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“Cravat” / Line-over:
In the event of some lines becoming tangled during flight (caused by whatever),
the following action is recommended:
Stabilize the glider by gently applying the opposite brake. Please be aware that in this
condition the brake pressure can be higher and the brake travel shorter.
Without pilot input, a line-over will result in a stable spiral dive.
Here are the various options to untangle a line-over:
- pumping the collapsed side.
-pulling the stabilizer line or a sharp pull on the D riser can sometimes solve the problem.
Attention!
If these manoeuvres fail or if in any doubt, the pilot should instantly use their
emergency reserve parachute system!
Frontal Collapse:
Frontal collapses provoked at higher speeds can lead to extremely deep collapses.
Recovery requires short and equal application of both brakes. When experiencing a very
large front tuck, a frontal rosette can occur (the wingtips move forwards: forming a
horseshoe shape). Short and gentle braking can avoid this.
A quick recognition of the situation and a quick reaction by braking on both sides helps the
recovery and limits the altitude loss.
Parachutal stall (deep stall):
A parachutal stall can be caused by having the glider fly too slowly. The most common
cause is from pulling too much brake, however, porous canopies (UV influence) or
canopies out of trim (stretched or shrunken lines) are much moresusceptible to a
parachutal stall. Gliders in poor condition should not be flown. This is the reason why
regular checks should be carried out on your glider. A wet canopy or temperatures below
zero centigrade (0°C) may also cause a stable parachutal stall.
When releasing the brakes
the Charger 2 will spontaneously recover from a parachutal stall within 2-3 seconds. If the
canopy remains in a parachutal stall, it is sufficient to release trims or to push the
accelerator.
Attention! If brakes are applied while in a parachutal stall, the glider may suddenly
enter a full stall!
Summary of Contents for Charger2
Page 1: ...1 Ze S a m u r a i...
Page 10: ...10 TRIMMING...
Page 35: ...35 LINE PLAN SCHEME...
Page 38: ...38 CHECKS Name Company Date Signature Stamp...
Page 40: ...40...