SECTION 3
EMERGENCY
PROCEDLIRES
CESSNA
MODEL 182T NAV I I I
STATIC SOURCE BLOCKED
If erroneous readings of the static source instruments (airspeed,
I
altimeter and vertical speed) are suspected, the ALT STATIC AIR
valve should be pulled ON, thereby supplying static pressure to
these instruments from the cabin.
When the ALT STATIC AIR valve is ON, the maximum airspeed
variation from normal static source operation is
5
knots and the
maximum altimeter variation is 80 feet (all windows closed). Refer
to Section
5,
Airspeed Calibration and Altimeter Correction tables
for Alternate Static Source for additional details.
Intentional spins are prohibited in this airplane, but 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
1
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 RLIDDER,
AhlD MAKE
A SMOOTH RECOVERY FROM THE RESULTING DIVE.
NOTE
If the rate of the spin makes determining the
direction of rotation difficult, the magenta turn rate
indicator at the top of the HSI compass card will
show the rate and direction of the turn. The HSI
compass card will rotate in the opposite direction.
Hold opposite rudder to the turn vector direction.
3-30 U.S.
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