MODEL
402C
...................
u
HANDLING, SERVICE & MAINTENANCE
5.
Tie
ropes
or chains of at least 700 pounds tensile strength to
the
wing
tie-down
fittings located
on
the
underside of
each
wing,
aft of
each
main
landing gear.
Secure the opposite ends of the ropes or Chains
to
ground anchors.
Chock
the
main landing gear tires; do not set the parking brake
if
a long period of inactivity is
anticipated,
as
brake
seizing
can
result
6. secure a rope (no chains
or
cables)
to
the upper nose gear trunnion and secure
opposite
end
of
rope
to a ground anchor. Chock the nose landing gear tire.
7.
Secure the middle of a
rope
or
chain
to the
tail
tie-down fitting.
Pull
each
end
of
the rope or chain
at
a 45-degree angle and secure to ground anchors at
each
side
of the tail.
8.
If at the
end
of 30
days,
the airplane
is
not
removed
from
storage,
the airplane
should
be
flown for 30 minutes, reaching, but not exceeding normal
oil
and
cylinder
temperatures. If the airplane cannot
be
flown, it should be represerved in
temporary
or
indefinite storage.
SERVICING
r-------NOTE
------.,
Refer to the Airplane Service Manual for complete
servicing requirements.
FUEL
(Approved Fuel Grades and Colors)
PRIMARY -
100
(Formerly 100/130) Grade Aviation Fuel (Green)
ALTERNATE -
100LL
Grade Aviation Fuel (Blue)
Tank capacities are:
Each Main Tank -
106_7
Gallons
Isopropyl alcohol, or ethylene
91yco1
monomethyl ether (EGME) may
be
added to the fuelI
supply. Additive concentrations by volume for alcohol shall not exceed 1%. Additive
concentrations
by
volume for EGME shall
be
0.10 percent minimum to 0.15 percent
maximum, either individually or mixed in a common tank. Fuel, when added to the tank,
should have a minimum concentration of 0.10 percent
by
volume. Refer to Fuel Additive
paragraphs in this section for additional information.
WARNING
• Do not operate any avionics or electrical equipment
on
the
airplane during fueling. Do not allow open flame or smoking in
the vicinity of the airplane while fueling.
• During all fueling operations, fire fighting equipment must
be
available.
Two
ground wires from different points on the airplane
to separate approved grounding stakes shall
be
used.
1 November
1979
Revision 5 -
18
March
1998
8-9
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