update to 1.1.14

This commit is contained in:
Kilian Hofmann 2026-02-05 01:04:29 +01:00
parent 818277edcf
commit 3b003f3363
10 changed files with 82 additions and 84 deletions

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@ -1,15 +1,15 @@
//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.7.1_GE 24JAN26 //TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.8.0_GE 04FEB26
[VERSION] [VERSION]
//KH Bump major //KH Bump major
major = 4 major = 4
minor = 2 minor = 8
[WEIGHT_AND_BALANCE] [WEIGHT_AND_BALANCE]
max_gross_weight = 630500 max_gross_weight = 630500
empty_weight = 283975 empty_weight = 283975
reference_datum_position = 0, 0, 0 reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 0, 0 empty_weight_CG_position = -10.0, 0, 0
CG_forward_limit = 0.12 CG_forward_limit = 0.12
CG_aft_limit = 0.34 CG_aft_limit = 0.34
empty_weight_pitch_MOI = 20897456 empty_weight_pitch_MOI = 20897456
@ -59,7 +59,7 @@ max_speed_decreasing_steering_castering = 35
emergency_extension_type = 2 emergency_extension_type = 2
hyd_need_power_to_function= 0 hyd_need_power_to_function= 0
min_castering_angle = 0.05236 min_castering_angle = 0.05236
max_castering_angle = 1.32645 max_castering_angle = 3.142
allow_stopped_steering = 1 allow_stopped_steering = 1
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8 point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8 point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
@ -88,9 +88,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00 RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00 External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
//KH From 5.00, -2.00, -3.00, 0.00, 10.00 //KH From 5.00, -2.00, -3.00, 0.00, 10.00
LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00 LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
//KH From 5.00, 2.00, -3.00, 0.00, 10.0 //KH From 5.00, 2.00, -3.00, 0.00, 10.0
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00 RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
fuel_type = 2 fuel_type = 2
number_of_tank_selectors = 3 number_of_tank_selectors = 3
electric_pump = 0 electric_pump = 0
@ -175,7 +175,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1 lift_coef_flaps = 1
lift_coef_spoilers = 0 lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539 drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.0789 drag_coef_flaps = 0.1339
drag_coef_gear = 0.0549 drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207 drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392 side_force_slip_angle = -0.77392
@ -265,7 +265,7 @@ cruise_lift_scalar = 1
parasite_drag_scalar = 1 parasite_drag_scalar = 1
induced_drag_scalar = 1 induced_drag_scalar = 1
flap_induced_drag_scalar = 1 flap_induced_drag_scalar = 1
elevator_effectiveness = 1 elevator_effectiveness = 1.1
elevator_maxangle_scalar = 1 elevator_maxangle_scalar = 1
aileron_effectiveness = 1 aileron_effectiveness = 1
rudder_effectiveness = 1 rudder_effectiveness = 1
@ -362,7 +362,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.1] [FLAPS.1]
@ -384,7 +384,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.2] [FLAPS.2]

