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-1.29450,-1.30808,-1.30763,-1.30267,-1.29873,&
-1.29013,-1.29921,-1.31215,-1.31578,-1.31067,&
-1.30216,-1.30826,-1.32260,-1.30085,-1.30780,&
-1.32801,-1.30845,-1.29379,-1.31837,-1.32354,&
-1.30182,-1.31707,-1.34122,-1.33728,-1.29928,&
-1.26473,-1.24858,-1.23360,-1.21667,-1.20075,&
-1.19259,-1.17065,-1.13473,-1.09576,-1.05647,&
-1.01627,-0.97416,-0.93471,-0.90394,-0.87912,&
-0.85150,-0.82113,-0.79423,-0.76751,-0.74274,&
-0.72071,-0.70026,-0.67875,-0.65563,-0.63129,&
-0.60738,-0.58319,-0.55662,-0.52999,-0.50503,&
-0.48014,-0.45503,-0.42987,-0.40221,-0.36724,&
-0.32885,-0.28896,-0.24699,-0.20322,-0.15936,&
-0.11700,-0.07826,-0.04194,-0.00601, 0.02865,&
0.06331, 0.09933, 0.13591, 0.17155, 0.20078,&
0.22495, 0.24723, 0.26669, 0.28571, 0.30512,&
0.33057, 0.36230, 0.39468, 0.42872, 0.46249,&
0.49528, 0.52814, 0.56066, 0.59247, 0.62509,&
0.65765, 0.68978, 0.72237, 0.75668, 0.77236,&
0.75175, 0.76499, 0.76381, 0.74495, 0.76561,&
0.78717, 0.76713, 0.74758, 0.76078, 0.76316,&
0.76337, 0.76334, 0.76336 /)
!
!* pressure of the segments ends (1st point is takeoff, last point is landing)
! (pascals)
!
IF (TAIRCRAFT9%ALTDEF) THEN
ALLOCATE(TAIRCRAFT9%SEGP (TAIRCRAFT9%SEG+1))
TAIRCRAFT9%SEGP = 100. * (/ 1014.8,1014.8,1014.8,1014.8,1005.5,&
987.8, 972.7, 959.2, 957.2, 978.1,&
993.8, 993.5, 992.9, 995.5, 997.4,&
997.7, 998.5, 998.3, 996.8, 997.7,&
1000.1, 999.3, 998.7, 997.4, 996.2,&
998.3,1000.0, 999.9, 999.1, 998.6,&
998.5, 998.0, 999.2, 999.1,1009.5,&
1003.4, 990.2, 978.4, 967.1, 956.2,&
945.9, 934.6, 924.2, 912.3, 901.3,&
889.8, 878.6, 866.9, 855.7, 844.9,&
834.2, 823.0, 812.0, 801.4, 800.1,&
806.9, 815.5, 824.4, 834.5, 845.2,&
856.3, 870.2, 884.9, 898.2, 913.0,&
927.0, 940.6, 953.4, 966.2, 979.8,&
992.8,1004.2,1006.7, 993.2, 982.3,&
972.7, 962.0, 950.9, 940.8, 928.6,&
917.0, 906.2, 895.3, 884.4, 874.0,&
864.1, 854.4, 844.5, 834.4, 823.4,&
812.3, 803.1, 806.5, 815.1, 824.1,&
836.3, 845.1, 854.7, 866.7, 884.2,&
903.2, 921.4, 938.5, 953.8, 969.2,&
986.8,1000.3,1007.3, 995.3, 983.3,&
986.5,1005.5,1005.5, 994.9, 985.4,&
973.9, 964.7, 954.5, 945.0, 935.2,&
924.2, 913.1, 902.7, 891.8, 881.8,&
871.0, 860.2, 850.3, 839.9, 830.3,&
820.3, 809.5, 801.3, 802.9, 813.4,&
825.9, 839.4, 855.4, 874.2, 894.0,&
909.5, 925.8, 940.5, 955.0, 969.2,&
983.7,1000.0,1008.1,1000.5, 988.9,&
982.3, 972.7, 960.7, 951.3, 939.8,&
929.0, 915.4, 904.9, 895.4, 884.3,&
873.4, 863.1, 852.1, 840.5, 829.5,&
819.2, 809.6, 800.6, 801.4, 809.6,&
818.1, 829.6, 840.8, 854.8, 868.4,&
882.0, 894.2, 908.1, 922.9, 937.5,&
950.9, 967.8, 987.5,1003.2,1005.1,&
1003.5,1003.3,1002.4,1002.3,1002.0,&
995.6, 995.5, 998.5, 999.5,1000.3,&
1000.6, 999.6, 998.8, 999.2, 998.0,&
997.3, 995.4, 995.1, 998.1, 988.4,&
976.2, 965.3, 956.4, 945.6, 947.8,&
965.9, 985.1,1003.1,1013.9,1013.9,&
1013.9,1013.9,1013.9 /)
ELSE
ALLOCATE(TAIRCRAFT9%SEGZ (TAIRCRAFT9%SEG+1))
TAIRCRAFT9%SEGZ = (/8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000,8000,8000,&
8000,8000,8000/)
ENDIF
!
!----------------------------------------------------------------------------
!
!
END SUBROUTINE INI_AIRCRAFT