[fltsim.0]
title=Spindrift
sim=Spindrift
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=spun
atc_id_color=0xff000000
atc_parking_types=RAMP
ui_manufacturer=Imagination
ui_type="Imagination"
ui_variation="Imagination"
description= You are the Captain of the Spindrift, a fine old ship with great character and a colourful history. Steampunk powered.
[General]
atc_type=spindrift
atc_model=spindrift
editable=1
performance= Full throttle in water will cause rotation at around 135 Knots. Keep the bow up a bit when landing or you'll swamp the engine room and kill the prop.
[WEIGHT_AND_BALANCE]
max_gross_weight = 8000 // (pounds)
empty_weight = 4895 // (pounds)
reference_datum_position = 13.1, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position = -13.6, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations = 50
station_load.0 = "170.0, -11.3, -1.5, 0.0, Pilot" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170.0, -11.3, 1.5, 0.0, Passenger 2" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "160.0, -13.9, -2.0, 0.0, Passenger 3" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "160.0, -13.9, 2.0, 0.0, Passenger 4" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "0.0, -18.8, -2.0, 0.0, Passenger 5" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "0.0, -18.8, 2.0, 0.0, Passenger 6" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = " 50.0, -21.0, 0.0, 0.0, Cargo Zone 3" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = "25.0, -23.5, 0.0, 0.0, Cargo Zone 4" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = "0.0, -25.6, 0.0, 0.0, Cargo Zone 5" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.9 = "0.0, -27.5, 0.0, 0.0, Cargo Zone 6" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.10 = "0.0, -9.9, -5.3, -6.5, Left Baggage" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.11 = "0.0, -9.9, 5.3, -6.5, Right Baggage" // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
;Moments of Inertia
empty_weight_pitch_MOI = 7241.36
empty_weight_roll_MOI = 5618.57
empty_weight_yaw_MOI = 10431.43
empty_weight_coupled_MOI = 0.0
[Flaps.0]
type=1
span-outboard=0.5 // Percent span for flap position
extending-time=5.7 // Seconds, time to fully extend
system_type=0 // 0 = electrical
damaging-speed = 175 // KIAS
blowout-speed = 175 // KIAS
flaps-position.0= 0 // degrees
flaps-position.1=10,175 // degrees
flaps-position.2=20,150 // degrees
flaps-position.3=30,125 // degrees
[flight_tuning]
cruise_lift_scalar = 1.0
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.0
elevator_effectiveness = 0.667 //Default for this whole section is 1.0. The aileron effectiveness is low low for nice effect
aileron_effectiveness = 0.1
rudder_effectiveness = 0.533
pitch_stability = 1.0
roll_stability = 1.0
yaw_stability = 1.0
elevator_trim_effectiveness = 1.0
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 = -1.3, 0.0, 0.0
//Engine.1 = //(feet) longitudinal, lateral, vertical distance from reference datum /default=-1.3, 0.0, 0.0
fuel_flow_scalar = 1.12 //Scalar for fuel flow efficiency
min_throttle_limit = -0.25 //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 = 8.8 //Propeller Diameter, (feet)
propeller_blades = 3 //Number of propeller blades
propeller_moi = 19 //Propeller moment of inertia
beta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min = 15.6 //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 = 17.4 //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 = 0 //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 = 88.0 //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 = 0.011 //Gain on fuel flow
inlet_area = 1.0 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 33000 //RPM, second stage compressor rated value
static_thrust = 350 // was138 It was 138 changed from default I think, then I added more.
