FLIGHT MANUAL ASTIR CS
Rev. 9 28. Nov. 2005
6
Classification Group
Standard Class (German N)
Centre of Gravity positions
Leveling
means
with
a
1000:40
Incidence
Board
set up horizontal on the
top of
the rear fuselage.
Datum Line (D, L.)
Front edge) of wing at root
Serial-No. 1002 – 1437:
Maximum forward position of C. of G. 250
mm
behind
D. L. (9.84 in)
Maximum rearward position
425 mm behind D. L. (16.73 in)
Serial–No. 1438 – 1536:
Maximum forward position of C. of G. 310 mm behind D. L. (12,20 in)
Maximum rearward position
480 mm behind D. L. (18,90 in)
Loading Limitations ASTIR CS
Empty weight of glider and maximum cockpit load, see page 7.
Minimum cockpit load: 154 lbs (70 kp)
The permissible all up weight must NEVER be exceeded.
Maximum all up weight
without water-ballast
836 lbs
(380 kp)
with water-ballast 990
lbs
(450 kp)
The weight of water-ballast is dependent on the cockpit weight (Pilot
with parachute and luggage). See page 7.
Weight deficiencies should be corrected by securing or removing some
ballast in the seat.
The C. of G. of the pilot with a parachute on lies 475 mm in front of
the Datum Line.
Summary of Contents for Astir CS G102
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