Arrow PA-28R-201 Pilot's Operating Handbook And Faa Approved Airplane Flight Manual page 114

o.~
'~
~--=
0
~
-<
t;e
I
...
"'t:I
w
Q\
0
0.
~
::d
00
~
.-3
.-3
!lIZ
~ ~
ca
~
I.f't;e
~
Nt"'
00
~~
00
,-,
d
t;e
~
~
'"
0
....
~
..
~
~00
!")
-<~
Q
=
~--=
Q
00.-3
~
~~
~:s:
' - '
:s:~
~~ ...
$'C~ ......
\0 \0
\000
0.00
Pressure
Altitude
Feet
S.L.
1000
2000
3000
4000
5000
5250
6000
7000
8000
8750
9000
10000
11000
12000
Power Setting Table for Lycoming ModeIIO-360-C1C6
Engine as Installed in PA-28R·201 Arrow Best Economy Mixture
55% Power
65% Power
ISA Temperature 110 BHP @ Propeller 130 BHP @Propeller
Mixture Peak EGT
Mixture Peak EGT
Manifold Pressure - In. Hg Manifold Pressure - In. Hg
OF
°C
2200 RPM 2500 RPM
2200 RPM 2500 RPM
59 15 24.8 22.2 27.5 24.5
55
13 24.4 22.0
27.1 24.3
52 11
24.0
21.8 26.7 24.1
48
9 23.7 21.5 26.3 23.8
45 7
23.3
21.3 26.0 23.6
41 5
22.9 21.1
25.6 23.3
40 4
22.8
21.0 F.T. 23.2
38
3 22.5 20.8
23.1
34
1
22.1
20.6 22.8
30 -1 21.8 20.4 22.6
28 -2 21.5 20.2
F.T.
27 -3 F.T. 20.1
23
-5 19.9
19 -7 19.7
16 -9 F.T.
Pressure
Altitude
Feet
S.L.
1000
2000
3000
4000
5000
5250
6000
7000
8000
8750
9000
10000
11000
12000
Note: 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 standard. Full throttle manifold pressure values may not be obtainable
when atmospheric conditions are non-standard.
~
---
~
"'t:Ir:tl
~~
~~
o~
~~
> 0 .
Z
~
~
~
Ci
~~
N.-3
OOCi
~o
N~
=--=
!"""O
~S
O~
~~