Mooney M20V Acclaim Ultra, Руководство по эксплуатации для пилотов

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MOONEY
M20V ACCLAIM ULTRA
SECTION V
PERFORMANCE
5 - 51
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE - 03-16-2017
RANGE
AND
ENDURANCE
-
(89
GAL
-
Cruise
MAP
=
19
inHG
/C
ruise
R
PM
=
2300)
M
ix
tu
re=B
es
t
P
o
w
er
C
ru
is
eM
A
P
=1
9i
n
H
G
C
ru
is
eR
P
M
=2
30
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
87
6
6.41
90
6
6.64
93
6
6.9
0
96
6
7.
18
997
7.5
0
40
00
7
89
8
6.00
92
8
6.19
95
7
6.4
1
98
8
6.
65
10
18
6.9
2
80
00
-1
92
0
5.76
94
8
5.93
97
7
6.1
1
10
04
6.
32
10
32
6.5
5
1200
0
-9
94
2
5.59
96
9
5.74
99
5
5.9
0
10
20
6.
07
10
44
6.2
5
1600
0
-1
7
95
5
5.45
98
0
5.57
1003
5.7
0
10
24
5.
83
10
43
5.9
8
1800
0
-2
1
96
0
5.37
98
3
5.48
1004
5.5
9
10
23
5.
71
10
39
5.8
3
2000
0
-2
5
96
0
5.28
98
1
5.37
1000
5.4
7
10
16
5.
57
10
30
5.6
7
2200
0
-2
9
95
8
5.18
97
8
5.26
99
5
5.3
4
10
09
5.
42
10
18
5.4
9
2400
0
-3
3
95
3
5.06
97
0
5.13
98
4
5.1
9
99
5
5.
25
10
01
5.3
0
2500
0
-3
5
94
8
5.00
96
4
5.06
97
7
5.1
1
98
6
5.
16
990
5.2
0
Mi
xtu
re
=
B
est
Eco
n
o
my
C
rui
se
MA
P
=
19
in
H
G
C
rui
se
RPM
=
23
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
98
7
7.69
10
12
7.95
1036
8.2
4
10
58
8.
56
10
77
8.9
1
40
00
7
101
6
7.12
10
43
7.34
1069
7.5
8
10
93
7.
84
11
15
8.1
4
80
00
-1
104
2
6.79
10
68
6.97
1093
7.1
8
11
17
7.
40
11
39
7.6
4
1200
0
-9
106
5
6.56
10
89
6.71
111
1
6.8
8
11
31
7.
06
11
49
7.2
6
1600
0
-1
7
107
9
6.36
11
00
6.48
11
19
6.6
1
11
35
6.
75
11
48
6.9
0
1800
0
-2
1
108
1
6.25
11
00
6.35
11
17
6.4
7
11
30
6.
59
11
40
6.7
1
2000
0
-2
5
108
0
6.12
10
98
6.22
11
12
6.3
1
11
22
6.
41
11
27
6.5
1
2200
0
-2
9
107
6
5.99
10
91
6.06
11
02
6.1
4
11
09
6.
21
11
11
6.2
9
2400
0
-3
3
106
5
5.83
10
79
5.89
1088
5.9
5
10
92
6.
00
10
89
6.0
4
2500
0
-3
5
105
9
5.74
10
72
5.80
1080
5.8
4
10
82
5.
88
10
77
5.9
1
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