SFC Cessna 182Q - POST LOSS of CONTROL Procedure; SPIN RECOVERY Procedure

CESSNA 182Q QRH
Page 31 of 33
C182Q QRH JAN 2022
3. Cabin Vents …………………………………………………………………………….. OPEN
4. Cabin Windows ……………………………………………….……………………. OPEN
If CO LVL HIGH annunciator remains on, land as soon as practicable.
SPIN RECOVERY Procedure
1. Throttle …….………………………..…………………………………………………….. IDLE
2. Ailerons ……………………………….……………………………………………. NEUTRAL
3. Rudder .…Apply and HOLD OPPOSITE to the DIRECTION OF
ROTATION
Just after the rudder reaches the stop
4. Elevator ………….…… BRISKLY FORWARD far enough to break the stall
full down elevator may be required at aft centre
of gravity loadings to assure optimum recoveries
5. Hold Control Inputs ……………………….…………… UNTIL ROTATION STOPS
premature relaxation of
the control inputs may
extend the recovery
6. As rotation stops ………………….…………………..…… NEUTRALIZE RUDDER
7. Dive ………………………….… SMOOTH RECOVERY from the resulting dive
EXECUTE POST LOSS OF CONTROL PROCEDURE
POST LOSS OF CONTROL procedure
1. Wing Flaps ………………….... CONFIRM UP / RETRACTED & NO DAMAGE
2. Overspeed ……………………………………………………………………. DETERMINE
3. Overstress ……………………………………………………………………. DETERMINE
4. If No Damage …………………….…… COMPLETE AFTER TAKE OFF CHECKS
5. Reason For Loss Of Control ………………………………….…….. DETERMINED
6. Orientation …………………… ALTITUDE, POSITION & HEADING CHECKED