MOONEY
M20V ACCLAIM ULTRA
SECTION V
PERFORMANCE
5 - 61
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE - 03-16-2017
RANGE
AND
ENDURANCE
-
(100
G
AL
-
C
rui
se
M
AP
=
24
inHG
/Cruise
RPM
=
2400)
M
ix
tu
re=B
es
t
P
o
w
er
C
ru
is
eM
A
P
=2
4i
n
H
G
C
ru
is
eR
P
M
=2
40
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
81
2
5.05
84
2
5.24
87
4
5.4
5
90
6
5.
68
940
5.9
4
40
00
7
83
8
4.88
86
8
5.05
89
8
5.2
3
93
0
5.
44
963
5.6
6
80
00
-1
86
2
4.78
89
1
4.92
92
1
5.0
9
95
1
5.
26
982
5.4
6
1200
0
-9
88
7
4.72
91
6
4.85
94
4
4.9
9
97
2
5.
15
10
01
5.3
1
1600
0
-1
7
91
1
4.69
93
8
4.81
96
4
4.9
3
99
0
5.
06
10
15
5.2
0
1800
0
-2
1
92
3
4.69
94
9
4.79
97
4
4.9
0
99
8
5.
02
10
21
5.1
4
2000
0
-2
5
93
2
4.67
95
7
4.77
98
1
4.8
7
10
03
4.
97
10
24
5.0
8
2200
0
-2
9
94
1
4.65
96
5
4.74
98
7
4.8
3
10
07
4.
92
10
24
5.0
1
2400
0
-3
3
94
7
4.62
96
9
4.70
98
9
4.7
7
10
07
4.
85
10
22
4.9
2
2500
0
-3
5
94
8
4.60
97
0
4.67
98
9
4.7
4
10
06
4.
80
10
19
4.8
7
Mi
xtu
re
=
B
est
Eco
n
o
my
C
rui
se
MA
P
=
24
in
H
G
C
rui
se
RPM
=
24
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
93
0
5.99
95
8
6.19
98
8
6.4
1
10
17
6.
66
10
47
6.9
4
40
00
7
95
8
5.77
98
6
5.94
1014
6.1
3
10
43
6.
34
10
72
6.5
8
80
00
-1
98
8
5.61
10
16
5.76
1043
5.9
3
10
70
6.
12
10
97
6.3
2
1200
0
-9
101
4
5.52
10
41
5.65
1066
5.7
9
10
91
5.
95
11
15
6.1
2
1600
0
-1
7
103
9
5.46
10
63
5.57
1086
5.6
9
11
08
5.
82
11
29
5.9
6
1800
0
-2
1
104
9
5.43
10
73
5.53
1095
5.6
4
11
14
5.
75
11
32
5.8
7
2000
0
-2
5
105
9
5.40
10
81
5.49
11
01
5.5
8
11
19
5.
68
11
35
5.7
9
2200
0
-2
9
106
5
5.36
10
85
5.44
11
03
5.5
2
11
19
5.
60
11
31
5.6
9
2400
0
-3
3
106
7
5.30
10
87
5.37
11
03
5.4
4
11
15
5.
50
11
24
5.5
7
2500
0
-3
5
106
8
5.26
10
86
5.32
11
01
5.3
8
11
12
5.
44
11
18
5.5
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