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Single engine, two-seater
side-by-side
high-wing monoplane with a metal structure
three versions with 4-stroke engines are available.
Alisport initiated development of the YUMA in 1994 with
the goal of surpassing the technical and flight characteristics
of existing light S.T.O.L. (Short Take-Off & Landing)
aircraft. The project focused on the following design requirements:
- assurance of an aircraft designed and constructed
to the most stringent aeronautical specifications;
- ability to take-off and land from virtually
any field having limited space or obstructions without sacrificing
good cruise speed;
- excellent control responsiveness and
harmony;
The techniques and materials used throughout
the construction of the YUMA are typical of the certified
aircraft industry. For example, all aircraft structural parts
are heat-treated and corrosion inhibiting coatings are used
throughout.
All aluminum skins are bonded to the underlying structure
prior to final riveting.
The use of materials matches the intended application. For
example, the cockpit structure is comprised of a welded tubular
steel frame providing the very best protection to the occupants,
the aluminum used for the wings, tail-cone, and empennage
provides for stiff and lightweight aerodynamic structures,
and the fabric-covered control surfaces improve response.
The flight characteristics of the YUMA are enhanced by an
optimized wing profile and carbon-fiber leading edge
slats (Handley-Page type) that directly address the requirements
of S.T.O.L. flight. The ability to perform challenging landings
in confined spaces is further enhanced by generous sizing
of the control surfaces.
These provide exceptional maneuverability and do not
lose control effectiveness at very low airspeeds. Additionally,
the large flaps permit steep final approaches to facilitate
descent over tall obstacles at the edges of an airfield without
wasting valuable field length.
The cockpit layout provides both comfort and unobstructed
visibility that an aircraft of this type must provide
whether used for sport flying, aerial work, or observation.
In response to the utility of long flights and range, the
fuel system is comprised of two wing tanks and a header tank
at the firewall providing a total endurance of up to five
hours.
To maximize the results possible with the aircraft, Alisport
provides its clients with complete technical assistance
and a specialized flight training program to both refine the
pilots flying techniques and make full use of the YUMAs
capability.
The training includes off-field take-offs and landings on
difficult terrain, obstacle clearance, mountain flying, plus
unusual attitude recovery and emergency procedures. The school
gives the pilot intimate knowledge of the aircraft and fully
addresses all aspects of flight safety.
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| TECHNICAL
DATA |
| |
|
| Wing
span:
| 9,75
m
|
| Cabin width: |
1,18
m
|
| Length:
| 6,45
m
|
| Height: |
2,45
m
|
| Wheelbase: |
2,00
m
|
| Wing area: |
13,4
m2
|
| Aspect ratio: |
6,6
|
| Empty weight: |
282
kg
|
| Maximum takeoff
weight: |
450
kg
|
| Wing loading: |
33,5
kg/m2
|
|
PERFORMANCE
| |
Rotax
912 UL
(80 HP) |
Rotax
912 ULS
(100 HP)
|
Rotax
914 UL
(115 HP) |
Maximum speed:
|
175 Km/h
|
185 Km/h
|
195 Km/h |
Cruise speed 75%:
|
150 Km/h
|
160 Km/h
|
170 Km/h |
Stall speed (without flaps):
|
55 Km/h
|
55 Km/h
|
55 Km/h |
| Stall speed (with flaps): |
50 Km/h
|
50 Km/h
|
50 Km/h |
Rate of climb:
|
6 m/s
|
8 m/s
|
10 m/s |
Takeoff distance
(with 1 person):
|
40 m
|
30 m
|
30 m |
Takeoff distance (full load):
|
45 m
|
40 m
|
40 m |
Landing distance:
|
55 m
|
55 m
|
55 m |
Max ceiling:
|
5000 m
|
5000 m
|
7000 m |
Fuel capacity:
|
85 l
|
85 l
|
85 l |
Endurance with max payload
at cruise speed 75%(5000 rpm):
| 5,2 h
|
4,5 h
|
4,1 h |
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