// 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=RIKI DESIGN ATR 72-211 BLANK
sim=ATR72-500_2k4v5.3
model=211
panel=MIO
sound=
texture=BLANK/BLANK_211
kb_checklists=ATR_check
kb_reference=ATR 72-500_ref
atc_id=F-WWEY
atc_airline=Aerospatiale
atc_flight_number=1548
atc_heavy=0
ui_manufacturer=Aerospatiale
ui_type=ATR-72-212
ui_variation=AEROSPATIALE BLANK
visual_damage=0
description=ATR is today the worlwide reference in regional turboprop aircraft.  Such success can be explained by the characteristics of the ATR aircraft family which combine high technology, comfort, reliability and profitability. - Jean-Michel Lйonard (Chairman of the Board - ATR)
atc_id_color=0000000000
atc_parking_types=GATE,RAMP
atc_parking_codes=AFR
visual_damage=0
ui_typerole=

[fltsim.1]
title=RIKI DESIGN ATR 72-211F BLANK
sim=ATR72-500_2k4v5.3
model=21F
panel=MIO
sound=
texture=BLANK/BLANK_211_F
kb_checklists=ATR_check
kb_reference=ATR 72-500_ref
atc_id=F-WWEY
atc_airline=Aerospatiale
atc_flight_number=1548
atc_heavy=0
ui_manufacturer=Aerospatiale
ui_type=ATR-72-212
ui_variation=AEROSPATIALE BLANK
visual_damage=0
description=ATR is today the worlwide reference in regional turboprop aircraft.  Such success can be explained by the characteristics of the ATR aircraft family which combine high technology, comfort, reliability and profitability. - Jean-Michel Lйonard (Chairman of the Board - ATR)
atc_id_color=0000000000
atc_parking_types=GATE,RAMP
atc_parking_codes=AFR
visual_damage=0
ui_typerole=

[fltsim.2]
title=RIKI DESIGN ATR 72-212 BLANK
sim=ATR72-500_2k4v5.3
model=212
panel=MIO
sound=
texture=BLANKBLANK_212
kb_checklists=ATR_check
kb_reference=ATR 72-500_ref
atc_id=F-WWEY
atc_airline=Aerospatiale
atc_flight_number=1548
atc_heavy=0
ui_manufacturer=Aerospatiale
ui_type=ATR-72-212
ui_variation=AEROSPATIALE BLANK
visual_damage=0
description=ATR is today the worlwide reference in regional turboprop aircraft.  Such success can be explained by the characteristics of the ATR aircraft family which combine high technology, comfort, reliability and profitability. - Jean-Michel Lйonard (Chairman of the Board - ATR)
atc_id_color=0000000000
atc_parking_types=GATE,RAMP
atc_parking_codes=AFR
visual_damage=0
ui_typerole=

[fltsim.3]
title=RIKI DESIGN ATR 72-212 CARGO BLANK
sim=ATR72-500_2k4v5.3
model=212
panel=MIO
sound=
texture=BLANK/BLANK_212_F
kb_checklists=ATR_check
kb_reference=ATR 72-500_ref
atc_id=F-WWEY
atc_airline=Aerospatiale
atc_flight_number=1548
atc_heavy=0
ui_manufacturer=Aerospatiale
ui_type=ATR-72-212
ui_variation=AEROSPATIALE BLANK
visual_damage=0
description=ATR is today the worlwide reference in regional turboprop aircraft.  Such success can be explained by the characteristics of the ATR aircraft family which combine high technology, comfort, reliability and profitability. - Jean-Michel Lйonard (Chairman of the Board - ATR)
atc_id_color=0000000000
atc_parking_types=GATE,RAMP
atc_parking_codes=AFR
visual_damage=0
ui_typerole=









