[fltsim.0]
title=DHC-3 Otter PZL
sim=DHC3 PZL
model=
panel=
sound=
texture=
kb_checklists=OtterPZL_check
kb_reference=OtterPZL_ref
atc_id=NW006A
ui_manufacturer=de Havilland
ui_type=DHC-3 Otter PZL
ui_variation=Neutral White
description=This Otter is the 1000hp conversion from Airtech Canada (R). With 400 more horsepower than the original P&W R1340, the 1000 hp PZL engine (reminiscent R1820 Wright "Cyclone") offers significant performance gains. Take off and climb are dramatically improved, especially on floats.
visual_damage=0
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0

[fltsim.1]
title=DHC-3 Otter PZL Paint1
sim=DHC3 PZL
model=
panel=
sound=
texture=1
kb_checklists=OtterPZL_check
kb_reference=OtterPZL_ref
atc_id=C-FODJ
ui_manufacturer=de Havilland
ui_type=DHC-3 Otter PZL
ui_variation=Green Airways
description=This Otter is the 1000hp conversion from Airtech Canada (R). With 400 more horsepower than the original P&W R1340, the 1000 hp PZL engine (reminiscent R1820 Wright "Cyclone") offers significant performance gains. Take off and climb are dramatically improved, especially on floats.
visual_damage=0
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
atc_airline=Green Airways

[fltsim.2]
title=DHC-3 Otter PZL Paint2
sim=DHC3 PZL
model=
panel=
sound=
texture=2
kb_checklists=OtterPZL_check
kb_reference=OtterPZL_ref
atc_id=GE006A
ui_manufacturer=de Havilland
ui_type=DHC-3 Otter PZL
ui_variation=Globe Explorer
description=This Otter is the 1000hp conversion from Airtech Canada (R). With 400 more horsepower than the original P&W R1340, the 1000 hp PZL engine (reminiscent R1820 Wright "Cyclone") offers significant performance gains. Take off and climb are dramatically improved, especially on floats.
visual_damage=0
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
atc_airline=Globe Explorer

[fltsim.3]
title=DHC-3 Otter PZL Paint3
sim=DHC3 PZL
model=
panel=
sound=
texture=3
kb_checklists=OtterPZL_check
kb_reference=OtterPZL_ref
atc_id=NA006A
ui_manufacturer=de Havilland
ui_type=DHC-3 Otter PZL
ui_variation=Northern Airways
description=This Otter is the 1000hp conversion from Airtech Canada (R). With 400 more horsepower than the original P&W R1340, the 1000 hp PZL engine (reminiscent R1820 Wright "Cyclone") offers significant performance gains. Take off and climb are dramatically improved, especially on floats.
visual_damage=0
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
atc_airline=Northern Airways

[fltsim.4]
title=DHC-3 Otter PZL Paint4
sim=DHC3 PZL
model=
panel=
sound=
texture=4
kb_checklists=OtterPZL_check
kb_reference=OtterPZL_ref
atc_id=AA006A
ui_manufacturer=de Havilland
ui_type=DHC-3 Otter PZL
ui_variation=Air Services
description=This Otter is the 1000hp conversion from Airtech Canada (R). With 400 more horsepower than the original P&W R1340, the 1000 hp PZL engine (reminiscent R1820 Wright "Cyclone") offers significant performance gains. Take off and climb are dramatically improved, especially on floats.
visual_damage=0
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
atc_airline=Air Services

[General]
atc_type=OTTER 
atc_model=DHC-3 
performance=Max. autorised Speed: 155 KIAS\nCruising speed: 120 KIAS @ 3.000 ft\nRange: ~ 1.500 km @ cruise Speed and alt.\nLength: 14,0 m (45,93') with floats\nHeight: 6,65m (21,82') with gear down\nWing Span: 17,80 m (58,40')\nEmpty weight: 5.100 pounds\nMax. gross weight: 8.000 pounds\nFuel capacity: 2x 165 gallons\nEngine: 9 cylinder PZL \nHorsepower: 1.000  
editable=1 

