Textron Lycoming IO-540 Series Operator's Manual page 40

Aircraft engines
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TEXTRON LYCOMING OPERATOR'S MANUAL
0-540 & 10-540 SERIES
SECTION 3
OPERATING CONDITIONS (CONT.)
FUEL PRESSURE (PSI)
IO-540-K1F5, -K1G5, -K1G5D,
-K1H5, -K1J5, -K1J5D
Inlet to fuel pump
Inlet to fuel injector
IO-540-M1B5D
Inlet to fuel pump
Inlet to fuel injector
IO-540-K1A5,1A 1A5D, -K1B5,
-K1B5D, -K1F5D, -K1K5,
-K2A5, -M1A5, -M1C5
Inlet to fuel pump
Inlet to fuel injector
MIN.
MAX.
IDLE MIN.
-2
40
18
55
-2
18
45
45
12
12
12
-2
55
18
55
IO-540-AC1A5
Inlet to fuel pump
Inlet to fuel injector
10-540-G1B5, -G1C5, -G1D5,
-K1D5, -P1A5, -S1A5
Inlet to fuel pump
Inlet
to fuel injector
IO-540-J4A5, -R1A5
Inlet to fuel pump
Inlet to fuel injector
-2
65
29
65
-4
18
40
40
12
12
12
-4
45
14
45
Revised April 1999
3-12A/B

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