15
Version 1.0 March 2017
5 Recovery Techniques
The normal method is to simply initiate a mild turn. As the canopy starts to turn it will automatically change to normal
flight, but it is very important not to turn too fast as this could induce a spin.
The second method is to pull gently on the A-risers. This helps the airflow to re-attach to the leading edge, but be
careful not to pull down too hard as this will induce a front collapse.
If the deep stall is particularly stubborn and the previous methods do not work then a full stall will solve the problem.
To do this apply both brakes again fairly quickly, as if to do a strong stall, then immediately release both brakes and
damp out the surge forward in the normal way. The canopy will swing behind you then automatically reinflate and surge
forward in front of you before returning to normal flight. It is the surge forward that exits the canopy from deep stall.
Spins
Spins are dangerous and should not be practised in the course of normal flying. Spins occur when the pilot tries to
turn too fast. In a spin the pilot, lines and canopy basically stay vertical and rotate around a vertical axis. The BASE
LITE will resist spinning, but if a spin is inadvertently induced the pilot should release the brake pressure but always
be ready to damp out any dive as the glider exits the spin. If the pilot does not damp the dive on exiting the spin the
glider may have an asymmetric deflation.
Symmetric Front Collapse
It is possible that turbulence can cause the front of the wing to symmetrically collapse, though active piloting can
largely prevent this from occurring accidentally. A pilot can reproduce the effect by taking hold of both the A-risers
and pulling down sharply on them. The BASE LITE will automatically recover on its own from this situation in around
3 seconds. During this recovery period it is advisable not to apply the brakes as this could stall the wing.