Textron Lycoming IO-540 Series - Page 52

TO FIND
ACTUAL
HORSEPOWER
FROM
ALTITUDE,R
PM, MANIFOLD
PRESSURE
AND AIR INLET
TEMPERATURE
L LOCATE
AN FULL THROTTLE
ALTITUDE
CURVE
FOR
GIVEN
RPM
MANIFOLD
PRESS
2 LOCATE
S ON SEA LEVEL
CURVE
0
m
m
n
w
m
0
r
m
Figure
3-7. Sea
Level
and
Altitude
Performance
- 0-540-J,-L