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  FLYSYNTHESIS > SYNCRO

Syncro Characteristics
  U.M. ULM LSA
Wing Span m 10,4 10,4
Length 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
Syncro progect - characteristic 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
[giri/min]
MAP
[mmHg]
IAS
[km/h]
  4300 24 194
  4800 26 228
  5000 26 235
  5500 28 272
Take off Engine IAS Take off run
  [giri/min] [mmHg] [km/h]
  5600   90
Climb / Sink Engine IAS Vertical Speed
  [giri/min] [mmHg] [km/h]
  5600 98 1050
  OFF 110 -520


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