Textron Lycoming IO-540 Series Operator's Manual page 45

Aircraft engines
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TEXTRON LYCOMING OPERATOR'S MANUAL
0-540 & 10-540 SERIES
SECTION 3
OPERATING CONDITIONS (CONT.)
Fuel
Max.
*Max.
Cons.
Oil Cons.
Cyl.Head
Operation
RPM
HP
Gal./Hr. Qts./Hr.
Temp..
Normal Rated
2400
Performance Cruise
(75% Rated)
2200
Economy Rated
(60% Rated)
2000
Normal Rated
2425
Performance Cruise
(75% Rated)
2200
Economy Cruise
(60% Rated)
1900
Normal Rated
2400
Performance Cruise
(75% Rated)
2200
Economy Cruise
(60% Rated)
2000
[O-540-W Series
235
----
0.78
175
12.5
0.58
140
10.1
0.47
IO-540-AA Series
250
---
0.83
190
14.5
0.63
150
11.5
0.50
IO-540-AB Series
230
----
0.78
175
12.5
0.58
500°F. (260°C.)
500°F.(260°C.)
500°F.(260°C.)
500°F.(260°C.)
500°F.(260°C.)
500 F.(260°C.)
500°F.(260°C.)
500°F.(260°C.)
140
10.1
0.47
500°F.(260°C.)
* - At Bayonet Location - For maximum service life of the engine main-
tain cylinder head temperatures between 150°F. and 435°F. during con-
tinuous operation.
Revised January 1997
3-17

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