Textron Lycoming IO-540 Series - 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