Mooney M20V Acclaim Ultra, Руководство по эксплуатации для пилотов

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MOONEY
M20V ACCLAIM ULTRA
SECTION V
PERFORMANCE
5 - 62
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE - 03-16-2017
RANGE
AND
ENDURANCE
-
(100
G
AL
-
C
rui
se
M
AP
=
21
inHG
/Cruise
RPM
=
2400)
M
ix
tu
re=B
es
t
P
o
w
er
C
ru
is
eM
A
P
=2
1i
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
89
7
6.07
92
9
6.30
96
1
6.5
4
99
4
6.
81
10
28
7.1
2
40
00
7
91
6
5.71
94
8
5.90
98
0
6.1
1
10
13
6.
35
10
47
6.6
1
80
00
-1
93
8
5.48
96
8
5.64
99
9
5.8
3
10
31
6.
03
10
62
6.2
5
1200
0
-9
96
0
5.34
99
0
5.49
1019
5.6
5
10
48
5.
82
10
77
6.0
1
1600
0
-1
7
98
4
5.28
10
12
5.40
1039
5.5
4
10
65
5.
68
10
90
5.8
3
1800
0
-2
1
99
4
5.25
10
21
5.36
1046
5.4
9
10
70
5.
62
10
93
5.7
5
2000
0
-2
5
100
3
5.22
10
29
5.32
1053
5.4
3
10
75
5.
54
10
94
5.6
6
2200
0
-2
9
101
0
5.17
10
34
5.26
1056
5.3
6
10
75
5.
46
10
92
5.5
6
2400
0
-3
3
101
0
5.10
10
32
5.18
1052
5.2
6
10
69
5.
34
10
83
5.4
2
2500
0
-3
5
100
8
5.05
10
29
5.13
1048
5.2
0
10
64
5.
27
10
76
5.3
4
Mi
xtu
re
=
B
est
Eco
n
o
my
C
rui
se
MA
P
=
21
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
101
7
7.24
10
47
7.49
1076
7.7
5
11
03
8.
05
11
28
8.3
9
40
00
7
104
4
6.76
10
74
6.97
11
03
7.1
9
11
32
7.
45
11
60
7.7
3
80
00
-1
106
6
6.45
10
94
6.62
11
22
6.8
2
11
50
7.
03
11
77
7.2
6
1200
0
-9
109
3
6.26
11
20
6.41
11
47
6.5
7
11
72
6.
75
11
95
6.9
5
1600
0
-1
7
111
7
6.15
11
42
6.27
11
65
6.4
1
11
86
6.
55
12
05
6.7
1
1800
0
-2
1
1127
6.10
11
51
6.21
11
73
6.3
3
11
92
6.
46
12
08
6.6
0
2000
0
-2
5
1135
6.04
11
57
6.14
11
77
6.2
5
11
94
6.
36
12
07
6.4
8
2200
0
-2
9
1137
5.97
11
57
6.06
11
75
6.1
5
11
90
6.
25
12
00
6.3
4
2400
0
-3
3
1137
5.87
11
56
5.94
11
71
6.0
2
11
83
6.
09
11
89
6.1
7
2500
0
-3
5
1133
5.80
11
51
5.87
11
65
5.9
4
11
75
6.
00
11
79
6.0
6
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