MOONEY
M20TN - MODEL TYPE-S
SECTION V
PERFORMANCE
5 -- 23
AIRPLANE FLIGHT MANUAL
ORIGINAL ISSUE -- 04-02-2008
2500
2400
2300
2200
RPM:
Ma
nifol
d
P
res
su
re
(inHg):
30.5
29.0
26.0
22.0
30.5
27.0
24.
0
21.0
28.0
25.0
22.0
19.0
21.0
S
TAN
DAR
D
DA
Y
C
R
U
IS
E
F
UE
L
F
LO
W
(ga
l/hr)
@
6.
0
lb
/ga
l
Pr
.A
lt.
S
TD
OA
T
21.4
20.6
18.7
16.1
20.4
18.0
15.
8
13.4
17.8
15.5
13.1
10.5
11.0
21.4
20.5
18.7
16.0
20.4
18.1
16.
0
13.7
17.9
15.9
13.9
11.7
12.5
21.3
20.4
18.6
15.9
20.3
18.1
16.
1
14.0
17.9
16.0
14.0
11.9
12.5
21.3
20.4
18.5
15.8
20.3
18.2
16.
2
14.2
17.8
16.0
14.0
12.0
12.5
21.2
20.3
18.4
15.8
20.2
18.2
16.
3
14.4
17.8
16.0
14.1
12.1
12.5
21.1
20.2
18.3
15.7
20.2
18.2
16.
4
14.5
17.8
16.0
14.1
12.1
12.4
21.1
20.1
18.2
15.7
20.2
18.2
16.
4
14.5
17.8
16.0
14.1
12.2
12.4
21.0
20.1
18.2
15.6
20.2
18.1
16.
3
14.5
17.8
15.9
14.1
12.2
12.4
21.0
20.0
18.1
15.6
20.2
18.1
16.
3
14.5
17.8
15.9
14.1
12.2
12.4
21.0
20.0
18.1
15.6
20.2
18.0
16.
2
14.5
17.8
15.9
14.1
12.3
12.5
20.9
19.9
18.0
15.6
20.2
18.0
16.
2
14.4
17.7
15.9
14.1
12.3
12.6
20.9
19.9
18.0
15.6
20.2
17.9
16.
2
14.5
17.7
15.9
14.1
12.4
12.7
0
2000
4000
6000
8000
10000
12000
14000
16000
18000
20000
22000
20.9
19.9
18.0
15.7
20.1
17.9
16.
2
14.5
17.7
15.9
14.2
12.6
12.8
20.9
19.9
18.0
15.7
20.1
17.9
16.
2
14.6
17.6
15.9
14.2
12.7
12.8
24000
25000
Note
1:
At
altitudes
above
22,000
feet,
power
settings
above
2300
rpm
m
ust
b
e
operated
at
1675
F
T
IT
or
richer
.
Note
2:
When
operating
above
30.5
inHg
m
anifold
p
ressure
only
F
ULL
R
ICH
m
ixture
is
permitted.
Note
3:
Decrease
Fuel
F
low
0.5
gal/hr
for
each
10
C
above
standard
temperature.
Note
4:
Increase
Fuel
F
low
0.5
gal/hr
for
each
10
C
b
elow
standard
temperature.
Example:
for
2500
RPM,
25000
ft
Pr
.A
lt.,
--25
C
O
A
T,
30.5
inHg
M
AP
the
fuel
flow
is:
21.3
--
0.5
=
20.8
g
al/hr
15
C5
9
F
11
C5
2
F
45
F
3
C
-1
C3
0
F
-5
C2
3
F
-9
C1
6
F
-1
3
C9
F
-1
7
C2
F
-2
1
C-
5
F
-2
5
C-
12
F
-2
9
C-
19
F
-3
3
C-
27
F
-3
5
C-
30
F
7
C
38
F
BEST
POWER
50
Rich
of
P
eak
TIT
Some
(low
)
pow
er
settings
may
not
be
attainable
due
to
low
cy
linder
o
r
o
il
temperatures
depending
on
ambient
conditions
CRUISE POWER SETTINGS & FUEL FLOWS -- BEST POWER
Содержание M20TN S type
Страница 4: ......
Страница 6: ...MOONEY M20TN BLANK ...
Страница 8: ...MOONEY M20TN MODEL TYPE S INTRODUCTION BLANK ...
Страница 20: ...MOONEY M20TN MODEL TYPE S INTRODUCTION xii ORIGINAL ISSUE 04 02 2008 BLANK ...
Страница 22: ...MOONEY M20TN MODEL TYPE S SECTION I GENERAL 1 2 ORIGINAL ISSUE 04 02 2008 AIRPLANE FLIGHT MANUAL BLANK ...
Страница 36: ...MOONEY M20TN MODEL TYPE S SECTION II LIMITATIONS 2 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 BLANK ...
Страница 170: ...MOONEY M20TN MODEL TYPE S SECTION VI WEIGHT AND BALANCE 6 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 BLANK ...
Страница 254: ...MOONEY M20TN MODEL TYPE S SECTION IX SUPPLEMENTAL DATA 9 4 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 BLANK ...
Страница 256: ...MOONEY M20TN MODEL TYPE S SECTION X SAFETY INFORMATION 10 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 BLANK ...