Mooney M20V Acclaim Ultra, Pilot Operating Handbook

Page: 159 / 265

MOONEY
M20V ACCLAIM ULTRA
SECTION V
PERFORMANCE
5 - 58
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE - 03-16-2017
RANGE
AND
ENDURANCE
-
(100
G
AL
-
C
rui
se
M
AP
=
22
inHG
/Cruise
RPM
=
2500)
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
50
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
R
S
0
15
79
0
4.96
82
1
5.15
85
1
5.3
5
88
3
5.
58
915
5.8
4
40
00
7
83
5
4.97
86
5
5.14
89
6
5.3
2
92
7
5.
53
960
5.7
6
80
00
-1
87
7
4.96
90
7
5.1
1
93
6
5.2
8
96
7
5.
47
998
5.6
7
1200
0
-9
91
1
4.94
93
9
5.07
96
8
5.2
2
99
6
5.
38
10
25
5.5
6
1600
0
-1
7
93
5
4.90
96
3
5.02
98
9
5.1
4
10
15
5.
28
10
40
5.4
2
1800
0
-2
1
94
4
4.87
97
2
4.98
99
7
5.0
9
10
21
5.
21
10
44
5.3
4
2000
0
-2
5
95
2
4.84
97
8
4.94
1001
5.0
4
10
23
5.
15
10
43
5.2
6
2200
0
-2
9
95
9
4.80
98
4
4.89
1006
4.9
8
10
26
5.
07
10
44
5.1
7
2400
0
-3
3
96
4
4.77
98
7
4.84
1007
4.9
2
10
25
5.
00
10
39
5.0
7
2500
0
-3
5
96
6
4.75
98
8
4.82
1007
4.8
9
10
23
4.
96
10
36
5.0
2
Mi
xtu
re
=
B
est
Eco
n
o
my
C
rui
se
MA
P
=
22
in
H
G
C
rui
se
RPM
=
25
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
NMI
H
R
S
0
15
90
2
5.91
93
0
6.1
1
95
8
6.3
3
98
6
6.
57
10
14
6.8
5
40
00
7
95
6
5.89
98
5
6.07
1014
6.2
6
10
42
6.
48
10
70
6.7
3
80
00
-1
100
2
5.86
10
29
6.01
1056
6.1
9
10
84
6.
38
11
10
6.6
0
1200
0
-9
104
0
5.80
10
67
5.94
1093
6.0
9
11
17
6.
26
11
41
6.4
4
1600
0
-1
7
106
7
5.72
10
91
5.84
11
14
5.9
6
11
36
6.
10
11
56
6.2
4
1800
0
-2
1
107
6
5.67
10
99
5.78
11
21
5.8
9
11
40
6.
01
11
57
6.1
4
2000
0
-2
5
108
1
5.62
11
06
5.71
11
26
5.8
1
11
43
5.
91
11
57
6.0
2
2200
0
-2
9
108
7
5.55
11
08
5.64
11
25
5.7
2
11
40
5.
81
11
52
5.9
0
2400
0
-3
3
109
0
5.49
11
09
5.56
11
24
5.6
3
11
36
5.
70
11
44
5.7
7
2500
0
-3
5
109
0
5.46
11
09
5.52
11
23
5.5
8
11
34
5.
65
11
40
5.7
0
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