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Converted with kit
NS402S with ROTAX 912 S3 and
HOFFMANN HO-V352F/170FQ+10
These distances are well within the available take-off field length. However, a correction for the
effect of wind may be made based on Note 3 of the takeoff chart. The correction for a 12-knot
headwind is:
12
kts
=
10
%
13
%
9
kts
to reduce
Ground run:
Takeoff distance:
If the available runway is not clearly longer than this, interpolation of values is needed. In this
case you must use distances of 0 ft and 4000 ft, and at temperatures of ISA and ISA +22°C.
Then:
ISA
At 0ft
At 4000ft
Interpolating for 1500ft at ISA conditions
(
H
=
x
x
roll
−
roll
H
2
H
1
1500
ft
=
x
roll
−
4000
ft
0
ft
(
H
=
x
x
D
15
−
D
H
2
H
1
1500
ft
=
x
D
15
−
4000
ft
0
ft
ISA+22°C
At 0ft
At 4000ft
Interpolating for 1500ft and ISA+22°C condition
(
H
=
x
x
roll
−
roll
H
2
H
1
1500
ft
=
x
roll
−
4000
ft
0
ft
(
H
=
x
x
D
15
−
D
H
2
H
1
1500
ft
=
x
D
15
−
4000
ft
0
ft
Manual Cessna F150L
387m –0.13*387 = 337m
770m –0.13*770 = 670m
Ground roll= 216m
Ground roll = 308m
)
−
+
x
x
−
−
−
2
roll
1
roll
1
(
)
−
+
308
m
216
m
216
)
−
+
x
x
−
−
−
15
2
D
15
1
D
15
1
(
)
−
+
609
m
426
m
426
Ground roll= 263m
Ground roll= 387m
)
−
+
x
x
−
−
−
2
roll
1
roll
1
(
)
−
+
387
m
263
m
263
)
−
+
x
x
−
−
−
15
2
D
15
1
D
15
1
(
)
−
+
770
m
516
m
516
Airplane Flight
Takeoff distance = 426m
Takeoff distance = 609m
=
m
251
m
=
m
495
m
Takeoff distance = 516m
Takeoff distance = 770m
=
m
310
m
=
m
611
m
Nr. 160
5-2
Page:
Revision 1
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