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The new Savage Cub, with his unique and new look (the main structure comes from our standard Savage Classic and Cruiser aircrafts but was totally redesigned) can be equipped with several professional options that offer to the Pilots the possibility to operate into the bush. We took care about all the aspects of the bushflying and we learned from the experience of the professional operators of the legendary Piper Super Cub.
With a basic Savage Cub you will fly an aircraft that will give you the feeling that only historical planes recall.
With some special options your Savage Cub will be able to land almost everywhere enjoying the freedom and the spirit of the real bushflying.
There are two ways for a Pilot to go from the classical point A to the point B...One of the most common way is to fly very fast, looking from the sky the beauty of the landscape.
We think there is another way...We offer to our customers another choice...
To fly slower, enjoying the special opportunity to put the wheels where we dream (according to the rules), immersing ourself into the nature and not only looking at the beautiful landscape that normally we observe from the sky...
Remember our philosophy : "runways are only an option for a Savage's Cub
Pilot..." |
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"Fly in a remote area near or far from your base.
Camp for a weekend ..alone..
only you and your plane, and you will discover a new side of your fantastic passion... and probably also something more about yourself.
That's our mission...".
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| New Savage Cub Features |
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New Fuselage Design
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New X brace in the tail section |
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New X brace at the top of the cabin |
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New reinforced landing gear attachments
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New landing gear design
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New suspensions and new safety cables |
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New reinforced battery box attachments
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New
battery door panel |
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New vertical tail and fin design
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New door and rear windows design
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New larger baggage area |
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New comfort seatings
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New aluminum bowl |
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New panel housing
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New instrument panel
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New firewall design
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| New aluminum cowling |
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New spinner
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New wing tip
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New reinforced flaps
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| Optionals |
| Landing Gear |
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6 inch HD extended landing gear
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Alaskan Bushwheels 29"
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Alaskan Bushwheels 31" |
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Step
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Reinforced axles 1 ¼" |
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Matcho Performance brake system |
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AOSS suspension system |
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Safety cables
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Reinforced tail leaf
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| Interiors-Cargo |
| De Luxe Leather seating
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| Aluminum side panels |
| Complete wooden floorboards |
| Left window partially extendable |
| Extended solid baggage compartment
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| Belly Pod Cargo |
| Cargo net
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| Cargo tie down rings |
| Camping Kit
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| Cessna style elevator trim |
| New Series
UMA engine instruments |
| Defroster |
| Safety |
| Rescue system
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| ELT |
| Airbag safety belts |
| Aerodinamic / Performance |
| Vortex |
| Thrust line |
| Climb propeller (2m) |
| Rotax 914 turbo
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| Lycoming IO-233 LSA |
| Generals |
| Personal Bush Flying training |
| Characteristics (with Rotax 912 S 100hp) |
| Engine |
ROTAX 912 S 100hp 5800 rpm |
| Fuel tank capacity: |
68 litres (18 Gallons) |
| Propeller: |
Wooden twin blade, diameter 183 cm (72 in) |
| Dimensions |
| Wing
span |
939 cm (369.7 in) |
| Length |
640 cm (252 in) |
| Height |
203 cm (80 in) |
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Height
with Al.Bw 29" and extended l. gear |
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223 cm (87.8 in) |
| Wing
surface area |
14,2 m2 (152.85 sq ft) |
| Wing
chord |
156 cm (61.4 in) |
| Cabin
width |
67 cm (26.3 in) |
| Undercarriage
gauge |
186 cm (73.2 in) |
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Undercarriage gauge
with Al.Bw 29" and extended l. gear |
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200 cm (78.7 in) |
| Weights |
| Max
take-off weight |
472,5 kg (1041 lbs) - 560 kg (1234 lbs) |
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Weight
unloaded
ULM-LSA version (basic) |
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296 kg (652 lbs) |
| Effective
load capacity |
176,5 kg (388.8 lbs) - 264 kg (581.6 lbs) |
| Max wing loading |
39,4 kg (86.9 lbs) |
| Load factor |
+6 - 3 G |
| Performance |
| Vne |
205 km/h (128 mph) |
| Max speed s.l. |
185 km/h (115 mph) |
| Cruising speed 75% |
165 km/h (103 mph) |
| Climb rate |
5 m/s (984 ft/m) |
| Climb rate (climb prop) |
> 6,4 m/s (> 1260 ft/m) |
| Stall speed with full flaps |
58 km/h (36 mph) |
| Max ceiling |
4400 m (14400 ft) |
| Range 65 % |
700 km (434 mi) |
| Required take-off space |
100 m (328 ft) |
| Required landing space |
85 m (278 ft) |
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Required take-off space
Configuration A |
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70 m (229 ft) |
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Required landing space
Configuration B |
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< 75 m (< 249 ft) |
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Required take-off space
Configuration C |
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45 m (147 ft) |
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Required landing space
Configuration D |
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< 30 m (< 98.4 ft) |
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Required landing space w 15m obst.
Configuration B |
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< 150 m (< 492 ft) |
| Cross wind component (max.) |
29 km/h (18 mph) |
| Specifications |
| Configuration A |
With Climb Prop, Vortex, Thrust Line and Extended Landing Gear |
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| Configuration B |
Required landing space, with Climb Prop, Vortex, Thrust Line, Extended Landing Gear and Performance Brake System |
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| Configuration C |
Required take-off space, with Climb Prop, Vortex, Thrust Line, Extended Landing Gear and Single Pilot |
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| Configuration D |
Required landing space, with Climb Prop, Vortex, Thrust Line, Extended Landing Gear, Performance Brake System and Single Trained Pilot |
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