12320.0
30.0
101.0
60.0
100.0
7000.0
0.669
50.0
1
20
20
15000
0.05
34
60
Engine power, function of airspeed and pressure
atmosphere/P-sl-psf
velocities/ve-kts
0 50 100 150 200 250
503 0.357 0.380 0.400 0.425 0.457 0.486
1048 0.586 0.589 0.600 0.621 0.650 0.686
1328 0.707 0.721 0.731 0.757 0.786 0.821
1496 0.779 0.786 0.808 0.821 0.857 0.900
1684 0.850 0.857 0.874 0.900 0.943 0.979
1896 0.914 0.929 0.946 0.971 1 1.057
2135 1 1.011 1.029 1.043 1.083 1.150
2213 1.029 1.043 1.057 1.079 1.114 1.171
Engine Power, function of RPM and N1
0 5 60 86 94 95 96 97 98 99 100 101
0 0.0 4.0 4.0 4.0 4.0 4.0 4.0 4.0 4.0 4.0 4.0 4.0
800 0.0 4.0 282.6 1615.1 2826.4 3068.6 3391.7 3714.7 4037.7 4279.9 4683.7 5006.7
1200 0.0 4.0 242.3 1857.3 3230.1 3472.4 3795.4 4078.1 4441.5 4764.5 5168.2 5491.3
1600 0.0 4.0 40.4 1938.1 3553.2 3835.8 4118.4 4441.5 4804.8 5087.5 5491.3 5814.3
2000 0.0 0.8 0.8 1817.0 3633.9 3997.3 4239.6 4562.6 4926.0 5249.0 5652.8 6016.2
2200 0.0 0.8 0.8 1655.5 3553.2 3876.2 4158.8 4522.2 4885.6 5208.6 5612.4 6000.0
Inter-Turbine Temperature ITT [deg C] depending on N1 and engine run (0=off / 1=running)
0 1
0 0 0
15 100 100
60 180 520
96 270 680
100 280 730