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19
Hoffmann
3
H 36 DIMONA
Emergency Procedures
3.1
Stalls, Power On:
On coming stall warning can be recognized by buffeting on the aircraft and a loss of positive control in
the stick and pedals. If permitted to continue, the aircraft will stall and roll over on the stalled wing. A
spin may result. When buffeting is encountered relax back pressure on the stick, and if available, add
power. Recovery from a clean stall will result in an altitude loss of about 40 meters (130 ft)
3.2
Stalls, Power Off, Prop Feathered:
On coming stall warning is buffeting as with power on, however, the aircraft will not roll on a wing and
can be held level with aileron and rudder control. The aircraft will sink vertically at a rate of 700 fpm.
Stall recovery in this mode is to relax back pressure on the stick.
3.3
Spin Recovery:
Reduce power and push control stick full forward. Apply fu11 rudder opposite to spin rotation. Recover
smoothly from the dive.
CAUTION
The aerodynamic clean form or the DIMONA permits speed to build up rapidly. Vne must not be
exceeded. Immediate spin recovery will result in an altitude loss of 280 ft.
C A U T I 0 N
if, under unfavorable circumstances with engine idle a flat spin will result, recover immediately as
above but add power.
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