2 - Schempp-Hirth

SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK
Ventus-2a MAINTENANCE MANUAL
Ventus-2b
15.0 m [ 49.21 ft ]
3°
TAILPLANE INCIDENCE
-2.5°
2.3 m [ 7.55 ft ]
ELEVATOR
+3 mm
2 mm
+0.12 in. ]
0.08 in. ]
44
0.23°
Up or down
[ 1.73
323 mm [ 12.72 in. ]
138 mm
[ 5.43 in. ]
Ventus-2a - 6.41 m [ 21.03 ft ]
RUDDER
To either side: 155 ± 15 mm [ 6.10 ± 0.59 in. ]
AILERONS (flaps set at "0")
33 ± 3 mm
Up
[ 1.30 ± 0.12 in. ]
25 ± 3 mm
Down
[ 0.98 ± 0.12 in. ]
126 mm
[ 4.96 in. ]
325 ± 25 mm
[ 12.80 ± 0.98 in. ]
30 ± 2 mm
[ 1.18 ± 0.08 in. ]
0 ± 2 mm
[ 0 ± 0.08 in. ]
22 ± 2 mm
[ 0.87 ± 0.08 in. ]
FLAPS
set at "S1" (up)
set at "0" (neutral)
Sailplane attitude for all measurements:
Tail jacked up such that a wedge-shaped block,
100 : 3.125, placed on the rear top fuselage, is
horizontal along its upper edge.
set at "L" (down)
RIGGING DATA AND CONTROL SURFACE DEFLECTIONS
January 2003
Revision 11 TN-No. 349-27 2.1.2