[fltsim.0]
title=DHC6-300 Short Nose Twin Sea Otter_Labrador Airways
sim=dhc6F_AI
model=
panel=
sound=
texture=
kb_checklists=DHC6_CHECK
kb_reference=DHC6_REF
atc_id=C-FAUS
ui_manufacturer=DeHavilland
ui_type=DHC6 Twin Sea Otter
ui_variation=Labrador Airways
atc_parking_codes=LA
description=FS2004\nDeHavilland\nDHC6-300S\nShort Nose Twin Sea Otter\nFOR AI USE ONLY\nAll files Copyright 2004\nPremier Aircraft Design\nhttp:\/\/www.flightsimnetwork.com\/premaircraft
atc_heavy=0
atc_airline=
atc_flight_number=

[General]
performance=Height 18 feet - 7 inches\nRate of Climb: 1000 fpm\nCeiling 21,000 feet\nEmpty Weight:7,415 lb\nMax T\/O wt. 12,500 lb\nPower: 2 x 652 SHP P&W PT6A-27\nStall: 74 kts Clean \/ 58 kts full flaps/nNormal AI Cruise Speed: 140 / 160  KIAS/nNormal AI Cruise Altitude: 4000 / 6000 Ft AGL
atc_type=DEHAVILLAND
atc_model=DHC6

[WEIGHT_AND_BALANCE]
empty_weight=7415		// (pounds)

reference_datum_position=0.0, 0, 0	// (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.9, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=20

station_load.0=170,  5.0, -2.0, 0.0		//Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170,  5.0,  2.0, 0.0		//Co-Pilot     Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=170, -2.1, -2.0, 0.0		//Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=170, -2.1,  2.0, 0.0		//Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

empty_weight_roll_MOI= 10059.000
empty_weight_pitch_MOI= 16474.000
empty_weight_yaw_MOI= 24137.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 10775.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[SMOKESYSTEM]
smoke.0=0.00, 2.00,  9.40, fx_engsmoke

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[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
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 , 1

[fuel]
LeftMain= 0.000, -14.500, -1.000, 135.000, 0.000
LeftAux= 0.000, -6.000, -1.500, 50.000, 0.000
RightMain= 0.000, 14.500, -1.000, 135.000, 0.000
RightAux= 0.000, 6.000, -1.500, 50.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0

[pitot_static]
vertical_speed_time_constant=100

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
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

[contact_points]
//Classes...What type of point    0=Unused or Ignore
//                                                      1=Wheel
//                                                      2=Scrape point
//                                                      4=Float
//                                                      5=Float Rudder
//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= 4.000, 11.000, -6.250, -8.300, 1600.000, 0.000, 0.000, 0.000, 0.850, 2.500, 0.650, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 4.000, 11.000, 6.250, -8.300, 1600.000, 0.000, 0.000, 0.000, 0.850, 2.500, 0.650, 0.000, 0.000, 0.000, 0.000, 0.000
point.2= 4.000, -16.000, -6.250, -8.000, 1600.000, 0.000, 0.000, 0.000, 0.950, 2.500, 0.650, 0.000, 0.000, 2.000, 0.000, 0.000
point.3= 4.000, -16.000, 6.250, -8.000, 1600.000, 0.000, 0.000, 0.000, 0.950, 2.500, 0.650, 0.000, 0.000, 3.000, 0.000, 0.000
point.4= 2.000, 1.500, -33.417, 4.417, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.5= 2.000, 1.500, 33.417, 4.417, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.6= 2.000, -26.417, 0.000, -0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.7= 2.000, 14.000, 0.000, -0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.8= 2.000, 1.500, 33.417, 4.417, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.9= 2.000, -26.417, 0.000, -0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.10= 2.000, 14.000, 0.000, -0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.11= 5.000, -16.000, 0.000, -8.000, 1600.000, 0.000, 0.000, 30.000, 0.000, 0.000, 0.700, 1.000, 1.200, 0.000, 0.000, 0.000

static_pitch= 1.000
static_cg_height=7.000

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3,  0.0, -32.75,  2.70, fx_navred ,
light.1=3,  0.0,  32.75,  2.70, fx_navgre ,
light.2=3,  -31.3,   0.00,  -0.3, fx_navwhi ,
light.3=2,   -0.4, -32.75,  2.7, fx_strobe ,
light.4=2,   -0.4,  32.75,  2.7, fx_strobe ,
light.5=1,  -28.9,   0.00,  12.0, fx_beacon ,
light.6=1,  -19.9,   0.00, -3.4, fx_beacon ,
light.7=4,   5.91,   0.00,  1.64, fx_vclight,


[airplane_geometry]
wing_area= 368.000
wing_span= 65.000
wing_root_chord= 6.167
wing_dihedral= 2.499
wing_incidence= 0.100
wing_twist= -1.500
oswald_efficiency_factor= 0.360
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 67.000
htail_span= 17.167
htail_pos_lon= -24.583
htail_pos_vert= 0.000
htail_incidence= 0.500
htail_sweep= 0.000
vtail_area= 42.000
vtail_span= 7.389
vtail_sweep= 0.000
vtail_pos_lon= -20.500
vtail_pos_vert= 4.083
elevator_area= 36.000
aileron_area= 32.000
rudder_area= 21.000
elevator_up_limit= 25.000
elevator_down_limit= 16.000
aileron_up_limit= 17.500
aileron_down_limit= 16.000
rudder_limit= 19.000
elevator_trim_limit= 19.500
spoiler_limit= 59.000
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[GeneralEngineData]
engine_type= 5
Engine.0= 5.833, -9.167, 0.000
Engine.1= 5.833, 9.167, 0.000
fuel_flow_scalar= 1.000
min_throttle_limit=-0.250000

[TurbineEngineData]
fuel_flow_gain= 0.025
inlet_area= 0.250
rated_N2_rpm= 29920.000
static_thrust= 158.000
afterburner_available= 0

[propeller]
propeller_type= 0
propeller_diameter= 8.950
propeller_blades= 4
propeller_moi= 120.000
beta_max= 45.000
beta_min= 15.000
min_gov_rpm= 25520.000
prop_tc= 0.004
gear_reduction_ratio= 17.600
fixed_pitch_beta= 20.000
low_speed_theory_limit= 80.000
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather= 700.000
beta_feather= 79.300
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 1
minimum_on_ground_beta= 1.000
minimum_reverse_beta= -18.000

[turboprop_engine]
maximum_torque= 2200.000

[Reference Speeds]
flaps_up_stall_speed= 74.000
full_flaps_stall_speed= 59.200
cruise_speed=160.000
max_indicated_speed=259.000000
max_mach=0.579980

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=8.740363,0.0000,2.742577

[direction_indicators]
direction_indicator.0=3,0

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time=8.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 20.000, 0.000
flaps-position.4=30.000, 0.000
[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0