[fltsim.0] title=DH114-2B Heron sim=Dh114-2B model= panel= sound= texture= kb_checklists=DH114_ref ui_manufacturer=de Havilland ui_type=DH114-2B Heron ui_variation=prinair atc_heavy=0 atc_id=N581PR atc_airline=prinair description=de Haviland DH114-2B, a 14 pax commuter airliner from the 1960's.\nFSDS2 design: Dee Waldron\ndewaldron@simufly.com [General] atc_type=DEHAVILLAND atc_model=HERN editable=0 performance=MTOW: 13,500 lbs\nLength: 48ft, 6in\nWing Span: 71ft, 6in\nPower: (4) de Havilland Gipsy Queen 30 Mk.2 engines\n\tIn-line, inverted 6 cylinder\n\t250 HP each\n \n [fuel] //Normal fuel is 378 USG=2268lbs (96 octane low lead AVGAS) //Some aircraft have further tankage for long range operation LeftMain=0, -6.45, 0, 122, 0 RightMain=0, 6.45, 0, 122, 0 Leftaux=0, -8.45, 0, 67, 0 Rightaux=0, 8.45, 0, 67, 0 fuel_type=1 number_of_tank_selectors=1 electric_pump=0 [WEIGHT_AND_BALANCE] max_gross_weight=13500 empty_weight=8492 ;before engine conversion and including lavatory, oil, avionics etc max_landing_weight=13150 reference_datum_position=0, 0, 0 empty_weight_CG_position=0, 0, 0 //Max payload with max fuel is 13500 - 8492 - 340 - 2268=2400 lbs = 12 pax plus bags station_load.0=340,0,0,0 ;Two crew station_load.1=2400,0,0,0 ;12 pax plus baggage is maximum with full normal tankage ;station_load.0=170.0, 11.8, -1.25, 2.5 //Captain ;station_load.1=170.0, 11.8, 1.25, 2.5 //First Officer ;station_load.2=170.0, 9.2, -1.25, 2.0 //Passenger ;station_load.3=170.0, 9.2, 1.25, 2.0 //Passenger ;station_load.4=170.0, 0.0, -1.25, 0.0 //Passenger ;station_load.5=170.0, 0.0, 1.25, 0.0 //Passenger ;station_load.6=100.0, 13.3, 0.0, 0.0 //Baggage Moments of Inertia empty_weight_roll_MOI=115000 empty_weight_pitch_MOI=27500 empty_weight_yaw_MOI=125000 empty_weight_coupled_MOI=0.0 [GeneralEngineData] engine_type=0 Engine.0=6.6, -13.250, 0.650 Engine.1=7.65, -6.750, 0.150 Engine.2=7.65, 6.750, 0.150 Engine.3=6.6, 13.250, 0.650 fuel_flow_scalar=1.0 min_throttle_limit=0.000000 [piston_engine] //de Havilland Gipsy Queen Mk.30 Series 2 cylinder_displacement=110.33 compression_ratio=6.5 number_of_cylinders=6 max_rated_rpm=2500 max_rated_hp=250 fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.300000 turbocharged=0 max_design_mp=0.000000 min_design_mp=0.000000 critical_altitude=0.000000 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 ;c/s prop must be used in lieu of real D.H. v/p props propeller_diameter=7.0 propeller_blades=2 propeller_moi=5 beta_max=40 beta_min=15 prop_tc=0.100000 gear_reduction_ratio=1.0 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=1 prop_auto_feathering_available=0 min_gov_rpm=1400.000000 fixed_pitch_beta=0.000000 low_speed_theory_limit=80.000000 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 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 [airplane_geometry] wing_area=499 wing_span=71.5 wing_root_chord=7.0 wing_pos_apex_lon=1.78 oswald_efficiency_factor=0.88 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_vert=0.000000 htail_area=110.000000 htail_span=21.000000 htail_pos_lon=-27.500000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=60.000000 vtail_span=8.831761 vtail_sweep=0.000000 vtail_pos_lon=-25.583333 vtail_pos_vert=1.500000 elevator_area=47.300000 aileron_area=49.900000 rudder_area=21.000000 elevator_up_limit=24.5 elevator_down_limit=16.5 aileron_up_limit=19 aileron_down_limit=19 rudder_limit=19 elevator_trim_limit=16 spoiler_limit=0 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 wing_dihedral=6 wing_incidence=0 wing_twist=0 [Flaps.0] type=1 span-outboard=0.5 extending-time=15 system_type=0 flaps-position.0=0,0 flaps-position.1=20,135 flaps-position.2=60,100 [Reference Speeds] flaps_up_stall_speed=84 full_flaps_stall_speed=65 cruise_speed=159 max_indicated_speed=174 [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 (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) //GEAR point.0=1, 18.85, 0.00, -3.8, 1200, 0, 0.633, 180, 0.42, 2.5, 0.90, 3.0, 3.0, 0, 135, 135 point.1=1, -1.50, -7.90, -4.0, 1600, 1, 0.886, 0, 0.50, 2.5, 0.85, 4.1, 4.3, 2, 135, 135 point.2=1, -1.50, 7.90 , -4.0, 1600, 2, 0.886, 0, 0.50, 2.5, 0.85, 4.3, 4.1, 3, 135, 135 //SCRAPES point.3=2, -26.500, 0.000, 2.000, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.4=2, 20.300, 0.000, 0.750, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.5=2, -1.500, -35.750, 2.200, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.6=2, -1.500, 35.750, 2.200, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 static_pitch=-0.56 //degrees (pitch when loaded on ground) static_cg_height=3.8 //feet, altitude of CG when at rest on the ground gear_system_type=0 [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=60.0 [exits] number_of_exits=1 exit_rate.0=0.4 ;Percent per second [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 [Views] eyepoint=11.80, -1.25, 4.40 //(ft) longitudinal, lateral, vertical distance from ref datum [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=150, 250 aileron=150, 250 rudder=150, 250 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -0.35, -35.30, 2.33, fx_navred , light.1=3, -0.35, 35.30, 2.33, fx_navgre , light.2=3, -28.30, 0.00, 3.18, fx_navwhi , light.3=1, -1.70, 0.00, 5.60, fx_beacon , light.4=4, -8.70, 0.00, -1.45, fx_beaconb, [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=100.000000 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 [direction_indicators] direction_indicator.0=1,0 [brakes] toe_brakes_scale=0.3 parking_brake=1 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [flight_tuning] Remove the // if you do not have rudder pedals // p_factor_on_yaw=0.2 // torque_on_roll=0.2 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000
