// iss 0504131900 v1.08 : -{1234}- refers to the equivalent entry number in the *.AIR file [fltsim.0] title=brigandB1 sim=brigandB1 model= panel= sound= texture= kb_checklists=brigand_check kb_reference=brigandB1_ref atc_id_enable=1 atc_id=VS584 atc_airline=Air Force atc_flight_number=VS584 ui_manufacturer=Bristol ui_type=Brigand ui_variation=B Mk I description=Light attack bomber. visual_damage=0 prop_anim_ratio=-1.76 [General] atc_type=Bristol atc_model=Brigand editable=1 performance="Maximum speed\n400 mph ~ 350 kts @ 15,000 ft.\nCruise speed\n207 mph ~ 180 kts\n\nEngines\nTwo Bristol Centaurus 57 2,810 hp. max.\n\nMaximum range\n2,800 nm with 2,000lb.+ bombload\n\nService ceiling\n25,000 ft\n\nFuel capacity\n1,270 gal.US. 1,058 gall.Imp.\n\nEmpty weight\n25,598 lb.\n\nMaximum gross weight\n39,000 lb. \n\nLength\n46 ft. 4 in.\n\nWingspan\n72 ft. 4in.\n\nHeight\n17 ft. 5 in.\" [WEIGHT_AND_BALANCE] max_gross_weight = 39000 empty_weight = 25598 reference_datum_position = 0.00, 0, 0 // (feet) from FSim Ref. pos: (Chord/4,centerline, waterline) empty_weight_CG_position = 0.35, 0, 0 // z,x,y -- (feet) from specified datum. max_number_of_stations =3 station_load.0 = "170, 5.00, 0.0, 1.3, P1" //Weight, Lat, Lon, Vert Position station_load.1 = "170, 0.60, 0.0, 0.0, Nav" station_load.2 = "170,-1.80, 0.0, 0.0, WOP" ;moments of inertia // -{no entries}- empty_weight_pitch_MOI = 66857 empty_weight_roll_MOI = 77307 empty_weight_yaw_MOI = 136474 empty_weight_coupled_MOI = 0.0 [flight_tuning] cruise_lift_scalar=0.8 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.5 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 p_factor_on_yaw=0.5 torque_on_roll=1.0 gyro_precession_on_yaw=1.0 gyro_precession_on_pitch=1.0 [fuel] //Long. Lat. Vertical (feet), Usable, Unusable (gallons US.) LeftTip = 0.0, -18.7, 0.0, 183.0, 0.0 RightTip = 0.0, 18.7, 0.0, 183.0, 0.0 // 152.0 imp. LeftAux = 0.0, -12.4, 0.0, 213.0, 0.0 RightAux = 0.0, 12.4, 0.0, 213.0, 0.0 // 177.0 imp. LeftMain = 0.0, -4.2, 0.0, 240.0, 0.0 RightMain= 0.0, 4.2, 0.0, 240.0, 0.0 // 200.0 imp. fuel_type = 1 // 1 = Avgas number_of_tank_selectors = 2 electric_pump=1 [airplane_geometry] wing_area = 726.0 //Square feet -{no entry}- wing_span = 72.0 //Feet wing_root_chord = 10.08 //Feet, MAC -- NOT Root wing_dihedral = 2.0 //Degrees On thickness c/l wing_incidence = 3.0 //Degrees wing_twist = -1.0 //Degrees oswald_efficiency_factor= 0.85 // 0.65 Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 5.0 //Degrees,on Mean Average Chord (MAC) wing_pos_apex_lon = 3.36 //Feet, long. dist. of MAC. LE. from reference point, negative going aft wing_pos_apex_vert = 0.0 //Feet, vert. dist. of MAC. LE. from reference point, positive going up htail_area = 93.2 // Square feet -{no entry}- htail_span = 22.0 // Feet htail_pos_lon = -25.2 // Feet, longitudinal distance from reference point, negative going aft htail_pos_vert = 1.56 // Feet, vertical distance from reference point, positive going up htail_incidence = -2.0 // Degrees htail_sweep = 0.0 // Degrees, on MAC vtail_area = 56.0 //Square feet -{no entry}- vtail_span = 6.00 //Feet, tip to body [b=9.48] vtail_sweep = 0.0 //Degrees, on MAC vtail_pos_lon = -25.2 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 2.0 //Feet, vertical distance from reference point, positive going up elevator_area = 52.2 //Square feet -{320}- aileron_area = 37.0 //Square feet rudder_area = 32.0 //Square feet elevator_up_limit = 17.0 //Degrees = 0.30 rad elevator_down_limit = 15.0 //Degrees = 0.26 rad aileron_up_limit = 20.0 //Degrees = 0.35 rad aileron_down_limit = 15.0 //Degrees = 0.26 rad rudder_limit = 25.0 //Degrees = 0.44 rad elevator_trim_limit = 12.0 //Degrees = 0.21 rad spoiler_limit = 70.0 //Degrees = 1.22 rad spoilerons_available = 0 //Spoilerons Available? aileron_to_spoileron_gain = 0 //Aileron to spoileron gain min_ailerons_for_spoilerons = 0 //Degrees min_flaps_for_spoilerons = 0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed = 105.0 //Knots True (KTAS) full_flaps_stall_speed = 90.0 //Knots True (KTAS) cruise_speed = 180.0 //Knots True (KTAS) max_indicated_speed = 350.0 //Red line (KIAS) //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] // GEAR. point.0=1, -30.39, 0.00, -3.80, 1200.0, 0, 0.88, 180.0, 0.42, 2.5, 0.87, 4.0, 4.0, 0, 185.0, 220.0 point.1=1, 2.52, -10.40, -9.75, 1600.0, 1, 2.00, 0.0, 0.50, 2.5, 0.85, 4.2, 5.2, 2, 185.0, 220.0 point.2=1, 2.52, 10.40, -9.75, 1600.0, 2, 2.00, 0.0, 0.50, 2.5, 0.85, 4.5, 5.8, 3, 185.0, 220.0 // SCRAPES. //point.3=2, 12.0, 0.0, 0.0, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 4, 0.0, 0.0 // Nose. //point.4=2, -33.2, 