曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

Richfield Div. Richfield A Richfield A-1
B.P. Trading B.P.A.T.K
Caltrex Petroleum Corp. Caltex Jet A-1
Chevron Chevron A-50 Chevron A-1
Cities Service Co. CITGO A
Continetal Oil Co. Conoco Jet-50 Conoco Jet-60
EXXON Co., USA EXXON A EXXON A-1
Gulf Oil Gulf Jet A Gulf Jet A-1
Mobil Oil Mobil Jet A Mobil Jet A-1
Phillips Petroleum Philijet A-50
Shell Oil Aeroshell 640 Aeroshell 650
Sinclair Superjet A Superjet A-1
Standard Oil Co. Jet A Kerosene Jet A-1 Kerosene
Texaco Avjet A Avjet A-1
Union Oil 76 Turbine Fuel
FOREIGN FUELS (NATO-F44)
Canada 3-GP-24e
West Germany UTL-9130-007.UTL-9130-010
Italy AMC-143
Netherlands D. Eng RD 2493
United Kingdom (Britain) D. Eng RD 2498
* Commercial fuel such as ASTM-D-1655 not containing a icing inhibitor per MIL-I-27686 (commercial name is
“PRIST”). Use PRIST in accordance with instructions on the can. Anti-icing and Biocidal Additive for Commercial
Turbine Engine Fuel - The fuel system icing inhibitor shall conform to MIL-L-27686. The additive provides anti-icing
protection and also functions as a biocide to kill microbial growths in helicopter fuel system,s. Icing inhibitor
conforming to MIL-I-27686 shall be added to commercial fuel not containing an icing inhibitor during refueling operations,
regardless of ambient temperatures. Refueling operations shall be accomplished in accordance with accepted
commercial procedures. Commercial product PRIST conforms to MIL-I-27686.
TM 1-1520-240-10
2-15-13
2-15-7. Gravity Refueling. Perform the following
steps:
a. Be sure the helicopter is at least 50 feet from any
hangar or structure.
b. Be sure the fueling vehicle is at least 10 feet from
the helicopter.
c. Electrically ground the helicopter as follows:
(1) Connect one end of an approved ground
cable to the aft landing gear eyebolt or to one of the jacks
on the side of the fuselage. Grounding jacks are located
at sta. 115 on the RH side and sta. 530 on the LH side in
the fuselage skin. Connect the other end to a grounding
rod or ramp ground point. Make sure the cable has no
broken strands and the clip are securely attached to the
cable and ground points.
(2) Make sure the fueling unit is grounded to the
same ground rod or ground point as the helicopter.
(3) Before opening the filler cap, ground the
nozzle to the ground jack directly above the fuel tank
filler.
d. When the fuel is at the desired level, remove the
nozzle. Secure the filler cap. Then, disconnect the nozzle
ground wire.
e. Remove the ground connection. If the helicopter
is to remain parked, do not disconnect the helicopter
ground.
2-15-8. ERFS Refueling and Fuel Transfer.
ERFS Refueling and Fuel transfer will be in accordance
with existing Air Worthiness Release (AWR).
2-15-9. ERFS II Refueling.
Refueling the ERFS II tanks is performed by either single
point pressure refueling or gravity refueling.
WARNING
The manually operated fuel/defuel vent
valve on each tank must be placed in the
closed position following pressure refueling.
Failure to do so could permit significant
fuel leakage in the event of a crash
and the vent self–sealing breakaway valve
fails to actuate.
CAUTION
If the fuel/vent valve is not opened, the
tank cannot be pressure refueled.
a. Single Point Pressure Refueling. The ERFS II
tanks are single point pressure refuled from a connection
at the motorized gate valve. The motorized gate valve
must be open to pressure refuel and is controlled by the
refuel valve switch on the ERFS II fuel control panel
located on the forward most ERFS II tank installed. The
fuel transfer hose is connected to the forward interconnecting
ERFS II fuel manifold. Fuel from the transfer
hose passes through the breakaway valve and the
manual fuel/defuel valve to the lower fuel/shutoff valve in
the tank bottom.
CAUTION
The operator must exercise caution to
avoid ERFS II tank overflow during gravity
refueling. There is no automatic fuel flow
shutoff.
b. Gravity Refueling. If pressure refueling of ERFS
II tanks is not performed or prevented, each tank can also
be gravity filled through the gravity filler opening on the
top of each tank. To gravity fill, the crashworthy filler cap
is removed and external fuel source nozzle is inserted
and the tank is filled. Low pressure flow rates must be
maintained as venting or vapors bypass the filler opening
and the fuel/defuel vent valve is closed during this operation.
Because fuel is not entering the tank through the
fuel/defuel line, the high level shutoff valve has no effect
　
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