// Douglas A4-C Skyhawk (updated 09 jan 2005)
[fltsim.0]
title=Douglas A-4C VA-66
sim=Skyhawk-1a
model=
panel=
sound=
texture=
checklists=
description=The A4D-2N flew for the first time on August 21, 1958. It first became operational in February of 1960, with the Marine Corps squadron VMA-225. 638 A4D-2Ns were built.The A4D-2N was redesignated A-4C in September of 1962. At that time, the A4D-2N was still in production. During the production run of the A-4C, the production line was moved from the El Segundo plant to the Long Beach plant, with final assembly being done at a government-owned plant in Palmdale, California. This move was carried out in several stages during 1963.
ui_manufacturer=Douglas
ui_type=A-4C U.S. NAVY
ui_variation=VA-66
atc_airline=Navy
atc_id=NAVY 220
atc_flight_number=300
visual_damage=1
FSInn_IDVers=2
FSInn_IDModel=42895E87
FSInn_IDTexture=0
[fltsim.1]
title=Douglas A-4C VA-216 Iron Hand
sim=Skyhawk-1a
model=1
panel=
sound=
texture=1
checklists=
description=The A4D-2N flew for the first time on August 21, 1958. It first became operational in February of 1960, with the Marine Corps squadron VMA-225. 638 A4D-2Ns were built.The A4D-2N was redesignated A-4C in September of 1962. At that time, the A4D-2N was still in production. During the production run of the A-4C, the production line was moved from the El Segundo plant to the Long Beach plant, with final assembly being done at a government-owned plant in Palmdale, California. This move was carried out in several stages during 1963.
ui_manufacturer=Douglas
ui_type=A-4C1 U.S. NAVY
ui_variation=VA-216 Iron Hand
atc_airline=Navy
atc_id=689
atc_flight_number=600
visual_damage=1
FSInn_IDVers=2
FSInn_IDModel=162F0C5E
FSInn_IDTexture=0
[fltsim.2]
title=Douglas A-4C VMF-324
sim=Skyhawk-1a
model=
panel=
sound=
texture=2
checklists=
description=The A4D-2N flew for the first time on August 21, 1958. It first became operational in February of 1960, with the Marine Corps squadron VMA-225. 638 A4D-2Ns were built.The A4D-2N was redesignated A-4C in September of 1962. At that time, the A4D-2N was still in production. During the production run of the A-4C, the production line was moved from the El Segundo plant to the Long Beach plant, with final assembly being done at a government-owned plant in Palmdale, California. This move was carried out in several stages during 1963.
ui_manufacturer=Douglas
ui_type=A-4C U.S. MARINES CORP
ui_variation=VMF-324
atc_airline=Navy
atc_id=685
atc_flight_number=610
visual_damage=1
FSInn_IDVers=2
FSInn_IDModel=42895E87
FSInn_IDTexture=0
[fltsim.3]
title=Douglas A4C VA-66 Iron Hand
sim=Skyhawk-1a
model=1
panel=
sound=
texture=
checklists=
description=The A4D-2N flew for the first time on August 21, 1958. It first became operational in February of 1960, with the Marine Corps squadron VMA-225. 638 A4D-2Ns were built.The A4D-2N was redesignated A-4C in September of 1962. At that time, the A4D-2N was still in production. During the production run of the A-4C, the production line was moved from the El Segundo plant to the Long Beach plant, with final assembly being done at a government-owned plant in Palmdale, California. This move was carried out in several stages during 1963.
ui_manufacturer=Douglas
ui_type=A-4C U.S. NAVY
ui_variation=VA-66 Iron Hand
atc_airline=Navy
atc_id=685
atc_flight_number=610
visual_damage=1
FSInn_IDTexture=0
FSInn_IDVers=2
FSInn_IDModel=162F0C5E
[fltsim.4]
title=Douglas A-4C VMF-324 Iron Hand
sim=Skyhawk-1a
model=1
panel=
sound=
texture=2
checklists=
description=The A4D-2N flew for the first time on August 21, 1958. It first became operational in February of 1960, with the Marine Corps squadron VMA-225. 638 A4D-2Ns were built.The A4D-2N was redesignated A-4C in September of 1962. At that time, the A4D-2N was still in production. During the production run of the A-4C, the production line was moved from the El Segundo plant to the Long Beach plant, with final assembly being done at a government-owned plant in Palmdale, California. This move was carried out in several stages during 1963.
