Tecnam P2002-JF, Flight Manual

Page: 355 / 435

Page VP5-13
Section 5 – Performances (Variable Pitch Propeller)
C
RUISE PERFORMANCES
3
rd
Edition, Rev.0
10. C
RUISE PERFORMANCES
Weight: 580 kg
Pressure Altitude: 0 ft
ISA – 30°C (-15°C) ISA (15°C) ISA + 30°C (45°C)
RPM
*
MAP
[inHg]
PWR KTAS
F.C.
**
PWR KTAS
F.C.
**
PWR KTAS
F.C.
**
[lt/hr] [lt/hr] [lt/hr]
2388 29.5 113% 128 29.5 106% 129 27.9 101% 131 26.6
2260 29.5 106% 127 28.6 100% 128 27.1 96% 129 25.8
2260 28 91% 119 24.5 86% 119 23.2 82% 119 22
2260 26 71% 106 19.2 67% 106 18.2 64% 105 17.3
2260 24 61% 98 16.6 58% 96 15.7 55% 94 14.9
2260 22 47% 81 12.8 45% 74 12.1 43% 70 11.5
*
Propeller RPM
**
Fuel Consumption
Weight: 580 kg
Pressure Altitude: 3000 ft
ISA – 30°C (-15°C) ISA (15°C) ISA + 30°C (45°C)
RPM
*
MAP
[inHg]
PWR KTAS
F.C.
**
PWR KTAS
F.C.
**
PWR KTAS
F.C.
**
[lt/hr] [lt/hr] [lt/hr]
2388 26.4 98% 125 25.7 93% 125 24.3 88% 124 23.1
2260 26.4 92% 122 25 87% 123 23.6 83% 123 22.4
2260 26 88% 120 23.9 84% 121 22.6 79% 121 21.5
2260 24 74% 110 20 70% 110 18.9 66% 109 18
2260 22 59% 97 16 56% 95 15.1 53% 91 14.3
2260 20 50% 85 13.4 47% 77 12.7 45% 73 12.1
*
Propeller RPM
**
Fuel Consumption
Weight: 580 kg
Pressure Altitude: 6000 ft
ISA – 30°C (-15°C) ISA (15°C) ISA + 30°C (45°C)
RPM
*
MAP
[inHg]
PWR KTAS
F.C.
**
PWR KTAS
F.C.
**
PWR KTAS
F.C.
**
[lt/hr] [lt/hr] [lt/hr]
2388 23.6 88% 121 23.3 84% 122 22 80% 120 20.9
2260 23.6 83% 120 22.6 79% 120 21.4 75% 119 20.3
2260 22 71% 110 19.1 67% 109 18.1 64% 107 17.2
2260 20 59% 98 15.8 55% 95 14.9 53% 88 14.2
2260 18 48% 81 12.9 45% 81 12.2 43% 80 11.6
*
Propeller RPM
**
Fuel Consumption
The weight does not affect significantly the cruise performances;
a reference weight of 580 kg has been taken into account.
NOTE