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@ -1,15 +1,15 @@
//TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.7.1_GE 24JAN26 //TFDi Designs MD-11 (GE CF6-80C2D1F) vRC1.8.0_GE 04FEB26
[VERSION] [VERSION]
//KH Bump major //KH Bump major
major = 4 major = 4
minor = 2 minor = 8
[WEIGHT_AND_BALANCE] [WEIGHT_AND_BALANCE]
max_gross_weight = 630500 max_gross_weight = 630500
empty_weight = 283975 empty_weight = 283975
reference_datum_position = 0, 0, 0 reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 0, 0 empty_weight_CG_position = -10.0, 0, 0
CG_forward_limit = 0.12 CG_forward_limit = 0.12
CG_aft_limit = 0.34 CG_aft_limit = 0.34
empty_weight_pitch_MOI = 20897456 empty_weight_pitch_MOI = 20897456
@ -59,7 +59,7 @@ max_speed_decreasing_steering_castering = 35
emergency_extension_type = 2 emergency_extension_type = 2
hyd_need_power_to_function= 0 hyd_need_power_to_function= 0
min_castering_angle = 0.05236 min_castering_angle = 0.05236
max_castering_angle = 1.32645 max_castering_angle = 3.142
allow_stopped_steering = 1 allow_stopped_steering = 1
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8 point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8 point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
@ -88,9 +88,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00 RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00 External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
//KH From 5.00, -2.00, -3.00, 0.00, 10.00 //KH From 5.00, -2.00, -3.00, 0.00, 10.00
LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00 LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
//KH From 5.00, 2.00, -3.00, 0.00, 10.0 //KH From 5.00, 2.00, -3.00, 0.00, 10.0
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00 RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
fuel_type = 2 fuel_type = 2
number_of_tank_selectors = 3 number_of_tank_selectors = 3
electric_pump = 0 electric_pump = 0
@ -175,7 +175,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1 lift_coef_flaps = 1
lift_coef_spoilers = 0 lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539 drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.0789 drag_coef_flaps = 0.1339
drag_coef_gear = 0.0549 drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207 drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392 side_force_slip_angle = -0.77392
@ -265,7 +265,7 @@ cruise_lift_scalar = 1
parasite_drag_scalar = 1 parasite_drag_scalar = 1
induced_drag_scalar = 1 induced_drag_scalar = 1
flap_induced_drag_scalar = 1 flap_induced_drag_scalar = 1
elevator_effectiveness = 1 elevator_effectiveness = 1.1
elevator_maxangle_scalar = 1 elevator_maxangle_scalar = 1
aileron_effectiveness = 1 aileron_effectiveness = 1
rudder_effectiveness = 1 rudder_effectiveness = 1
@ -362,7 +362,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.1] [FLAPS.1]
@ -384,7 +384,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.2] [FLAPS.2]

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@ -1,4 +1,4 @@
; TFDi Designs MD-11 (PW4462) vRC1.7.1_PW 24JAN26 ; TFDi Designs MD-11 (PW4462) vRC1.8.0_PW 04FEB26
[MODULAR_MERGE] [MODULAR_MERGE]
auto = true auto = true
@ -6,13 +6,13 @@ auto = true
[VERSION] [VERSION]
//KH Bump major //KH Bump major
major = 4 major = 4
minor = 2 minor = 8
[WEIGHT_AND_BALANCE] [WEIGHT_AND_BALANCE]
max_gross_weight = 630500 max_gross_weight = 630500
empty_weight = 283975 empty_weight = 283975
reference_datum_position = 0, 0, 0 reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 0, 0 empty_weight_CG_position = -10.0, 0, 0
CG_forward_limit = 0.12 CG_forward_limit = 0.12
CG_aft_limit = 0.34 CG_aft_limit = 0.34
empty_weight_pitch_MOI = 20897456 empty_weight_pitch_MOI = 20897456
@ -62,7 +62,7 @@ max_speed_decreasing_steering_castering = 35
emergency_extension_type = 2 emergency_extension_type = 2
hyd_need_power_to_function= 0 hyd_need_power_to_function= 0
min_castering_angle = 0.05236 min_castering_angle = 0.05236
max_castering_angle = 1.32645 max_castering_angle = 3.142
allow_stopped_steering = 1 allow_stopped_steering = 1
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8 point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8 point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
@ -90,10 +90,8 @@ Center3 = 0.00, 0.00, -5.00, 1958.00, 11.00
LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00 LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00 RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00 External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
//KH From 5.00, -2.00, -3.00, 0.00, 10.00 LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00 RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
//KH From 5.00, 2.00, -3.00, 0.00, 10.0
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00
fuel_type = 2 fuel_type = 2
number_of_tank_selectors = 3 number_of_tank_selectors = 3
electric_pump = 0 electric_pump = 0
@ -178,7 +176,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1 lift_coef_flaps = 1
lift_coef_spoilers = 0 lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539 drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.0789 drag_coef_flaps = 0.1339
drag_coef_gear = 0.0549 drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207 drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392 side_force_slip_angle = -0.77392
@ -268,7 +266,7 @@ cruise_lift_scalar = 1
parasite_drag_scalar = 1 parasite_drag_scalar = 1
induced_drag_scalar = 1 induced_drag_scalar = 1
flap_induced_drag_scalar = 1 flap_induced_drag_scalar = 1
elevator_effectiveness = 1 elevator_effectiveness = 1.1
elevator_maxangle_scalar = 1 elevator_maxangle_scalar = 1
aileron_effectiveness = 1 aileron_effectiveness = 1
rudder_effectiveness = 1 rudder_effectiveness = 1
@ -365,7 +363,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.1] [FLAPS.1]
type = 1 type = 1
@ -386,7 +384,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.2] [FLAPS.2]
type = 2 type = 2

