THE PREMISE

At AERO (D) 2016, after having manufactured, sold and delivered around the world over the previous 18 years, few hundreds of Savage aircraft, each one with its own specific personality, aesthetics and performance range, Zlin Aviation managed to offer a new chapter to this varied and fascinating family of aircraft.
To reinvent itself continuously, to innovate, to formulate new exciting performance features, has always been important to our small but determined “skunk works” team. Anyone who has met us in person can certainly attest to, among other things, the presence of one great denominator and catalyst for all our achievements….: a strong passion for the“Bushflying”.

THE DEVELOPMENT

First the name.
A name that should not only be able to represent our real intentions but could even “shock” the aficionados of this type of aircrafts. The word “Cub”, first of all, aims to express the typical DNA of our production, which is a fundamental aspect to us and to our Clients. It was time to emphasize this proven winning formula, innovating it with originality and new technical features. The word “Shock”, on the other hand, was added with strong conviction, and it aims to underline some important facts relating to the entire project – to pleasantly “shock”, with specific aerodinamic features and through the “shock absorbers” installed on our plane for the first time, specifically designed to be terribly efficient during landing.

THE NEW FUSELAGE FRAMEWORK

Since the beginning we proceeded from the well known Savage Cub (and from one his derivate now discontinued “the Cub-S”), reinforcing and refining the fuselage framework, increasing the cockpit height, improving the accessibility and the general ergonomics on board. We have increased the surface of the elevators and rudder, fundamental elements when you are flying very very slow (during final approach for example). The stabilizer vertical travel, due to the new jack screw trim system, has been increased to balance the new specific “Hyper Stol Wing” aerodynamic characteristics. On request, the cockpit can be equipped with carbonfiber details, such as, instrument panel, the new floorboards, the kevlar reinforced light weight seats. The engine mount for the Rotax Engines is a dynafocal type as standard and the engine cowling can accommodate up to 180 hp engines such as Lycoming / Titan or other make (on request).

THE NEW LANDING GEAR

The Landing Gear is totally new, already reinforced as standard and is equipped with ultra-performing shock absorbers. The front and rear suspensions innovative design shows an unimaginable shock absorbing capability and the static drop tests, have shown that with a weight of 800 kg (1.763 lbs) and from an height of 1,21 mt (4 ft) the structure still keeps its full integrity after the impact. Landing on a bumpy surface it will never be, since today, easier. The landing gear position has been generously moved forward to allow an exceptional breaking capability without the risk of overturning.

THE NEW WING

The Wing is totally new and, obviously, is one of the most important feature of this new airplane. It is equipped with a new customized Hyper Stol profile. The new spars, together with many other structural improvements, have allowed us to test the wing above the 600 Kg ( 1.322 lbs) MTOW x 6g required by the rules, with no residual permanent deformations. The wing tip is shaped to increase the lift in its area and is available also in carbonfiber. The innovative new “double slotted” flaps, have a surface increased by 70% compared to our previous models. The aileron surface has been increased by 40% to allow the Pilot to keep full control authority at extremely low speed. The fuel tanks capacity has been increased to 110 liter (on request). On the leading edge, four pivoting “slats” have been installed , allowing to fly the plane to unbelievably low speeds if necessary or even to increase the AoA over the imagination. Being fixed, just pivoting according to the airflow (they are not spring actuated) there is not risk of having an half wing with slats extended and an half wing with slats retracted at the approach, in turbulence, during tight turns or sideslip and close to the ground.

NEW FLYING CHARACTERISTICS

With the slats, its huge flaps and that specific landing gear, a different type of performance can be achieved. Using a low speed approach and contacting the ground with the tail wheel first (if needed), spectacular and ultra short stopping distances are achievable. The braking action will be amplified by the main landing gear damping system which, dissipating the energy due to the high vertical deceleration, will subtract longitudinal kinematic energy to the airplane and reduce to a minimum, the necessary landing distance. With just a relatively small head wind it will be possible to have almost virtually vertical landings, which make the airplane even safer in its natural habitat. The new slats installed on the Shock Cub will make spin, in practice, almost impossible, while making easier to control the stall.
It is not a secret that during a famous STOL competition in Alaska (in Valdez) in May 2019, one our customer’s Shock Cub has marked the shortest landing distance in his category.

Specifications

POWER PLANT

ENGINE Rotax 915 iS
141 hp/5800 rpm
PROPELLER Standard: 200 cm (78,7") Wooden Prop

Optional: 4 blade Carbon Prop 203 cm Ground Adj. (80")

CAPACITIES

FUEL TANK CAPACITY Standard: 68lt (18 U.S.Gal.) + header tank: 10lt (2,6 U.S.Gal.)

Optional:
110 lt (29 U.S.Gal.)
FUEL CONSUMPTION 75%: ~25,2 lt/h (~6,65 U.S.Gal./h)

DIMENSIONS

WING SPAN 900 cm (29,5 ft)
LENGTH 684 cm (22,4 ft)
HEIGTH 225 cm with Alaskan Bw 29" (88,5")
WING SURFACE AREA
(no slats)
15,21 m2 (163,7 sq ft)
WING CHORD
(no slats)
169 cm (66,5")
CABIN WIDTH 69 cm (27,1")

WEIGHTS

MAX TAKE-OFF WEIGHT 600 kg (1.322 lbs)
EMPTY WEIGHT including optional light weight program and no slats: from 390 kg (860 lbs)
USEFUL LOAD 210 kg (463 lbs)
MAX WING LOADING 40 kg/m2 (8,2 lb/sq ft)
LOAD FACTOR +6/-3 G

PERFORMANCES *

VNE
(with slats)
185 km/h (115 mph)
MAX SPEED S.L. 180 km/h (112 mph) with slats
STALL SPEED WITH FULL FLAPS/SLATS 50 km/h (31 mph)
MINIMUM FLIGHT SPEED WITH FULL FLAPS/SLATS/ENGINE ON (single pilot) 35 km/h (22 mph)
CRUISING SPEED 155 km/h (96 mph)
CLIMB RATE up to 1.450 fpm (single pilot)
SERVICE CEILING > 15.000 ft
RANGE 65% 640km (397 Nm)
TAKE-OFF ROLL at MTOW <65 m (213 ft)
TAKE-OFF ROLL (single pilot) 28 mt (92 ft)
LANDING ROLL at MTOW <70 m (229 ft)
CROSS WIND COMPONENT (MAX.) 25 km/h (15 mph)
* [MTOW and Std. Atmosphere]

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