EasyManua.ls Logo

Learjet 60 - Ground Idle System; Pressure System

Default Icon
408 pages
Print Icon
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
Pilot's
Manual
Learjet
60
ENG
SYNC
LIGHT
The
amber
ENG
SYNC
light
on
the
glareshield
annunciator
panel
will
be
illuminated
when
the
nose
gear
is
not
up
and
the
SYNC-OFF
switch
is
in the
SYNC
position
.
GROUND
IDLE
SYSTEM
The
ground
idle
system
provides
reduced
engine
idle
speeds
for
ground
operations
.
When
the
thrust
lever
is in
the
IDLE
detent
and
the
squat
switch
is
in
the
ground
mode,
idle
speed
is
reduced
from
approximately
65%
N2
(flight
idle)
to
approximately
52%
N2
(ground
idle)
.
In
flight,
the idle
speed
setting
is
selected
to
ensure
adequate
transient
response
to
full
takeoff
power
.
The
system
incorporates
a
10-second
delay
after
touchdown
before
ground
idle
is
activated
.
ENGINE
OIL
SYSTEM
The
engine
oil
system
provides
lubrication
and
cooling
for the
main-
shaft
bearings,
all
accessory
drive
gears
and
all
accessory
bearings
.
The
system
consists of a
pressure
system,
a
scavenge
system,
and
a
breather
system
.
PRESSURE
SYSTEM
The
oil
tank
is
an
integral
part
of the
engine
intermediate
case
.
Oil
is
drawn
from
the
tank
by
a
gear-type
pressure
pump
.
Pump
output
is
directed
through
a
pressure
adjusting
valve
which
bleeds
excess
pres-
sure
back
to
the
pump
inlet
.
From
there,
oil
passes
through
an
oil
fil-
ter
and
fuel/oil
heat
exchanger
before
being
routed
to the
mainshaft
bearings,
accessory
drive
gears,
and
accessory
bearings
.
A
cold-start
valve
diverts
oil
from
the
pump
outlet
into
the
accessory
gearbox
sump
if
pressure
exceeds
200
psi
during
cold
weather
operation
.
The
oil filter
incorporates
a
bypass
valve
allowing
oil
to
bypass
the
fil-
ter
should
it
become
clogged
.
An
impending
bypass
indicator
pro-
vides
both
a
pop-up
type
visual
indicator
and an
electrical
signal to
activate the
ENG
FILTERS
light
in
the
cockpit
.
To
avoid
false
indica-
tions
at
engine
start-up
with
cold
oil,
a
thermal
lockout
inhibits
the
impending
bypass
indication
if
oil
temperature
is
below
38°
C
(100°
F)
.
An
anti-siphon
device
is
incorporated
to
prevent
oil
from
being
si-
phoned
out
of
the
oil
tank
following
engine
shutdown
.
The
device
contains
a
small
hole
drilled
through
to
the
expansion
space
at
the top
of the
oil
tank
.
This breaks
the
siphon
action
caused
by
the
oil
tank
level
being
higher
than
the
main
bearing
oil
jets
.
2-
8
PM-123
Change
2

Table of Contents

Related product manuals