[fltsim.0]
title=F-14D Tomcat
sim=F14D
model=
panel=
sound=
texture=
kb_checklists=Grumman_F14D_check
kb_reference=Grumman_F14D_ref
atc_id=N001
atc_airline=NAVY
atc_flight_number=001
ui_manufacturer="Grumman"
ui_type="F-14D Tomcat"
ui_variation="Last flight"
ui_typerole="Twin Engine Jet"
ui_createdby="Dino Cattaneo"
description="The F-14 Tomcat is a supersonic, twin-engine, variable sweep wing, two-place fighter signed to attack and destroy enemy aircraft at night and in all weather conditions. The F-14 can track up to 24 targets simultaneously with its advanced weapons control system and attack six with Phoenix AIM-54A missiles while continuing to scan the airspace. Armament also ncludes a mix of other air intercept missiles, rockets and bombs."
[General]
atc_type=GRUMMAN
atc_model=F14
editable=0
performance="Function: Carrier-based multi-role strike fighter\nUnit Cost: $38 million\nPropulsion:
Category = airplane
[WEIGHT_AND_BALANCE]
max_gross_weight = 74350.0 // (pounds)
empty_weight = 43500.0 // (pounds)
;Moments of Inertia
empty_weight_roll_MOI= 35000.00
empty_weight_pitch_MOI= 93000.00
empty_weight_yaw_MOI= 95000.00
empty_weight_coupled_MOI= 5000.00
reference_datum_position = 29.00, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -34.20, 0, -0.6 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = 200, -15.0, 0, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.0 = "Pilot"
station_load.1 = 200, -18.5, 0, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.1 = "RIO"
station_load.2 = 190, -33.5, -11.6, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.2 = "1A" // Sidewinder
station_load.3 = 500, -33.5, -9.7, -1.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.3 = "1B" // Sparrow
station_load.4 = 0, -27.5, -1.65, -1.25 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.4 = "3" // Station 3 empty
station_load.5 = 0, -43.5, -1.65, -1.25 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.5 = "4" // Statio 4 empty
station_load.6 = 0, -27.5, 1.65, -1.25 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.6 = "5" // Station 7 empty
station_load.7 = 0, -43.5, 1.65, -1.25 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.7 = "6" // Station 6 empty
station_load.9 = 500, -33.5, 9.7, -1.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.9 = "8A" // LANTIRN
station_load.8 = 190, -33.5, 11.6, 0.0 // Weight(lbs), longitudinal, lateral, vertical positions from datum (feet)
station_name.8 = "8B" // Sidewinder
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
[flight_tuning]
cruise_lift_scalar = 1.6
parasite_drag_scalar = 0.9
induced_drag_scalar = 0.9
elevator_effectiveness = 1.8
aileron_effectiveness = 0.82
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 = -45.8, -2.5, -0.1 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -45.8, 2.5, -0.1 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = 0 //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain = 0.006 //Gain on fuel flow
inlet_area = 6.000 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 16728 //RPM, second stage compressor rated value
static_thrust = 19000 //Lbs, max rated static thrust at Sea Level
afterburner_available = 5 //Afterburner stages available?
afterburner_throttle_threshold = 0.85 //Percent of throttle range where a/b begins
reverser_available = 0 //Thrust reverser available?
ThrustSpecificFuelConsumption = 0.81 //Thrust specific fuel consumption (Jets)
AfterBurnThrustSpecificFuelConsumption = 1.74 //TSFC with afterburn/reheat engaged
[jet_engine]
thrust_scalar = 0.95
//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]
;Gear
point.0=1, -15.00, 0.00, -6.71, 1800, 0, 0.6349, 60.0, 0.3000, 5, 0.500, 9.5, 9.5, 0, 0.0, 0.0
point.1=1, -37.50, -7.4, -7.4, 1800, 1, 0.6349, 0.0, 1.23, 1.7, 0.8, 9.0, 9.0, 2, 0.0, 0.0
point.2=1, -37.50, 7.4, -7.4, 1800, 2, 0.6349, 0.0, 1.23, 1.7, 0.8, 9.0, 9.0, 3, 0.0, 0.0
;Wingtips
point.3=2, -43.30, -32.00, 1.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -43.30, 32.00, 1.00, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
;Bottom
point.5=2, -7.50, 0.00, -1.71, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.6=2, -50.00, -4.80, -4.70, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.7=2, -50.00, 4.80, 4.70, 1000, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
;Top
point.8=2, -18.00, 0.00, 6.10, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
point.9=2, -59.00, -5.2, 9.81, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.10=2,-59.00, 5.2, 9.81, 800, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
static_pitch = 0.0
static_cg_height = 6.5
gear_system_type=1 //Hydraulic
emergency_extension_type=1 //None=0,Pump=1,Gravity=2
[gear_warning_system]
gear_warning_available = 0 //Normal
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 3.0 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
auto_brakes = 0
hydraulic_system_scalar = 1 //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint = -13.8, 0.0, 4.72
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//Lights encoded into MDL file
light.1 = 10, -13.50, 0.00, 4.00, fx_F14_vclight,
light.2 = 10, -19.00, 0.00, 4.00, fx_F14_vclight,
[flaps.0]
type = 2 // 1 - tail, 2 - lead
span-outboard = 0.95 // 0.0 .. 1.0
extending-time = 2.05 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 10 // degrees
flaps-position.2 = 17 // degrees
max_on_ground_position = 1
maneuvering_flaps=0
damaging-speed = 450
[flaps.1]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.95 // 0.0 .. 1.0
extending-time = 2.05 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 17
flaps-position.2 = 35 // degrees
maneuvering_flaps=0
damaging-speed = 450
[Radios]
// Radio Type = available, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 0
Adf.1 = 1
Adf.2 = 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 = 2
