POH FK 14 B
FK Lightplanes
Revision 23
System Description
page 7-3
document code: FK 14 des.002
The main harnesses are con-
nected to the fuselage tubes and
are installed on top of the tubes to
allow undisturbed unfolding.
The softpack container is con-
nected to the aircraft frame. The
connection must withstand a load
of at least 75 kp!
The installation of the rocket can
be seen on the picture. The
activating housing must not be
stretched, coiled or crimped! The
rocket must hit the roof of the
fuselage within the cap area
when fired.
