SA 160
AIRCRAFTA I R C R A F T
Symphony
AIRCRAFT
SECTION 3
EMERGENCY PROCEDURES
(q) Spin Recovery Procedure
1. Throttle ..........................................................................................IDLE
2. Ailerons ................................................................................NEUTRAL
3. Rudder ..........FULL OPPOSITE TO DIRECTION OF ROTATION
At the same time
4. Elevator ................................................................................NEUTRAL
5. Rudder (when rotation stops) ..........................................NEUTRAL
As rotation stops make a smooth recovery from the dive. If flaps
were extended, retract and establish horizontal flight with engine
powerasrequired.
3-10
Icing has a very strong negative effect on the aerodynamic
characteristicsoftheaircraft. Stalling speed increases.
Continuedflightinicingconditionsisprohibited.
1. Pitot Heat Switch.............................................................................ON
2. Carburetor Heat...............................................................................ON
3.
4. Wind shield Heat
With an ice accumulation of 5mm ore more on the wing leading
edges, perform landing with flaps retracted or in 20° position.
Airspeed in final approach must be higher corresponding the ice
accumulationandtheflapposition.
Cabin Heat / Ventilation.................................................................ON
Land at the nearest airfield.
.............................................................................ON
(p) Static Source Blockage (IFR)
1. Alternate Static Source ....................................................................OPEN
2. Airspeed .........................................................................................ADJUST
According to the Airspeed Calibration
(Alternate Static Source) table in Section 5. P.5.11
WARNING !
Feb 25, 2005