ICP Savannah - Airplane Technical Description; General Aircraft Specifications

l I.C.P. Sri (
Savannah FLIGHT MANUAL
Pag. 71
I.I GENERAL SPECIFICATIONS
Dimensions
Wing span 30.0/9.0
ft/m
Wing area
I41/I2.7 sq. ft/m
2
Length 2I.3/6.5
ft/m
Height
8.0/2.45 ft/m
Propeller diameter
68/I.73 in/m
w, . h
· · ezgJ ts
Maximum take-off weight
I000/454 Ibs/kg
Em_Qty weight 600/272 Ibs/kg
Usefulload
400/I82 l b s/kg
NOTE: empty weight may increase and is depended on the optional equipment instalied as per the
customer requirements
p l
owerp, ant
Engine
Take
off performance
Dispiacement
Compression ratio
Fuei consumption (75% power)
Fuel and oil
Fuel capacity
Fuel grade
Oil capacity
L
d.
an mg gear
Wheel track
Tire size
Tire pressure
Issue l /Revision 2
Ott.
02
DIMENSION
ROTAX9I2 UL
ROTAX9I2 ULS
59.6 kW (5800 rpm)
75.3 kW (5800 rpm)
cu.in/cm
3
73.9/12II 82.5/1352
9.0:I I0.5:I
gphllt/h 4.3/16.2 4.9/18.5
72 l t
Mogas/ A vgas
IOO/IOO LL
3/3.I6
lt/US qts
5.6/1.7
ft/m
6
m
I4.5/I p silbar
ICP Sri- Via Torino I2, I4020 PIOVA' MASSAIA (AT)- Italy
Phone +39-0I4I-996503 • Fax +39-0I41-996506