Tecnam P92-JS - LANDING DISTANCE

FLIGHT MANUAL
Date: Issue 3: 25
th
May 2010
5-13
P92-JS
S E C T I O N 5
PERFORMANCE
LANDING DISTANCE (Approved data)
CONDITIONS:
- Maximum weight = 550 kg (600kg) - Engine: throttle idle
- Brakes: maximum braking - Runway: dry, compact, grass
- Slope: 0° - Wind: zero
- Conditions: ISA - Flaps: 38°
Hp (ft)
0
1000
2000
3000
4000
5000
6000
7000
GR (m)
100
103
106
109
112
116
119
123
LD (m)
252
256
260
264
268
273
279
282
- Maximum weight = 600kg - Engine: throttle idle
- Brakes: maximum braking - Runway: dry, compact, grass
- Slope: 0° - Wind: zero
- Conditions: ISA - Flaps: 38°
Hp (ft)
0
1000
2000
3000
4000
5000
6000
7000
GR (m)
120
124
127
131
134
139
143
148
LD (m)
302
307
312
317
322
328
335
338
NOTE
1. Decrease distances by 10% for each 10 Kts of headwind. Increase
distances by 20 % for each 10 Kts of tailwind;
2. For dry and paved runway operation increase ground run by 10%;
3. If it becomes necessary to land without flap extension (flap
malfunction), increase approach speed by 10 Kts, increase by 40%
distance pertaining to flap setting at 38° and increase V
obs
to 58 KIAS
(61KIAS) for 550 kg MTOW (600 kg);
4. V
obs
(speed over obstacle) is 48 KIAS (50 KIAS) for 550 kg MTOW
(600 kg);