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Cessna 150M - General Description

Cessna 150M
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SECTION
1
GENERAL
DESCRIPTION
TABLE
OF
CONTENTS
GENERAL
DESCRIPTION
Model
150
and
Fl50-Series
Description
. . . . .
Model
A150
and
FAl50-Series
1-1.
GENERAL
DESCRIPTION.
1-2.
MODEL 150 AND
FI50-SERIES.
Page
1-1
1-1
1-1
1-1
1-3.
DESCRIPTION.
Cessna
Model
150
and
F150-
Series
aircraft,
described
in
this
manual,
are
high-
wing
monoplanes
of
all-metal,
semimonocoque
con-
struction.
These
aircraft
are
equipped
with
a
fixed
tricycle
landing
gear.
Through
1970
Models,
they
are
equipped
with
flat
spring-steel
main
landing
gear
struts
and
a
steerable
nose
gear.
Beginning
with
1971
Models,
these
aircraft
are
equipped
with
tubu-
lar
spring-steel
main
gear
struts
and
a
steerable
nose
gear.
The
steerable
nose
gear
is
equipped
with
an
air/hydraulic
fluid
shl
.•
strut.
Two-place
seat-
ing
is
standard,
and
a
double-width,
fold-up
auxiliary
rear
seat
may
be
installed
as
optional
equipment.
Each
Model
150 and
Fl50-Series
aircraft
is
equipped
with
a
four-cylinder,
horizontally
opposed,
air-
cooled
Continental
or
Rolls
Royce
engine,
driving
an
all-metal,
fixed-pitch
propeller.
These
aircraft
fea-
ture
a
"wrap
around"
rear
window
and
a
swept-back
fin and
rudder.
1-4.
MODEL A150
and
FAI50-SERIES.
1-5.
DESCRIPTION.
Aerobatic
Model
A150
and
F
Al50-Series
aircraft
are
a
modification
of
the
cur-
rently
produced
Model
150.
Structure
has
been
Description
. . . . .
Aircraft
SpeCifications
Stations
...
Torque
Values
. . . .
1-1
1-1
1-1
1-1
"beefed-up"
in
some
areas
in
order
to
meet
require-
ments
of
the
Acrobatic
Category,
FAR
Part
23. In
addition
to
the
"beef-up",
quick-release
cabin
doors,
two-strap
shoulder
harnesses,
and
aerobatic
paint
design
are
standard.
Only
momentary
inverted
flight
is
approved,
therefore
no
inverted
system
is
offered,
Removable
seat
and
back
cushions
are
provided
to
allow
occupants
to
use
either
a
seat-pack
or
back-
pack
type
parachute
during
aerobatic
maneuvers.
1-6.
AIRCRAFT
SPECIFICATIONS.
Leading
partic-
ulars
of
these
aircraft,
with
dimensions
based
on
gross
weight,
are
given
in
figure
1-1.
If
these
di-
mensions
are
used
for
constructing
a
hangar
or
com-
puting
clearances,
remember
that
such
factors
as
nose
gear
strut
inflation,
tire
pressures,
tire
sizes,
and
load
distribution
may
result
in
some
dimensions
that
are
considerably
different
from
those
listed.
1-7.
STATIONS.
Station
diagrams
are
shown
in
fig-
ures
1-2
and
1-3
to
assist
in
locating
equipment
when
a
written
description
is
inadequate
or
impractical.
1-8.
TORQUE VALUES. A
chart
of
recommended
nut
torque
values
is
shown
in
figure
1-4.
These
tor-
que
values
are
recommended
for
all
installation
pro-
cedures
contained
in
this
manual,
except
where
other
values
are
stipulated.
They
are
not
to
be
used
for
checking
tightness
of
installed
parts
during
service.
1-1

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