SCHEMPP-HIRTH FLUGZEUGBAU GmbH, KIRCHHEIM/TECK
Ventus-3M „Performance“
FLIGHT MANUAL
March 2019
CS 22
Revision –
4.3.1.6
o
Check the correct installation of the battery in the fin according to the
loading chart.
o
Check the horizontal tailplane for correct installation.
o
Check elevator and rudder for free movement.
o
Check trailing edge of the elevator and rudder for damage.
o
Check elevator and rudder for unusual play by gently shaking the trailing
edge.
o
See
o
See
o
Check that the pitot pressure probe in the fuselage nose is clear. When
blowing carefully into the pitot pressure probe, the airspeed indicator must
register.
Inspection after hard landings:
After heavy landings or after the aircraft has been subjected to excessive loads,
the resonant wing vibration frequency should be checked
(its value is to be extracted from the last inspection report for this serial number).
Check the entire aircraft thoroughly for surface cracks and other damage. For this
purpose, it should be de-rigged.
After a ground loop, especially the rear part of the fuselage tube and the transition
to the vertical tail has to be checked for damage and detached bulkheads.
To do so, support the wings of the rigged glider (without horizontal tail) and apply
hand force to the side at the bracket for the horizontal tail. Check the fuselage
structure for excessive deformation, buckling and crackling noise.
If damage is discovered (i.e. surface cracks in the fuselage tail boom or tailplane,
or if delamination is found at the wing roots or at the bearings in the root ribs etc.),
then the aircraft must be grounded until the damage has been judged respectively
repaired by a qualified person.
This inspection must also include a complete check of the power plant system.
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Содержание Ventus-3M Performance
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