POH FK 14 B
FK Lightplanes
Revision 23
System Description
page 7-2
document code: FK 14 des.002
7.3.
Rescue system
The rescue system of the FK 14 is installed in front of the instrument panel
on the left side. Detailed information concerning max. speed, capacity and
maintenance cycles are provided in the respective rescue system manual.
The system is activated by pulling the red handle in front of the pilot below
the instrument panel.
The safety pin
must
be removed before flight.
The
safety pin should be installed again during storage / parking of the aircraft to
avoid inadvertent activation.
The length of the main harness in
relation to the balance harness is
calculated to result in a nose-
down attitude of 15 to 20°.
Observe installation advice of
BRS!
The balance harness is installed
in a duct along the fuselage to the
aft airframe connection.
It is protected by a foil, is
maintenance-free and cannot be
exchanged.
