Performance
DA 40 NG AFM
Page 5 - 10
Rev. 3
01-Jul-2014
Doc. # 6.01.15-E
0°
10°
20°
30°
40°
32°
50°
60°
70°
80°
90°
100°
110°
120°
130°
160°
180°
0
10
20
16
30
40
Crosswind Component [kts]
10
20
10
20
30
40
H
ea
d
w
in
d
C
o
m
p
one
nt [
k
ts
]
Flight Direction
0
M
a
ximu
m d
e
m
o
n
s
trat
e
d
Cr
os
s
w
in
d
Co
m
p
o
n
e
n
t
5.3.6 WIND COMPONENTS
Example:
Flight direction
:
360°
Wind
:
32°/30 kt
Result:
Crosswind component
:
16 kt
Max. demonstrated crosswind component
:
25 kt
Содержание DA 40 NG
Страница 1: ......
Страница 2: ...DA 40 NG AFM Introduction Page 0 0a Rev 3 01 Jul 2014 Doc 6 01 15 E Intentionally left blank...
Страница 160: ...Normal Operating Procedures DA 40 NG AFM Page 4A 40 Rev 3 01 Jul 2014 Doc 6 01 15 E Intentionally left blank...
Страница 190: ...Abnormal Operating Procedures DA 40 NG AFM Page 4B 30 Rev 3 01 Jul 2014 Doc 6 01 15 E Intentionally left blank...
Страница 197: ...DA 40 NG AFM Performance Doc 6 01 15 E Rev 3 01 Jul 2014 Page 5 7 5 3 4 INTERNATIONAL STANDARD ATMOSPHERE...
Страница 240: ...Mass Balance DA 40 NG AFM Page 6 8 Rev 3 01 Jul 2014 Doc 6 01 15 E 6 4 2 LOADING DIAGRAM...
Страница 260: ...DA 40 NG AFM Mass and Balance Doc No 6 01 15 E Rev 3 01 Jul 2014 Page 6 28 Intentionally left blank...
Страница 287: ...DA 40 NG AFM Airplane Description Doc 6 01 15 E Rev 3 01 Jul 2014 Page 7 27 7 9 4 FUEL SYSTEM Standard Tank Schematic...
Страница 288: ...Airplane Description DA 40 NG AFM Page 7 28 Rev 3 01 Jul 2014 Doc 6 01 15 E Long Range Tank Schematic...
Страница 316: ...Handling DA 40 NG AFM Page 8 8 Rev 3 01 Jul 2014 Doc 6 01 15 E...
Страница 322: ...Handling DA 40 NG AFM Page 8 14 Rev 3 01 Jul 2014 Doc 6 01 15 E Intentionally left blank...