Tecnam P92-JS, Flight Manual

Page: 59 / 116

F
LIGHT
M
ANUAL
Date : Issue 3: 25
th
May 2010
5-13
P92-JS
SECTI ON 5
PERFORMANCE
LANDING DISTANCE
(Approved data)
C
ONDITIONS
:
- 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);