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Press.
Std. Alt.
Alt.
Temp.
Feet
'C
2100
SL
15
23.2
1000
13
22.9
2000
11
22.5
3000
9
22.2
4000
7
21.9
5000
5
21.6
6000
3
21.3
7000
I
21.0
8000
-I
20.7
9000
-3
20.5
10,000
-5
20.2
. 11,000
-7
19.9
12,000
-9
-
13,000
-ll
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14,000
-13
-
POWER SETTING TABLE
SARATOGA II HP
LONG RANGE
ECONOMY
RPM
RPM
2200 . 2300
2400
2100
2200
2300
2400
MANIFOLD PRESSURE- INCHES MERCURY
22.7
22.2
21.7
25.6
25.0
24.4
23.8
22.3
21.9
21.4
25.2
24.6
24.0
23.5
22.0
21.5
21.1
24.9
24.3
23.7
23.2
21.7
21.2
20.8
24.6
23.9
23.4
22.9
21.4
20.9
20.5
24.3
23.7
23.1
22.6
21.1
20.6
20.2
24.0
23.4
22.8
22.3
20.8
20.3
19.9
23.7
23.1
22.5
22.0
20.5
20.0
19.6
23.3
22.8
22.3
21.7
20.2
19.8
19.3
-
22.4
22.0
21.4
20.0
19.5
19.1
-
-
-
21.2
19.7 .
19.2
18.8
-
-
-
-
19.4
19.0
18.5
19.0
18.7
18.3
-
-
18.0
-
-
-
-
- - · - · - - -
NORMAL
HIGH
RPM
SPEED
2200
2300
2400
2500
2700
28.0
n2
26.5
25.9
27.0
27.6
26.9
26.2
25.6
26.8
27.3
26.6
25.9
25.3
26.5
26.8
26.2
25.6
24.9
26.2 '
-
25.8
25.3
24.7
25.8
-
-
25.0
24.4
-
-
-
24.1
-
-
-
-
APPROX. FUEL FLOW
I
MIXTURE
Long range . I 4.5 GPH
I
so•
Rich of Peak EGT
Economy
16.5 GPH /50" Rich of Peak EGT
Normal
18.5 GPH
I
50" Rich of Peak EGT
High Speed 29.0 GPH
I
Full Rich
I
To maintain constant power, correct manifold pressure approximately 0.5 in Hg for each IO'C variation in induction air temperature from
standard altitude temperature. Add manifold pressure for air temperature above standard; subtract for temperature below standard.
NOTE:
Full throttle manifold pressure values may not be obtainable when atmospheric conditions are non-standard.
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