[fltsim.0] title=SB Halifax BII Charleys Aunt sim=Halifax BII model= panel= sound= texture= visual_damage=1 atc_id=Halifax B II ui_manufacturer=Handley Page ui_type=Halifax "Charleys Aunt" ui_variation=WW2 Bomber description= RAF Handley Page Halifax BII Srs. 1A painted to represent tha of 'Charleys Aunt' of No. 102 Squadron based at RAF Pocklington. [WEIGHT_AND_BALANCE] empty_weight = 39912 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 = 20 station_load.0 = 160, 0.0, -2.0, 3.5 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 160, 0.0, 2.0, 3.5 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = 160, 8.0, 0.0, 0.0 //Nav/bombardier Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3 = 160, -10.1, 0.0, 4.5 //Radio/top turret station_load.4 = 160, -16.6, -2.0, 0.0 //engineer station_load.5 = 160, -16.6, 2.0, 0.0 //waist station_load.6 = 160, -37.9, 0.0, 0.0 //tail ;Moments of Inertia empty_weight_pitch_MOI =163411 empty_weight_roll_MOI =303766 empty_weight_yaw_MOI = 319667 empty_weight_coupled_MOI=0.000000 max_gross_weight=61548.000000 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.0 aileron_effectiveness = 0.75 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 [piston_engine] power_scalar = 1.4 cylinder_displacement=136.470000 compression_ratio=7.000000 number_of_cylinders=14 max_rated_rpm=2700.000000 max_rated_hp=1390.000000 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.035000 turbocharged=-1 max_design_mp=47.999999 min_design_mp=1.000000 critical_altitude=22800.000000 emergency_boost_type=3 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] thrust_scalar = 1.1 propeller_type=0 propeller_diameter=11.500000 propeller_blades=3 propeller_moi=39.920000 beta_max=65.000000 beta_min=23.000000 min_gov_rpm=1800.000000 prop_tc=0.010000 gear_reduction_ratio=2.237000 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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn startup=fx_engstrt [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [electrical] max_battery_voltage = 24.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps = 60.0 [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 point.0=1, -32.00, 0.00, -5.45, 1600, 0, 0.90, 75.0, 0.20, 2.5, 0.80, 7.50, 9.50, 0 point.1=1, 2.27, -13.00, -11.20, 2200, 1, 2.00, 0.0, 0.90, 2.5, 0.80, 5.5, 5.50, 2 point.2=1, 2.27, 13.00, -11.20, 2200, 2, 2.00, 0.0, 0.90, 2.5, 0.80, 7.5, 9.50, 3 point.3=2, 0, -51.50, -1.30, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5 point.4=2, 0, 51.50, -1.30, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6 point.5=2, -42.00, 0.00, -1.00, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9 point.6=2, 17.16, 0.00, -2.83, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4 static_pitch = 8 //degrees (pitch when loaded on ground) static_cg_height= 10.0 //(feet) altitude of CG when at rest (altitude when loaded on ground) gear_system_type=1 [Views] eyepoint=12.00, -1.15 4.40 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.125 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=14 // degrees, KIAS flaps-position.2=28 // degrees, KIAS flaps-position.3=42 // degrees, KIAS flaps-position.4=55 // degrees, KIAS damaging-speed=172 // KIAS blowout-speed=260 // KIAS [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 [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.11 ;Percent per second [General] performance=\n\n\n\n [fuel] LeftMain=0.000000,-30.000000,1.600000,903.000000,0.000000 RightMain=0.000000,30.000000,1.600000,903.000000,0.000000 External1=-0.600000,-1.200000,-2.400000,150.000000,0.000000 External2=-0.600000,1.200000,-2.400000,150.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=1280.000000 wing_span=98.833333 wing_root_chord=15.833333 wing_dihedral=1.796265 wing_incidence=0.549316 wing_twist=-0.999756 oswald_efficiency_factor=5.904079 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=91.000000 htail_span=28.000000 htail_pos_lon=-35.000000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=67.000000 vtail_span=9.332738 vtail_sweep=0.000000 vtail_pos_lon=-35.000000 vtail_pos_vert=12.083333 elevator_area=81.000000 aileron_area=15.002000 rudder_area=73.000000 elevator_up_limit=28.000447 elevator_down_limit=22.998526 aileron_up_limit=26.000825 aileron_down_limit=18.999280 rudder_limit=28.000447 elevator_trim_limit=19.996227 spoiler_limit=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [GeneralEngineData] engine_type=0 Engine.0=-2.500000,-27.500000,-2.500000 Engine.1=0.000000,-10.833333,-2.083333 Engine.2=0.000000,10.833333,-2.083333 Engine.3=-2.500000,27.500000,-2.500000 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=85.000000 full_flaps_stall_speed=68.000000 cruise_speed=231.755716 max_indicated_speed=760.500000 [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=200.000000,1000.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 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 [LIGHTS] //#1=beacon #2=strobe #3=nav #10=reheat //#4=cockpit #5=landing #6=taxi //#7=recog #8=wing #9=logo //---------------originals---------------------------- light.0=5, 1.60, -17.67, -0.50, fx_navred light.1=5, 1.60, 17.67, -0.50, fx_navgre light.2=5, -1.66, 0.00, -3.20, fx_beacon light.3=5, -18.30, 0.00, 5.80, fx_beacon light.4=5, 2.10, -5.70, -1.80, fx_landing light.5=5, 2.10, 5.70, -1.80, fx_landing //------------ ExhaustFlames--------uses wing/taxi/logo //index,type, long, lat, vert, fx_filename light.6=8, 6.00, 10.05, 0.45, fx_pistonpower light.7=8, 6.00, 14.15, 0.45, fx_pistonpower light.8=8, 6.00, -10.15, 0.45, fx_pistonpower light.9=8, 6.00, -14.15, 0.45, fx_pistonpower light.10=8, 5.00, 22.35, 0.55, fx_pistonpower light.11=8, 5.00, 26.75, 0.55, fx_pistonpower light.12=8, 5.00, -22.75, 0.55, fx_pistonpower light.13=8, 5.00, -27.15, 0.55, fx_pistonpower [brakes] toe_brakes_scale=0.694815 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] electric_pumps=0 engine_map=1,1,1,1 normal_pressure=6.930556 [stall_warning] type=-1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
