulates are included
as part of the FARE kit. The 45 inch x 44 inch x 35 inch
container for FARE component storage is secured to the
cargo floor (fig. 4-4-3).
TM 1-1520-240-10
4-4-5
Figure 4-4-2. ERFS II Fuel Control Panel
TM 1-1520-240-10
4-4-6
Figure 4-4-3. ERFS Fuel System Schematic
TM 1-1520-240-10
4-4-7/(4-4-8 blank)
4-4-9. FARE Transfer.
CAUTION
Some fuel will remain trapped in the FARE
pump module, suction hose, filters, and
collapsible hoses after suctioning and
rolling of the FARE hoses has been completed.
To avoid spilling trapped fuel, the
valves in the Unisex couplings must remain
closed and the couplings capped after
the FARE system is disassembled. All
trapped fuel should be drained into an appropriate
container when the operational
situation permits.
WARNING
The manually operated FUEL/DEFUEL
valve must be placed in the CLOSED position
following FARE operation. Failure to
do so could permit significant fuel leakage
in the event of a crash and the vent selfsealing
breakaway valve fails to actuate.
a. Single-Point Pressure Refueling Hose Assembly
– Unisex valve at ERFS II tank — check CLOSE.
b. Valve in the base of the Unisex “T” coupling on
tanks that are NOT the fuel source — CLOSE.
c. Valve in the base of the Unisex “T” coupling on
tank that is the fuel source — OPEN.
d. Manual FUEL/DEFUEL Valve on the tank that is
the fuel source — OPEN.
e. FARE Valve Control Handle — OFF-LOAD.
f. Flowmeter DISPLAY button — Press until TOTAL
2 is displayed. Press and hold three seconds to zero
batch total.
g. FARE PUMP switch — REMOTE.
h.To begin FARE transfer.
i. Remote Control Handle trigger switch —
Squeeze.
When FARE transfer is complete:
j. FARE Valve Control Handle — SUCTION.
k. Valves in the Unisex couplings adjoining the
nozzle(s), and filter(s) — CLOSE. Remove nozzles and
filters from dispensing hoses, replace dust caps, and
stow in FARE container. Reconnect hoses. Valves in the
Unisex couplings, except at nozzle end — OPEN. Valve
in Unisex coupling at far end of hose assembly —
CLOSE.
l. Remote Control Handle trigger switch —
Squeeze to suction fuel from hose assemblies and return
it to tank. While the FARE pump is running, slightly open
the Unisex valves at the nozzle ends of the collapsible
hoses to permit the pump to evacuate most of the fuel
prior to rolling the hose.
m. Collapsible Fuel Hose Assemblies — Lift and
tightly roll from the nozzle end toward the pump module
while the pump is suctioning fuel from the hose. Close the
valves in the Unisex couplings as they are reached in the
disassembly process. Disconnect the hoses, replace
dust caps, and stow in the FARE container. Repeat this
process until all collapsible fuel hose assemblies are
recovered.
n. Remote Control Handle trigger switch — Release.
o. FARE PUMP switch — OFF.
p. Manual FUEL/DEFUEL valve(s) — CLOSED.
q. Valve in the base of the Unisex “T” coupling on all
tanks — check OPEN.

TM 1-1520-240-10
5-1-1/(5-1-2 blank)
CHAPTER 5
OPERATING LIMITS AND RESTRICTIONS
SECTION I. GENERAL
5-5-1. Purpose.
This chapter identifies or refers to all important operating
limits and restrictions that shall be observed during
ground and flight operations.
5-5-2. General.
The operating limitations set forth in this chapter are the
direct result of design analysis, test, and operating experience.
Compliance with these limits will allow the pilot to
safely perform the assigned missions and to
derive maximum utility from the aircraft. Limits concerning
maneuvers, weight, and center of gravity limitations
are also covered in this chapter. If any operating limitations
are exceeded, an entry will be made on DA Form
2408-13-1.
5-5-3. Minimum Crew Requirement.
The minimum crew required to fly this helicopter is two
pilots, and flight engineer. Additional crewmembers, as
required, will be added at the discretion of the commander,
in accordance with pertinent Department of the Army
directives.

TM 1-1520-240-10
5-2-1
SECTION II. SYSTEM LIMITS
5-2-1. Instrument Markings.
5-2-2. Instrument Marking Color Codes.
Operating limitations and ranges are identified by the
colored markings on the dials of engine, flight and utility
　
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