Rally 

With the Rally, the sky is yours. It’s developed in order to ensure sustainable safety and stability through high wing structure. Its main assets are a fuel-efficient autotechnologies, unequalled reliability and performance. Conceived and designed for aviation enthusiasts, aero-clubs, flight training, monitoring and lifting activities, aerial agricultural spraying, towing advertising banners and recreation scenic flight

You’ll be pleasantly surprised by its high maintainability and low operating cost

Technology :

A structural basis of carbon fiber which gives the lightness and strength make it one of the most attractive in its category

Wing profiles have been especially conceived to generate additional lift for pilot to stabilize and maintain the hover. Special winglets are a trademark of our wing, serve in reducing induced drag. The aerodynamic behavior of the Rally guarantees his superiority during all phases of flight

Interior design :

Make yourself comfortable, the two seater cabin combines unrivalled interior space with modern styling distinguished by an ergonomic high quality seats design and workmanship.

The rally gives a wide panoramic field of vision thanks to its oversize windows.

Avionics:

We equipped our Rally with finesse avionic configuration and a high level of technologies.

· 2 HD SkyView screen

· EFIS D-100

· Attitude Indicator

· Airspeed Indicator

· Altimeter

· Vertical Speed Indicator

· Turn Coordinator /Ball

· Compass Heading Turn Rate

· Clock/Timer

· G-Meter,

· Voltmeter

· Angle of Attack indicator

· Transponder

We are relying on “Dynon Avionics” leader for Light Sport and Experimental Aircraft.

Engine

Only renowned engine are purchased. Bombardier- Rotax 914 ULS (100 hp) engines are renowned for operating economy (75% power 3.9 gal/h), longevity and torque

the engine has TBO of 2000 hours,4 horizontally opposed cylinders in boxer configuration

, four stroke, a mixed cooler (liquid for cylinder head and air for the cylinders) taking the rotational speed of the propeller to 2 387 rpm at the engine maximal power mode to 5 800 rpm.

Characteristics :integrated reduction drive I = 2,43, torque limiter, double electronic ignition system, expansion vessel and integrated water pump, 2 constant depression carburetors, fuel pump, an electrical starter with relay, oil injector and filter, two temperature probes for cylinder head, an oil temperature probe and an oil pressure probe.

Propeller:

We ensure the most appropriate equipment therefore we chose DUC propeller provider services since 1997. The SWIRL three bladed model made with Fiber Carbon, ground adjustable, with TBO of 800h.

Landing gears:

Tricycle with a nose gear filled with a single directional wheel and a duals wheel with brakes

 

 

RALLY SPECIFICATION  

 

Exterior Dimensions

Span ……………………………………………………………..    30 ft 1 in

Length…………………………………………………………….    23.2 ft

Height…………………………………………………………….      7 ft

Wing Area……………………………………………………….  124.96 sq ft

Interior Dimensions

Cabin Height (top of seats to roof)…………………………..    40 in

Cabin Width (door to door, at the handle) …………………    43.7 in

Cabin Length (instrument panel to rear bulkhead) ………    70 in

Baggage Space…………………………………………………    16 cubic ft

Powerplant/Systems

Model……………………………………………………………..     Rotax 912 UL S2

Power/rpm……………………………………………………….     100 hp / 5800 rpm

Propeller

Type ……………………………………………………………..      3 blades ground adjustable

Diameter ………………………………………………………..      70 inches

 

  PERFORMANCES CHART

 

Speed

Maximum at sea level………………………………………    120 knots

Cruise (75% power at 2000 ft, ISA conditions) ……….    107 knots

34 Gal Usable Fuel   ……………………………………….    Time 7.2 hours

Cruise

75% at 2000 ft (ISA conditions)…………………………..   Range 800 Nm

Rate of climb at sea level…………………………………..   800 ftm

Service ceiling………………………………………………… 12000 ft

Takeoff Performance – (ISA Conditions – Sea Level)

Ground roll ……………………………………………………    360 ft

Total Distance over 50 ft obstacle………………………..    600 ft

Landing Performance – (ISA Conditions – Sea Level)

Ground roll ……………………………………………………    450 ft

Total Distance over 50 ft obstacle………………………..   1000ft

Stall Speed

Flaps up, power off…………………………………………………………      44 knots

Flaps down, power off……………………………………………………..      35 knots

Maximum Weight

Light Sport Aircraft rules …………………………………………………..  1320 lbs

Standard Empy Weight

Light Sport Aircraft……………………………………………………………   760 lbs

Maximum Useful Load

Light Sport Aircraft……………………………………………………………   560 lbs

Wing Loading                                                                                      

Light Sport Aircraft………………………………………………………….  10.34 lbs/sq ft

Power Loading……………………………………………………………..   13.2 lbs/hp

Total Fuel Capacity

Standard Wing Tanks……………………………………………………..   35 gal/34 usable

Oil Capacity …………………………………………………………………   0.8 gal