MOONEY
M20V ACCLAIM ULTRA
SECTION V
PERFORMANCE
5 - 60
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE - 03-16-2017
RANGE
AND
ENDURANCE
-
(100
G
AL
-
C
rui
se
M
AP
=
27
inHG
/Cruise
RPM
=
2400)
M
ix
tu
re=B
es
t
P
o
w
er
C
ru
is
eM
A
P
=2
7i
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
74
6
4.34
77
4
4.51
80
4
4.6
9
83
5
4.
89
868
5.1
2
40
00
7
77
4
4.28
80
2
4.43
83
1
4.5
9
86
2
4.
77
894
4.9
8
80
00
-1
80
0
4.25
82
8
4.38
85
7
4.5
3
88
6
4.
69
916
4.8
7
1200
0
-9
82
4
4.23
85
2
4.35
87
9
4.4
8
90
6
4.
62
934
4.7
7
1600
0
-1
7
84
8
4.23
87
4
4.33
89
9
4.4
4
92
4
4.
56
949
4.6
9
1800
0
-2
1
85
9
4.23
88
5
4.32
90
9
4.4
3
93
3
4.
53
955
4.6
5
2000
0
-2
5
87
0
4.23
89
4
4.31
91
7
4.4
0
93
9
4.
50
959
4.6
0
2200
0
-2
9
87
8
4.22
90
2
4.30
92
4
4.3
8
94
4
4.
46
962
4.5
5
2400
0
-3
3
88
4
4.21
90
8
4.28
92
7
4.3
5
94
5
4.
42
960
4.4
9
2500
0
-3
5
88
9
4.20
90
9
4.27
92
8
4.3
3
94
5
4.
39
959
4.4
6
Mi
xtu
re
=
B
est
Eco
n
o
my
C
rui
se
MA
P
=
27
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
85
9
5.15
88
6
5.32
91
4
5.5
1
94
2
5.
73
973
5.9
6
40
00
7
89
4
5.07
92
1
5.22
94
8
5.3
8
97
6
5.
57
10
05
5.7
8
80
00
-1
92
4
5.01
95
0
5.14
97
6
5.2
9
10
02
5.
45
10
29
5.6
3
1200
0
-9
95
1
4.96
97
5
5.08
1000
5.2
0
10
24
5.
34
10
48
5.5
0
1600
0
-1
7
97
4
4.93
99
7
5.02
1020
5.1
3
10
41
5.
24
10
62
5.3
7
1800
0
-2
1
98
3
4.91
10
05
4.99
1026
5.0
9
10
46
5.
19
10
65
5.3
0
2000
0
-2
5
99
2
4.88
10
13
4.96
1033
5.0
5
10
50
5.
14
10
66
5.2
3
2200
0
-2
9
99
9
4.86
10
19
4.93
1037
5.0
0
10
52
5.
07
10
65
5.1
5
2400
0
-3
3
100
3
4.82
10
22
4.88
1039
4.9
4
10
52
5.
00
10
62
5.0
6
2500
0
-3
5
100
4
4.80
10
23
4.86
1039
4.9
1
10
51
4.
96
10
59
5.0
2
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
