Aircrafts

Kama Hydro FP 6 amphibious aircraft

The Hydran aircraft was constructed in 1988 by the well-known designer Fabrizio Pisani (P92 echo) initially powered by a Rotax 80 HP and 100 HP. In 1998, together with the constructor, we began the modernisation of the aircraft, which included changing: the power unit to a Rotax 912 IS engine, the fuel system, the avionics, the shape of the boat’s hull, and the selection of a variable pitch propeller to match the engine parameters. The purpose of these changes was to adapt the aircraft for certification according to JAR-VLA, LSA, UL regulations. An important change was the adaptation of the aircraft for firefighting purposes. The aircraft can draw water during take-off from the water. The aircraft’s design is laminates based on resins, glass and carbon fabrics. The attachment nodes for the landing gear engine, wing struts are of metal construction. The aircraft can be powered by a Rotax 912IS engine working with a three-blade Porchellinni variable pitch propeller with reverse thrust. The high-mounted wings and tail with no side floats on the wings provide very good manoeuvrability and piloting qualities – this version of the aircraft is called KAMA-hydro FP6. Based on our experience, we are currently preparing an 8-person multi-purpose hybrid amphibious aircraft with an innovative system to assist take-off from and manoeuvre on water. The aircraft will be equipped with folding wings and will be designed for firefighting, rescue operations, water monitoring and long-distance tourism.

Landing gear of the cabin

The aircraft is equipped with retractable landing gear. Transparent viewfinders inside the cabin allow a visual indication of the position of the landing gear. The main landing gear wheels are fitted with disc brakes. The front wheel is steerable. The generously glazed 124 cm-wide two-person cabin with side-by-side seating provides comfort and very good visibility. The cabin is equipped with: heating, a luggage compartment behind the adjustable crew seats and dual controls. Avionics is a combination of analogue instrumentation with navigation display, piloting and engine control.
Cabin width 120cm.

Performance with 912IS engine

Maximum speed:
185km/h
Cruising speed:
170km/h
Minimum speed on flaps:
65km/h
Permissible speed:
210km/h
Range:
800km
Practical ceiling:
3,500m
Average fuel consumption:
8-12l/h
Length of take-off from land:
150m
Length of take-off from water:
200m
Landing run:
100m
Take-off over 15 m obstacle:
200m
Climb:
5.5m/s

Weight of KAMA HYDRO FP6

Empty aircraft weight:  350kg
Take-off weight: 500kg-620kg
Maximum permissible load: -3 +7G
Luggage weight: 35-100kg

Aircraft dimensions

Wingspan: 9,22m
Length: 6,30m
Height: 2,90m
Carrier surface: 12,6m2

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