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We would like to tell you a little more about the story that brings out a new product inside the Fly Synthesis company. It is a special story, that of a research and development of new forms, of design and creativity, bringing to light new concepts in the panorama of materials, forms and safety.
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.
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.
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.
Syncro Characteristics

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

10,54

10,54

Wing Chord

m

1,045

1,045

Laminar Wing Profiles

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.

Syncro progect - caracteristic speeds
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]
Flight Performance
Airplane loaded conditions
( pilot + pass + 30lt fuel )
Engine: Rotax 912 100 CV
Prop: Idrovario bipala PVV

TOW:
600 kg

Low speeds (mesured)

[km/h]

Stall no flap

VS

67

Stall flap 30°

VS30

53

Stall flap 45°

VS45

48

Performance
Airplane loaded conditions
( pilot + pass + 30lt fuel )
Engine: Rotax 912 100 CV
Elica: Idrovario bipala PVV

TOW:
600 kg

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