MOONEY
M20V ACCLAIM ULTRA
SECTION V
PERFORMANCE
5 - 59
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE - 03-16-2017
RANGE
AND
ENDURANCE
-
(100
G
AL
-
C
rui
se
M
AP
=
30.5
inHG
/Cruise
RPM
=
2400)
M
ix
tu
re=B
es
t
P
o
w
er
C
ru
is
eM
A
P
=3
0.
5i
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
68
4
3.75
71
1
3.89
73
9
4.0
5
76
9
4.
23
801
4.4
3
40
00
7
71
4
3.76
74
1
3.89
76
9
4.0
4
79
8
4.
20
829
4.3
8
80
00
-1
74
0
3.78
76
7
3.90
79
4
4.0
3
82
2
4.
17
851
4.3
3
1200
0
-9
76
4
3.79
78
9
3.89
81
6
4.0
1
84
2
4.
14
869
4.2
8
1600
0
-1
7
78
5
3.79
80
9
3.88
83
4
3.9
8
85
8
4.
09
882
4.2
1
1800
0
-2
1
79
3
3.79
81
8
3.87
84
1
3.9
7
86
5
4.
06
887
4.1
7
2000
0
-2
5
80
1
3.79
82
4
3.87
84
6
3.9
5
86
8
4.
04
888
4.1
3
2200
0
-2
9
80
8
3.79
83
0
3.86
85
1
3.9
3
87
1
4.
01
890
4.0
9
2400
0
-3
3
81
6
3.79
83
6
3.85
85
6
3.9
2
87
5
3.
98
891
4.0
5
2500
0
-3
5
82
0
3.79
83
9
3.85
85
9
3.9
1
87
6
3.
97
890
4.0
3
Mi
xtu
re
=
B
est
Eco
n
o
my
C
rui
se
MA
P
=
30
.5
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
80
1
4.49
82
6
4.63
85
3
4.8
0
88
0
4.
98
909
5.1
8
40
00
7
83
5
4.49
86
1
4.62
88
7
4.7
6
91
3
4.
93
941
5.1
1
80
00
-1
86
6
4.48
89
0
4.60
91
5
4.7
3
94
0
4.
87
966
5.0
3
1200
0
-9
89
0
4.46
91
3
4.56
93
7
4.6
8
96
0
4.
80
984
4.9
3
1600
0
-1
7
90
8
4.43
93
0
4.51
95
2
4.6
1
97
2
4.
71
992
4.8
2
1800
0
-2
1
91
5
4.41
93
6
4.48
95
6
4.5
7
97
6
4.
66
994
4.7
6
2000
0
-2
5
92
0
4.38
94
1
4.45
96
1
4.5
3
97
8
4.
61
994
4.6
9
2200
0
-2
9
92
4
4.36
94
4
4.42
96
2
4.4
9
97
7
4.
55
991
4.6
2
2400
0
-3
3
92
9
4.34
94
6
4.39
96
2
4.4
4
97
6
4.
50
986
4.5
5
2500
0
-3
5
93
1
4.32
94
7
4.37
96
2
4.4
2
97
5
4.
47
984
4.5
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
