ICP Savannah User Manual

l I.C.P. Sri l
Savannah FLIGHT MANUAL
l Pag. 32j
5.4 RATE OF CLIMB (Rotax 912 UL)
Rate of climb
Maximum weight (l 000/454
Full power setting
Ibs/kg)
Sea level (MSL)
1,100 fpm/5.5 m/s
48 mph/77 km/h
3,000 ft/900 m pressure altitude
790 fpm/4.0 m/s
45 mph/72 km/h
6,000 ft/1 ,800 m press. al titude
520 fpm/2.6 m/s
40 mph/64 km/h
9,000 ft/2,700 m press. attitude 300 fpm/1.5 m/s
3 7
mph/60 km/h
The maximum ceiling is
14,000 ft/4200 m pressure attitude at the maximum weight.
The hest rate o f climb speed is
48177 mph/kmlh.
The hest angle
of climb speed is 45172 mphlkm/h.
The hest gliding angle with flaps retracted is achieved at a
60/96 mph/km/h airspeed. The
Lift to Drag ratio is 12.
The fuel consumption at 75% power setting amounts to 4.9/18.5
gphllt/h for Rotax 912 ULS
and 4.3/16.2 gphllt/h for Rotax 912 UL
lssue l /Revision 2
Ott. 02
ICP Sri- Via Torino 12, 14020 PlOV A' MASSAIA (AT)- Italy
Phone +39-0141-996503 • Fax +39-0141-996506

ICP Savannah Specifications

General

Brand	ICP
Model	Savannah
Category	Tools
Language	English