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@ -1,4 +1,4 @@
; TFDi Designs MD-11 (PW4462) vRC1.7.1_PW 24JAN26 ; TFDi Designs MD-11 (PW4462) vRC1.8.0_PW 04FEB26
[MODULAR_MERGE] [MODULAR_MERGE]
auto = true auto = true
@ -6,13 +6,13 @@ auto = true
[VERSION] [VERSION]
//KH Bump major //KH Bump major
major = 4 major = 4
minor = 2 minor = 8
[WEIGHT_AND_BALANCE] [WEIGHT_AND_BALANCE]
max_gross_weight = 630500 max_gross_weight = 630500
empty_weight = 283975 empty_weight = 283975
reference_datum_position = 0, 0, 0 reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 0, 0 empty_weight_CG_position = -10.0, 0, 0
CG_forward_limit = 0.12 CG_forward_limit = 0.12
CG_aft_limit = 0.34 CG_aft_limit = 0.34
empty_weight_pitch_MOI = 20897456 empty_weight_pitch_MOI = 20897456
@ -62,7 +62,7 @@ max_speed_decreasing_steering_castering = 35
emergency_extension_type = 2 emergency_extension_type = 2
hyd_need_power_to_function= 0 hyd_need_power_to_function= 0
min_castering_angle = 0.05236 min_castering_angle = 0.05236
max_castering_angle = 1.32645 max_castering_angle = 3.142
allow_stopped_steering = 1 allow_stopped_steering = 1
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8 point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8 point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
@ -91,9 +91,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00 RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00 External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
//KH From 5.00, -2.00, -3.00, 0.00, 10.00 //KH From 5.00, -2.00, -3.00, 0.00, 10.00
LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00 LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
//KH From 5.00, 2.00, -3.00, 0.00, 10.0 //KH From 5.00, 2.00, -3.00, 0.00, 10.0
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00 RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
fuel_type = 2 fuel_type = 2
number_of_tank_selectors = 3 number_of_tank_selectors = 3
electric_pump = 0 electric_pump = 0
@ -178,7 +178,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1 lift_coef_flaps = 1
lift_coef_spoilers = 0 lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539 drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.0789 drag_coef_flaps = 0.1339
drag_coef_gear = 0.0549 drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207 drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392 side_force_slip_angle = -0.77392
@ -268,7 +268,7 @@ cruise_lift_scalar = 1
parasite_drag_scalar = 1 parasite_drag_scalar = 1
induced_drag_scalar = 1 induced_drag_scalar = 1
flap_induced_drag_scalar = 1 flap_induced_drag_scalar = 1
elevator_effectiveness = 1 elevator_effectiveness = 1.1
elevator_maxangle_scalar = 1 elevator_maxangle_scalar = 1
aileron_effectiveness = 1 aileron_effectiveness = 1
rudder_effectiveness = 1 rudder_effectiveness = 1
@ -365,7 +365,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.1] [FLAPS.1]
type = 1 type = 1
@ -386,7 +386,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.2] [FLAPS.2]
type = 2 type = 2

