Thanks for the reply. The current retardant drop is configured on the smoke system. I would like to change it because when the throttles are full, it triggers the smoke system on and a retardant drop is made. If I could configure it to a light, I could map that light on the control page to a button on my joystick. Here is the aircraft.cfg for the Captain Sim C-130 (Minus the Camera Definitions due to over max characters)
Thanks for your help with this!
[fltsim.0]
title=CS C130Extra2 0
sim=C130
model=9
panel=
sound=
texture=fra
kb_checklists=
kb_reference=
atc_id=FAF
atc_airline=FAF
atc_flight_number=
ui_manufacturer=Lockheed
ui_type="C-130H"
ui_variation="French AF"
ui_typerole="Multi-Engine TurboProp"
ui_createdby="Captain Sim"
description="'C-130 X-perience' Pro Pack v.1.3\n(c) 2008 Captain Sim
www.captainsim.com"
flg="France"
[fltsim.1]
title=CS C130Extra2 1
sim=C130
model=10
panel=
sound=
texture=jap
kb_checklists=
kb_reference=
atc_id=JAF
atc_airline=JAF
atc_flight_number=
ui_manufacturer=Lockheed
ui_type="C-130H"
ui_variation="Japan AF"
ui_typerole="Multi-Engine TurboProp"
ui_createdby="Captain Sim"
description="'C-130 X-perience' Pro Pack v.1.3\n(c) 2008 Captain Sim
www.captainsim.com"
flg="Japan"
[fltsim.2]
title=CS C130Extra2 2
sim=C130
model=14
panel=
sound=
texture=us_space
kb_checklists=
kb_reference=
atc_id=USSG
atc_airline=USSC
atc_flight_number=
ui_manufacturer=Lockheed
ui_type="NC-130"
ui_variation="US Space Command"
ui_typerole="Multi-Engine TurboProp"
ui_createdby="Captain Sim"
description="'C-130 X-perience' Pro Pack v.1.3\n(c) 2008 Captain Sim
www.captainsim.com"
flg="USA"
[fltsim.3]
title=CS C130Extra2 XX
sim=C130
model=10g
panel=g
sound=
texture=MAFFS2
kb_checklists=
kb_reference=
atc_id=130
atc_airline=MAFFS
atc_flight_number=2
ui_manufacturer=Lockheed
ui_type="C-130H3"
ui_variation="302d AW, 731st/52nd Airlift Squadron, MAFFS2, Peterson AFB, CO"
ui_typerole="Multi-Engine TurboProp"
ui_createdby="Captain Sim"
description="'C-130 X-perience' Pro Pack v.1.3\n(c) 2008 Captain Sim
www.captainsim.com"
flg="USA Marines"
[General]
atc_type=Hercules
atc_model=C130
editable=1
performance=See Flight Manual
Category=airplane
[weight_and_balance]
max_gross_weight=174000
empty_weight=75600
reference_datum_position=0, 0, 0
empty_weight_CG_position=-2, 0, -8
empty_weight_pitch_MOI=4000000
empty_weight_roll_MOI=4500000
empty_weight_yaw_MOI=6500000
empty_weight_coupled_MOI=0
max_number_of_stations=8
station_load.0="200, 34, -2, -7, Captain"
station_load.1="200, 34, 2, -7, First Officer"
station_load.2="200, 31, 0, -7, Second Officer"
station_load.3="200, 29, 3, -7, Navigator"
station_load.4="200, 25, 0, -9, Flight Engeneer"
;------------ ENGINES -------------------------------
[GeneralEngineData]
engine_type=5
fuel_flow_scalar=0.46 ;H:fuel_flow_scalar(0.487)
engine.0=10, -34.1, -4
engine.1=10, -16.85, -4
engine.2=10, 16.85, -4
engine.3=10, 34.1, -4
min_throttle_limit=-0.22
[TurbineEngineData]
fuel_flow_gain=0.02
inlet_area=1.0
rated_N2_rpm=29920
static_thrust=158
afterburner_available=0
reverser_available=1
[turboprop_engine]
power_scalar=1.0
maximum_torque=19600 ;H:maximum_torque(23030)
powerspecificfuelconsumption=1
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=13 //Propeller Diameter, (feet)
propeller_blades=4 //Number of propeller blades
propeller_moi=23 //Propeller moment of inertia