attitude_indicator.1 = 2
[altimeters]
altimeter.0 = 1
altimeter.1 = 1
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_m, 1
EngineFire=fx_engfire_f18
[fuel]
Center1= 0.00, 0.00, 1.00,1054.00, 0.00
LeftAux = -34.5, -4.6, -4.0, 575, 0.0 ;Tank 1 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -27.0, 0.0, 2.5, 700, 0.0 ;Tank 2 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -32.0, 0.0, 2.5, 700, 0.0 ;Tank 3 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = -34.5, 4.6, -4.0, 575, 0.0 ;Tank 4 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
electric_pump=1
fuel_dump_rate = 0.0021 //Percent of max quantity per second
[airplane_geometry]
wing_area = 650.5 //Square feet 565sqft+15% to take account of body effect
wing_span = 64.0 //Feet
wing_root_chord = 21.5 //Feet
wing_dihedral = 1.5 //Degrees
wing_incidence = -0.5 //Degrees
wing_twist = -2 //Degrees
oswald_efficiency_factor= 0.85 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 20.0 //Degrees, wing leading edge
wing_pos_apex_lon = -27.7 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_area = 375 //Square feet
htail_span = 21.6 //Feet
htail_pos_lon = -47.6 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0 //Degrees
htail_sweep = 50.0 //Degrees, horizontal tail leading edge
vtail_area = 500 //Square feet
vtail_span = 16 //Feet, tip to body
vtail_sweep = 40.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -42.3 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 4.5 //Feet, vertical distance from reference point, positive going up
elevator_area = 75.0 //Square feet
aileron_area = 27.5 //Square feet
rudder_area = 50.0 //Square feet
elevator_up_limit = 15.5 //Degrees
elevator_down_limit = 12.5 //Degrees
aileron_up_limit = 18.0 //Degrees
aileron_down_limit = 18.0 //Degrees
rudder_limit = 25.0 //Degrees
elevator_trim_limit = 15.0 //Degrees
spoiler_limit = 60.0 //Degrees
spoiler_extension_time = 0.4 //Seconds
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 2 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 5 //Degrees
min_flaps_for_spoilerons= 0.0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available = 0
positive_g_limit_flaps_up = 7.5 //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down= 7.5 //Design G load tolerance (positive, flaps down)
negative_g_limit_flaps_up = -5.0 //Design G load tolerance (negative, flaps up)
negative_g_limit_flaps_down= -5.0 //Design G load tolerance (negative, flaps down)
load_safety_factor = 1.5 //Design G load safety factor
[Reference Speeds]
flaps_up_stall_speed = 134.0 //Knots True (KTAS)
full_flaps_stall_speed = 110.0 //Knots True (KTAS)
cruise_speed = 580.0 //Knots True (KTAS)
max_mach = 1.88
max_indicated_speed = 720 //Red line (KIAS)
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga= 1
pitch_takeoff_ga = 8;
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=27,14
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=11.00
nav_integrator_control=0.20
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=2
stick_shaker=1
[deice_system]
structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots
[Pressurization]
design_cabin_pressure = 10.9 ;PSI (~8000 feet)
max_pressure_differential = 4.96 ;PSI
[folding_wings]
wing_fold_system_type=1 // Available
fold_rates = 0.25,0.25 // Left,Right: 1/sec
[GPWS]
max_warning_height = -1 //No need for GPWS
[VoiceAlerts]
LowFuelPct = 0.1, -1, 60 //Low Fuel limit (percent), Check BELOW, Check every 60 seconds
OverGLimit = 6.0, 1, 1 //High G limit, Check ABOVE, Check every 1 seconds
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[CameraDefinition.0]
Title = "Tail"
Guid = {5D23AC3D-6949-4dae-8FB7-E913545D1641}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = -3, 4.5, -30.5
InitialPbh = 6, 0, 3.4
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
[CameraDefinition.1]
Title = "Side View (left)"
Guid = {E095506E-D7E4-4d4e-B5D2-923B4F9D08FF}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 18.5, 7.5, -6.0
InitialPbh = 25, 0, 280
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
[CameraDefinition.2]
Title = "Side view (right)"
Guid = {4B6E64F5-D9E2-4f08-9295-BBD59B9F9B56}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
ShowWeather = Yes
InitialXyz = -20.5, 10.5, 5.0
InitialPbh = 27, 0, 107
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum
[CameraDefinition.3]
Title = "Cinematic back view 1"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description =Looking forward from over the left wing
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 3, 6.5, -30.5
InitialPbh = 9, 0, -3.4
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
[CameraDefinition.4]
Title = "Cinematic back view 2"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description =Looking forward from over the right wing
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 7, 10.0, -21.0
InitialPbh = 27, 0, -20
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
[CameraDefinition.5]
Title = "Cinematic front view 1"
Guid = {195EAB58-9E4A-2E2A-A34C-A8D9D948F078}
Description =
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 5, 15.0, 22.0
InitialPbh = 35, 0, 185
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
[CameraDefinition.6]
Title = "Cinematic front view 2"
Guid = {765CCF83-D7CD-4486-8983-A5714310CDD5}
Description =
Origin = Center
SnapPbhAdjust = Ordinal
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = -4, 10.5, 30.5
InitialPbh = 17, 0, 175
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
// Modified by James F. Chams @2009.
// =================================
[TailHook]
tailhook_length=4 ;(feet)
tailhook_position=-59.30, 0.0, -2.81, // -48.0, 0.0, -0.81, ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.4
[exits]
number_of_exits=4
exit_rate.0=0.4
exit_rate.1=0.4
exit_rate.2=0.4
exit_rate.3=0.4
