// Dash 7 Cargo for AI 
//
// Original Model designed and animated in GMAX by Milton Shupe - March-August 2002
// FS2004 Updates by Milton Shupe August 2003
// FS2004 AI Version by Milton Shupe, March 2006
//
// Flight Dynamics by Milton Shupe, with AI tweaks by Holger Sandmann
//
// !!!Copyright remains with the original authors!!!
//


[fltsim.0]
title=Dash 7-101 AI TF Northwind Air Cargo
sim=dash7c_ai
model=
panel=
sound=
texture=NAC
kb_checklists=
kb_reference
atc_heavy=0
atc_id=N939NC
atc_airline=NORDAIR
atc_flight_number=
ui_manufacturer=AI Aircraft
ui_type=de Havilland DASH 7-101 Cargo
ui_variation=Northwind Air Cargo
atc_parking_types=RAMP, CARGO
atc_parking_codes=NAC
description=by Milton Shupe, for AI only. Repaint by Bill Womack.

[fltsim.1]
title=Dash 7-101 AI TF Wrangell Air Cargo
sim=dash7c_ai
model=
panel=
sound=
texture=WAC
kb_checklists=
kb_reference=
atc_heavy=0
atc_id=N101WA
atc_airline=
atc_flight_number=
ui_manufacturer=AI Aircraft
ui_type=de Havilland DASH 7-101 Cargo
ui_variation=Wrangell Air Cargo
description=by Milton Shupe, for AI only. Repaint by Bjoern Erik Henriksen.


[General]
performance=Range:  1,170 nm\nCargo:  11,310 lb\nPassengers:  50\nDesigner:  Milton Shupe\nDate:  March 2002
atc_type=DEHAVILLAND
atc_model=DHC7
editable=0


[WEIGHT_AND_BALANCE]
max_gross_weight = 34500                        // (pounds)
empty_weight = 22730                            // (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

;Moments of Inertia
empty_weight_pitch_MOI   = 111701
empty_weight_roll_MOI    =  61201
empty_weight_yaw_MOI     = 161691
empty_weight_coupled_MOI = 0


[Reference Speeds]
flaps_up_stall_speed=103.000   //at 38,000lbs
full_flaps_stall_speed=60.000  //at 27,000lbs
cruise_speed=223               //at 10,000'
max_indicated_speed=280.000000
max_mach=0.500000


[contact_points]
//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 / Water Rudder Effectiveness  (0=Undamped, 1=Critically Damped) / 1.0 = normal
//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)
point.0=1,   21.6,   0.0,  -5.5, 3200, 0, 1.4,    32,	0.6,   2.1, 0.70, 3, 3, 0, 160, 230
point.1=1,   -3.8, -13.6,  -5.9, 2200, 1, 1.7,     0,   0.8,   1.3, 0.70, 8, 7, 2, 160, 230	
point.2=1,   -3.8,  13.6,  -5.9, 2200, 2, 1.7,     0,   0.8,   1.3, 0.70, 8, 7, 3, 160, 230	
//point.3=2,  -1.11, -46.5,   6.3, 1200, 0, 0,       0,     0,     0,    0, 0, 0, 5				
//point.4=2,  -1.11,  46.5,   6.3, 1200, 0, 0,       0,     0,     0,    0, 0, 0, 6					
//point.5=2,    -44,     0,   6.3, 2400, 0, 0,       0,     0,     0,    0, 0, 0, 9					
//point.6=2,   31.4,     0,    .8, 1200, 0, 0,       0,     0,     0,    0, 0, 0, 4					
//point.3=4,  -3.8,  0.00, -5.50, 30000, 0, 0.519, 90.000, 0.500, 0.750, 0.850, 0.000, 0.000, 0.000, 0.000, 0.000

max_number_of_points=21
static_pitch= -0.500             //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=5.413           //altitude of CG when at rest on the ground
gear_system_type=0

