// This aircraft configuration file is made for the ATR 72-500
// made by Mikko Maliniemi and developed for Flight 1
// Flight dynamics developed by Alexander M. Metzger 

[fltsim.0]
title=ATR-42-400 RIKI AIR BLANK
sim=ATR42-400_2k4v5.3
model=
panel=MIO
sound=
texture=
checklists=
kb_checklists=checklist
ui_manufacturer=Aerospatiale
ui_type=ATR-42-400
ui_variation=RIKI AIR BLANK
atc_heavy=0
atc_id=CRN
atc_airline=RIKI AIR
atc_flight_number=2105
description=FS2004 ATR42-400\nDesign: Ricardo garcia Marrero\nTextures: ricardo garcia Marrero\Other info later
atc_parking_types=GATE,RAMP
atc_parking_codes=CRN
atc_id_color=0000000000
visual_damage=0


[General]
atc_type=ATR 42 400
atc_model=AT44 
editable=1 
performance=ATR42-400 "Technical Data \nAccommodation : 2 crew + 44 to 50 pax \nDimensions \nSpan : 22.57m (80'61ft) \nLength : 22.67m (74'38ft) \nHeight : 7.59m (24'9ft) \nWeight \nEmpty: 10,280kg (22,663lbs) \nMax: 16,700kg (36,820lbs) \nPower Plant: 2x 2100shp Pratt Whitney Canada P&W-121 \nPerformance \nMax speed: 580km/h (270mph-313knots) \nMax climb: 1,968ft/min (10m/sec) \nCeiling: 25,000ft (7,620m) \nRange: 2,100km (1,134nm)" 
Category=airplane

[weight_and_balance]

max_gross_weight = 36861
empty_weight = 22663
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 157504
empty_weight_roll_MOI = 81403
empty_weight_yaw_MOI = 181337
empty_weight_coupled_MOI = 0
max_number_of_stations = 8

station_load.0 = 1058,  17.0,  2.9, 0, 0
station_load.1 = 1058,  17.0, -2.9, 0, 0
station_load.2 = 1693, -23.7,    0, 0
station_load.3 = 2960,   6.8,    0, 0,
station_load.4 = 2960,  -2.0,    0, 0,
station_load.5 = 2590, -11.0,    0, 0,
station_load.6 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.7 = "0.0, 0.0, 0.0, 0.0, FsStation"


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=Taxi, 7=Recognition, 8=Wing, 9=Logo, 10=Cabin

light.0 = 3, -0.55, -39.77, 6.59, Rd_rnav
light.1 = 3, -0.55, 39.77, 6.59, Rd_gnav
light.2 = 2, -0.33, -39.73, 6.59, Rd_wstrb
light.3 = 2, -0.33, 39.73, 6.59, Rd_wstrb
light.4 = 2, -41.9, -0.3, 3.87, Rd_wstrb_tail
light.5 = 3, -41.9, 0, 3.36, Rd_wnav
light.6 = 1, -39.74, 0, 19.10, Rd_redbcn_top
light.7 = 1, -1.71, 0, -3.94, Rd_redbcn_btm
light.8 = 4, 22.8, 0, 4.37, Rd_vclight                          //iFly737_fx_vcligh
light.9 = 5, 15.9, 1.585, -4.51, Rd_land_light,                 //fx_shockwave_landing_light , 
light.10 = 7, 15.9, -1.585, -4.51, Rd_land_light,               //fx_shockwave_landing_light , 
light.11 = 5, 5.97, 2.585, -2.599, Rd_land, 
light.12 = 7, 5.97, -2.585, -2.599, Rd_land,
light.13 = 9, -36.6, -4.9, 16.45, Rd_logo
light.14 = 9, -36.6, 4.9, 16.45, Rd_logo
//light.15 = 9, -36.6, -4, 11.5, Rd_logo_wide
//light.16 = 9, -36.6, 4, 11.5, Rd_logo_wide



//[smokesystem]
//smoke.0 = -4, 9, 13.32, Prop_revspray
//smoke.1 = -4, 9, -13.32, Prop_revspray

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn24, 1
startup= fx_ffs_engstrt_saab340B

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 2

LeftMain = -2.2, -13.35, 6, 740.4, 6
RightMain = -2.2, 13.35, 6, 740.4, 6
electric_pump=1


[contact_points]
        //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)

gear_system_type=1
static_pitch = -1.20
static_cg_height = 5.4
max_number_of_points = 3
          0        1     2     3     4  5     6   7    8     9     10    11    12 13   14   15
point.0 = 1, 25.8866,    0, -5.0, 1500, 0, 0.75, 65, 0.35, 0.65, 0.55,    7,  7.5, 0, 250, 250
point.1 = 1,    -3.1, -6.4, -5.9, 2500, 1, 1.44,  0, 0.69, 0.95, 0.55, 10.5, 12.5, 2, 250, 250
point.2 = 1,    -3.1,  6.4, -5.9, 2500, 2, 1.44,  0, 0.69, 0.95, 0.55, 11.3, 10.3, 3, 250, 250


[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 0.725       // 1.0//0.825
engine.0 = 6.4, -13.3, 2.7
engine.1 = 6.4,  13.3, 2.7
min_throttle_limit=-0.12
max_contrail_temperature=-35

[propeller]
thrust_scalar=1.0                    //Propeller thrust scalar
propeller_type=0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=11.4 //12.9       //Propeller Diameter, (feet)
propeller_blades=6                   //Number of propeller blades
propeller_moi=50          //77       //Propeller moment of inertia
beta_max=33                          //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=5.5                         //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=14171                    //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)
//rotation=-1 -1 -1 -1    //clockwise rotation               
//rotation=1 1 1 1     //anti clockwise rotation