View File

@ -1,4 +1,4 @@
; TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.7.1_GE_F 24JAN26 ; TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.8.0_GE_F 04FEB26
[MODULAR_MERGE] [MODULAR_MERGE]
auto = true auto = true
@ -6,13 +6,13 @@ auto = true
[VERSION] [VERSION]
//KH Bump major //KH Bump major
major = 4 major = 4
minor = 2 minor = 8
[WEIGHT_AND_BALANCE] [WEIGHT_AND_BALANCE]
max_gross_weight = 630500 max_gross_weight = 630500
empty_weight = 248567 empty_weight = 248567
reference_datum_position = 0, 0, 0 reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 0, 0 empty_weight_CG_position = -10.0, 0, 0
CG_forward_limit = 0.12 CG_forward_limit = 0.12
CG_aft_limit = 0.34 CG_aft_limit = 0.34
empty_weight_pitch_MOI = 20897456 empty_weight_pitch_MOI = 20897456
@ -56,7 +56,7 @@ max_speed_decreasing_steering_castering = 35
emergency_extension_type = 2 emergency_extension_type = 2
hyd_need_power_to_function= 0 hyd_need_power_to_function= 0
min_castering_angle = 0.05236 min_castering_angle = 0.05236
max_castering_angle = 1.32645 max_castering_angle = 3.142
allow_stopped_steering = 1 allow_stopped_steering = 1
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8 point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8 point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
@ -85,9 +85,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00 RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00 External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
//KH From 5.00, -2.00, -3.00, 0.00, 10.00 //KH From 5.00, -2.00, -3.00, 0.00, 10.00
LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00 LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
//KH From 5.00, 2.00, -3.00, 0.00, 10.0 //KH From 5.00, 2.00, -3.00, 0.00, 10.0
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00 RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
fuel_type = 2 fuel_type = 2
number_of_tank_selectors = 3 number_of_tank_selectors = 3
electric_pump = 0 electric_pump = 0
@ -172,7 +172,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1 lift_coef_flaps = 1
lift_coef_spoilers = 0 lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539 drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.0789 drag_coef_flaps = 0.1339
drag_coef_gear = 0.0549 drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207 drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392 side_force_slip_angle = -0.77392
@ -262,7 +262,7 @@ cruise_lift_scalar = 1
parasite_drag_scalar = 1 parasite_drag_scalar = 1
induced_drag_scalar = 1 induced_drag_scalar = 1
flap_induced_drag_scalar = 1 flap_induced_drag_scalar = 1
elevator_effectiveness = 1 elevator_effectiveness = 1.1
elevator_maxangle_scalar = 1 elevator_maxangle_scalar = 1
aileron_effectiveness = 1 aileron_effectiveness = 1
rudder_effectiveness = 1 rudder_effectiveness = 1
@ -354,7 +354,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.1] [FLAPS.1]
@ -376,7 +376,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.2] [FLAPS.2]
type = 2 type = 2

