Mooney M20V Acclaim Ultra, Pilot Operating Handbook

Page: 166 / 265

MOONEY
M20V ACCLAIM ULTRA
SECTION V
PERFORMANCE
5 - 65
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE - 03-16-2017
RANGE
AND
ENDURANCE
-
(100
G
AL
-
C
rui
se
M
AP
=
22
inHG
/Cruise
RPM
=
2300)
M
ix
tu
re=B
es
t
P
o
w
er
C
ru
is
eM
A
P
=2
2i
n
H
G
C
ru
is
eR
P
M
=2
30
0
Pr
ess
A
lt
Ft
STD
O
A
T

C
ISA
-30

C
NM
I
H
RS
IS
A
-15

C
NM
I
HRS
ISA
+0

C
NM
I
H
R
S
ISA
+1
5

C
NMI
H
RS
ISA
+3
0

C
NMI
H
RS
0
15
90
1
5.96
93
3
6.17
96
6
6.4
1
10
00
6.
68
10
36
6.9
8
40
00
7
92
8
5.73
96
0
5.92
99
3
6.1
4
10
26
6.
37
10
59
6.6
3
80
00
-1
95
8
5.60
98
9
5.77
1020
5.9
6
10
52
6.
16
10
85
6.3
9
1200
0
-9
98
4
5.51
10
14
5.66
1044
5.8
2
10
73
6.
00
11
02
6.2
0
1600
0
-1
7
100
5
5.43
10
33
5.56
1060
5.6
9
10
87
5.
84
11
11
6.0
0
1800
0
-2
1
101
5
5.38
10
42
5.50
1068
5.6
3
10
92
5.
76
11
15
5.9
0
2000
0
-2
5
102
1
5.33
10
46
5.44
1070
5.5
5
10
92
5.
67
11
12
5.7
9
2200
0
-2
9
102
5
5.28
10
49
5.37
1071
5.4
7
10
91
5.
57
11
08
5.6
7
2400
0
-3
3
102
8
5.21
10
51
5.30
1071
5.3
8
10
88
5.
46
11
01
5.5
4
2500
0
-3
5
102
8
5.18
10
50
5.25
1069
5.3
3
10
84
5.
40
10
96
5.4
7
Mi
xtu
re
=
B
est
Eco
n
o
my
C
rui
se
MA
P
=
22
in
H
G
C
rui
se
RPM
=
23
00
Pr
ess
A
lt
Ft
STD
O
A
T

C
ISA
-30

C
NMI
H
R
S
IS
A
-15

C
NM
I
HRS
ISA
+0

C
NM
I
H
R
S
ISA
+1
5

C
NMI
H
RS
ISA
+3
0

C
NM
I
H
R
S
0
15
102
2
7.04
10
52
7.28
1082
7.5
3
11
12
7.
82
11
40
8.1
5
40
00
7
105
2
6.74
10
82
6.94
11
12
7.1
7
11
43
7.
42
11
73
7.7
0
80
00
-1
108
7
6.56
111
6
6.73
11
45
6.9
3
11
73
7.
15
12
00
7.3
9
1200
0
-9
111
6
6.42
11
43
6.58
11
70
6.7
4
11
95
6.
93
12
20
7.1
3
1600
0
-1
7
1139
6.29
11
64
6.42
11
87
6.5
6
12
09
6.
71
12
28
6.8
7
1800
0
-2
1
1144
6.22
11
68
6.34
11
90
6.4
7
12
10
6.
60
12
27
6.7
4
2000
0
-2
5
1150
6.15
11
73
6.25
11
93
6.3
6
12
10
6.
48
12
23
6.5
9
2200
0
-2
9
1153
6.07
11
73
6.15
11
91
6.2
5
12
06
6.
34
12
16
6.4
4
2400
0
-3
3
1152
5.97
11
71
6.05
11
86
6.1
3
11
97
6.
20
12
03
6.2
7
2500
0
-3
5
1150
5.92
11
68
5.99
11
82
6.0
6
11
92
6.
12
11
95
6.1
9
So
me
(l
o
w
)
pow
er
se
tt
ings
may
n
ot
be
attainable
due
to
low
cylin
de
r
o
r
o
il
te
mp
er
atu
re
s
depending
on
ambient
cond
it
ions