Lycomin 0-360 - Page 92

TOFINDACTUALHORSEPOWERFROMALTITUDE.
RPMMANIFOLDPRESSUREANDAIRINLETTEMPERATURE
CURVENO
13516-A
1. LOCATE
A ON FULL
THROTTLE
ALTITUDE
CURVE
FOR
GIVEN R
P M MANIFOLD
PRESS
2 LOCATE
B ON
SEA LEVEL
CURVE FOR
R P.M & MANIFOLD
PRESSURE
& TRANSFER
TO
C
LYCOMING
3 CONNECTA&C
BY STRAIGHT
LINE AND -READ
HORSEPOWER
AT GIVEN
ALTITUDE D
AIRCRAFTENGINE
D
4 MODIFY
HORSEPOWER
ATDFOR VARIATION
OFAIR INLETTEMPERATURE
TS FROM
PERFORMANCE
DATA
STANDARD ALTITUDE TEMPERATURE T
MIXTURE