Tecnam P2006T - 6. Stall Speed

Page 5 - 5
Section 5 - Performances
STALL SPEED
4
th
Edition, Rev. 0
6. STALL SPEED
W
W
e
e
i
i
g
g
h
h
t
t
:
:
1
1
1
1
8
8
0
0
k
k
g
g
T
T
h
h
r
r
o
o
t
t
t
t
l
l
e
e
L
L
e
e
v
v
e
e
r
r
s
s
:
:
I
I
D
D
L
L
E
E
L
L
a
a
n
n
d
d
i
i
n
n
g
g
G
G
e
e
a
a
r
r
:
:
D
D
o
o
w
w
n
n
C
C
G
G
:
:
M
M
o
o
s
s
t
t
F
F
o
o
r
r
w
w
a
a
r
r
d
d
(
(
1
1
6
6
.
.
5
5
%
%
)
)
N
N
o
o
g
g
r
r
o
o
u
u
n
n
d
d
e
e
f
f
f
f
e
e
c
c
t
t
W
W
E
E
I
I
G
G
H
H
T
T
B
B
A
A
N
N
K
K
A
A
N
N
G
G
L
L
E
E
S
S
T
T
A
A
L
L
L
L
S
S
P
P
E
E
E
E
D
D
F
F
L
L
A
A
P
P
S
S
0
0
°
°
F
F
L
L
A
A
P
P
S
S
T
T
/
/
O
O
F
F
L
L
A
A
P
P
S
S
F
F
U
U
L
L
L
L
[kg]
[deg]
KIAS
KCAS
KIAS
KCAS
KIAS
KCAS
1230
(FWD C.G.)
0
66
64
56
56
53
54
15
67
65
57
57
54
55
30
70
69
60
60
58
58
45
77
76
67
67
64
64
60
93
90
81
79
78
76
Altitude loss during conventional stall recovery, as demonstrated
during flight tests is approximately 200 ft with banking below 30°.
NOTE