B&F Fk14 Polaris

Fk14 Polaris
Role Two seat sports ultralight
National origin Germany
Manufacturer B&F Technik Vertrieb gmbh, Speyer
First flight May 1999
Status In production
Number built 90 by September 2008

The B&F Fk14 Polaris is a single engine, low wing ultralight aircraft which seats two side-by side. Designed in Germany in the late 1990s, it remains in production.

Contents

Design and development

Design of the B&F Fk14 Polaris, sometimes known as the Funk Fk 14 Polaris but not by its makers,[1] began in 1998. It first flew in May 1999 and started in production the next year. It is a low wing, single engine ultralight, with enclosed accommodation for two. seated side-by side. Its largely glass fibre (carbon on the Fk14B variant) wing is mostly of parallel chord but toward the tips, where short span aluminium ailerons occupy the trailing edges, the leading edge is swept. Electrically operated Fowler flaps are fitted. Four flap settings are available: +0°, +10°, +20° and +32°. The wingtips incorporate short winglets. The fin and rudder are gently swept; the rudder is deep, reaching the lower fuselage line and moving in a cut-out between the elevators. These rear flying surfaces are mass balanced. The Polaris has spring trimmed controls.[2]

Until 2007 B&F offered a choice of steel framed or monocoque fuselage structures, but since then have only produced the latter. The occupants sit side-by-side under a single piece, forward hinged canopy. The standard undercarriage is of tricycle configuration, though a conventional undercarriage is an option. The main legs are fuselage mounted spring cantilevers and the nosewheel is steerable. All wheels are spatted. The Polaris may be fitted with a ballistic parachute (BRS 5) as an option.[2]

There is a choice between two of the Rotax 912 series flat four cylinder engines: either the 60 kW (80 hp) 912 UL or the 74 kW (99 hp) 912 ULS may be fitted. These drive 3 blade, ground adjustable pitch propellers.[2]

Operational history

The 90th Polaris was completed in September 2008. In mid-2010, the European registers (excluding Russia) listed 72 aircraft.[3]

Variants

Fk14
Standard version.
Fk14B
Introduced about 2003, with new carbon fibre wing, greater range, improved access with greater canopy opening angle; baggage space behind seats; altered engine cowling.
Cirrus SRS
Under development by Cirrus Design Co. in the US, this meets local LSA rules: test bed has flown.

Specifications (Rotax 912ULS)

Data from Jane's All the World's Aircraft 2010/11[2]

General characteristics

Performance

References

  1. ^ "Fk lightplanes - History". http://www.fk-lightplanes.com/html/fk_history.html. Retrieved 2011-01-09. 
  2. ^ a b c d Jackson, Paul (2010). Jane's All the World's Aircraft 2010-11. Coulsdon, Surrey: IHS Jane's. pp. 228. ISBN 9780 7106 2916 6. 
  3. ^ Partington, Dave (2010). European registers handbook 2010. Air Britain (Historians) Ltd. ISBN 9780 85130 425 0. 

External links

Official website