Rotax CESSNA 150, Manual

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Airplane Flight
Manual Cessna
F
150
L
Nr. 160
Converted with kit
NS402S with ROTAX 912 S3 and Page:
5-7
HOFFMANN HO-V352F/170FQ+10 Revision 1
TAKEOFF DISTANCE
Sea
level 4000 ft 8000 ft
Deviation
from
ISA
°C
OAT
°C
Ground
run
m
Total to
clear 15-m
obst.
m
OAT
°C
Ground
run
m
Total to
clear 15-m
obst.
m
OAT
°C
Ground
run
m
Total to clear
15-m obst.
m
-33 -18 158 314 -26 221 438 -34 312 621
0 +15 216 426 +7 308 609 -1 456 915
+22 +37 263 516 +29 387 770 +21 589 1204
Fig. 5 - 4
– Takeoff distance
Conditions:
•
Takeoff weight 726kg
•
Wind calm
•
Paved level, Dry Runway
•
Wind calm
Note:
•
Airspeed at 15m 65mph (IAS).
•
Decrease distances 10% for each 9 knots headwind. For operation with tailwinds up to 10
knots, increase distances by 10% for each 2 knots.
•
For operation on a dry, grass runway, increase distances by 15% of the "ground roll" figure