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Power Setting Table
-
Lycoming Model 10-360-C Series, 200 HP Engine
-
Press.
Std. Alt
110 HP
-
55% Rated
A I
1
T y p
1
RPMAND MAN. PRESS.
Feet
2100
2400
SL
59
22.9
20.4
2 5 . 9
22.9
2 5 . 5
SL
1 ,ooO
55
22.7
20.2
2 5 . 6
22.7
2 5 . 2
1,000
2,oOO
52
2 2 . 4
20.0
25.4
22.5
25.0
2,000
3,000
48
2 2 . 2
1 9 . 8
2 5 . 1
22.2
2 4 . 7
3,000
4,000
45
2 1 . 9
1 9 . 5
24.8
2 2 . 0
2 4 . 4
4,000
5,000
4 1
2 1 . 7
1 9 . 3
IT
21.7
IT
5,000
6,000
3 8
21.4
1 9 . 1
-
-
21.5
- -
6,000
7,000
34
21.2
1 8 . 9
-
-
2 1 . 3
-
-
7,000
8,oOO
3 1
21.0
1 8 . 7
- -
2 1 . 0
8,oOO
9,000
27
IT
1 8 . 5
-
-
IT
9,000
10,000
2 3
-
-
1 8 . 3
10,000
1 1,000
1 9
--
1 8 . 1
1 1,000
12,000
1 6
- -
1 7 . 8
12,000
1 3,000
1 2
- -
1 7 . 6
1 3,000
14,000
9
- -
IT
14,000
To maintain constant power, correct manifold pressure approximately 0.16" Hg for each 10°F variation in inlet air
temperature from standard altitude temperature. Add manifold pressure for air temperatures above standard; subtract for
temperatures below standard.
130 HP
-
65% Rated
RPM AND MAN. PRESS.
2100
2400
150 HP
-
75% Rated
Press.
RPM AND MAN. PRESS.
I
AIt
2400
Feet
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