Tecnam P92 Eaglet - Cruise

P92 Eaglet
Flight Manual
Revision Date: 12-14-2007
Revision Number: 1.00
Doc n° 27-13-100-00
47
4.9 Cruise
Maximum takeoff weight = 600 kg (1320 lbs)
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
(gal/h)
Endurance (hrs)
Range (N.m.)
55% 4600 96 4 5.8 599
65% 5000 102 4.8 4.9 495
75% 5200 108 5.3 4.4 472
Pressure altitude H
P
: 2000 ft OAT: +11°C
Engine
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
Range (N.m.)
55% 4600 98 4
65% 5000 106 4.8
73% 5200 109 5.2
5.8
4.9
4.6
571
515
501
Pressure altitude H
P
: 4000 ft OAT: +7°C
Engine
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
Range (N.m.)
55% 4600 101 4 5.8 588
60% 5000 105 4.5 5.1 540
70% 5200 110 4.9 4.7 520
Pressure altitude H
P
: 6000 ft OAT: +3°C
Propeller
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
Range (N.m.)
55% 5000 104 4 5.8 606
60% 5200 108 4.5 5.1 556
1
Range and endurance are intended approximate and referred to a “zero” wind condition.
Pressure altitude H
P
: 8000 ft OAT: -0.8°C
Propeller
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
Range (N.m.)
55% 5150 99 4 5.8 578
58% 5200 102 4.3 5.4 556
Pressure altitude H
P
: 10000 ft OAT: -5°C
Propeller
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
Range (N.m.)
55% 5200 100 4 5.8 585
Pressure altitude H
P
: 12000 ft OAT: -9°C
Propeller
RPM
Speed
KTAS
Consumption
(gal/h)
Endurance (hrs)
Range (N.m.)
50% 5200 98 3.7 6.2 617