Re: JYAI C-130J Specials
Posted: 04 May 2021, 21:55
by ado4567
// Based on original FDE by Henry Tomkiewicz and modified with thanks.
// ****** Uses C-130H model ****** //
[fltsim.0]
title=JYAI_C130H_Iraq_YI-301
sim=JYAI_Lockheed_C-130J
model=C-130H_open
texture=Iraq_YI-301
prop_anim_ratio=-0.18
atc_airline=Egyptian Air Force
atc_parking_types=MIL_CARGO
atc_parking_codes=16SQ,C130
ui_manufacturer=JYAI
ui_type=Lockheed C-130H Hercules Iraqi
ui_variation=Iraqi Air Force - 23rd transport/utility Sqn, Mohammed Alaa AB. YI-301
description=Repaint by Jim Rodger
[fltsim.1]
title=JYAI_C130H_Iraq_YI-302
sim=JYAI_Lockheed_C-130J
model=C-130H_open
texture=Iraq_YI-302
prop_anim_ratio=-0.18
atc_airline=Egyptian Air Force
atc_parking_types=MIL_CARGO
atc_parking_codes=16SQ,C130
ui_manufacturer=JYAI
ui_type=Lockheed C-130H Hercules Iraqi
ui_variation=Iraqi Air Force - 23rd transport/utility Sqn, Mohammed Alaa AB. YI-302
description=Repaint by Jim Rodger
[fltsim.2]
title=JYAI_C130H_Iraq_YI-303
sim=JYAI_Lockheed_C-130J
model=C-130H_closed
texture=Iraq_YI-303
prop_anim_ratio=-0.18
atc_airline=Egyptian Air Force
atc_parking_types=MIL_CARGO
atc_parking_codes=16SQ,C130
ui_manufacturer=JYAI
ui_type=Lockheed C-130H Hercules Iraqi
ui_variation=Iraqi Air Force - 23rd transport/utility Sqn, Mohammed Alaa AB. YI-303
description=Repaint by Jim Rodger
[General]
atc_type=SILENT
atc_model=C130
editable=1
performance=AI Aircraft
Category=airplane
[WEIGHT_AND_BALANCE]
empty_weight=71000
max_gross_weight=155000
reference_datum_position=0.0, 0.0, 0.0 // (feet)
empty_weight_CG_position=4.8, 0.0, 0.0 // (feet)
max_number_of_stations=50
station_load.0 = "170.0, 31.0, -1.5, 0.0, Pilot"
station_load.1 = "170.0, 31.0, 1.5, 0.0, Co-Pilot"
station_load.2 = "510.0, 25.0, 0.0, 0.0, Crew"
station_load.3 = "7000.0, 5.0, 0.0, 0.0, Payload"
;Moments of Inertia
empty_weight_pitch_MOI=1000000
empty_weight_roll_MOI=696271
empty_weight_yaw_MOI=1289428
empty_weight_coupled_MOI=0
[GeneralEngineData]
engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0= -5.0, -33.8, 4.0 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1= -5.0, -16.8, 4.0
Engine.2= -5.0, 16.8, 4.0
Engine.3= -5.0, 33.8, 4.0
fuel_flow_scalar=1.00 //Scalar for fuel flow efficiency
min_throttle_limit= -0.30
[propeller]
thrust_scalar = 1.0 //Propeller thrust scalar
propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter = 13.0 //Propeller Diameter, (feet)
propeller_blades = 4 //Number of propeller blades
propeller_moi = 100 //Propeller moment of inertia
beta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min = 12 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm = 25520 //Miminum governed RPM
prop_tc = 0.004 //Prop time-constant
gear_reduction_ratio = 17.0 //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 = 0.9 //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 = -14.0 //Minimum pitch angle in reverse, (degrees)
[TurbineEngineData]
fuel_flow_gain = 0.011 //Gain on fuel flow
inlet_area = 1.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 6000 //Lbs, max rated static thrust at Sea Level
[turboprop_engine]
power_scalar = 1.0 //Scalar on Turboprop power
maximum_torque = 12000 //Maximum torque available (ft-lbs)
[SMOKESYSTEM]
smoke.0= -5.0, -33.8, 4.0, fx_smoke_r
smoke.1= -5.0, -16.8, 4.0, fx_smoke_r
smoke.2= -5.0, 16.8, 4.0, fx_smoke_r
smoke.3= -5.0, 33.8, 4.0, fx_smoke_r
