Symphony SA-160 - Page 117

SA 160
AIRCRAFTA I R C R A F T
Symphony
AIRCRAFT
5-21
SECTION 5
PERFORMANCE
Feb 25, 2005
CRUISE PERFORMANCE (Continued)
EXAMPLE:
WEIGHT 975 kg (2150 lbs)
TEMPERATURE 7 °C
PRESSURE ALTITUDE 4000 ft
ENGINE SPEED 2400 RPM
% BHP 65%
TRUE SPEED 114 KTAS
MIN. FUEL CONSUMPTION 29 l/h (7.7 U.S. Gal. /h)
U.S.GAL./h
Pressure
Altitude
ft
RPM
Standard Temperature
%BHP
KTAS
A l/h
10000 2700 ----
2600 63,1 123 28 7.4
2500 56,9 118 25 6.6
2400 53,8 114 24 6.3
2300 46,9 107 21 5.5
2100 43,1 101 19 5.0
2000 35,0 88 15 4.0
12000 2700 ----
2600 59,4 123 26 6.9
2500 53,8 118 24 6.3
2400 50,0 114 22 5.8
2300 44,4 107 19 5.0
2100 40,6 101 18 4.8
2000 34,4 88 15 4.0
(Minimum)
Figure 5-9(2)