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Cessna 1971 Super Skymaster - Page 15

Cessna 1971 Super Skymaster
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PROPELLER
SYNCHROSCOPE.
An
electrically-operated
synchroscope
is
installed
to allow
more
accurate
propeller
synchronization.
The
synchroscope,
located
on the
left
upper
portion
of the
instrument
panel
provides
a
visual
indicator
for
synchronization.
The
system
utilizes
a
transmitter
electrically
connect-
ed
in
parallel
with
the
dual engine
tachometers,
and
electrical
pick-up
coils
mounted on
the
right
magneto of
each
engine. The individual
signals
on
each
magneto
are
compared
in the
synchroscope
transmitter
and
their
variation
in
electrical
phase
is
displayed
by
the
sweeping
pointer
on the
synchroscope.
A
large
variation
in
electrical
phase
(caused
by
RPM
differential
between engines)
causes
a
rapid
oscillation
of the
pointer.
As
the RPM of the engines
are
more
closely
adjusted,
pointer
oscillation
will
slow until finally, with
properly
synchronized
engines, pOinter motion
is
minimal.
When synchronizing engine RPM,
either
engine RPM may be
established
as
a
"master,
" and the
other
engine
synchronized
to
match
it.
WING
FLAP
SYSTEM.
Wing flap
settings
are
accomplished
in one Simple up
or
down
move-
ment
of
the wing flap
control
knob to the flap
setting
deSired. To extend
the wing
flaps
from
"UP"
to
"1/3"
down
(normal
take-off
range),
merely
push the
control
knob down until
it
hits
the
mechanical
stop.
For
flap
settings
greater
than"
1/3"
down, move the
control
knob to the
right
to
clear
the stop, and position it
as
desired.
To
retract
the flaps, Simply
raise
the
control
knob to the
setting
deSired,
Flap
positiOns
are
identi-
fied
as
"UP,
"
"1/3,
"
"2/3"
and
"FULL.
" The
"FULL"
flap position
is
25
degrees.
flaps
are
retracted,
the
interconnect
will
automatically
rotate
the
trim
wheel
back
to the
"TAKE-OFF"
range.
COWL
FLAP
SYSTEM.
Two
three-pOSition toggle
switches
located
on
the
left
switch
and con-
trol
panel
near
the landing
gear
handle
operate
the
front
and
rear
engine
cowl
flaps.
The
switches
are
labeled "COWL FLAPS,
ff
ilFRONT" and
"REAR, " and
their
pOSitions
are
labeled
"OPEN" (up),
"OFF"
(center)
and "CLOSE" (down).
Two
blue
indicator
lights, one located
beside
each
switch,
illuminate
when the cowl flaps have
reached
either
the
full open
or
full
closed
position
and
remain
lighted until the
switches
are
placed
in
,
the
"OFF"
pOSition. The
indicator
lights
also
incorporate
dimming
1['
.
shutters
for
night
operation.
I"
Ii
To fully open
or
close
the cowl flaps,
place
the cowl flap
switches
in
;1
j
either
the
"OPEN"
or
"CLOSE" position. When the opening
or
closing
operation
is
completed
(approximately two seconds) the blue
indicator
lights
will
illuminate.
If
intermediate
positioning of the cowl
flaps
is
re-
quired,
for
example half open,
actuate
the
switches
for
approximately
one
second
and
return
them to the
"OFF"
position.
Other
settings
can
be
ap-
proximated
in a
similar
manner.
Proper
cowl flap
settings
should be
de-
termined
by
carefully
monitoring the
cylinder
head
temperature
gages.
LANDING
GEAR
SYSTEM.
WING
FLAP-ELEVATOR
TAB
INTERCONNECT
SYSTEM.
The wing flap
system
is
mechanically
interconnected
with the
elevator
trim
tab
system
to
automatically
eliminate
excessive
nose-up
trim
while
the wing
flaps
are
being
retracted.
With the
flaps
retracted,
the
trim
control
wheel
can
be
rotated
in one
direction
until the
trim
position
indicator
reaches
the "NOSE DN" position,
or
In the opposite
direction
until
it
reaches
the lower half of the "TAKE-
OIrF"
range
marking
for
nose-up
trim.
As the flaps
are
extended,
addi-
tional
nose-up
trim
beyond the
"TAKE-OFF"
range
can
be
utilized.
Maxi-
mum
nose-up
trim
is
available when the
flaps
are
fully extended.
As
the
The
retractable
tricycle
landing
gear
is
extended and
retracted
by
hydraulic
actuators,
powered by
an
engine-driven
hydraulic pump on the
front
engine. An optional
engine-driven
hydraulic
pump
is
offered
for
the
rear
engine to provide
decreased
gear
operation
time
and dual pump
safety.
Two pOSition
indicator
lights
show
that
the
gear
is
either
up
or
down
and
locked. The
lights
are
"press-to-test"
type. The
gear-down
indica-
tor
llght
(green)
has
two
test
positions; with the
light
pushed
in
half-way
and
either
throttle
retarded,
the
gear
warning
horn
should sound, and
with
the
light
pushed full in,
the
light should
illuminate.
The
gear-up
indicator
light
(amber)
has
only one
test
poSition; with the
light
pushed
2-13
d
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2-12