Cessna 172R, Руководство по эксплуатации

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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