Tecnam P2006T, Aircraft Flight Manual

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GARMIN G950 IFDS – Increased MTOW (1230 kg)
Page SW5 - 5
4
th
Edition, Rev.0
Section 5 - Performances
STALL SPEED
5. S
TALL SPEED
W
W
e
e
i
i
g
g
h
h
t
t
:
:
1
1
2
2
3
3
0
0
k
k
g
g
(
(
2
2
7
7
1
1
2
2
l
l
b
b
)
)
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 65 59 57 54 55
15 67 66 58 58 55 56
30 71 70 61 61 59 59
45 79 78 68 68 65 65
60 95 93 83 81 79 78
Altitude loss during conventional stall recovery, as demonstrated
during flight tests is approximately 250 ft with banking below 30°.
NOTE