[General]
atc_type=ATR 72 212
atc_model=AT72
editable=0 
performance=ATR72-212\nWing span: 27.05 m \/ 88.7 ft\nLength: 27.16 m \/ 89.08 ft\nHeight: 7.59 m \/ 24.9 ft\nWing area: 61.1 m2 \/ 657 sqft\nDry Operating Weight: 13,500 kg \/ 29,762 lb\nMax. Fuel Weight: 5,006 kg \/ 1,672 gal\nMax. Take Off Weight: 22,000 kg \/ 48,500 lb\nZero Fuel Weight FDX: 18,520 kg \/ 40,829 lb\nEngine: PW127\nPropeller HS 568F, 6 blade\nPassengers: 51 max. 68\nMax. speed Vmo: 250 KIAS\nCruise speed: 285 KTAS at FL170 

[weight_and_balance]

// ACM V2.3
max_gross_weight = 48502
empty_weight = 29762
reference_datum_position = 2, 0, 0
empty_weight_CG_position = -1.3, 0, 0
empty_weight_pitch_MOI = 327405
empty_weight_roll_MOI = 258835
empty_weight_yaw_MOI = 676702
empty_weight_coupled_MOI = 0
max_number_of_stations = 7

station_load.0 = 1980, 15,0,0, Front Cargo
station_load.1 = 1593,-19,0,0, Aft Cargo
station_load.2 = 4440, 8,0,0, Zone A
station_load.3 = 5180, -2,0,0, Zone B
station_load.4 = 3330,-12,0,0, Zone C
station_load.5 = "0.0, 0.0, 0.0, 0.0, FsStation"
station_load.6 = "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, -2.60, -43.22, 6.41, Rd_rnav
light.1 = 3, -2.60, 43.37, 6.42, Rd_gnav
light.2 = 2, -2.35, -43.16, 6.41, Rd_wstrb
light.3 = 2, -2.35, 43.33, 6.41, Rd_wstrb
light.4 = 2, -50.7, -0.21, 3.52, Rd_wstrb
light.5 = 3, -50.7, 0, 2.97,  Rd_wnav
light.6 = 1, -48.53, 0, 19.00, Rd_redbcn_top
light.7 = 1, -3.38, 0, -4.36, Rd_redbcn_btm
light.8 = 4, 28.02, 0, 4.84, Rd_vclight
light.9 = 5, 13.25, 3.17, -4.51, Rd_land_light
light.10 = 7, 13.25, -3.17, -4.51, Rd_land_light
light.11 = 5, 5.50, 3.15, -2.72, Rd_land, 
light.12 = 7, 5.50, -3.15, -2.72, Rd_land,

light.13 = 9, -46.555, -5.52, 16.39, Rd_logo
light.14 = 9, -46.555, 5.52, 16.39, Rd_logo

light.15 = 8, 13.75, 4.5, 0, Rd_WingLights
light.16 = 8, 13.75, -4.5, 0, Rd_WingLights

//light.17 = 9, -45.655, -4.52, 12.5, Rd_logo_wide
//light.18 = 9, -45.655, 4.52, 12.5, Rd_logo_wide



[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 = -4.13, -14.9, 6, 836, 5
RightMain = -4.13, 14.9, 6, 836, 5
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)

static_pitch = -0.75
static_cg_height = 5.4
max_number_of_points = 3
gear_system_type=1

          0        1     2        3     4  5     6   7    8     9     10    11    12 13   14   15
point.0 = 1,  31.548,    0, -5.6739, 1500, 0,  0.8, 60,  0.42, 2.1,  0.5,    7,   7.5, 0, 250, 250
point.1 = 1,  -4.565, -6.4, -6.5677, 2000, 1, 1.38,  0,  0.62, 1.8,  0.4, 10.5,  10.5, 2, 250, 250
point.2 = 1,  -4.565,  6.4, -6.5677, 2000, 2, 1.38,  0,  0.62, 1.8,  0.4, 10.3,  10.3, 3, 250, 250


