[fltsim.0]
title=DHC-2
sim=DHC-2
model=
panel=
sound=
texture=
kb_checklists=DHC2_check
kb_reference=DHC2_ref
atc_id=N930AJ
editable=1
ui_manufacturer=De Havilland
ui_type=DHC-2 Beaver MKI (Wheels)
ui_variation=Royal Dutch Air Force
description=The Beaver was the second design from de Havilland Canada, and is well known for its 'bush' flying role. The aircraft was developed with an eye to the Ontario Department of Lands and Forests which was looking to replace its Stinson SR-9s. The aircraft might have looked very different as it was originally planned for the 295hp Gypsy Queen 50, but development delays for that engine resulted in a change to the 450hp Pratt & Whitney R-985 Wasp Junior. First flying on August 16 1947, and beginning deliveries in April 1948, production did not cease until 1967 for a total of 1,657 aircraft (not counting the Mk.3 'Turbo' Beaver). 

[WEIGHT_AND_BALANCE]

max_gross_weight=5100                  // (pounds)
empty_weight=2850                     // (pounds)

reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=-0.250000,0.000000,0.000000

max_number_of_stations=50
station_load.0=215.00,  2.25, -1.20, 1.75  //Pilot
station_load.1=000.00,  2.25,  1.20, 1.75  //CoPilot
station_load.2=000.00, -2.25, -1.20, 1.75  //Passenger1
station_load.3=000.00, -2.25,  1.20, 1.75  //Passenger2
station_load.4=000.00, -5.00, -1.20, 1.75  //Passenger3
station_load.5=000.00, -5.00,  1.20, 1.75  //Passenger4
station_load.6=000.00, -6.80,  0.00, 0.70  //Baggage

empty_weight_roll_MOI=5343.00000
empty_weight_pitch_MOI=5767.00000
empty_weight_yaw_MOI=9367.00000
empty_weight_coupled_MOI=0.00000

[fuel]
Center1=-1.50, 0.00, -0.75, 35.00, 0.00   //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain=0.30, 0.00, -0.75, 35.00, 0.00   //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-3.00, 0.00, -0.75, 26.00, 0.00   //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=1.00
number_of_tank_selectors=1

[flight_tuning]
cruise_lift_scalar=0.6
parasite_drag_scalar=0.92
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=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[airplane_geometry]
wing_area=250.00
wing_span=48.00
wing_root_chord=5.25
wing_dihedral=1.999512
wing_incidence=1.499634
wing_twist=0.000000
oswald_efficiency_factor=0.750294
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.00
wing_pos_apex_vert=4.00
htail_area=65.00
htail_span=15.83
htail_pos_lon=-21.00
htail_pos_vert=2.00
htail_incidence=0.417480
htail_sweep=0.00
vtail_area=30.00
vtail_span=6.244998
vtail_sweep=0.00
vtail_pos_lon=-20.00
vtail_pos_vert=4.00
elevator_area=27.95
aileron_area=25.00
rudder_area=10.50
elevator_up_limit=28.00
elevator_down_limit=20.00
aileron_up_limit=18.00
aileron_down_limit=11.00
rudder_limit=25.00
elevator_trim_limit=19.480565
spoiler_limit=0.000057
spoilerons_available=0
aileron_to_spoileron_gain=0.00
min_ailerons_for_spoilerons=0.00
min_flaps_for_spoilerons=0.00

//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                (0=Undamped, 1=Critically Damped)
//11 Extension Time               (seconds)
//12 Retraction Time              (seconds)
//13 Sound Type

[contact_points]
point.0=1.00, -20.41,   0.00, -1.60, 1574.80, 0.00, 0.34, 0.45, 0.52, 2.50, 0.73, 5.00, 5.00, 0.00
point.1=1.00,   2.00,  -5.08, -5.40, 1574.80, 1.00, 0.53, 0.00, 0.52, 2.50, 0.73, 5.00, 5.00, 2.00
point.2=1.00,   2.00,   5.08, -5.40, 1574.80, 2.00, 0.53, 0.00, 0.52, 2.50, 0.73, 5.00, 5.00, 2.00
point.3=2.00,   0.00, -24.00,  4.00,  308.47, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00
point.4=2.00,   0.00,  24.00,  4.00,  308.47, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00
point.5=2.00, -21.83,   0.00,  0.33,  916.56, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00
point.6=2.00,   6.50,   0.00, -2.16, 1274.43, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00
point.7=2.00,   0.00, -24.00,  4.00,  308.47, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 7.00
point.8=2.00, -19.58,   0.00,  7.50,   30.03, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 8.00

static_pitch=10.00
static_cg_height=4.489594

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit        
light.0=3,    1.00, -24.90, 4.45, fx_navred
light.1=3,    1.00,  24.90, 4.45, fx_navgre
light.2=3,  -23.00,   0.00, 1.95, fx_navwhi
light.3=2,    0.85, -24.90, 4.45, fx_strobe
light.4=2,    0.85,  24.90, 4.45, fx_strobe
light.5=1,   -5.95,   0.00, 4.50, fx_beacon

[SMOKESYSTEM]
smoke.0=-0.20, 1.20, -1.55, fx_smoke_d3_fx

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

[Flaps.0]
type=1
span-outboard=0.50
extending-time=7.00
system_type=0
flaps-position.0=00.00
flaps-position.1=08.25
flaps-position.2=16.50
flaps-position.3=25.00
flaps-position.4=33.00
flaps-position.5=41.00
flaps-position.6=49.00
flaps-position.7=58.00
damaging-speed=100                                 // KIAS
blowout-speed=120                                  // KIAS
lift_scalar=1.8                                     
drag_scalar=0.6
pitch_scalar=0.2

[GeneralEngineData]
engine_type=0
Engine.0=6.00, 0.00, 0.75
fuel_flow_scalar=0.92

[piston_engine]
cylinder_displacement=109.440000
compression_ratio=6.700000
number_of_cylinders=9
max_rated_rpm=2300.000000
max_rated_hp=450.000000
fuel_metering_type=2
cooling_type=0
normalized_starter_torque=0.18
turbocharged=1
max_design_mp=37.000000
min_design_mp=8.000000
critical_altitude=5000.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000

[propeller]
propeller_type=0
propeller_diameter=9.00
propeller_blades=3
propeller_moi=8.00
beta_max=24.00
beta_min=10.50
min_gov_rpm=1400.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000

[Reference Speeds]
flaps_up_stall_speed=52.00
full_flaps_stall_speed=38.00
cruise_speed=112.00

[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000

[Views]
eyepoint=1.5,-1.0,3.35

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=1,0

[General]
atc_type=DeHavilland
atc_model=DHC2
performance=-Dimensions \nSpan : 48'0 ft \nLength : 30'4 ft \nHeight : 9'0 ft \n-Weight \nempty : 2,850 lb \nmax : 5,100 lb \n-Power Plant : 450hp P&W R-985-AN Wasp Junior \n-Performance : \nmax speed : 140 mph \nceiling : 18.000ft\nrange : 778 miles \n\nAircraft by: Steven Grant - August 2002