ui_manufacturer=Douglas
ui_type=A-4C U.S. MARINES CORP
ui_variation=VMF-324 Iron Hand
atc_airline=Navy
atc_id=685
atc_flight_number=610
visual_damage=1
FSInn_IDVers=2
FSInn_IDModel=162F0C5E
FSInn_IDTexture=0
[fltsim.5]
title=Douglas A-4C VA-216
sim=Skyhawk-1a
model=
panel=
sound=
texture=1
checklists=
description=The A4D-2N flew for the first time on August 21, 1958. It first became operational in February of 1960, with the Marine Corps squadron VMA-225. 638 A4D-2Ns were built.The A4D-2N was redesignated A-4C in September of 1962. At that time, the A4D-2N was still in production. During the production run of the A-4C, the production line was moved from the El Segundo plant to the Long Beach plant, with final assembly being done at a government-owned plant in Palmdale, California. This move was carried out in several stages during 1963.
ui_manufacturer=Douglas
ui_type=A-4C U.S. NAVY
ui_variation=VA-216
atc_airline=Navy
atc_id=689
atc_flight_number=600
visual_damage=1
FSInn_IDTexture=0
FSInn_IDVers=2
FSInn_IDModel=42895E87
[General]
performance=Length : 40 ft 3 in\nWing span : 27 ft 6 in\nWeight : 9,146lbs (Empty)15,359 pounds combat weight 17,535 pounds gross, 22,500 pounds maximum. Armament: Two 20-mm cannon with 100 rpg. 3 underwing pylons.
\nSpeed : Maximum speed 649 mph at 4000 feet Cruising speed 493 mph. Stalling speed 137 mph. Combat ceiling 44,000 feet(clean).\n Engine: One Wright J65-W-20 turbojet, rated at 8400 lb.s.t.\nOriginal Designer: Ronald Zambrano M\n(radzamb@hotmail.com)
atc_type=SKYHAWK
atc_model=A4
[WEIGHT_AND_BALANCE]
max_gross_weight = 22500.0 // (pounds)
empty_weight = 9142.0 // (pounds)
reference_datum_position=0.000, 0.000, 0.000
empty_weight_CG_position=0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.00,0.00,0.00,0.00
empty_weight_pitch_MOI=40000 // 154663.770
empty_weight_roll_MOI= 12000 // 19777.370
empty_weight_yaw_MOI= 30000 // 134102.200
empty_weight_coupled_MOI=0
CG_forward_limit=0.000
CG_aft_limit=1.000
[electrical]
max_battery_voltage = 25.0
generator_alternator_voltage = 28
max_generator_alternator_amps = 100.0
// BusType, MaxAmpLoad, MinVoltage
// BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
avionics_bus = 0, 5 , 9.5
avionics = 1, 5 , 9.5
additional_system = 0, 2 , 9.5
marker_beacon = 1, 2 , 9.0
fuel_pump = 0, 5 , 9.0
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -4, -13, 1.25, fx_navredm ,
light.1=3, -4, 13, 1.25, fx_navgrem ,
light.2=2, -0.63, 0.0, 5.3, fx_beaconb ,
light.3=4, 10, 0.00, 5.50, fx_vclight ,
light.4=3, -4, -3.6, -0.9, fx_navredm ,
[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
[GeneralEngineData]
engine_type = 1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -10.0, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain = 0.0025 //Gain on fuel flow
inlet_area = 1.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 12353 //RPM, second stage compressor rated value
static_thrust = 8400 //Lbs, max rated static thrust at Sea Level
afterburner_available = 0 //Afterburner available?
reverser_available = 0 //Thrust reverser available?