View File

@ -1,4 +1,4 @@
; TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.7.1_GE_F 24JAN26 ; TFDi Designs MD-11F (GE CF6-80C2D1F) vRC1.8.0_GE_F 04FEB26
[MODULAR_MERGE] [MODULAR_MERGE]
auto = true auto = true
@ -6,13 +6,13 @@ auto = true
[VERSION] [VERSION]
//KH Bump major //KH Bump major
major = 4 major = 4
minor = 2 minor = 8
[WEIGHT_AND_BALANCE] [WEIGHT_AND_BALANCE]
max_gross_weight = 630500 max_gross_weight = 630500
empty_weight = 248567 empty_weight = 248567
reference_datum_position = 0, 0, 0 reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 0, 0 empty_weight_CG_position = -10.0, 0, 0
CG_forward_limit = 0.12 CG_forward_limit = 0.12
CG_aft_limit = 0.34 CG_aft_limit = 0.34
empty_weight_pitch_MOI = 20897456 empty_weight_pitch_MOI = 20897456
@ -56,7 +56,7 @@ max_speed_decreasing_steering_castering = 35
emergency_extension_type = 2 emergency_extension_type = 2
hyd_need_power_to_function= 0 hyd_need_power_to_function= 0
min_castering_angle = 0.05236 min_castering_angle = 0.05236
max_castering_angle = 1.32645 max_castering_angle = 3.142
allow_stopped_steering = 1 allow_stopped_steering = 1
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8 point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8 point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
@ -85,9 +85,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00 RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00 External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
//KH From 5.00, -2.00, -3.00, 0.00, 10.00 //KH From 5.00, -2.00, -3.00, 0.00, 10.00
LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00 LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
//KH From 5.00, 2.00, -3.00, 0.00, 10.0 //KH From 5.00, 2.00, -3.00, 0.00, 10.0
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00 RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
fuel_type = 2 fuel_type = 2
number_of_tank_selectors = 3 number_of_tank_selectors = 3
electric_pump = 0 electric_pump = 0
@ -172,7 +172,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1 lift_coef_flaps = 1
lift_coef_spoilers = 0 lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539 drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.0789 drag_coef_flaps = 0.1339
drag_coef_gear = 0.0549 drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207 drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392 side_force_slip_angle = -0.77392
@ -262,7 +262,7 @@ cruise_lift_scalar = 1
parasite_drag_scalar = 1 parasite_drag_scalar = 1
induced_drag_scalar = 1 induced_drag_scalar = 1
flap_induced_drag_scalar = 1 flap_induced_drag_scalar = 1
elevator_effectiveness = 1 elevator_effectiveness = 1.1
elevator_maxangle_scalar = 1 elevator_maxangle_scalar = 1
aileron_effectiveness = 1 aileron_effectiveness = 1
rudder_effectiveness = 1 rudder_effectiveness = 1
@ -354,7 +354,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.1] [FLAPS.1]
@ -376,7 +376,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.2] [FLAPS.2]
type = 2 type = 2

View File

@ -1,4 +1,4 @@
; TFDi Designs MD-11F (P&W PW4662) vRC1.7.1_PW_F 24JAN26 ; TFDi Designs MD-11F (P&W PW4662) vRC1.8.0_PW_F 04FEB26
[MODULAR_MERGE] [MODULAR_MERGE]
auto = true auto = true
@ -6,13 +6,13 @@ auto = true
[VERSION] [VERSION]
//KH Bump major //KH Bump major
major = 4 major = 4
minor = 2 minor = 8
[WEIGHT_AND_BALANCE] [WEIGHT_AND_BALANCE]
max_gross_weight = 630500 max_gross_weight = 630500
empty_weight = 248567 empty_weight = 248567
reference_datum_position = 0, 0, 0 reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 0, 0 empty_weight_CG_position = -10.0, 0, 0
CG_forward_limit = 0.12 CG_forward_limit = 0.12
CG_aft_limit = 0.34 CG_aft_limit = 0.34
empty_weight_pitch_MOI = 20897456 empty_weight_pitch_MOI = 20897456
@ -56,7 +56,7 @@ max_speed_decreasing_steering_castering = 35
emergency_extension_type = 2 emergency_extension_type = 2
hyd_need_power_to_function= 0 hyd_need_power_to_function= 0
min_castering_angle = 0.05236 min_castering_angle = 0.05236
max_castering_angle = 1.32645 max_castering_angle = 3.142
allow_stopped_steering = 1 allow_stopped_steering = 1
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8 point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8 point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
@ -85,9 +85,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00 RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00 External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
//KH From 5.00, -2.00, -3.00, 0.00, 10.00 //KH From 5.00, -2.00, -3.00, 0.00, 10.00
LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00 LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
//KH From 5.00, 2.00, -3.00, 0.00, 10.0 //KH From 5.00, 2.00, -3.00, 0.00, 10.0
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00 RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
fuel_type = 2 fuel_type = 2
number_of_tank_selectors = 3 number_of_tank_selectors = 3
electric_pump = 0 electric_pump = 0
@ -172,7 +172,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1 lift_coef_flaps = 1
lift_coef_spoilers = 0 lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539 drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.0789 drag_coef_flaps = 0.1339
drag_coef_gear = 0.0549 drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207 drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392 side_force_slip_angle = -0.77392
@ -262,7 +262,7 @@ cruise_lift_scalar = 1
parasite_drag_scalar = 1 parasite_drag_scalar = 1
induced_drag_scalar = 1 induced_drag_scalar = 1
flap_induced_drag_scalar = 1 flap_induced_drag_scalar = 1
elevator_effectiveness = 1 elevator_effectiveness = 1.1
elevator_maxangle_scalar = 1 elevator_maxangle_scalar = 1
aileron_effectiveness = 1 aileron_effectiveness = 1
rudder_effectiveness = 1 rudder_effectiveness = 1
@ -354,7 +354,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.1] [FLAPS.1]
type = 1 type = 1
@ -375,7 +375,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.2] [FLAPS.2]
type = 2 type = 2

