Grob G 103 TWIN II User Manual

FLIGHT MANUAL GROB G 103 27
The temporary control force to overcome the
force reversal or rudder lock
is calculated
approximately
5 to 6 daN (rudder pressure).
The aileron does not change its force direc-
tion, rather it returns independently from the
full deflected position.
Rudder lock can be relieved without pilot in-
puton the rudder. After moving the aileron
into neutral position, the Sailplane
rolldhut
of the Slip into wing level position. There-
after the rudder frees itself from the full
deflected position and the force reversal is
relieved. Using this method to end the
Slip
the Sailplane does not adopt unusual flight
attitudes and deviates only slightly from its
h. -
+..
i
original flight course.
IV. 10 Storage
When the glider is stored the canopy should
be locked. To
tPe down the wing, a rope can
be pulled through the wing tip skids.
17 th march 1982.

Grob G 103 TWIN II Specifications

General

Manufacturer	Grob Aircraft
First flight	1976
Crew	2
Gross weight	580 kg (1, 279 lb)
Max. takeoff weight	580 kg (1, 279 lb)
Maximum glide ratio	38:1
Type	Sailplane
Role	Sailplane
Maximum speed	250 km/h
Stall speed	65 km/h