[jet_engine]
thrust_scalar = 1.0
//0 Class
//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
[contact_points]
point.0=1, 10.20, 0.00, -6.00, 2000.00, 0.00, 0.78, 15.00, 0.28, 3.20, 1.60, 5.00, 5.00, 0.00, 0.00, 0.00
point.1=1, -1.25, -4.20, -5.35, 2000.00, 1.00, 1.10, 0.00, 0.90, 2.50, 0.68, 5.00, 5.00, 2.00, 0.00, 0.00
point.2=1, -1.25, 4.20, -5.35, 2000.00, 2.00, 1.10, 0.00, 0.90, 2.50, 0.68, 5.00, 5.00, 3.00, 0.00, 0.00
point.3=2, -8.00,-13.83, -1.33, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00
point.4=2, -8.00, 13.83, -1.33, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00
point.5=2,-18.67, 0.00, -1.00, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00
point.6=2, 18.58, 0.00, -0.50, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00
static_pitch=5.861694
static_cg_height=4.7
gear_system_type=1 // 0
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 25.5 //Flap angle that activates warning at idle
flap_limit_power = 5.04 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.0 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,0,0,0 //pumps on Eng1,2
[Views]
// longitunal, lateral, vertical distance from reference datum
eyepoint=10.43, 0.00, 4.83
[Flaps.0]
type=1
span-outboard=0.50
extending-time=5.00
system_type=0
flaps-position.0= 0.00,0.00
flaps-position.1=20.00,0.00
flaps-position.2=40.00,0.00
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 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
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1 =0.00,0.00,0.00,230.00,5.00
LeftMain=-0.50,-3.0,-0.2,280.00,5.0
RightMain=-0.50,3.0,-0.2,280.00,5.0
LeftTip =0.00, -7.0, -1.5, 295.0, 5.0
RightTip =0.00, 7.0, -1.5, 295.0, 5.0
fuel_type=2.00
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=260.00
wing_span=27.50
wing_root_chord=12.5
wing_dihedral=2.0
wing_incidence=0.00
wing_twist=2
oswald_efficiency_factor=0.6
wing_winglets_flag=0
wing_sweep=40
wing_pos_apex_lon=5.3
wing_pos_apex_vert=0.8
htail_area=49.00
htail_span=11.33
htail_pos_lon=-12.00
htail_pos_vert=6.00
htail_incidence=-1.0
htail_sweep=40
vtail_area=60.00
vtail_span=10.062258
vtail_sweep=45.00
vtail_pos_lon=-15.00
vtail_pos_vert=8.33
elevator_area=7.50
aileron_area=5.720000
rudder_area=6.800000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.00
min_ailerons_for_spoilerons=0.00
min_flaps_for_spoilerons=0.00
[Reference Speeds]
flaps_up_stall_speed = 120.0 //Knots True (KTAS)
full_flaps_stall_speed = 100.0 //Knots True (KTAS)
cruise_speed = 464.0 // 310 //Knots True (KTAS)
max_mach = 1.2
max_indicated_speed=863.281250
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 2000.0
autothrottle_available= 0
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 0
pitch_takeoff_ga = 12
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=30.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[forcefeedback]
stick_shaker_magnitude=5000 ; 0 - 10000
stick_shaker_direction=0 ; 0 - 35999 degrees
stick_shaker_period=111111 ; in microseconds
gear_bump_nose_magnitude=3000 ; 0 - 10000
gear_bump_nose_direction=18000 ; 0 - 35999 degrees
gear_bump_nose_duration=250000 ; in microseconds
gear_bump_left_magnitude=2700 ; 0 - 10000
gear_bump_left_direction=9000 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=27000 ; 0 - 35999 degrees
gear_bump_right_duration=250000 ; in microseconds
ground_bumps_magnitude1=1300 ; 0 - 10000
ground_bumps_angle1=08900 ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200 ; 0 - 10000
ground_bumps_angle2=09100 ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000 ; 0 - 10000
crash_direction1=01000 ; 0 - 35999 degrees
crash_magnitude2=10000 ; 0 - 10000
crash_direction2=9000 ; 0 - 35999 degrees
crash_period2=75000 ; in microseconds
crash_duration2=2500000 ; in microseconds
[stall_warning]
type=1
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position=-23.6, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0