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=0.7
induced_drag_scalar=1.0
elevator_effectiveness=0.7
aileron_effectiveness=1.7
rudder_effectiveness=1.0
pitch_stability=1.9
roll_stability=0.4
yaw_stability=1.0
elevator_trim_effectiveness=1.8
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 17.0
autopilot=0, 5 , 17.0
avionics_bus=0, 10, 17.0
avionics=1, 5 , 17.0
pitot_heat=0, 2 , 17.0
additional_system=0, 20, 17.0
marker_beacon=1, 2 , 17.0
gear_warning=0, 2 , 17.0
fuel_pump=0, 5 , 17.0
starter1=0, 20, 17.0
light_nav=0, 5 , 17.0
light_beacon=0, 5 , 17.0
light_landing=0, 5 , 17.0
light_taxi=0, 5 , 17.0
light_strobe=0, 5 , 17.0
light_panel=0, 5 , 17.0
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[contact_points]
point.0=1, 29.80, 0.00, -9.0, 5000, 0, 1.60, 80.0, 0.8, 0.8, 0.5, 11, 11, 0, 0, 0
point.1=1, -4.50, -7.00, -9.1, 5000, 1, 1.60, 0.0, 0.8, 0.8, 0.5, 7, 7, 2, 0, 0
point.2=1, -4.50, 7.00, -9.1, 5000, 2, 1.60, 0.0, 0.8, 0.8, 0.5, 7, 7, 3, 0, 0
static_pitch=-0.167
static_cg_height=8.287
gear_system_type=0
[Views]
eyepoint=35.0, -1.20, 5.0
[flaps.0]
type=1
span-outboard=0.8
extending-time=10
flaps-position.0=0
flaps-position.1=5
flaps-position.2=15
flaps-position.3=25
flaps-position.4=40
damaging-speed=250
blowout-speed=300
lift_scalar=0.5
drag_scalar=0.5
pitch_scalar=0.0
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator=150, 250
aileron=150, 250
rudder=150, 250
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type=4
direction_indicator.0=3,0
[Lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=taxi
light.0= 1, -48.50, 0.00, 30.00, fx_strobeh, // Upper Strobe
light.1= 1, 23.50, 0.00, -7.00, fx_strobeh, // Lower Strobe
light.2= 3, 0.20, -66.30, 7.00, fx_navredm, // LH Nav Light
light.3= 3, 0.20, 66.30, 7.00, fx_navgrem, // RH Nav Light
light.4= 3, -58.30, 0.00, 6.10, fx_navwhi, // Rear Nav Light
light.5=5, 1.00, -66.30, 7.00, fx_landing, // LH Wingtip Landing Light
light.6=5, 1.00, 66.30, 7.00, fx_landing, // RH Wingtip Landing Light
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
LeftMain=0,-16,0,1605,0
LeftAux=0,-20,0,1662,0
RightMain=0,16,0,1605,0
RightAux=0,20,0,1662,0
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=1
[airplane_geometry]
wing_area=2200
wing_span=125
wing_root_chord=20.0
wing_dihedral=3.0
wing_incidence=3.0
oswald_efficiency_factor=0.7
wing_twist=0.0
wing_winglets_flag=0
wing_sweep=20.0
wing_pos_apex_lon=8.0
wing_pos_apex_vert=0.0
htail_area=338.0
htail_span=52.0
htail_pos_lon=-50.0
htail_pos_vert=0.0
htail_incidence=0.0
htail_sweep=0.0
vtail_area=224.0
vtail_span=20.0
vtail_sweep=20.0
vtail_pos_lon=-40.0
vtail_pos_vert=3.0
elevator_area=80.0
aileron_area=52.28
rudder_area=58.0
elevator_up_limit=27.0
elevator_down_limit=20.0
aileron_up_limit=19.0
aileron_down_limit=14.0
rudder_limit=23.0
elevator_trim_limit=19.0
spoiler_limit=90.0
spoilerons_available=0
aileron_to_spoileron_gain=0.0
min_ailerons_for_spoilerons=0.0
min_flaps_for_spoilerons=0.0
[Reference Speeds]
flaps_up_stall_speed=117
full_flaps_stall_speed=96
cruise_speed=340
max_indicated_speed=320
max_mach=0.6
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
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=0.000000
[brakes]
toe_brakes_scale=0.8
parking_brake=1
[gear_warning_system]
gear_warning_available=1
[hydraulic_system]
electric_pumps=1
engine_map=1,1,1,1
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0