[fltsim.0] title=DHC-6-300 Twin Otter Armada de Venezuela sim=DHC-6 model= panel= sound= texture= kb_checklists=DHC6_CHECK kb_reference=DHC6_REF atc_id_enable=1 atc_id_color=Armada ui_manufacturer=DeHavilland ui_type=DHC-6-300 Twin Otter ui_variation=Armada de Venezuela description=Twin Otter Armada de Venezuela. Panel + Model : Eric Dantès. Repaint by Juan Ernesto Oropeza. atc_id=ARV-014 atc_airline= atc_flight_number=134 atc_heavy=0 [General] performance=Wingspan: 65'3"\nLength : 53'8"\nHeight : 19'6"\nZFW : 7,4150 lbs\nMTOW : 12,500 lbs\nSpeeds : Max Cruise 190 Kts \nHigh Speed Cruise : 180 Kts\nEco Cruise : 172 Kts ( all KIAS ).\nStall Speed : Clean - 74 Kts\nStall Dirty - 58 Kts ( with full Flaps )\nPower : Two 652 SHP P&W Canada PT6A-27 \nTurboshaft Engines driving Hartzell 3 blade 8'-4" Dia Propellers.\nFuel : 400\nAircraft By:Steven Grant\n atc_type=DEHAVILLAND atc_model=DHC6 [WEIGHT_AND_BALANCE] max_gross_weight=12500 // (pounds) empty_weight=7415 // (pounds) CG_forward_limit=0.000 CG_aft_limit=1.000 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=50 station_load.0=220, 9.60, -1.70, 3.00 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=000, 9.60, 1.70, 3.00 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=200, 4.60, 0.00, 0.00 //Station 1 Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=200, 2.88, 0.00, 0.00 //Station 2 Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=200, 1.67, 0.00, 0.00 //Station 3 Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5=200, -0.55, 0.00, 0.00 //Station 4 Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6=000, -2.27, 0.00, 0.00 //Station 5 Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7=300, -3.98, 0.00, 0.00 //Station 6 Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.8=000, -5.70, 0.00, 0.00 //Station 6 Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.9=300, 14.60, 0.00, 0.50 //Nose Compartment(300lbs Max) Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.10=500,-11.80, 0.00, 0.50 //Aft Compartment(500lbs Max) Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_roll_MOI=26000.000 empty_weight_pitch_MOI=92500.000 empty_weight_yaw_MOI=36500.000 empty_weight_coupled_MOI=2275.000p [fuel] LeftMain= -0.20, 0.00, -1.50, 181.00, 6.00 RightMain=-5.50, 0.00, -1.50, 197.00, 7.00 fuel_type= 2.000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=420.000 wing_span=65.000 wing_root_chord=6.417 wing_dihedral=3.000 wing_incidence=0.000 wing_twist=0.275 oswald_efficiency_factor=0.926 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=1.000 wing_pos_apex_vert=5.000 htail_area=85.000 htail_span=20.000 htail_pos_lon=-28.55 htail_pos_vert=6.833 htail_incidence=0.417 htail_sweep=0.000 vtail_area=91.000 vtail_span=10.877 vtail_sweep=0.000 vtail_pos_lon=-28.55 vtail_pos_vert=5.50 elevator_area=22.800 aileron_area=14.250 rudder_area=20.500 elevator_up_limit=25.000 elevator_down_limit=16.000 aileron_up_limit=17.5.000 aileron_down_limit=16.000 rudder_limit=19.000 elevator_trim_limit=20.000 spoiler_limit=60.000 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 //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] point.0=1.000, 13.000, 0.000, -5.000, 1600, 0.000, 0.568, 44.100, 0.166, 2.500, 1.043, 0.000, 0.000, 0.000, 0.000, 0.000 point.1=1.000, -1.000, -6.417, -5.500, 1600, 1.000, 0.568, 0.000, 0.309, 2.500, 0.774, 0.000, 0.000, 2.000, 0.000, 0.000 point.2=1.000, -1.000, 6.417, -5.500, 1600, 2.000, 0.568, 0.000, 0.309, 2.500, 0.774, 0.000, 0.000, 3.000, 0.000, 0.000 point.3=2.000, 0.000, -33.417, 5.000, 2500, 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, 0.000, 33.417, 5.000, 2500, 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,-34.750, 0.000, -0.533, 2500, 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, 13.000, 0.000, -2.533, 2500, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=0.000 static_cg_height=5.820 [GeneralEngineData] engine_type=5 Engine.0=-8.333, -4.833, 0.500 Engine.1=-8.333, 4.833, 0.500 fuel_flow_scalar=0.900 min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain=0.015 inlet_area=1.000 rated_N2_rpm=25000.000 static_thrust=158.000 afterburner_available=0 [propeller] thrust_scalar = 1.0 //Propeller thrust scalar propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter = 8.800 //Propeller Diameter, (feet) propeller_blades = 3 //Number of propeller blades propeller_moi = 22.000 //Propeller moment of inertia beta_max = 62.000 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min = 15.000 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm = 25520.000 //Miminum governed RPM prop_tc = 0.004 //Prop time-constant gear_reduction_ratio = 17.600 //Propeller gear reduction ratio fixed_pitch_beta = 20 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit = 80.000 //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 = 700.000 //Minimum RPM for prop feathering beta_feather = 79.300 //Feathering pitch angle (degrees) power_absorbed_cf = 0.900 //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 = 8.300 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta = -13.500 //Minimum pitch angle in reverse, (degree [turboprop_engine] power_scalar=1.0 maximum_torque=3000.000 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -1.7, -32.2, 5.15, fx_navred , light.1=3, -1.7, 32.2, 5.15, fx_navgre , light.2=3, -32.3, 0.00, 0.9, fx_navwhi , light.3=2, -2.1, -32.2, 5.2, fx_strobe , light.4=2, -2.1, 32.2, 5.2, fx_strobe , light.5=1, -29.75, 0.00, 14.15, fx_beacon , light.7=4, 5.91, 0.00, 1.64, fx_vclight, light.8=5, -0.1, -11.8, 4.10, fx_landing.fx , light.9=5, -0.1, 11.8, 4.10, fx_landing.fx , light.10=5, 11.4, -1.00, -3.10, fx_landing.fx , [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_smoke_pt6 smoke.1=0.00, 2.00, -9.40, fx_smoke_pt6 [Reference Speeds] flaps_up_stall_speed=63.000 full_flaps_stall_speed=50.400 cruise_speed=243.361 max_indicated_speed=185.671875 max_mach=0.350000 [keyboard_response] elevator=150.000, 250.000 aileron=150.000, 250.000 rudder=150.000, 250.000 [Views] eyepoint=7.2,-1.3,3.3 [autopilot] use_no_default_bank=1 use_no_default_pitch=1 autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.000 autothrottle_available=0 pitch_takeoff_ga=8.000 default_pitch_mode=0 default_bank_mode=0 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 [direction_indicators] direction_indicator.0=3,0 [Flaps.0] type=1 span-outboard=0.500 extending-time=5.000 system_type=4 damaging-speed=160 blowout-speed=185 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=0.50 flaps-position.0=0.000, 0.000 flaps-position.1=11.750, 0.000 flaps-position.2=23.500, 0.000 flaps-position.3=35.250, 0.000 flaps-position.4=47.000, 0.000 [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 [brakes] toe_brakes_scale=1.000031 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