View File

@ -1,4 +1,4 @@
; TFDi Designs MD-11F (P&W PW4662) vRC1.7.1_PW_F 24JAN26 ; TFDi Designs MD-11F (P&W PW4662) vRC1.8.0_PW_F 04FEB26
[MODULAR_MERGE] [MODULAR_MERGE]
auto = true auto = true
@ -6,13 +6,13 @@ auto = true
[VERSION] [VERSION]
//KH Bump major //KH Bump major
major = 4 major = 4
minor = 2 minor = 8
[WEIGHT_AND_BALANCE] [WEIGHT_AND_BALANCE]
max_gross_weight = 630500 max_gross_weight = 630500
empty_weight = 248567 empty_weight = 248567
reference_datum_position = 0, 0, 0 reference_datum_position = 0, 0, 0
empty_weight_CG_position = -13.3, 0, 0 empty_weight_CG_position = -10.0, 0, 0
CG_forward_limit = 0.12 CG_forward_limit = 0.12
CG_aft_limit = 0.34 CG_aft_limit = 0.34
empty_weight_pitch_MOI = 20897456 empty_weight_pitch_MOI = 20897456
@ -56,7 +56,7 @@ max_speed_decreasing_steering_castering = 35
emergency_extension_type = 2 emergency_extension_type = 2
hyd_need_power_to_function= 0 hyd_need_power_to_function= 0
min_castering_angle = 0.05236 min_castering_angle = 0.05236
max_castering_angle = 1.32645 max_castering_angle = 3.142
allow_stopped_steering = 1 allow_stopped_steering = 1
point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8 point.0 = 1, 64.22, 0.00, -17.31, 1500, 0, 1.67, 70, 1.15, 1.183, 0.9, 49, 50, 0, 200, 250, 8
point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8 point.1 = 1, -19.00, -17.15, -18.02, 2000, 1, 2.25, 0, 1.60, 1.116, 0.9, 51, 52, 2, 200, 250, 8
@ -85,9 +85,9 @@ LeftTip = -39.00, -74.00, 0.00, 884.00, 10.00
RightTip = -39.00, 74.00, 0.00, 884.00, 10.00 RightTip = -39.00, 74.00, 0.00, 884.00, 10.00
External1 = -70.00, 0.00, -3.00, 2371.00, 10.00 External1 = -70.00, 0.00, -3.00, 2371.00, 10.00
//KH From 5.00, -2.00, -3.00, 0.00, 10.00 //KH From 5.00, -2.00, -3.00, 0.00, 10.00
LeftAux = 5.00, -2.00, -3.00, 1917.00, 10.00 LeftAux = 5.00, -2.00, -3.00, 1973.00, 10.00
//KH From 5.00, 2.00, -3.00, 0.00, 10.0 //KH From 5.00, 2.00, -3.00, 0.00, 10.0
RightAux = 5.00, 2.00, -3.00, 1917.00, 10.00 RightAux = 5.00, 2.00, -3.00, 1973.00, 10.00
fuel_type = 2 fuel_type = 2
number_of_tank_selectors = 3 number_of_tank_selectors = 3
electric_pump = 0 electric_pump = 0
@ -172,7 +172,7 @@ lift_coef_horizontal_incidence = 0.91357
lift_coef_flaps = 1 lift_coef_flaps = 1
lift_coef_spoilers = 0 lift_coef_spoilers = 0
drag_coef_zero_lift = 0.02539 drag_coef_zero_lift = 0.02539
drag_coef_flaps = 0.0789 drag_coef_flaps = 0.1339
drag_coef_gear = 0.0549 drag_coef_gear = 0.0549
drag_coef_spoilers = 0.05207 drag_coef_spoilers = 0.05207
side_force_slip_angle = -0.77392 side_force_slip_angle = -0.77392
@ -262,7 +262,7 @@ cruise_lift_scalar = 1
parasite_drag_scalar = 1 parasite_drag_scalar = 1
induced_drag_scalar = 1 induced_drag_scalar = 1
flap_induced_drag_scalar = 1 flap_induced_drag_scalar = 1
elevator_effectiveness = 1 elevator_effectiveness = 1.1
elevator_maxangle_scalar = 1 elevator_maxangle_scalar = 1
aileron_effectiveness = 1 aileron_effectiveness = 1
rudder_effectiveness = 1 rudder_effectiveness = 1
@ -354,7 +354,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.1] [FLAPS.1]
type = 1 type = 1
@ -375,7 +375,7 @@ flaps-position.3 = 20, 200, 0.46, 1.1, 0, 0, 0, 1
flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1 flaps-position.4 = 24, 185, 0.48, 1.0, 0, 0, 0, 1
flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0 flaps-position.5 = 28, 177, 0.3, 1.0, 1.5, 0, 0
flaps-position.6 = 35, 160, 0.32, 1 flaps-position.6 = 35, 160, 0.32, 1
flaps-position.7 = 50, 155, 0.54, 1 flaps-position.7 = 50, 155, 0.43, 1
[FLAPS.2] [FLAPS.2]
type = 2 type = 2