[EFFECTS]
dirt=fx_tchdrt
concrete=fx_dustcloud_l
//fx_sparks
touchdown=fx_tchdwn, 1
water=fx_spray

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3,  -1.9, -46.4,  8.7, fx_navred ,
light.1=3,  -1.9,  46.3,  8.7, fx_navgre ,
light.2=2,  -2.3,  46.3,  8.7, fx_strobe ,
light.3=2,  -2.3, -46.4,  8.7, fx_strobe ,
light.4=1, -43.4,   0.2, 22.2, fx_beacon ,
light.5=1,   5.3,   0.0, -2.8, fx_beacon ,
//light.6=4, 21.50, 0.0, 4.5, Fx_D7cbn2 ,
//light.7=4, 14.20, -4.2, 3.0, Fx_D7cbn4 ,
//light.8=4, 4.00, 0.0, 2.0, Fx_D7cbn1 ,
//light.9=4, 0.00, 0.0, 2.0, Fx_D7cbn3 ,
//light.10=4, -4.00, 0.0, 2.0, Fx_D7cbn1 ,
//light.11=4, -9.00, 0.0, 2.0, Fx_D7cbn3 ,
//light.12=4, -16.00, -1.0, 1.5, Fx_D7cbn2 ,
//light.13=3,  -46.3, 0.1,  6.2, fx_navwhi ,
light.6=1, 10.0,  24.0,  0.0, fx_helismoke ,
light.7=1, 10.0,  12.0,  0.0, fx_helismoke ,
light.8=1, 10.0, -24.0,  0.0, fx_helismoke ,
light.9=1, 10.0, -12.0,  0.0, fx_helismoke ,


[brakes]
toe_brakes_scale=0.677996
parking_brake=1

[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second

[flaps.0]
type             = 2                                    // 1 - trail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 22                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 15                                   // degrees
flaps-position.2 = 25                                   // degrees
flaps-position.3 = 45                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 0.7
drag_scalar = 0.5
pitch_scalar= 0.6
system_type = 1                                         //Hydraulic

[flaps.1]
type             = 1                                    // 1 - trail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 11                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 15                                   // degrees
flaps-position.2 = 25                                   // degrees
flaps-position.3 = 45                                   // degrees
damaging-speed   = 200                                  // KIAS
blowout-speed    = 250                                  // KIAS
lift_scalar = 0.3
drag_scalar = 0.5
pitch_scalar= 0.4
system_type = 1                                         //Hydraulic


[flight_tuning]
cruise_lift_scalar=1.0		//the angle of attack (and thus pitch) for a cruise condition
parasite_drag_scalar=1.00	//air flow interference and skin friction
induced_drag_scalar=1.0		//from production of lift
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[GeneralEngineData]
engine_type=5                    //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=0.0, -24.5, 0.500       //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=0.0, -12.5, 0.000
Engine.2=0.0,  12.5, 0.000
Engine.3=0.0,  24.5, 0.500
fuel_flow_scalar        = 1.0                   //Scalar for fuel flow efficiency
min_throttle_limit = -0.25                      //Minimum percent throttle.  Generally negative for turbine reverser

[TurbineEngineData]
fuel_flow_gain          = 0.011                 //Gain on fuel flow
inlet_area              = 1.0                   //Square Feet, engine nacelle inlet area
rated_N2_rpm            = 29920                 //RPM, second stage compressor rated value
static_thrust           = 200                   //Lbs, max rated static thrust at Sea Level

afterburner_available=0
reverser_available=1


[propeller]
thrust_scalar           = 1.0                   //Propeller thrust scalar
propeller_type          = 0                     //0=Constant Speed, 1=Fixed Pitch
propeller_diameter      = 13.0                  //Propeller Diameter, (feet)
propeller_blades        = 4                     //Number of propeller blades
propeller_moi           = 77                    //Propeller moment of inertia
beta_max                = 45                    //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min                = 12                    //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm             = 25520                 //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)

