Textron Lycoming IO-540 Series Operator's Manual page 44

Aircraft engines
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TEXTRON LYCOMING OPERATOR'S MANUAL
SECTION 3
0-540 & 10-540 SERIES
OPERATING CONDITIONS (Cont.)
Fuel
Cons.
RPM
HP
Gal./Hr.
Max.
Oil Cons.
Qts./Hr.
*Max
Cyl. Head
Temp
Operation
IO-540-A, -B, -E, -G, -P Series
Normal Rated
Performance
Cruise
(75% Rated)
Economy Cruise
(60% Rated)
2575
290
-----
0.97
500°F. (260°C.)
2350
220
16.5
0.73
500°F. (260°C.)
2200
175
12.0
0.5
500°F. (260°C.)
IO-540-C, -J Series **
2575
250
-----
0.83
500°F. (260°C.)
Normal Rated
Performance
Cruise
(75% Rated)
Economy Cruise
(60% Rated)
2350
190
16.5
0.63
500°F. (260°C.)
2200
150
12.5
0.50
500°F. (260°C.)
IO-540-D, -N, -R, -T, -V Series
Normal Rated
Performance
Cruise
(75% Rated)
Economy Cruise
(60% Rated)
2700
260
2450
195
--
0.87
500°F. (260°C.)
15.0
0.65
500°F. (260°C.)
2350
155
12.0
0.52
500°F. (260°C.)
IO-540-K, -L, -M, -S Series
Normal Rated
Performance
Cruise
(75% Rated)
Economy Cruise
(60% Rated)
2700
300
--
2450
225
18.0
1.0
500°F. (260°C.)
0.75
500°F. (260°C.)
2350
180
12.8
0.60
500°F. (260°C.)
* - At Bayonet Location - For maximum service life of the engine maintain
cylinder head temperatures
between 150°F. and 435°F. during continuous
operation.
** - Limiting manifold pressure for continuous operation of IO-540-C4B5,
-C4C5, -J4A5 with Hartzell propeller HCE2Y type hub and 8465-7R blades.
Do not exceed 27 inches manifold pressure below 2300 RPM.
3-16

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