![Cessna 172R Operating Handbook Download Page 88](http://html.mh-extra.com/html/cessna/172r/172r_operating-handbook_2584466088.webp)
SECTION
3
EMERGENCY
PROCEDURES
CESSNA
MODEL 172R
RECOVERY FROM
SPIRAL
DIVE
IN
THE
CLOUDS
If
a
spiral
is
encountered in
the
clouds,
proceed
as
follows:
1
.
Retard throttle
to
idle position.
2.
Stop the
turn
by
using
coordinated aileron
and rudder control
to
align
the symbolic
airplane
in
the
turn
coordinator
with the
horizon reference
line.
3. Cautiously apply elevator back
pressure
to
slowly
reduce the
airspeed
to
80
KIAS.
4. Adjust
the elevator
trim control
to
maintain
an
80
KIAS
glide.
5. Keep
hands off the control wheel, using rudder control
to
hold
a straight heading.
6.
Clear
engine occasionally,
but avoid using
enough
power
to
disturb the trimmed
glide.
7. Upon breaking
out
of
clouds,
resume
normal cruising
flight.
INADVERTENT FLIGHT INTO ICING CONDITIONS
|
Flight
into
icing
conditions is
prohibited
and
extremely
dangerous.
An inadvertent
encounter
with these conditions
can
best
be
handled using the checklist procedures. The best procedure, of
course,
is
to turn
back or
change altitude
to
escape
icing
conditions.
During these
encounters,
an
unexplained
loss
in
engine
speed
could
be caused
by
ice blocking the air intake
filter, or, in extremely
rare
instances,
ice completely blocking the fuel injection air
reference
tubes. In either
case,
the throttle should be positioned
to
obtain
maximum RPM
(in
some
instances, the
throttle may
need
to
be
retarded
for
maximum
power).
The mixture should
then
be
adjusted, as
required,
to
obtain maximum
RPM.
STATIC SOURCE
BLOCKED
If
erroneous readings of
the static source instruments
(airspeed,
altimeter
and vertical
speed)
are
suspected, the
static pressure
lalternate
source
valve should be pulled ON, thereby supplying static
pressure
to
these
instruments
from
the cabin.
3-18
Revision 7
Summary of Contents for 172R
Page 4: ... I ...
Page 16: ......
Page 18: ......
Page 20: ... ...
Page 21: ...cr ...
Page 22: ......
Page 49: ...CESSNA MODEL 172R SECTION 1 GENERAL I Figure 1 10 Quick Conversions Revision 7 1 27 1 28 ...
Page 50: ......
Page 51: ......
Page 52: ......
Page 54: ......
Page 68: ......
Page 69: ...r r r r r r r ...
Page 70: ......
Page 96: ......
Page 97: ...f ...
Page 98: ......
Page 102: ......
Page 112: ......
Page 114: ......
Page 118: ......
Page 120: ......
Page 132: ......
Page 134: ......
Page 149: ...rcnruntnHHbc in v ...
Page 150: ... PERFORMANCE U1 ...
Page 152: ......
Page 172: ......
Page 174: ......
Page 175: ......
Page 176: ......
Page 178: ......
Page 184: ......
Page 186: ...y ...
Page 188: ... ...
Page 192: ... I 1 ...
Page 194: ......
Page 196: ...tv ...
Page 215: ......
Page 216: ......
Page 220: ......
Page 224: ...SECTION 7 AIRPLANE SYSTEMS DESCRIPTION CESSNA MODEL 172R ELEVATOR TRIM 7 8 Dec 2 96 ...
Page 226: ...SECTION 7 AIRPLANE SYSTEMS DESCRIPTION CESSNA MODEL 172R 7 10 Revision 7 ...
Page 244: ......
Page 271: ......
Page 272: ......
Page 297: ......
Page 298: ......
Page 300: ......
Page 302: ......
Page 304: ......
Page 306: ......
Page 308: ......
Page 310: ......
Page 312: ......
Page 314: ......
Page 316: ......
Page 318: ...V J ...
Page 320: ......
Page 322: ......
Page 324: ......
Page 326: ......
Page 328: ......
Page 330: ......
Page 332: ......
Page 334: ......
Page 336: ......
Page 338: ... ...
Page 342: ......
Page 344: ......
Page 360: ......
Page 370: ......
Page 380: ...r ...
Page 396: ......
Page 430: ......
Page 500: ... i i I y r ...