[turboprop_engine]
power_scalar = 1.0 //Scalar on Turboprop power
maximum_torque = 1865 //Maximum torque available (ft-lbs)
[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
[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 = 4, -4.00, -5.250, -5.00, 1600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 0, 0.0, 0.0
point.1 = 4, -4.00, 5.250, -5.00, 1600, 0, 0.00, 0.0, 0.85, 2.5, 0.65, 0.0, 0.0, 1, 0.0, 0.0
point.2 = 4, -26.35, -5.250, -5.00, 1600, 0, 0.00, 0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 2, 0.0, 0.0
point.3 = 4, -26.35, 5.250, -5.00, 1600, 0, 0.00, 0.0, 0.95, 2.5, 0.65, 0.0, 0.0, 3, 0.0, 0.0
point.4 = 2, 71.00, 21.88, 54.25,
point.5 = 2, 71.00, -21.88, 54.25,
point.6 = 2, -10.00, -27.13, 54.25,
point.7 = 2, -10.00, 27.13, 54.25,
point.8 = 2, -10.00, 0.00, 79.00,
point.9 = 2, 122.90, 0.00, 54.25,
point.10 = 2, 97.00, 16.17, 54.25,
point.11 = 2, 97.00, -16.17, 54.25,
point.12 = 2, 83.00, 0.00, 72.90,
point.13 = 2, 87.50, 0.00, 3.40,
point.14 = 2, 37.00, 0.00, 78.00,
point.15 = 2, 37.00, 14.10, -0.60,
point.16 = 2, 37.00, -14.10, 0.60,
point.17 = 2, 57.00, -11.72, -0.60,
point.18 = 2, 57.00, 11.72, -0.60,
max_number_of_points = 21
static_pitch=0.983 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=4.244 //feet, altitude of CG when at rest on the ground
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 2 //Amphib
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 20.1 //Flap angle that activates warning at idle
flap_limit_power = 13.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.68 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,0,0,0 //pump on Eng1
[Views]
eyepoint= -10.5, -1.4, 2.4 //(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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//light.0 = 3, -13.80, -5.75, 20.72, fx_smoke_w ,
//light.1 = 3, -13.80, 5.75, 20.72, fx_smoke_w ,
light.2 = 3, -16.55, -5.75, 20.72, fx_engsmoke ,
light.3 = 3, -16.55, 5.75, 20.72, fx_engsmoke ,
[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= 100, 180
aileron= 200, 1000
rudder= 200, 1000
[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
[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
[airspeed_indicators]
airspeed_indicator.0 = 1.16, -22.0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[fuel]
LeftMain = -15.3, -1.1, 2.5, 166.0, 3.6 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -15.3, 1.1, 2.5, 166.0, 3.6 //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 = 279.0 //Square feet
wing_span = 52.1 //Feet
wing_root_chord = 6.4 //Feet
wing_dihedral = 3.9 //Degrees
wing_incidence = 2.5 //Degrees
wing_twist = -1.7 //Degrees
oswald_efficiency_factor= 0.7 //Measure of lift effeciency of wing
wing_winglets_flag = 0 //Are winglets available?
wing_sweep = 2.96 //Degrees, wing leading edge
wing_pos_apex_lon = -12.3 //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 = 39.0 //Square feet
htail_span = 11.7 //Feet
htail_pos_lon = -27.8 //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 = 2.0 //Degrees
htail_sweep = 5.0 //Degrees, horizontal tail leading edge
vtail_area = 18.0 //Square feet
vtail_span = 4.8 //Feet, tip to body
vtail_sweep = 45.0 //Degrees, vertical tail leading edge
vtail_pos_lon = -25.7 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 1.5 //Feet, vertical distance from reference point, positive going up
elevator_area = 16.6 //Square feet
aileron_area = 18.3 //Square feet
rudder_area = 6.7 //Square feet
elevator_up_limit = 28.0 //Degrees
elevator_down_limit = 21.0 //Degrees
aileron_up_limit = 20.0 //Degrees
aileron_down_limit = 15.0 //Degrees
rudder_limit = 24.0 //Degrees
elevator_trim_limit = 19.5 //Degrees
spoiler_limit = 20.0 //Degrees
spoilerons_available = 1 //Spoilerons Available?
aileron_to_spoileron_gain = 1 //Aileron to spoileron gain
min_ailerons_for_spoilerons = 0 //Degrees
min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate
spoiler_handle_available = 0 //Defaults to True if spoiler limit > 0, else False. Should be False for spoilerons only
[Reference Speeds]
flaps_up_stall_speed = 72.0 //Knots True (KCAS)
full_flaps_stall_speed = 58.0 //Knots True (KCAS)
cruise_speed = 143.0 //Knots True (KTAS)
max_mach = 0.60
max_indicated_speed = 175 //Red line (KIAS)
[autopilot]
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 = 0.0
[forcefeedback]
gear_bump_nose_magnitude=3000 ; 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=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 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
[stall_warning]
type=2
