Shark 600 - Spin Recovery; Stall Recovery

FLIGHT MANUAL
SHARK 600
Section 3
Emergency
Procedures
2024-02-25
Rev. B
Doc. No.: SHARK600_MA_075
3-17
3.23 STALL RECOVERY
Simultaneously Side-stick centrally forward until buffet and
all stall indications stop
Max power
Once stall indications stop and at a safe speed
Roll wings level
Select desired flight path (climb)
NOTE
Loss of altitude after stall in straight direction is 100 ft, in turn 150 ft.
3.24 SPIN RECOVERY
If an inadvertent spin is detected (uncommanded roll and aircraft
stalled):
Immediately select IDLE power and centralise the rudder and
side-stick.
If the spin continues and below 3000 ft AGL
BRS Handle PULL
If above 3000 ft AGL
Turn indicator identify direction of turn
Rudder apply full opposite rudder
Side-stick continue to move centrally forward until
the spin stops
When the spin stops centralise controls and pull out of the dive
to desired flight path (climb) .
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