Textron Lycoming IO-540 Series Operator's Manual page 56

ALTITUDE RPM, MUANIFOLDPRE P ESS RORANCE
AN AIR ;LET TEMPERATURE.
I LAATE AO IULTTTL ALTITUE
RATED POWER j-
SuRvW E ADEM
S
TAI.
O
O
PBRM
.
—
R "6, HW
mDIM° AHRR~ %'O /
1:; —
TRAMPRU TO C
3 COWCT aC
vr
SuMRT uNE AWI -
RfEA HO O.WER AT GIVEN TITUE 0
8
oruY RMACKiT r D RWIARTO V
— —T j 260
T LITU
RE TERTUe
/ o *
APIEMIX
IIATIT I% C—RT/RC / FMR 240
E. ACI0 F ATIOR T T
ErHalUI//
/
220
e-'z e - vrl^Ters
Frr
xs
>
200
< A t /' ¢ t X
cURVE NO 12ss
O
ALTITUDE PERFORMANCE LYCOMING
AIRCRAFT ENGINE
PERFORMANCE DATA
MAXIMUM POWER MIXTURE
MARVEL SCHEBLER MA-45
-
Performance Curve - O-540-E, -G, -II Z
Figure 3-10. Sea Level and Altitude Performance Curve