Tecnam P92 Echo MKII - Page 80

Page 5 - 12
Section 5 - Performance
CRUISE PERFORMANCE
1
st
Edition - Rev. 0
9. CRUISE PERFORMANCE
Maximum takeoff weight = 600 kg (1320 lbs)
(2) Fuel tanks 2x45 liters (11.9 gal) (less the unusable fuel)
Pressure altitude H
P
: 0 ft OAT: +15°C
Engine
RPM
Speed
KTAS
Consumption
(lt/h)
4300
102
14
4800
107
18
5200
110
21
Pressure altitude H
P
: 3000 ft OAT: +9°C
Engine
RPM
Speed
KTAS
Consumption
(lt/h)
4300
100
14
4800
107
18
5200
109
21
Pressure altitude H
P
: 6000 ft OAT: +3°C
Engine
RPM
Speed
KTAS
Consumption
(lt/h)
4300
97
14
4800
105
18
5200
108
21