Table of Contents
Advertisement
~~
~~
oo~
~
..
•• 00
;s:~
~~
"'d
QC;S:
0
~
t;C
~
tCtIj
~~
....
~
,!II
00
....
tIj
Ie
1-3
QC
'Ij1-3
QC
.... Z
~ ~
(;l
!-3
Vl~
't;C
~t""
tIj
---
t;C
III
'" ....
"'d
0
~
::;J
III
~
.:!-
"'d
0
~
~
.
Ill ....
• w
NCI'I
W III
Power Setting Table for Lycoming Model IO-360-C1 C6
Engine as Installed in PA-28R·201 Arrow
Best Power Mixture
55% power
65% power
75% power
Pressure
ISA
110 BHP@ Prop
130 BHP @ Prop
150 BHP@ Prop
Pressure
I
Altitude
Temperature
Mixture Peak EGT
+
100° F Mixture Peak EGT
+
100° F Mixture Peak EGT
+
100° F
Altitude
Note:
RPM and Manifold Press.
RPM and Manifold Press.
RPM and Manifold Press.
Feet
OF
°C
2200 RPM
2500 RPM
2200 RPM
2500 RPM
2500 RPM
Feet
S.L.
59
15
23.7
21.7
26.1
24.1
26.3
S.L.
1000
55
13
23.4
21.4
25.8
23.7
26 .. 0
1000
2000
52
11
23.0
21.1
25.4
23.4
25.6
2000
3000
48
9
22.6
20.8
25.1
23.1
25.3
3000
4000
45
7
22.3
20.5
24.7
22.8
24.9
4000
,
5000
41
5
21.9
20.2
24.3
22.4
24.6
5000
6000
38
3.
21.6
19.9
24.0
22.1
24.3
6000
6800
35
2
21.3
19.7
23.7
21.9
F.T.
6800
7000
34
1
21.2
19.6
23.6
21.8
7000
7500
32
0
21.0
19.4
F.T.
21.6
7500
8000
30
-1
20.8
19.3
21.5
8000
9000
27
-3
20.5
19.0
21.1
9000
9400
25
-4
20.3
18.9
F.T.
9400
10000
23
-5
F.T.
18.7
10000
11000
19
-7
18.4
11000
12000
16
-9
18.1
12000
13000
12
-11
17.8
13000
14000
9
-13
17.5
14000
- - - -
- -
_ . -
To maintain constant power, correct manifold pressure approximately 0.16" Hg for each 10° F (5.5° C) variation in inlet air temperature
from standard altitude temperature. Add manifold pressure for air temperatures above standard: subtract for temperatures below
staooard.Fuli throttle manifold
pr~ure
values may n?t be obtainable when atmospheric conditions are non-standard.
~::s
N~
QC~
~>
N~
Q~
!""("')
;;~
~~
01-3
:;;("')
o
~
o
~
~
~
~
0
00
~B
ZO
("')Z
~1Il
Advertisement
Chapters
Table of Contents
