Table of Contents
Advertisement
OPTIONAL WING LOCKER FUEL SYSTEM
Optional wing locker fuel tanks (20 gal. usable each
wing) are installed in the forward portion of the nacelle
wing lockers.
There are no separate fuel selector controls
for the wing locker fuel tanks.
The wing locker fuel is
pumped directly into the main tanks with a fuel transfer
pump.
Indicator lights mounted on the instrument panel are
illuminated by pressure switches to indicate fuel has been
transferred.
The wing locker fuel should not be transferred
until there is 180 lbs. or less in the main fuel tanks to
prevent overflow of the main tank fuel.
Fuel should be
crossfed as required to maintain fuel balance after wing
locker fuel has been transferred.
NOTE
Wing locker transfer pump switches provided
on the instrument panel, energize the wing
locker fuel transfer pumps for transferring
fuel.
These switches should be turned ON
only to transfer fuel and turned OFF when
the indicator lights come ON indicating fuel
has been transferred.
OXYGEN SYSTEM
The oxygen system is designed to provide adequate oxygen
flow rates for altitudes up to 30,000 feet.
The pilot and
passengers shall always use the blue hose assemblies.
The
system consists of a 48.3 or 76.6 cubic foot oxygen bottle,
an altitude compensated regulator, oxygen bottle pressure
indicator, a mechanically actuated on-off valve and the
necessary outlets and plumbing.
See Figure 7-1 for oxygen
consumption rates at various altitudes.
7-3
Advertisement
Table of Contents
