Skyranger - The Story so far!

The Skyranger was created in Toulouse, the capital of the French aviation industry by Phillippe Prevot and BestOff engineering. Phillippe was well known as an innovator in flexwing microlight design, and he designed the first Skyranger in 1991, with first flights of the prototype in 1992.

The design brief was to produce a high performance fixeding aircraft of conventional layout which would conform to the Microlight category definition, with good creature comforts, whilst doing so with the simplest possible construction, in order to create a machine with good affordability, and suited to amateur construction, and ease of maintenance.

During the design and development phase, Phillippe partnered with with one of the most respected aeronautical colleges. ENSICA, under the direction of Jean Poulain. This partnership enabled detailed professional studies to be made of structural elements and optimisation of flight performance.

Initially  the production was in France, where the first 200 kits were manufactured, between 1993 and 1998. Following this, manufacture of the main structure was subcontracted  to Aeros, in Kiev Ukraine. At the same time the design was reviewed and updated with several improvements. Aeros is a well respected company primarily known for their Hang glider production, where they are class leaders with several world championship wins to their credit. Formed during the decline of the Former Soviet Union, most of the staff are highly trained aviation engineers, formerly working in the Kiev Antonov aircraft factory.

Since then over a further 1300 Skyranger series aircraft have been produced, bring total production to over 1500. The Skyranger proving extremely popular in Europe, USA, South America, Australia, and many other parts of the globe.

The UK connection is provided by Flylight Airsports Ltd, who recognised the potential market for the Skyranger in the UK. In partnership with BestOff, Flylight put the Skyranger through the tough UK certification system, and several changes and improvements were incorporated during the process. The first kits were delivered to UK customers in 2003. The Skyranger was extremely well received in the UK, rapidly becoming a best seller, and now has the prestige of being the most numerous three axis microlight type on the UK register.

The first variant in the UK was the Skyranger ‘classic’, initially certified with the Rotax 912 80hp engine option. The range of approved engines was then expanded to include the 65hp Rotax 582 two stroke, 85hp jabiru2200, and the 100hp Rotax 912ULS.

This was followed by the introduction of the Skyranger Swift model. The Swift shares the same fuselage design with the Skyranger classic, but features a shorter wingspan. This takes advantage of the 80hp and up engine options, and delivers higher cruise speeds. at the same time as the introduction of the Swift, several other improvements were introduced to the range, including the more durable Xlam covering option, and upgraded interior options.

Then came the  Skyranger Nynja. The Nynja shares the same wing frame with the Swift, but features a redesigned fuselage structure, with full composite panels to form the exterior, giving enhanced aesthetics, and reducing drag. As befits the top of the range machine it also has several other enhancements as standard equipment.

After this the Swift was re visited, to incorporate some of the features and development work learned with the Nynja project, and named Swift2. The Swift 2 is distinguished form the earlier model with a new vertical tail shape, doors, instrument panel, exhaust system and undercarriage shared with the Nynja. The cowlings have been facelifted too. The result is a lighter structure, enhanced visibility and better looks, whilst retaining its unbeatable low entry price.

The Swift2 and Nynja now form the current range with standard engine options rationalised to the Rotax 912UL (80hp) and 912ULS (100hp).

Not confined to operation within the Microlight category both Nynja and Swift 2 have LS varients with small detail changes that allow them to be operated in the light aircraft category with increased maximum takeoff weights and load carrying capability.