POH FK 14 B
FK Lightplanes
Revision 23
System Description
page 7-1
document code: FK 14 des.002
7.
Systems Description
7.1.
General
The FK 14 is a two-seat low wing ultralight aircraft with aerodynamic
steering. The wing has flaps which are operated electrically. The nose / tail
wheel is steered by use of the rudder pedals. The aircraft is fitted with dual
controls and can be flown from either seat.
7.2.
Instrument Panel
The instrument panel contains all required flight
and engine instruments.
Controls to operate flaps, choke, cabin heat,
carburetor heat, brakes and trim are located at the
center console.
This describes a standard equipment configuration,
different options can be provided on request.
1 Electric panel
5 Vertical speed
9 Oil pressure
2 Speed indicator
6 Altimeter
10 Oil temperature
3 Slip indicator
7 Compass
4 open
8 ULMIP / engine instruments
