[fltsim.0]
title=JELAIR - Ford LTD Country Squire 1979
sim=Ford_LTD-CountrySquire-1979

ui_manufacturer="JELAIR - CarCenter"
ui_type="Ford LTD Country Squire"
ui_variation="1979"

model=
panel=
sound=
texture=

checklists=
description=RWD (RearWheelDrive), Automatic transmission & Enormous driving-pleasure signifies the Squire. Jacob Larsen.

[General]
performance=Length 5.453m (17.9 feet), Height 1.443m (4.74 feet), Width 2.009m (6.6 feet), Weight 1.709 ton (3768 lbs), Engine V8cyl-5.8ltr (5732 cc, 349.788 cu.in (called a '351' engine), 716.5 cc/cylinder) OHV (OverHead Valve), 142 HorsePower (net-rating) at 3200 rpm, topspeed 170 km/h\/t, 0-100 km/h (0-60 mph) 10.0s, Fuel 76 liter (20.1 US gallon)
Category=airplane

[WEIGHT_AND_BALANCE]
reference_datum_position=0.0, 0.0, 0.0
//ref-point is centered at the: center, top, rear
//from this point use pos-numbers when going forward, and neg-numbers when going down
//from this point neg-numbers are RED wing (left or captain-side), and pos-numbers are GREEN wing (right or pilot-side)

//empty_weight_CG_position=9.85, 0.0, -3.0 //CoG right betwheen the wheel-sets and slightly above
empty_weight_CG_position=11.5, 0.0, -3.0 //CoG for more correct handling (under-steering)
//assumed CoG from images

empty_weight=3768
max_gross_weight=5000.000000

;Moments of Inertia
empty_weight_roll_MOI=15500.000000
empty_weight_pitch_MOI=15500.000000
empty_weight_yaw_MOI=7500 //13500.000000
empty_weight_coupled_MOI=0.000000

max_number_of_stations=10
//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

station_load.0="137, 9.8, -1.5, -2.4, Driver"
station_load.1="0,   9.8,  0.0, -2.4, front-center passanger"
station_load.2="126, 9.8,  1.5, -2.4, front-right passanger"

station_load.3="0, 7.3, -1.5, -2.4, rear-left passenger"
station_load.4="0, 7.3,  0.0, -2.4, rear-center passenger"
station_load.5="0, 7.3,  1.5, -2.4, rear-right passenger"

station_load.6="0, 2.6, -1.5, -2.5, back-left passenger"
station_load.7="0, 2.6,  1.5, -2.5, back-right passenger"

station_load.8="0, 3.9,  0.0, -2.0, inside cargo"
station_load.9="0, 4.9,  0.0,  1.0, rooftop-carrier cargo"



[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) 

Center1=2.5, 0.0, -3.5, 20.1, 0.0 //real location
fuel_type=1 //1 is Avgas, 2 is JetA
number_of_tank_selectors=1
electric_pump=0




[flight_tuning]
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000

cruise_lift_scalar=1.000

hi_alpha_on_roll=1.0
hi_alpha_on_yaw=1.0

p_factor_on_yaw=1 //-1 //1.0
torque_on_roll=1.0
gyro_precession_on_roll=1.0
gyro_precession_on_yaw=1.0

parasite_drag_scalar=1.000
induced_drag_scalar=1.000




[airplane_geometry]
wing_area=1
wing_span=1
wing_root_chord=2
wing_dihedral=0
wing_incidence=90
wing_twist=0
oswald_efficiency_factor=0.7
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=0
htail_span=0
htail_pos_lon=0
htail_pos_vert=0
htail_incidence=0
htail_sweep=0
vtail_area=0
vtail_span=0
vtail_sweep=0
vtail_pos_lon=0
vtail_pos_vert=0
elevator_area=0
aileron_area=0
rudder_area=0
elevator_up_limit=0
elevator_down_limit=0
aileron_up_limit=0
aileron_down_limit=0
rudder_limit=25 //must be above zero, or the vehicle will tumble wildly around
elevator_trim_limit=0
spoiler_limit=0
spoilerons_available=0
aileron_to_spoileron_gain=0
min_ailerons_for_spoilerons=0
min_flaps_for_spoilerons=0



//0  Class                        <0=None, 1=Wheel, 2=Scrape, 3=Skid, 4=Float, 5=Water Rudder>
//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) //radius er halv diameter
//7  Steer Angle                  (degrees)
//8  Static Compression           (feet)  (0 if rigid)
//9  Max/Static Compression Ratio
//10 Damping Ratio                (0=Undamped, 1=Critically Damped)
auto_spoiler_available=0
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-1.500000
negative_g_limit_flaps_down=-1.500000
//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]
//      0,    1,    2,    3,    4, 5,    6,  7,   8,   9,   10, 11, 12, 13, 14, 15
point.0=1, 14.7, -2.2, -4.0, 1574, 0, 1.15, 30, 0.3, 2.5, 0.54,  0,  0,  2,  0,  0
point.1=1, 14.7,  2.2, -4.0, 1574, 0, 1.15, 30, 0.3, 2.5, 0.54,  0,  0,  3,  0,  0
point.2=1,  5.0, -2.2, -4.0, 1574, 1, 1.15,  0, 0.3, 2.5, 0.54,  0,  0,  2,  0,  0
point.3=1,  5.0,  2.2, -4.0, 1574, 2, 1.15,  0, 0.3, 2.5, 0.54,  0,  0,  3,  0,  0
//wheels are 2.3 feet in diameter (1.15 foot radius)