[TurbineEngineData]
fuel_flow_gain=0.011                 //Gain on fuel flow
inlet_area=0.8                   //Square Feet, engine nacelle inlet area
rated_N2_rpm=20016                 //RPM, second stage compressor rated value
static_thrust=230                   //Lbs, max rated static thrust at Sea Level
afterburner_available=0

[turboprop_engine]
power_scalar=1.0                   //Scalar on Turboprop power
maximum_torque=10241               //Maximum torque available (ft-lbs)
max_rpm_mechanical_efficiency_scalar=1.0
idle_rpm_mechanical_efficiency_scalar=1.0
max_rpm_friction_scalar=1.0
idle_rpm_friction_scalar=1.0

[keyboard_response]
elevator = 150, 200
aileron = 150, 200
rudder = 150, 200


[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 = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 9000
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
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
wing_area = 586.60000
wing_span = 81.55
wing_root_chord = 8.81
wing_dihedral = 0.80
wing_incidence = 0.00000
wing_twist = 0.00000
oswald_efficiency_factor = 0.80000
wing_winglets_flag = 0
wing_sweep = 5
wing_pos_apex_lon = 3.52
wing_pos_apex_vert = 6.00
htail_area = 97.20000
htail_span = 22.35
htail_pos_lon = -35.31
htail_pos_vert = 16.85
htail_incidence = 0.00000
htail_sweep = 9
vtail_area = 119.05000
vtail_span = 14.59
vtail_sweep = 32
vtail_pos_lon = -26.98
vtail_pos_vert = 4.53
elevator_area = 34.91000
aileron_area = 16.40000
rudder_area = 33.87000
elevator_up_limit = 30.00000
elevator_down_limit = 25.00000
aileron_up_limit = 25.00000
aileron_down_limit = 25.00000
rudder_limit = 30.00000
elevator_trim_limit = 50.00     //30.00
spoiler_limit = 60.00000
aileron_to_spoileron_gain = 0.00000
min_ailerons_for_spoilerons = 0.00000
min_flaps_for_spoilerons = 0.00000
spoilerons_available = 1

[electrical]
max_battery_voltage = 28
generator_alternator_voltage = 28
max_generator_alternator_amps = 40
electric_always_available = 0
flap_motor = 0, 0, 17
gear_motor = 0, 0, 17
autopilot = 0, 0, 17
avionics_bus = 0, 0, 17
avionics = 1, 0, 17
pitot_heat = 0, 0, 17
additional_system = 0, 0, 17
marker_beacon = 1, 0, 17
gear_warning = 0, 0, 17
fuel_pump = 0, 0, 17
starter1 = 0, 0, 17
starter2 = 0, 0, 17
starter3 = 0, 0, 17
starter4 = 0, 0, 17
light_nav = 0, 0, 17
light_beacon = 0, 0, 17
light_landing = 0, 0, 17
light_taxi = 0, 0, 17
light_strobe = 0, 0, 17
light_panel = 0, 0, 17
prop_sync = 0, 0, 17
auto_feather = 0, 0, 17
auto_brakes = 0, 0, 17
standby_vacuum = 0, 0, 17
hydraulic_pump = 0, 0, 17
fuel_transfer_pump = 0, 0, 17
propeller_deice = 0, 0, 17

[Reference Speeds]
flaps_up_stall_speed=122 
full_flaps_stall_speed=88 
cruise_speed=285 
max_indicated_speed=250
max_mach=0.55

[flight_tuning]
cruise_lift_scalar=1.1 
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=1.1
aileron_trim_effectiveness=1.0 
rudder_trim_effectiveness=1.0 
p_factor_on_yaw=1.0
torque_on_roll=1.0
qyro_precission_on_roll=1.0
qyro_precission_on_yaw=1.0

[Flaps.0] 
type= 1
span-outboard= 0.7
extending-time= 12
system_type= 1
damaging-speed= 180
blowout-speed= 190
lift_scalar= 1.0
drag_scalar= 1.0
pitch_scalar= 1.0
flaps-position.0= 0
flaps-position.1= 15
flaps-position.2= 30
flaps-position.3= 45


[Views]
// (feet) longitudinal, lateral, vertical distance from reference datum 
eyepoint=27.10, -1.60, 2.5 // Captain

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=0 
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=115
pitch_takeoff_ga=10.0 
autoland_available=1

max_pitch=15.0
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=25.0                                        //27.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.05                               //0.10

nav_proportional_control=9.0                         //15.0
nav_integrator_control=0.1
nav_derivative_control=0.0
nav_integrator_boundary=2.5                          //0.2
nav_derivative_boundary=0.0
gs_proportional_control=9.5                          //15.0
gs_integrator_control=0.25                           //0.5
gs_derivative_control=0.0
gs_integrator_boundary=0.5
gs_derivative_boundary=0.0

yaw_damper_gain = 1.0
default_pitch_mode=1
default_bank_mode=1

[attitude_indicators]
attitude_indicator.0=1
[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 

[turn_indicators]
turn_indicator.0=1,0
[pitot_static]
vertical_speed_time_constant=0.5

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.1
flap_limit_power=15.5
flap_limit_idle=15.5
[stall_warning]
type=1
[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, 1 
Adf.2=1, 1
Transponder.1=1 
Marker.1=1 

[brakes]
toe_brakes_scale=0.90
parking_brake=1
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000

[exits]
number_of_exits=2
exit_rate.0=0.15
exit_rate.1=0.15   //0.05

[folding_wings]
wing_fold_system_type = 4
fold_rates = 0.07,0.1
[tailhook]
tailhook_length=1
tailhook_position = -15.0, 0.0, -1.0
cable_force_adjust = 1.0