Tecnam P92-JS - Page 57

FLIGHT MANUAL
Date: Issue 3: 25
th
May 2010
5-11
P92-JS
S E C T I O N 5
PERFORMANCE
Pressure altitude H
P
: 8000 ft OAT: -0.8°C
Propeller
RPM
Speed
KTAS
Consumption
(l/h)
1
Endurance (hrs)
1
Range (N.m.)
(1)
(2)
(1)
(2)
55%
2120
99
15
4.5
5.8
445
578
58%
2150
102
16
4.2
5.4
428
556
Pressure altitude H
P
: 10000 ft OAT: -5°C
Propeller
RPM
Speed
KTAS
Consumption
(l/h)
1
Endurance (hrs)
1
Range (N.m.)
(1)
(2)
(1)
(2)
55%
2150
100
15
4.5
5.8
450
585
Pressure altitude H
P
: 12000 ft OAT: -9°C
Propeller
RPM
Speed
KTAS
Consumption
(l/h)
1
Endurance (hrs)
1
Range (N.m.)
(1)
(2)
(1)
(2)
50%
2150
98
14
4.8
6.2
475
617
1
Range and endurance are intended approximate and referred to a “zero” wind
condition.