Download Assembly and Operating Instructions Lifting, rolling and

C.4.1Loading
Before rolling up to the aircraft ramp, on the side facing the aircraft it is necessary to remove
the rack extension according to the aircraft type (see B 1.2 + picture page 36). The cabin is
now pushed via the two-wheel caster assembly until it is close to the aircraft ramp.
Fitting:
B.4 Basic structure – loading via the horizontal ramp
B.4.1 Fitting the two-wheel caster assembly and the steering rod.
When pushing the cabin into position, the sets of wheels (10) on the side facing away from the
two-wheel caster assembly can be blocked to prevent rotation. If positional correction of the
cabin is required, the connected sets of wheels (10) can be steered via the steering lever (21)
and the steering rod (22). ⇒ Page 35.
Attention:
Risk of collision between operator and material in the vicinity of the aircraft ramp.
The cabin is pushed up to about 100 mm away from the ramp end. The brakes are released on
all sets of wheels (10). Brake function not active. The sets of wheels (10) in the vicinity of the
aircraft ramp are blocked to prevent rotation. The connecting shafts (14 / 15) and crankcase
(12) are fitted.
 With the crankcase (12), raise the cabin until the aircraft ramp can be safely rolled over.
The cabin can be rolled further across the ramp manually.
Alternatively, the aircraft’s cable winch can be used to secure the deflection roller with the
cable to the bar (7 / 8).
Attention:
 Roll in slowly.
 The roll-in distance up until the corner units near to the aircraft are removed is very short.
 During rolling-in, the booms (2) enter the angular opening between the bottom of the ramp
and the aircraft’s fuselage profile ⇒ Page 36
a
b
c
a = steering rod; b = aircraft ramp; c = roller way
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