Tecnam P2006T, Aircraft Flight Manual

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GARMIN G950 IFDS – Increased MTOW (1230 kg)
Page SW5 - 16
4
th
Edition, Rev. 1
Section 5 - Performances
CRUISE PERFORMANCES
14. C
RUISE PERFORMANCES
Weight: 1150 kg (2535 lb)
Pressure Altitude: 0 ft
ISA – 30°C (-15°C) ISA (15°C) ISA + 30°C (45°C)
RPM
*
MAP
PWR KTAS
F.C.
**
PWR KTAS
F.C.
**
PWR KTAS
F.C.
**
[inHg] [lt/hr] [lt/hr] [lt/hr]
2250 29.5 103% 143 28.6 97% 145 27.1 92% 146 25.8
2250 28 88% 134 24.5 83% 136 23.2 79% 138 22
2250 26 69% 122 19.2 65% 124 18.2 62% 125 17.3
2250 24 59% 115 16.6 56% 116 15.7 53% 117 14.9
2250 22 46% 103 12.8 43% 103 12.1 41% 103 11.5
2250 20 39% 96 11 37% 95 10.4 35% 94 9.9
2100 28 84% 132 23.5 80% 134 22.2 76% 135 21.1
2100 26 66% 121 18.5 63% 122 17.5 60% 123 16.7
2100 24 57% 114 16 54% 114 15.1 52% 115 14.4
2100 22 43% 100 12.1 41% 100 11.5 39% 100 10.9
2100 20 37% 92 10.2 35% 91 9.7 33% 89 9.2
1900 26 61% 117 17.1 58% 118 16.2 55% 119 15.4
1900 24 53% 110 14.9 50% 111 14.1 48% 111 13.4
1900 22 41% 97 11.4 39% 97 10.8 37% 96 10.2
1900 20 35% 89 9.6 33% 88 9.1 31% 85 8.7
*
Propeller RPM
**
Fuel Consumption for each Engine