FLIGHT MANUAL
Doc. No. SP2006FMENKT
December 20, 2006
5 - 7
Section 5
Performance
5.2.3 Take-off distance
Conditions:
- engine:
max. take-off power
- flaps:
Take-off (15
°)
- carburetter preheating:
OFF
- airplane weight:
1268 lbs / 575 kg
- altitude:
0 ft ISA
- ambient air temperature:
ISA
Take-off run
Take-off distance to
height of 50 ft (15 m)
Dray concrete
620 ft / 190 m
1440 ft / 440 m
Grass
720 ft / 220 m
1540 ft / 470 m
Corrections:
- Influence of wind: Add 4% on every 1 kt
(1.15 mph) of tail wind
- RWY inclination: Add 8% of the take-off run
distance on 1% of ruway
inclination up the slope
5.2.4 Landing distance
Conditions:
- engine:
idle
- flaps:
Landing 50
°
- carburetter preheating:
OFF
- airplane weight:
1268 lbs / 575 kg
- altitude:
0 ft ISA
- ambient air temperature:
ISA
Landing distance from
height of
50 ft (15 m)
Braked landing run
Dray concrete
1310 ft / 400 m
590 ft /180 m
Grass
1250 ft /380 m
520 ft / 160 m
Corrections:
- Influence of wind: Add 4.5 % on every 1 kt
(1.15 mph) of tail wind
- RWY inclination: Add 8% of the landing run
distance on 1% of ruway
inclination down the slope
