Tecnam P92-JS - CRUISE

FLIGHT MANUAL
Date: Issue 3: 25
th
May 2010
5-10
P92-JS
S E C T I O N 5
PERFORMANCE
CRUISE
CONDITIONS:
- ISA
- Maximum takeoff weight = for both MTOW
(1) Fuel tanks 2x35 liters (less the unusable fuel)
(2) Fuel tanks 2x45 liters (less the unusable fuel)
Pressure altitude H
P
: 0 ft OAT: +15°C
Propeller
RPM
Speed
KTAS
Consumption
(l/h)
1
Endurance (hrs)
1
Range (N.m.)
(1)
(2)
(1)
(2)
55%
1900
96
15
4.5
5.8
431
599
65%
2050
102
18
3.7
4.9
382
495
75%
2150
108
20
3.4
4.4
364
472
Pressure altitude H
P
: 2000 ft OAT: +11°C
Propeller
RPM
Speed
KTAS
Consumption
(l/h)
1
Endurance (hrs)
1
Range (N.m.)
(1)
(2)
(1)
(2)
55%
1950
98
15
4.5
5.8
440
571
65%
2070
106
18
3.7
4.9
397
515
73%
2150
109
19
3.5
4.6
387
501
Pressure altitude H
P
: 4000 ft OAT: +7°C
Propeller
RPM
Speed
KTAS
Consumption
(l/h)
1
Endurance (hrs)
1
Range (N.m.)
(1)
(2)
(1)
(2)
55%
2020
101
15
4.5
5.8
454
588
60%
2080
105
17
4.0
5.1
416
540
70%
2150
110
18.5
3.6
4.7
401
520
Pressure altitude H
P
: 6000 ft OAT: +3°C
Propeller
RPM
Speed
KTAS
Consumption
(l/h)
1
Endurance (hrs)
1
Range (N.m.)
(1)
(2)
(1)
(2)
55%
2060
104
15
4.5
5.8
467
606
60%
2150
108
17
4.0
5.1
429
556
1
Range and endurance are intended approximate and referred to a “zero” wind
condition.