// AI only FDE for Dan Watkins Shorts Skyvan
[General]
atc_type=Shorts
atc_model=SC7
editable=1
performance=Max Cruise Speed\t280 kts\nMaximum Range\t1,049 nm\nService Ceiling\t35,000 ft\nMax Gross Weight\t25,700 lb\nSeating\t\tUp to 11\nUseful Load\t5,810 lb\n
[WEIGHT_AND_BALANCE]
max_gross_weight = 34500 // (pounds)
empty_weight = 22730 // (pounds)
reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = 0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 19
//station_load.0 = "170, -9.8, -1.75, 0.0, Pilot" //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.1 = "170, -9.8, 1.75, 0.0, Co-Pilot" //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
//station_load.2 = "5660, -17.0, 0.0, 0.0, Payload" //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 111701
empty_weight_roll_MOI = 61201
empty_weight_yaw_MOI = 161691
empty_weight_coupled_MOI = 0
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 1.5
aileron_effectiveness = 1.0
rudder_effectiveness = 1.0
pitch_stability = 1.5
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 2.0
aileron_trim_effectiveness = 1.0
rudder_trim_effectiveness = 1.0
[GeneralEngineData]
engine_type = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = -28.4, -9.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = -28.4, 9.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency
min_throttle_limit = -0.20 //Minimum percent throttle. Generally negative for turbine reverser
[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)
[TurbineEngineData]
fuel_flow_gain = 0.005 //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
[turboprop_engine]
power_scalar = 0.8 //Scalar on Turboprop power
maximum_torque = 7878 //Maximum torque available (ft-lbs)
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3, 1.43, -32.35, 6.43, fx_navred ,
light.1 = 3, 1.43, 32.35, 6.43, fx_navgre ,
light.2 = 3, -23.71, 10.25, 2.82, fx_navwhi ,
light.3 = 3, -23.71, -10.25, 2.82, fx_navwhi ,
light.4 = 2, 1.83, -32.35, 6.43, fx_strobe ,
light.5 = 2, 1.83, 32.35, 6.43, fx_strobe ,
light.6 = 2, -1.28, 0.00, 6.92, fx_beacon ,
[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, 5 , 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 2 , 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
//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)
[contact_points]
//wheels
point.0= 1, 14.0, 0.0, -4.7, 1500.0, 0, 1.0, 40.0, 0.15, 2.5, 0.8, 0.0, 0.0, 0, 0.0, 0.0
point.1= 1, -2.0, -6.5, -5.0, 1800.0, 1, 1.6, 0.0, 0.50, 2.5, 0.7, 0.0, 0.0, 2, 0.0, 0.0
point.2= 1, -2.0, 6.5, -5.0, 1800.0, 2, 1.6, 0.0, 0.50, 2.5, 0.7, 0.0, 0.0, 3, 0.0, 0.0
//scrapes
point.3= 2.000, -3.330, -23.920, -3.000, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -3.330, 23.920, -3.000, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -22.670, 0.000, 0.000, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 23.080, 0.000, -1.500, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = 0.0
static_cg_height = 5.5
gear_system_type=0
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 15.0 //Flap angle that activates warning at idle
flap_limit_power = 30.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.20 //Brake scalar
[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= -8.8, -1.45, 2.1 //(feet) longitudinal, lateral, vertical distance from reference datum
[flaps.0]
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.8 // 0.0 .. 1.0
extending-time = 5 // seconds
flaps-position.0 = 0 // degrees, KIAS
flaps-position.1 = 10 // degrees, KIAS
flaps-position.2 = 30 // degrees, KIAS
flaps-position.3 = 40 // degrees, KIAS
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain = -31.1, -9.1, 3.9, 417.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -31.1, 9.1, 3.9, 417.5, 0.0 //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
[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
[Reference Speeds]
flaps_up_stall_speed = 92.0 //Knots True (KTAS)
full_flaps_stall_speed = 72.0 //Knots True (KTAS)
cruise_speed = 165.0 //Knots True (KTAS)
max_indicated_speed = 180.0 //Red line (KIAS)
max_mach=0.579980
[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= 150.0, 250.0
aileron= 150.0, 250.0
rudder= 150.0, 250.0
[autopilot]
default_bank_mode=0
default_pitch_mode=0
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1000.0
autothrottle_available= 0
pitch_takeoff_ga=8.0
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=25.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
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
[stall_warning]
type=2
[direction_indicators]
direction_indicator.0=3,0
[forcefeedback]
gear_bump_nose_magnitude = 6000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 6000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 6000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5#
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1#
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
//
//Default FF Code installed by FFUtil 22:27:41 10-09-2004
[fltsim.0]
title=Skyvan
sim=Shorts Skyvan AI
model=c
panel=
sound=
texture=
kb_checklists=
kb_reference=Skyvan_ref
ui_manufacturer=Shorts
ui_type=Skyvan
ui_variation=BLANK
atc_id=GSKYV
atc_airline=
description=Shorts Skyvan
[fltsim.1]
title=Skyvan Skylift
sim=Shorts Skyvan AI
model=c
panel=
sound=
texture=Skylift
kb_checklists=
kb_reference=Skyvan_ref
ui_manufacturer=Shorts
ui_type=Skyvan
ui_variation=Skylift
atc_id=PT-PQD
atc_airline=
description=Shorts Skyvan Skylift
[fltsim.2]
title=Skyvan Arctic Circle Air
sim=Shorts Skyvan AI
model=c
panel=
sound=
texture=aca
kb_checklists=
kb_reference=Skyvan_ref
ui_manufacturer=Shorts
ui_type=Skyvan
ui_variation=Arctic Circle Air
atc_id=N101WA
atc_airline=ARTIC CIRCLE AIR
description=Shorts Skyvan Arctic Circle Air
[fltsim.3]
title=Skyvan North Star Air Cargo
sim=Shorts Skyvan AI
model=c
panel=
sound=
texture=nsac
kb_checklists=
kb_reference=Skyvan_ref
ui_manufacturer=Shorts
ui_type=Skyvan
ui_variation=North Star Air Cargo
atc_id=N53NS
atc_airline=NORTH STAR
description=Shorts Skyvan North Star Air Cargo
[fltsim.4]
title=Skyvan Austrian Air Force
sim=Shorts Skyvan AI
model=nc
panel=
sound=
texture=aaf
kb_checklists=
kb_reference=Skyvan_ref
ui_manufacturer=Shorts
ui_type=Skyvan
ui_variation=Austrian Air Force
atc_id=
atc_airline=AIR FORCE
description=Shorts Skyvan North Star Air Cargo
[fltsim.5]
title=Skyvan RAFO-Royal Air Force Oman
sim=Shorts Skyvan AI
model=nc
panel=
sound=
texture=RAFO-Royal Air Force Oman
kb_checklists=
kb_reference=Skyvan_ref
ui_manufacturer=Shorts
ui_type=Skyvan
ui_variation=RAFO Royal Air Force Oman
atc_id=
atc_airline=MAJAN
description=Shorts Skyvan
atc_parking_codes=C23,M003
atc_parking_types=MIL_CARGO