[weight_and_balance]
max_gross_weight = 8000
empty_weight = 5100
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 250000
empty_weight_roll_MOI = 150000
empty_weight_yaw_MOI = 250000
empty_weight_coupled_MOI = 0
max_number_of_stations = 2
station_load.0 = 180.000000, 6.230000, -1.540000, 1.300000, Pilot
station_load.1 = 1.000000, -0.800000, 0.000000, 0.550000, Passenger
station_load.2 = 180.000000, 6.230000, 1.540000, 1.300000, Copilot
station_load.3 = 1.000000, -10.000000, 0.000000, 0.550000, Luggage

[lights]
light.0 = 3, 1.68, 29.33, 4.5, fx_navgre
light.1 = 3, 1.68, -29.33, 4.5, fx_navred
light.2 = 1, -6.71, 0, 4.83, fx_beacon
light.3 = 3, -27.68, 0, -1.12, fx_navwhi
light.4 = 2, 1.07, 29.28, 4.5, fx_strobe
light.5 = 4, 0.76, 0, 1.7, fx_vclight
light.6 = 4, -7.84, 0, 1.7, fx_vclight
light.7 = 4, -3.72, 0, 1.7, fx_vclight
light.8 = 4, 6.15, 0, 2.71, fx_vclight
light.9 = 2, 1.07, -29.28, 4.5, fx_strobe

[GeneralEngineData]
engine_type = 0
fuel_flow_scalar = 1.0
min_throttle_limit = 0.0
master_ignition_switch = 1
engine.0 = 14, 0, 0, 

[effects]
wake = fx_wake_ss
water = fx_spray
waterspeed = fx_wtrspray_s
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
windshield_rain_effect_available = 1

[fuel]
fuel_type = 1
number_of_tank_selectors = 1
electric_pump = 1
LeftMain = 4, 0, -1.85, 165, 3
RightMain = -4, 0, -1.85, 165, 3

[contact_points]
static_pitch = 0
static_cg_height = 11.4
tailwheel_lock = 0
gear_system_type = 1
max_number_of_points = 14
point.0 = 1, 17.568, -7.4, -11.5, 2500, 0, 1.4, 45, 0.3, 2.5, 0.9, 4, 4, 0, 0, 0
point.1 = 1, 17.6, 7.4, -11.5, 2500, 0, 1.4, 45, 0.3, 2.5, 0.9, 4, 4, 0, 0, 0
point.2 = 1, -6, -7.4, -11.5, 2800, 1, 1.5, 0, 0.4, 2.5, 0.9, 4, 4, 2, 0, 0
point.3 = 1, -6, 7.4, -11.5, 2800, 2, 1.5, 0, 0.4, 2.5, 0.9, 4, 4, 3, 0, 0
point.4 = 4.000, 15.700, -7.400, -9.100, 1600.000, 0.000, 0.000, 0.000, 0.950, 2.500, 0.950, 0.000, 0.000, 0.000, 0.000, 0.000
point.5 = 4.000, 15.700, 7.400, -9.100, 1600.000, 0.000, 0.000, 0.000, 0.950, 2.500, 0.950, 0.000, 0.000, 1.000, 0.000, 0.000
point.6 = 4.000, -15.400, -7.400, -8.500, 1600.000, 0.000, 0.000, 0.000, 0.850, 2.500, 0.950, 0.000, 0.000, 2.000, 0.000, 0.000
point.7 = 4.000, -15.400, 7.400, -8.500, 1600.000, 0.000, 0.000, 0.000, 0.850, 2.500, 0.950, 0.000, 0.000, 3.000, 0.000, 0.000
point.8 = 2.000, 1.500, -29.500, 4.500, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.9 = 2.000, 1.500, 29.500, 4.500, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.10 = 2.000, -23.800, 0.000, -2.800, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.11 = 2, 13.0164, 0, -2.9488, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.12 = 2.000, -27.500, 0.000, -1.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.13 = 5, -15.3991, 0, -8.4996, 2500, 0, 0, 45, 0.4, 2.5, 1, 1.2, 1.2, 4, 0, 0

