BEECHCRAFT
Duchess
76
section
VII
Systems
Description
priming, starting, taxiing, takeoff, and landing. Also, the auxil-
iary fuel pump provides sufficient pressure for continued
engine operation in case the engine-driven fuel pump be-
comes inoperative.
ENGINE PRIMING
Each engine is equipped with a
three+p6ifif
i
(nO:,T,2.;iand4
'
(cylinders
))juelptlID)J!I!gzj~ystertl.Hhe
magneto/start switches
incorporate a PUSH
TO
PRIME function to aid
in
engine
starting. The BATTERY MASTER and the
AUX
FUEL PUMP
(L or R) switches
must
be
turned on prior to activating
the
fuel
priming system.
The
PUSH TO PRIME switch may
be
ac-
tuated in either the
BOTH
or
START position.
By.~12iLlgli!liQni
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.~Q~;nIi~~gU;lilil.e.g~j;:ldngg~lJ§jlgliJ~'!~MRRli!~§i:tl,l,~.!;,gireGtIYiintb·.the
no:.J;'(2(J~lJg;4.GyllDQe[slJQrj;engine:;.primingfwEngine
priming
should be used in accordance with the recommendations in
the
NORMAL
PROCEDURES
section.
FUEL CROSSFEED
The
fuel lines for
the
engines are interconnected by cross-.
feed lines. During normal operation each engine uses its own
fuel pumps to draw fuel from its respective wing fuel system.
However, on emergency crossfeed operations, either engine
can consume all
the
available fuel from the opposite side.
The
fuel crossfeed system is provided for use during level
flight, emergency conditions only.
The
system cannot trans-
fer fuel from one
wing
system to the other. The procedure for
using the crossfeed system is
described
in
the
EMER-
GENCY
PROCEDURES section.
FUEL REQUIRED
FOR
FLIGHT
Flight planning and fuel loading are facilitated by the use of
fuel quantity indicators that have been coordinated with the
usable fuel supply. It is
the
pilot's responsibility to ascertain
April
1979
7-25