曝光台 注意防骗
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minute (rate varies with engine(s) fuel flow). If the receiving side tank is at or near maximum capacity,
care should be taken to assure fuel is not being lost through the fuel vents.
Fuel transfer will not occur if the fuel boost pump is operating in the receiving tank. The Fuel Boost
Switches must be in NORM, or the Fuel Boost switch for the tank at the head of the arrow on the
FUEL TRANSFER selector must be OFF, and for the opposite tank, ON. During EMER power
operations, the fuel transfer valve will close and fuel transfer will not be possible.
An amber FUEL FLTR BP L-R CAS message and MASTER CAUTION will indicate an impending
bypass of the fuel filter if the differential pressure across the fuel filter reaches approximately 10 PSI.
An amber FUEL LVL LO L-R CAS message will illuminate when the respective fuel quantity is less
than approximately 170 pounds. This message is delayed for 30 seconds to minimize nuisance
indications in turbulent conditions.
NOTE
The FUEL BOOST switches should be positioned to ON if the FUEL LVL LO message
is displayed or if the indicated fuel quantity is below 170 pounds. It is permissible to
turn the boost pump to NORM on the receiving side while fuel transfer is in progress.
Total usable fuel for flight planning purposes is 1290 pounds per wing (192.5 U.S. gallons), 2580
pounds total, when filled to bottom of the filler standpipe. Filling above the bottom of the standpipe
should not be intentionally done as there may not be sufficient room for expansion and fuel vent
spillage may result.
ANTI-ICE ADDITIVES
NOTE
EGME and DIEGME additives are not required but may be used if desired, in
accordance with the following procedures.
(Continued Next Page)
3-164 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
NORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
ANTI-ICE ADDITIVES (Continued)
PROCEDURE FOR ADDING ETHYLENE GLYCOL MONOMETHYL ETHER (EGME)
FUEL ADDITIVE
Use the following procedure to blend anti-icing additive as the airplane is being refueled through the
wing filler caps:
1. Attach MIL-I-27686 additive to refuel nozzle, making sure blender tube discharges in the
refueling stream.
2. Start refueling while simultaneously fully depressing and slipping ring over trigger of
blender.
WARNING
Anti-icing additives containing Ethylene Glycol Monomethyl Ether
(EGME) are harmful if inhaled, swallowed, or absorbed through the skin,
and will cause eye irritation. Also, it is combustible. Before using this
material, refer to all safety information on the container.
CAUTION
Make sure that the additive is directed into the flowing fuel stream and that the
additive flow is started after the fuel flow starts and is stopped before fuel flow
stops. Do not allow concentrated additive to contact coated interior of fuel tank
or airplane painted surface. Use not less than 20 fluid ounces of additive per
156 gallons of fuel or more than 20 fluid ounces of additive per 104 gallons of
fuel.
PROCEDURE FOR ADDING DIETHYLENE GLYCOL MONOMETHYL ETHER (DIEGME)
FUEL ADDITIVE
NOTE
Service experience has shown that DIEGME has provided acceptable protection from
bacterial growth in fuel systems.
Use the following procedure to blend anti-icing additive as the airplane is being refueled through the
wing filler caps:
1. Attach MIL-I-85470 additive to refuel nozzle, making sure blender tube discharges in the
refueling stream.
2. Start refueling while simultaneously fully depressing and slipping ring over trigger of
blender.
(Continued Next Page)
510FM-07 AA 3-165
SECTION III - OPERATING PROCEDURES MODEL 510
NORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
PROCEDURE FOR ADDING DIETHYLENE GLYCOL MONOMETHYL ETHER (DIEGME)
FUEL ADDITIVE (Continued)
CAUTION
• Diethylene Glycol Monomethyl Ether (DIEGME) is slightly toxic if
swallowed and may cause eye redness, swelling, and irritation. It is also
combustible. Before using this material, refer to all safety information on
the container. Make sure the additive is directed into the flowing fuel stream
with the additive flow started after the fuel flow starts and stopped before
fuel flow stops. Do not allow concentrated additive to contact coated
interior of fuel tank or airplane painted surface.
• Use not less than 20 fluid ounces of additive per 156 gallons of fuel nor
more than 20 fluid ounces of additive per 104 gallons of fuel.
PROCEDURE FOR CHECKING FUEL ADDITIVES
Prolonged storage of the airplane will result in a water buildup in the fuel which “leaches out” the
additive. An indication of this is when an excessive amount of water accumulates in the fuel tank
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Citation Mustang airplane flight manual 1(114)
