Textron Cessna 172R User Manual

CESSNA
MODEL
172R
SECTION
3
EMERGENCY
PROCEDURES
When
using
the alternate static
source,
refer
to
the Alternate
Stat¬
ic
Source
Airspeed
Calibration
table
in
Section
5,
Performance,
for
additional
information.
Maximum
airspeed
and
altimeter variation
from
normal is
4
knots
and
30
feet
over
the normal
operating
range
with
the
window(s)
I
closed.
See
Section
5,
Performance,
for
additional
airspeed
calibration
data.
SPINS
Should
an
inadvertent
spin
occur,
the
following
recovery
procedure
should be used:
1.
RETARD
THROTTLE
TO
IDLE
POSITION.
2.
PLACE
AILERONS
IN
NEUTRAL
POSITION.
3.
APPLY
AND
HOLD
FULL
RUDDER
OPPOSITE
TO
THE
DIRECTION
OF
ROTATION.
4.
JUST
AFTER
THE
RUDDER
REACHES
THE
STOP,
MOVE
THE
CONTROL
WHEEL
BRISKLY
FORWARD
FAR
ENOUGH
TO
BREAK
THE
STALL.
Full down
elevator
may
be
required
at
aft
center
of
gravity
loadings
to
assure
optimum
recoveries.
5.
HOLD
THESE
CONTROL
INPUTS
UNTIL
ROTATION
STOPS.
Premature
relaxation
of
the
control
inputs
may
extend
the
recovery.
6.
AS
ROTATION
STOPS,
NEUTRALIZE
RUDDER,
AND
MAKE
A
SMOOTH
RECOVERY
FROM
THE
RESULTING
DIVE.
NOTE
If
disorientation
precludes
a
visual
determination
of
the
direction
of
rotation,
the
symbolic
airplane
in
the
turn
coordinator
may
be
referred
to
for
this
information.
For
additional
information
on
spins
and
spin
recovery,
see
the
discussion
under
SPINS
in
Normal
Procedures
(Section
4).
Revision
7
3-19
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Textron Cessna 172R Specifications

General

Brand	Textron
Model	Cessna 172R
Category	Aircrafts
Language	English