[keyboard_response]
elevator = 100, 180
aileron = 200, 1000
rudder = 200, 1000

[forcefeedback]
gear_bump_nose_magnitude = 1000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2000
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2000
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 450
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1
crash_magnitude1 = 2000
crash_direction1 = 1000
crash_magnitude2 = 2000
crash_direction2 = 9000
crash_period2 = 7500
crash_duration2 = 2500000
stick_shaker_magnitude = 2000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
wing_area = 336.85
wing_span = 58.54
wing_root_chord = 6.86
wing_dihedral = 2
wing_incidence = 0
wing_twist = 0
oswald_efficiency_factor = 0.900
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 3.51
wing_pos_apex_vert = 3.42
htail_area = 82.85
htail_span = 20.18
htail_pos_lon = -21.79
htail_pos_vert = 3.70
htail_incidence = -1.475
htail_sweep = 3
vtail_area = 80.74
vtail_span = 13.07
vtail_sweep = 40
vtail_pos_lon = -13.58
vtail_pos_vert = -2.75
elevator_area = 42.53
aileron_area = 45.18
rudder_area = 26.19
elevator_up_limit = 25.000
elevator_down_limit = 25.000
aileron_up_limit = 20.000
aileron_down_limit = 20.000
rudder_limit = 25.000
elevator_trim_limit = 20.000
spoiler_limit = 0
aileron_to_spoileron_gain = 0.000
spoiler_handle_available = 0
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 100
engine_generator_map = 1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 20, 17
marker_beacon = 1, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
light_nav = 0, 5, 17
light_beacon = 0, 5, 17
light_landing = 0, 5, 17
light_strobe = 0, 5, 17
light_panel = 0, 5, 17
light_cabin = 0, 5, 17
directional_gyro = 0, 5, 17
directional_gyro_slaving = 0, 5, 17

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000 
drag_scalar= 1.200
pitch_scalar= 0.0
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 30.000, 0.000
flaps-position.4= 40.000, 0.000

[Reference Speeds]
flaps_up_stall_speed=70.000 
full_flaps_stall_speed=52.000 
cruise_speed=120.000 
max_indicated_speed=155.000000
max_mach=0.275000

[flight_tuning]
cruise_lift_scalar=1.000 
parasite_drag_scalar=1.000 
induced_drag_scalar=1.000 
elevator_effectiveness=1.000 
aileron_effectiveness=1.000 
rudder_effectiveness=1.000 
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 

[piston_engine]
power_scalar=1.0
cylinder_displacement=202.5
compression_ratio=6.4
number_of_cylinders=9
max_rated_rpm=2000
max_rated_hp=1000
fuel_metering_type=2
cooling_type=0
normalized_starter_torque=0.3
turbocharged=1
max_design_mp=47
min_design_mp=10
critical_altitude=7000
emergency_boost_type=0
emergency_boost_mp_offset=0
emergency_boost_gain_offset=0
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.0
idle_rpm_mechanical_efficiency_scalar=1.0
max_rpm_friction_scalar=1.0
idle_rpm_friction_scalar=1.0

[propeller]
propeller_type=0 
propeller_diameter=11.811 
propeller_blades=4 
propeller_moi=8.000000 
beta_max=34.000000 
beta_min=11.000000 
min_gov_rpm=1400.000000 
prop_tc=0.100000 
gear_reduction_ratio=1
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=1.000000 
defeathering_accumulators_available=0 
prop_reverse_available=0 
minimum_on_ground_beta=0.000000 
minimum_reverse_beta=0.000000 

[Radios]
Audio.1=1 
Com.1=1, 1 
Com.2=1, 1 
Nav.1=1, 1, 1 
Nav.2=1, 1, 1 
Adf.1=1 
Transponder.1=1 
Marker.1=1 

[direction_indicators]
direction_indicator.0=2,0 

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=1500.000 
autothrottle_available=0 
pitch_takeoff_ga=8.000 
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

[views]
eyepoint=5.85, -1.75, 3.00 

[exits]
number_of_exits = 1
exit_rate.0 = 0.65

[brakes]
toe_brakes_scale=1.0
parking_brake=1

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0
flap_limit_power=0
flap_limit_idle=0

[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=3000.0

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0