beta_max=50 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=8 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25520 //Miminum governed RPM
prop_tc=0.008 //Prop time-constant
gear_reduction_ratio=15.4 //Propeller gear reduction ratio
fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=700 //Minimum RPM for prop feathering
beta_feather=79.3 //Feathering pitch angle (degrees)
power_absorbed_cf=0.95 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-6.0 //Minimum pitch angle in reverse, (degrees)
;------------ END of ENGINES -------------------------------
[fuel]
fuel_type=2
number_of_tank_selectors=4
electric_pump=1
fuel_dump_rate=0.00085
engine_driven_pump=0
External1= -0.75, -25.49, -7.03, 1400.00, 10 // EXT Left
LeftAux= -0.75, -25.49, -2.03, 910.00, 9 // Aux Left
LeftTip= 0.00, -16.86, -2.09, 1350.00, 10 // Tank 1
Center2= 13.64, 0.00, -4.19, 1240.00, 10 // Tank 2
Center3= -20.95, 0.00, -4.19, 1240.00, 10 // Tank 3
RightTip= 0.00, 16.86, -2.09, 1350.00, 10 // Tank 4
RightAux= -0.75, 25.49, -2.03, 910.00, 9 // Aux Right
External2= -0.75, 25.49, -7.03, 1400.00, 10 // Ext Right
[contact_points]
static_pitch=-0.4
static_cg_height=17.3
max_number_of_points=14
point.0=1, 30.21, 0.0, -17.30, 1500, 0, 1.46, 65, 0.30, 1.20, 0.7, 9, 8, 0, 250, 300
point.1=1, -10.00, -7.2, -18.05, 2000, 1, 2.25, 0, 1.60, 0.80, 0.9, 11, 9, 2, 220, 250
point.2=1, -10.00, 7.2, -18.05, 2000, 2, 2.25, 0, 1.60, 0.80, 0.9, 11, 9, 3, 220, 250
point.3=2, 0, -66.5065, -0.98, 700, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4=2, 0, 66.5209, -0.98, 700, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5=2, 41.8013, 0, -10.6646, 700, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6=2, 35.5844, 0, -14.2174, 700, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7=2, 27.9076, 0, -15.4425, 700, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.8=2, -13.0022, 0, -15.4035, 700, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.9=2, -58.327, 0, -2.1478, 700, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.10=2, -49.121, 0, 21.6318, 700, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.11=2, 42.4571, 0, -1.9023, 700, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.12= 5, -30.90, -5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.0, 1.2, 0, 0.0, 0.0
point.13= 5, -30.90, 5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.1, 1.5, 0, 0.0, 0.0
gear_system_type=0
[lights]
; X, Z, Y
light.1 = 6, 3.0, -8.10, -15.50, cs130_taxi //right
light.2 = 6, 3.0, 8.10, -15.50, cs130_taxi //left
light.3 = 7, 6.00, 18.7, -7.4, cs130_landing //right1
light.4 = 7, 9.00, 23.90, -4.00, cs130_landing //right2
light.5 = 5, 6.00, -18.4, -7.4, cs130_landing //left1
light.6 = 5, 9.00, -23.90, -4.00, cs130_landing //left2
light.7 = 8, 9, 14.50, -2.50, cs130_edge2 //right
light.8 = 8, 9, -14.50, -2.50, cs130_edge2 //left
light.9 =4, 33.00, 0.00, -6.00, cs130_vcwt
light.10 =4, 27.00, -1.00, -5.00, cs130_vcwt
[smokesystem]
smoke.0=-8,-34, 0, cs130_smoke
smoke.1=-9,-17, 0, cs130_smoke
smoke.2=-9, 17, 0, cs130_smoke
smoke.3=-8, 34, 0, cs130_smoke
[effects]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
startup=cs130_engstart, 1
[keyboard_response]
elevator=150, 250
aileron=150, 250
rudder=150, 250
[forcefeedback]
gear_bump_nose_magnitude=3000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=2700
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=2700
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=1300
