DG Flugzeugbau DG-800A, Руководство по обслуживанию, Страница: 14 / 163

Maintenance Manual DG-808C
Issued: June 2005 1.1
1 System description and adjustment data
1.1 Wing and tailplane setting data
Wing:
Sweep back (Leading edge): 0 + 3 mm (+ 0.12 in.) at wing taper change
Dihedral (Leading edge line): 2.5° = 196 mm (7.72 in.) at wing taper
change (y = 4.5 m)
Angles of Incidence: -1° measured at wing flap setting -5°
Horizontal tailplane:
Angles of Incidence -3,5°
chord lines
fuselage centre line
(corresponding to boom slope 1000:37)
Wing oscillation
frequency:
approx. 160/min 15 m span with winglets
approx. 130/min 18 m span without parting
approx. 124/min 18 m span with parting and
winglets
Aircraft should rest on both wheels during frequency measurements.
1°
3,5°