View File

@ -32,7 +32,7 @@
/******************************** Constants ********************************/ /******************************** Constants ********************************/
// Module identification // Module identification
#define MODULE_NAME "[KHOFMANN TFDi MD-11 Load Manager] " #define MODULE_NAME "[KHOFMANN TFDi MD-11 Load Manager] "
#define VERSION_STRING "1.14" #define VERSION_STRING "1.15"
// COMM BUS // COMM BUS
#define COMM_BUS_LIVE_DATA_EVENT "khofmann_tfdi_md-11_load_manager_live_data" #define COMM_BUS_LIVE_DATA_EVENT "khofmann_tfdi_md-11_load_manager_live_data"
#define COMM_BUS_UPDATE_TARGET_EVENT "khofmann_tfdi_md-11_load_manager_update_target" #define COMM_BUS_UPDATE_TARGET_EVENT "khofmann_tfdi_md-11_load_manager_update_target"

View File

@ -26,7 +26,7 @@
#define MAX_FUEL(IS_IMPERIAL) ((IS_IMPERIAL) ? (256207) : (116213)) #define MAX_FUEL(IS_IMPERIAL) ((IS_IMPERIAL) ? (256207) : (116213))
#define MAX_FUEL_ER(IS_IMPERIAL) ((IS_IMPERIAL) ? (282619) : (128193)) #define MAX_FUEL_ER(IS_IMPERIAL) ((IS_IMPERIAL) ? (282619) : (128193))
// Arms Shared // Arms Shared
#define ARM_EMPTY -159.6 #define ARM_EMPTY -120.0
#define ARM_PILOT 984.0 #define ARM_PILOT 984.0
#define ARM_FIRST_OFFICER 984.0 #define ARM_FIRST_OFFICER 984.0
#define ARM_ENGINEER 960.0 #define ARM_ENGINEER 960.0