[turboprop_engine]
power_scalar            = 1.0                   //Scalar on Turboprop power
maximum_torque          = 7878                  //Maximum torque available (ft-lbs)

[fuel]
LeftMain=-0.100,-31.500000,7.700,120.000000,0.000000
LeftAux=-0.100,-18.000000,7.100, 310.500000,0.000000
RightMain=-0.100,31.500000,7.700, 120.000000,0.000000
RightAux=-0.100,18.000000,7.100, 310.500000,0.000000
fuel_type=2.000
number_of_tank_selectors=1
electric_pump=0

[airplane_geometry]
wing_area               = 585.0                 //Square feet
wing_span               = 85.0                  //Feet
wing_root_chord         = 7.0                   //Feet
wing_dihedral           = 2.5                   //Degrees
wing_incidence          = 1.0                   //Degrees
wing_twist              = -3.0                  //Degrees
oswald_efficiency_factor= 0.7                   //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 3.0                   //Degrees, wing leading edge
wing_pos_apex_lon       = -25.0                 //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              = 97.0                  //Square feet
htail_span              = 26.0                  //Feet
htail_pos_lon           = -58.9                 //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         = 1.0                   //Degrees
htail_sweep             = 8.0                   //Degrees, horizontal tail leading edge
vtail_area              = 106.0                 //Square feet
vtail_span              = 11.7                  //Feet, tip to body
vtail_sweep             = 30.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -54.9                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 3.4                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 53.5                  //Square feet
aileron_area            = 12.1                  //Square feet
rudder_area             = 46.4                  //Square feet
elevator_up_limit       = 17.0                  //Degrees
elevator_down_limit     = 15.5                  //Degrees
aileron_up_limit        = 18.0                  //Degrees
aileron_down_limit      = 18.0                  //Degrees
rudder_limit            = 30.0                  //Degrees
elevator_trim_limit     = 15.0                  //Degrees
spoiler_limit           = 60.0                  //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 0                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0                 //Degrees
min_flaps_for_spoilerons = 0                    //Minimum flap handle position when spoilerons activate

[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=150.000, 250.000
aileron=150.000, 250.000
rudder=150.000, 250.000

[Views]
eyepoint=20.650, -1.550, 1.500        //(feet)22.250 - 3.8 longitudinal, lateral, vertical distance from reference datum


[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1200.000
autothrottle_available=1
pitch_takeoff_ga=8.000
autothrottle_max_rpm=28000.000000
use_no_default_bank=1
use_no_default_pitch=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000



[direction_indicators]
direction_indicator.0=3,0


[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor           =0, 5 , 17.0
gear_motor           =0, 5 , 17.0
autopilot            =0, 5 , 17.0
avionics_bus         =0, 10, 17.0
avionics             =1, 5 , 17.0
pitot_heat           =0, 2 , 17.0
//additional_system  =0, 20, 17.0
additional_system    =0, 5 , 17.0 
marker_beacon        =1, 2 , 17.0
gear_warning         =0, 2 , 17.0
fuel_pump            =0, 5 , 17.0
starter1             =0, 20, 17.0
light_nav            =0, 5 , 17.0
light_beacon         =0, 5 , 17.0
light_landing        =0, 5 , 17.0
light_taxi           =0, 5 , 17.0
light_strobe         =0, 5 , 17.0
light_panel          =0, 5 , 17.0
max_battery_voltage  =24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=60.0

[forcefeedback]
stick_shaker_magnitude=4000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
gear_bump_nose_magnitude=2000           ; 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

[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

Transponder.1=1
Marker.1=1

[pitot_static]
vertical_speed_time_constant=9                //Increasing this value will cause a more instantaneous reaction in the VSI     

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.069458
flap_limit_power=25.439326
flap_limit_idle=13.865579

[hydraulic_system]
electric_pumps=0
engine_map=1,1,1,1
normal_pressure=3000.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0