ground_bumps_angle1=08900
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200
ground_bumps_angle2=09100
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000
[airplane_geometry]
wing_area=2750
wing_span=134
wing_root_chord=14.60
wing_dihedral=1
wing_incidence=0
wing_twist=0
oswald_efficiency_factor=0.99
wing_winglets_flag=0
wing_sweep=0
wing_pos_apex_lon=3.6
wing_pos_apex_vert=-2
htail_area=610
htail_span=55.20
htail_pos_lon=-42.2
htail_pos_vert=-2
htail_incidence=0.0
htail_sweep=0
vtail_area=400
vtail_span=24.80
vtail_sweep=0
vtail_pos_lon=-32.68
vtail_pos_vert=-2.01
elevator_area=232
aileron_area=200
rudder_area=230
elevator_up_limit=25
elevator_down_limit=15
aileron_up_limit=25
aileron_down_limit=15
rudder_limit=31.5
elevator_trim_limit=25
spoiler_limit=45
aileron_to_spoileron_gain=0
min_ailerons_for_spoilerons=0
min_flaps_for_spoilerons=0
spoilerons_available=0
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[Reference Speeds]
flaps_up_stall_speed=120.0
full_flaps_stall_speed=92.0
cruise_speed=340.0
max_indicated_speed=350.0
max_mach=0.64
[electrical]
max_battery_voltage=24
generator_alternator_voltage=28
max_generator_alternator_amps=60
electric_always_available=1
autopilot=0, 5, 17
avionics_bus=0, 10, 17
avionics=1, 5, 17
gear_warning=0, 2, 17
fuel_pump=0, 5, 17
fuel_transfer_pump = 0, 5, 17
light_nav=0, 5, 17
light_beacon=0, 5, 17
light_landing=0, 5, 17
light_taxi=0, 5, 17
light_strobe=0, 5, 17
light_panel=0, 5, 17
[flaps.0]
type=1
span-outboard=0.8
extending-time=13
flaps-position.0=0
flaps-position.1=3.5
flaps-position.2=7
flaps-position.3=14
flaps-position.4=17.5
flaps-position.5=21
flaps-position.6=24.5
flaps-position.7=28
flaps-position.8=31.5
flaps-position.9=35
damaging-speed=200
blowout-speed=250
lift_scalar=0.7
drag_scalar=0.99
pitch_scalar=0.9
system_type=1
[flaps.1]
type=2
span-outboard=0.8
extending-time=10
flaps-position.0=0
flaps-position.1=1.0
flaps-position.2=1.0
flaps-position.3=1.0
flaps-position.4=1.0
flaps-position.5=1.0
flaps-position.6=1.0
flaps-position.7=1.0
flaps-position.8=1.0
flaps-position.9=1.0
damaging-speed=250
blowout-speed=300
lift_scalar=0.3
drag_scalar=0.1
pitch_scalar=0.1
system_type=1
[exits]
number_of_exits=4
exit_rate.0=0.4
exit_rate.1=0.4
exit_rate.2=0.4
exit_rate.3=10000
[Radios]
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1, 0, 1
Nav.2=1, 0, 1
Adf.1=1
Transponder.1=1
Marker.1=1
[Views]
eyepoint=32.05, -1.63, -5.28
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=0
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8
use_no_default_bank=1
use_no_default_pitch=1
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=1.000000
default_pitch_mode=0
default_bank_mode=0
[direction_indicators]
direction_indicator.0=3,0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.2
flap_limit_idle=0
flap_limit_power=27
[brakes]
toe_brakes_scale=1.00
parking_brake=1
auto_brakes=4
[hydraulic_system]
normal_pressure=3000.000000
electric_pumps=0
engine_map=1,1,1,1
[stall_warning]
type=1
stick_shaker=1
[pitot_static]
vertical_speed_time_constant=1
pitot_heat=1.000000
[TailHook]
tailhook_length=1
tailhook_position=0,0,0,
cable_force_adjust=0.00001
[folding_wings]
wing_fold_system_type=4
fold_rates=0.20
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=2
[GPWS]
max_warning_height = 1000
sink_rate_fpm = -1500
excessive_sink_rate_fpm = -2000
climbout_sink_rate_fpm = -100
flap_and_gear_sink_rate_fpm= -100