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So, before even to offer splendid photos and evocative environments, we chose a more technical and also more “intimate” way to present our product through some technical drawings that capture a few moments in the planning stages.
So, before even to offer splendid photos and evocative environments, we chose a more technical and also more “intimate” way to present our product through some technical drawings that capture a few moments in the planning stages.
We present you an entire team of designers, managers, workers and specialists working together to achieve a common objective.
All our aircrafts are born in that way, and are the result of a work based on the precision, commitment, skills and cooperation.
Our immediate objective is to share with you this magic.
We have always dreamed something new, different, without renouncing a set of functions. Simple and functional airplanes.
All our aircrafts are born in that way, and are the result of a work based on the precision, commitment, skills and cooperation.
Our immediate objective is to share with you this magic.
We have always dreamed something new, different, without renouncing a set of functions. Simple and functional airplanes.
The SYNCRO project is based on this concept.
Innovative in design and technology of assembly. Essentiality and harmony, personality and versatility of ergonomics and prestige.
The Syncro maintains the characteristics that distinguish all Fly Synthesis’s airplanes, wide view , capable and comfortable cockpits, excellent maneuverability.
The mission of this project is to transform the spirit of flight, making the airplane an object with which to test the most advanced concepts of aerodynamics and fluidity.
Innovative in design and technology of assembly. Essentiality and harmony, personality and versatility of ergonomics and prestige.
The Syncro maintains the characteristics that distinguish all Fly Synthesis’s airplanes, wide view , capable and comfortable cockpits, excellent maneuverability.
The mission of this project is to transform the spirit of flight, making the airplane an object with which to test the most advanced concepts of aerodynamics and fluidity.
The organic and fluid shapes alongside the rigorous design and shiny surfaces softly curved in total freedom.
Every detail is designed to ensure the highest elegance and performance maintaining the highest level of safety at the top of the category. The string and sports shapes involve the pilot into an experience of pure aesthetic and concrete functionality.
Every detail is designed to ensure the highest elegance and performance maintaining the highest level of safety at the top of the category. The string and sports shapes involve the pilot into an experience of pure aesthetic and concrete functionality.
U.M. |
ULM |
LSA |
|||
|---|---|---|---|---|---|
Wing Span |
m |
10,4 |
10,4 |
||
Lenght |
m |
6,75 |
6,75 |
||
Height |
m |
2,26 |
2,26 |
||
Empty Weight |
kg |
289 |
305 |
||
MTOW |
kg |
472,5 |
472,5 |
||
Engine |
- |
Rotax 912 ULS |
Rotax 912 ULS |
||
Wing Area |
m² |
10,54 |
10,54 |
||
Wing Chord |
m |
1,045 |
1,045 |
||
Laminar Wing Profiles |
n° |
4 |
4 |
||
VNE |
km/h |
295 |
272 |
||
VC (Max cruising speed in rough air) |
km/h |
230 |
220 |
||
VS0 (MTOW) |
km/h |
64 |
73 |
||
Load Factor |
G |
+5 - 3 |
+4,5 - 2,5 |
||
Endurance with 30' reserve |
km |
1200 |
1200 |
EXPERIMENTAL TECHNICAL DATA
Some data collected during test flights.
Some data collected during test flights.
Syncro 450 |
km/h |
Syncro 600 |
km/h |
||
|---|---|---|---|---|---|
Stall speed with flap |
VS0 |
65 |
VS0 |
73 |
|
Stall speed no flap |
Vs1 |
79 |
Vs1 |
89 |
|
Max speed extended flaps |
VF |
120 |
VF |
124 |
|
Manuvering speed |
VA |
176 |
VA |
188 |
|
Max speed in rough air |
VC |
230 |
VC |
225 |
|
Never exceed speed |
VNE |
276 |
VNE |
272 |
|
White arc |
VS0-VF |
[65-120] |
VS0-VF |
[73-124] |
|
Green Arc |
VS1-VC |
[79-230] |
VS1-VC |
[89-225] |
|
Yellow arc |
VC-VNE |
[120-176] |
VC-VNE |
[124-188] |
|
Airplane loaded conditions ( pilot + pass + 30lt fuel ) Engine: Rotax 912 100 CV Prop: Idrovario bipala PVV |
TOW: |
||||
|---|---|---|---|---|---|
Low speeds (mesured) |
[km/h] |
||||
Stall no flap |
VS |
67 |
|||
Stall flap 30° |
VS30 |
53 |
|||
Stall flap 45° |
VS45 |
48 |
|||
Airplane loaded conditions ( pilot + pass + 30lt fuel ) Engine: Rotax 912 100 CV Elica: Idrovario bipala PVV |
TOW: |
||||
|---|---|---|---|---|---|
Horizontal flight |
Engine |
Speed |
|||
RPM |
MAP |
IAS |
|||
[giri/min] |
[mmHg] |
[km/h] |
|||
4300 |
24 |
194 |
|||
4800 |
26 |
228 |
|||
5000 |
26 |
235 |
|||
5500 |
28 |
272 |
|||
Take off |
Engine |
IAS |
Take off run |
||
[giri/min] |
[km/h] |
[m] |
|||
5600 |
90 |
||||
Climb / Sink |
Engine |
IAS |
Vertical Speed |
||
[giri/min] |
[km/h] |
[ft/min] |
|||
5600 |
98 |
1050 |
|||
Off |
110 |
-520 |