0.0, 1.0, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0 // Tail. //point.5=2, -2.8, -36.3, 1.2, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5, 0.0, 0.0 // Left. //point.6=2, -2.8, 36.3, 1.2, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6, 0.0, 0.0 // Right. //point.7=2, 10.7, -10.4, -8.2, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0 // L.Prop. //point.8=2, 10.7, 10.4, -8.2, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9, 0.0, 0.0 // R.Prop. //point.9=2, -28.4, -10.9, 8.4, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 7, 0.0, 0.0 // L.Fin. //point.10=2,-28.4, 10.9, 8.4, 800.0, 0, 0.00, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 8, 0.0, 0.0 // R.Fin. static_pitch = 10.8 static_cg_height = 8.5 gear_system_type=1 //Hydraulic -{no entry}- tailwheel_lock = 1 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.33 //Percent throttle that activates warning flap_limit_idle = 0.0 //Flap angle that activates warning at idle ~ NOT USED! flap_limit_power = 70.0 //Flap angle that activates warning at above idle ~ NOT USED! [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.6 //Brake scalar ~ 0.3 differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -0.82, -34.7, 1.075, fx_navredm , light.1 = 3, -0.82, 34.7, 1.075, fx_navgrem , light.2 = 3, -32.95, 0.0, 0.838, fx_navwhi , light.3 = 4, 5.50, 0.0, 3.000, fx_vclight, light.4 = 5, 0.80, -25.4, 0.300, fx_landing, // Beam done in FSDS. [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 17 [flaps.0] //Trailing Edge Flaps -{524}- type = 1 // 1 - tail. span-outboard = 0.33 // 0.0 .. 1.0 extending-time = 5 // seconds flaps-position.0 = 0 // degrees = 0.00 rad flaps-position.1 = 15 // degrees = 0.26 rad flaps-position.2 = 60 // degrees = 1.05 rad damaging-speed = 145 // KIAS blowout-speed = 250 // KIAS lift_scalar = 1.0 drag_scalar = 2.0 pitch_scalar= 1.0 system_type = 1 // 1=Hydraulic. [GeneralEngineData] engine_type = 0 //0=Piston. Engine.0 = 10.44, -10.4, -1.0 //(ft.) long, lat, vert. dist. from ref. datum Engine.1 = 10.44, 10.4, -1.0 fuel_flow_scalar= 1.0 //Fuel flow scalar min_throttle_limit = 0.0 //Minimum percent throttle. max_contrail_temperature= -10 // A bit of fun. [piston_engine] power_scalar = 1 cylinder_displacement = 181.72 compression_ratio = 7.2 number_of_cylinders = 18 max_rated_rpm= 2700 max_rated_hp= 2810 //Max rated HP ( Sound effect only ) fuel_metering_type = 0 cooling_type = 0 normalized_starter_torque = 0.033 turbocharged = 1 max_design_mp = 49.26 min_design_mp = 9 // ~1 critical_altitude = 16000 emergency_boost_type = 0 emergency_boost_mp_offset = 0 emergency_boost_gain_offset = 0 fuel_air_auto_mixture = 1 auto_ignition = 0 max_rpm_mechanical_efficiency_scalar = 1.2 idle_rpm_mechanical_efficiency_scalar = 1 max_rpm_friction_scalar = 0.9 idle_rpm_friction_scalar = 1 emergency_boost_duration = 0 [propeller] thrust_scalar = 1 propeller_type = 0 propeller_diameter = 13.68 propeller_blades = 4 propeller_moi = 70 beta_max = 65 beta_min = 15 min_gov_rpm = 400 prop_tc = 0.1 gear_reduction_ratio = 2.273 fixed_pitch_beta = 25 low_speed_theory_limit = 80 prop_sync_available = 0 prop_deice_available = 0 prop_feathering_available = 1 prop_auto_feathering_available = 0 min_rpm_for_feather = 700 beta_feather = 88.5 power_absorbed_cf = 0.9 defeathering_accumulators_available = 0 feathering_switches = 1 // Available? 1=TRUE prop_reverse_available = 0 minimum_on_ground_beta = 0 minimum_reverse_beta =0 [keyboard_response] elevator=150.0,250.0 aileron =150.0,250.0 rudder =150.0,250.0 [Views] eyepoint = 3.4, 0.0, 3.80 // z,x,y. [exits] number_of_exits=2 exit_rate.0=0.1 ;Percent per second exit_rate.1=0.1 ;Percent per second [Radios] Audio.1 =1 Com.1 =1, 0 Nav.1 =1, 0, 1 Nav.2 =1, 0, 0 Adf.1 =1 Transponder.1=1 Marker.1=0 [direction_indicators] direction_indicator.0=1,0 [hydraulic_system] normal_pressure = 800.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1 //pumps on Eng1,2 // Vacuum systems -{1512}- AIR file entry needed for vacuum selector and gauge. [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 //------------------------------------------------------------------------------------------------- [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.0 autothrottle_available=0 pitch_takeoff_ga=8.0 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.0 max_throttle_rate=0.1 nav_proportional_control=9.0 nav_integrator_control=0.25 nav_derivative_control=0.0 nav_integrator_boundary=2.5 nav_derivative_boundary=0.0 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.0 gs_integrator_boundary=0.7 gs_derivative_boundary=0.0 yaw_damper_gain=0.0