ARROWil
DRAINING FUEL VAL YES AND LINES
The fuel strainer, located on the lower left side of the firewall, is provided with a
quick drain which should be drained before the frrst flight of the day or after refueling, to
check for fuel contamination. If contamination is found, fuel should be drained until the
contamination stops. If contamination persists after draining fuel for a minute, contact a
mechanic to check the fuel system.
Each fuel tank
is
provided with a fuel quick drain to check for contamination. Each
tank should be checked for contamination in accordance with the above procedure.
DRAINTNG FUEL SYSTEM
The bulk of the fuel may be drained from the fuel cells by the use of a siphon hose
placed in the cell or
tank
through the filler neck. The remainder of the fuel may be drained
by opening all the drain valves.
TIRE INFLATION
For maximum service from the tires, keep them inflated to the proper pressure of 30 psi
for nose tire and 27 psi for main tires. Interchange the tires periodically' for even wear. All
wheels and tires are balanced before original installation, and the relationship of tire, tube and
wheel should be maintained upon reinstallation. In the installation of new components, it may
be necessary to rebalance the wheels with the tires mounted. Unbalanced wheels can cause
extreme vibration in the landing gear.
BATTERY SERVICE
Access to the battery is gained through the baggage compartment. It is located just aft of
the baggage compartment, The battery container has a plastic drain tube which
is
normally
closed off. This tube should be drained periodically to remove battery acid which may have
collected in the tube.
The battery fluid level must not be brought above the baffle plates. It should be checked
every 30 days to determine that the fluid level is proper and the connections are
tight
and free
of corrosion.
If the battery is not properly charged, recharge it starting with a rate of four amperes and
finishing with a rate of two amperes. The battery should be removed from the airplane for
charging, and quick charges are not recommended.
The external power receptacle, if installed,
is
located on the right side of the fuselage aft of
the baggage compartment door.
9-8
Refer to the Arrow II Service Manual for battery servicing procedure.
HANDLING AND SERVICING
REVISED: December S, 1975
(
v-
N16422 POH
Содержание Cherokee Arrow II
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Страница 37: ...AIRPLANE AND SYSTEMS ISSUED Novemoer 15 1971 Main Wheel Assembly ARROWil BRAKE HOUSING 2 7 N16422 POH...
Страница 47: ...AIRPLANE AND SYSTEMS ISSUED November 1s 1971 Static System ARROW IT 2 17 _ I N16422 POH...
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