Update to latest configs
Add pax
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@@ -1,4 +1,4 @@
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//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.6.5_GE_F 04APR25
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//TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.7.0_GE_F 15MAY25
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[VERSION]
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//KH Bump major
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@@ -22,16 +22,16 @@ max_number_of_stations = 15
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station_load.0=170.0, 82.0, -2.0, 4.0, Pilot, 1
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station_load.1=170.0, 82.0, 2.0, 4.0, First Officer, 2
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station_load.2=170.0, 80.0, 3.3, 4.0, Engineer, 0
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station_load.3=8675.0, 60.0, -5.0, 4.0, Upper zone 1 L, 0
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station_load.4=8675.0, 60.0, 5.0, 4.0, Upper zone 1 R, 0
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station_load.5=11675.0, 10.0, -5.0, 4.0, Upper zone 2 L, 0
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station_load.6=11675.0, 10.0, 5.0, 4.0, Upper zone 2 R, 0
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station_load.7=11675.0, -40.0, -5.0, 4.0, Upper zone 3 L, 0
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station_load.8=11675.0, -40.0, 5.0, 4.0, Upper zone 3 R, 0
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station_load.9=14675.0, -90.0, -5.0, 4.0, Upper zone 4 L, 0
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station_load.10=14675.0, -90.0, 5.0, 4.0, Upper zone 4 R, 0
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station_load.11=44648.0, 30.0, 0.0, -4.5, Lower forward cargo, 0
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station_load.12=64685.0, -50.0, 0.0, -4.5, Lower rear cargo, 0
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station_load.3=8675.0, 55.0, -5.0, 4.0, Upper zone 1 L, 0
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station_load.4=8675.0, 55.0, 5.0, 4.0, Upper zone 1 R, 0
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station_load.5=11675.0, 20.0, -5.0, 4.0, Upper zone 2 L, 0
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station_load.6=11675.0, 20.0, 5.0, 4.0, Upper zone 2 R, 0
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station_load.7=11675.0, -20.0, -5.0, 4.0, Upper zone 3 L, 0
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station_load.8=11675.0, -20.0, 5.0, 4.0, Upper zone 3 R, 0
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station_load.9=14675.0, -50.0, -5.0, 4.0, Upper zone 4 L, 0
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station_load.10=14675.0, -50.0, 5.0, 4.0, Upper zone 4 R, 0
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station_load.11=64648.0, 30.0, 0.0, -4.5, Lower forward cargo, 0
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station_load.12=44685.0, -30.0, 0.0, -4.5, Lower rear cargo, 0
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station_load.13=0.0, 5.0, -2.0, -4.5, Left aux tank, 0
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station_load.14=0.0, 5.0, 2.0, -4.5, Right aux tank, 0
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@@ -111,7 +111,7 @@ htail_area = 920
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htail_span = 59.5
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htail_pos_lon = -88
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htail_pos_vert = 5.0
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htail_incidence = 1.0
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htail_incidence = 0.8
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htail_sweep = 36.5
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htail_thickness_ratio = 0.02
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vtail_area = 760
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@@ -155,7 +155,7 @@ fly_by_wire = 0
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elevator_elasticity_table = 0:0.7, 87:0.3, 210:0.5, 315:0.5
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aileron_elasticity_table = 0:1, 300:0.7, 600:0.6, 1500:0.4
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rudder_elasticity_table = 0:1, 300:1, 800:1, 1000:0.7
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elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.44, 290:0.44, 315:0.40
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elevator_trim_elasticity_table = 0:0.0, 87:0.40, 240:0.60, 295:1.00, 315:1.00
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[AERODYNAMICS]
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lift_coef_pitch_rate = -8.09375
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@@ -403,4 +403,4 @@ drag_scalar = 0.475
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pitch_scalar = 1
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max_on_ground_position = 1
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flaps-position.0 = 0, -1, 0
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flaps-position.1 = 20, 215, 0.5, 0.5
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flaps-position.1 = 20, 215, 0.5, 0.5
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