[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 = 657.0
wing_span = 88.69
wing_root_chord = 9.80
wing_dihedral = 1
wing_incidence = 2.0
wing_twist = 0.0
oswald_efficiency_factor = 0.6
wing_winglets_flag = 0
wing_sweep = 5
wing_pos_apex_lon = 1.60
wing_pos_apex_vert = 5.81
htail_area = 128.0
htail_span = 22.65
htail_pos_lon = -45.45
htail_pos_vert = 16.77
htail_incidence = -0.33
htail_sweep = 9                                                //0
vtail_area = 163.0
vtail_span = 14.52
vtail_sweep = 32
vtail_pos_lon = -35.44
vtail_pos_vert = 4.57
elevator_area = 51.2
aileron_area = 61.4
rudder_area = 55.2
elevator_up_limit = 30.0                                       //23.0
elevator_down_limit = 25.0                                     //13.0
aileron_up_limit = 25.0                                        //14.0
aileron_down_limit = 25.0                                      //14.0
rudder_limit = 27.0
elevator_trim_limit = 45.0
aileron_trim_limit = 50.00                                     //30.00
rudder_trim_limit = 50.00                                      //30.00
spoiler_limit = 60
aileron_to_spoileron_gain = 3.0
min_ailerons_for_spoilerons = 2.5
min_flaps_for_spoilerons = 0.0
spoilerons_available = 1

[electrical]
max_battery_voltage = 28
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
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


[GeneralEngineData]
engine_type = 5
Engine.0 = 3.392, -13.579, 3.701
Engine.1 = 3.392, 13.579, 3.701
fuel_flow_scalar=0.825
min_throttle_limit=-0.25     //-0.12
max_contrail_temperature=-35

[TurbineEngineData]
fuel_flow_gain=0.01 //adjusted to have only slight overshot
inlet_area=0.800 
rated_N2_rpm=20016 //spec=20016 was 23850
static_thrust=280 //was 343
afterburner_available=0 

[turboprop_engine]
power_scalar=1.0 
maximum_torque=11305   //12305 
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

[propeller]
thrust_scalar=1.13 
propeller_type=0 
propeller_diameter=11.4 //12.9
propeller_blades=4 
propeller_moi=90 //60 //was 90
beta_max=30 //spec=24 was 65
beta_min=5.5 // spec=14 adjusted to small NP drop when blade pitch jumps
min_gov_rpm=14171  //was 16695 //0.708 x rated RPM = min NP=70.8%
prop_tc=0.0003 //adjusted to have only slight overshot
gear_reduction_ratio=15.68  //spec=16.68 was 19.875
fixed_pitch_beta=0.0 
low_speed_theory_limit=70 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=700 //was 480 //840
beta_feather=78.5  //spec=78.5
power_absorbed_cf=0.990 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0.0 //spec=-1 adjusted to supress rev sound
minimum_reverse_beta=-14   //-10.5  //spec=-14 adjusted to avoid drop on NP
//rotation=-1 -1 -1 -1    //clockwise rotation               
//rotation=1 1 1 1     //anti clockwise rotation


[Flaps.0]
type= 1
system_type=1
span-outboard= 1.000
extending-time= 14.0
damaging-speed=235.0
blowout-speed=255.0
flaps-position.0=0.00
flaps-position.1=15.00
flaps-position.2=40.00
lift_scalar=1.00
drag_scalar=1.00
pitch_scalar=1.00

[Views]
// (feet) longitudinal, lateral, vertical distance from reference datum 
//eyepoint=-2.4, -1.7, 1.0 // Captain
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=100
pitch_takeoff_ga=10.0 
autoland_available=1
max_pitch=16.0
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=27.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=15.0
nav_integrator_control=0.1
nav_derivative_control=0.0
nav_integrator_boundary=0.2
nav_derivative_boundary=0.0
gs_proportional_control=15.0
gs_integrator_control=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 
Adf.2=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=0.05

[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