//JEL    0     1      2      3     4  5  6  7  8  9 10 11 12 13 14 15
point.4 = 2, 16.1, -3.1,  -3.8, 1575, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 //front-fuselage bottom-left
point.5 = 2, 16.1,  3.1,  -3.8, 1575, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 //front-fuselage bottom-right
point.6 = 2,  3.5, -3.1,  -3.8, 1575, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 //rear-fuselage bottom-left
point.7 = 2,  3.5,  3.1,  -3.8, 1575, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 //rear-fuselage bottom-right

point.8= 2,  0.0,  0,  -3.2, 1575, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 //rear-fender
point.9= 2, 17.9,  0,  -3.2, 1575, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 //front-fender

max_number_of_points=10

static_pitch=0.0 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=4.0 //feet, altitude of CG when at rest on the ground
gear_system_type=0 //0 is no retractable gear

[brakes]
toe_brakes_scale=5 //1.000000
parking_brake=1

[Flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard = 0.0 // 0.0 .. 1.0
extending-time = 0.0 // seconds
system_type = 4 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
flaps-position.0 = 0.0 ,0.0 // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS

[GeneralEngineData]
engine_type=0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=5.0, 0.0 , -4.8 //(feet) longitudinal, lateral, vertical distance from reference datum
//engine is placed at rear-wheel thread-point, since this is where the wheel pushes the car forward
fuel_flow_scalar=1.000000
min_throttle_limit=0 //-0.5

[piston_engine]
max_rpm_mechanical_efficiency_scalar=1.2 //1.2
idle_rpm_mechanical_efficiency_scalar=1.5 //1.5
max_rpm_friction_scalar=1 //1
idle_rpm_friction_scalar=0.1 //0.1
power_scalar = 1 //1

cylinder_displacement=43.7235 //Cubic inches per cylinder //43.7235 is real for this 8-cyl 5.7-liter (5732 cc) engine
//1 cubic inch ( cu.in. ) = 16.387064 cubic centimetres ( cu.cm. cm3 or cc )
//svarer til 8 cylindre der tilsammen gi'r 5732 cc

compression_ratio=8.3 //8.3 is real
number_of_cylinders=8 //8 is real
max_rated_rpm=5000 //5000
max_rated_hp=142 //142 is real at 3200 rpm //200 to 250 hp defined on other web-pages
fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=1 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=1 //8 //0.3
turbocharged=0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=41 //Max design manifold pressure, (inHg)
min_design_mp=1 //Min design manifold pressure, (inHg)
critical_altitude=18000 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=1 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE


[propeller]
thrust_scalar = 3.51 //3.51
propeller_type=1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 5 //5 //1 //Propeller Diameter, (feet)
propeller_blades=8 //4 //Number of propeller blades
propeller_moi=0.1 //0.1 //Propeller moment of inertia (will roll the car when rpm is changed, like a muscle-car)
beta_max=20 //0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=15 //0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=0 //600 //Miminum governed RPM
prop_tc=0.1 //0 //Prop time-constant
gear_reduction_ratio=0.5 //1 //0.55 //Propeller gear reduction ratio

fixed_pitch_beta=10 //10 //Fixed pitch angle of fixed pitch prop, (degrees)
//lavere value gi'r hurtigere acceleration

low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=0 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=0 //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available=0 //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=0 //Minimum RPM for prop feathering
beta_feather=0 //Feathering pitch angle (degrees)
power_absorbed_cf=0 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE 
prop_reverse_available=0 //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees)





[Reference Speeds]
flaps_up_stall_speed=500.000000
full_flaps_stall_speed=400.000000
cruise_speed=90.295761
max_indicated_speed=180.000000

[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=30, 80

[Views]
eyepoint=9.4, -1.5, -0.8 //driver-side is left
//(feet) longitudinal, lateral, vertical distance from reference datum

[Radios]
// Radio Type=availiable, 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
Transponder.1=1
Marker.1=1

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=93
pitch_takeoff_ga=10
use_no_default_pitch=1
use_no_default_bank=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10
max_pitch_acceleration=10
max_pitch_velocity_lo_alt=9.8
max_pitch_velocity_hi_alt=5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank=30
max_bank_acceleration=2.8
max_bank_velocity=4.8
max_throttle_rate=0.05
nav_proportional_control=20
nav_integrator_control=0.15
nav_derivative_control=5
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control=20
gs_integrator_control=0.26
gs_derivative_control=5
gs_integrator_boundary=1.5
gs_derivative_boundary=0

yaw_damper_gain=0.4615
//use yaw-damping to simulate the deflection-restriction.
//when yaw-damper is on, the rudder can only deflect 6 degrees


[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=0
stick_shaker=0

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[direction_indicators]
direction_indicator.0=1,0
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0
