//Mods (air & cfg) by C. Backus (napamule). 06Jan27 //Orig Model, Panel, Sound, and Textures by Dave ('Big D') //Dave at 'daveanjackie@netzero.com'. filename:'Pickupcb.zip' [fltsim.0] title=Pickup sim=PickupCb model= panel= sound= texture= kb_checklists= ui_manufacturer=Robbins Motorworks //o=Shipworks ui_type=100ft Jackie ui_variation=Yacht atc_heavy=0 atc_airline= [General] atc_type= atc_model= editable=1 performance=Maximum Speed\t60 mph (err...how's 250 kts?) [WEIGHT_AND_BALANCE] max_gross_weight = 7500.000 empty_weight = 3500.000 reference_datum_position = 0.0000, 0.0000, 0.0000 // (ft) dist from FSim Ref pos: (1/4 chord, centerline, waterline) empty_weight_CG_position = -3.000,0.000, 0.500 //ZXY dist from specified datum max_number_of_stations = 30 station_load.0= 190.000, 0.000, -1.000, 0.000 //Driver station_load.1= 200.000, 0.000, 1.000, 0.000 // Passengers station_load.3= 1000.000, -4.000, 0.000, 0.000 // Luggage, misc. ;Moments of Inertia empty_weight_pitch_MOI = 74110.000 empty_weight_roll_MOI = 42310.000 empty_weight_yaw_MOI = 29000.000 empty_weight_coupled_MOI = 0.000 // 0 Class (0=floats) // 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) [N/A] // 6 Wheel Radius (feet) // 7 Steer Angle (degrees) // 8 Static Compression (feet) (0=rigid) // 9 Max/Static Compression Ratio //10 Damping Ratio/Water Rudder Effectiveness (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, 3.500, -3.000, -1.660, 9999.000, 1, 2.500, 25.000, 0.400, 2.5, 0.950, 1.000, 1.000, 0, 60.00, 100.00 point.1=1, 3.500, 3.000, -1.660, 9999.000, 2, 2.500, 25.000, 0.400, 2.5, 0.950, 1.000, 1.000, 0, 60.00, 100.00 point.2=1, -10.300, -3.600, -1.680, 9999.000, 1, 2.500, 0.000, 0.250, 2.5, 0.950, 1.000, 1.000, 0, 60.00, 100.00 point.3=1, -10.300, 3.600, -1.680, 9999.000, 2, 2.500, 0.000, 0.250, 2.5, 0.950, 1.000, 1.000, 0, 60.00, 100.00 static_pitch = 0.1000 //degrees (pitch when loaded on ground) static_cg_height=1.525 //feet, altitude of CG when at rest on the ground gear_system_type = 0 [GeneralEngineData] engine_type = 1 // 1=Jet Engine.0 = -4.000, 0.000, 0.000 //ZXY distance from ref datum fuel_flow_scalar = 0.050000 //Scalar for fuel flow efficiency min_throttle_limit = -0.490000 //neg for turbine reverser [TurbineEngineData] fuel_flow_gain =0.002000 //Gain on fuel flow inlet_area = 1.0 // Square Feet, engine nacelle inlet area rated_N2_rpm = 5920.000000 //RPM, 2nd stage compressor rated value static_thrust = 1800.000000 // Lbs, max rated static thrust at SL afterburner_available = 0 //Afterburner available? reverser_available = 1 //Thrust reverser available? [jet_engine] thrust_scalar =1.0 [brakes] parking_brake = 1 // Parking brake available toe_brakes_scale = 1.0 //Brake scalar differential_braking_scale =1.0 [Reference Speeds] flaps_up_stall_speed = 40.000 full_flaps_stall_speed = 0.000 cruise_speed = 70.000 max_indicated_speed = 210.000 max_mach = 0.26 [Views] ;ZXY distance from reference datum (feet) eyepoint= -4.99, -1.12, 4.36 //(feet) longitudinal, lateral, vertical distance from reference datum [flight_tuning] cruise_lift_scalar = .000 parasite_drag_scalar = 1.000 induced_drag_scalar = 2.000 elevator_effectiveness = .000 aileron_effectiveness = 000 rudder_effectiveness = 1 pitch_stability = 1.000 roll_stability = 1.000 yaw_stability =1.000 elevator_trim_effectiveness = .000 aileron_trim_effectiveness = .000 rudder_trim_effectiveness = 1.000 [airplane_geometry] wing_area =12.500000 //Square feet wing_span =4.600000 //o= 111.4 wing_root_chord= 8.8 wing_dihedral =0.000000 //Degrees wing_incidence =0.000000 //Degrees wing_twist= -1.0 //Degrees oswald_efficiency_factor= 0.000100 //Measure of lift effeciency of wing wing_winglets_flag= 0 //Are winglets available? wing_sweep=0.000000 //Degrees, wing leading edge wing_pos_apex_lon = -1.000000 //Z distance from ref point wing_pos_apex_vert =0.000000 //Y distance from ref point htail_area =144.000000 //Square feet htail_span =4.000000 htail_pos_lon=-9.000000 //Z distance from ref point htail_pos_vert=1.000000 //Y distance from ref point htail_incidence =0.000000 //Degrees htail_sweep=0.000000 // horizontal tail leading edge vtail_area= 144.000000 //Square feet vtail_span= 3.000000 //tip to body vtail_sweep =0.000000 //Degrees, vertical tail leading edge vtail_pos_lon=-10.000000 //Z distance from ref point vtail_pos_vert =4.000000 //Y from ref point elevator_area = 0 //Square feet aileron_area = 0 //Square feet rudder_area=70.000000 //Square feet elevator_up_limit=5.000000 //Degrees elevator_down_limit=5.000000 //Degrees aileron_up_limit=5.000000 //Degrees aileron_down_limit=5.000000 //Degrees rudder_limit= 25.5 //Degrees elevator_trim_limit=15.000000 //Degrees spoiler_limit = 0 //Degrees 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 [Flaps.0] type=0 span-outboard=0.500000 extending-time=0.000000 system_type=0 [fuel] Center1 = -6.000, 0.000, -2.000,18.000, 0.000 //ZXY GAL MIN fuel_type = 1 // ;2 = JetA number_of_tank_selectors = 1 electric_pump = 1 [electrical] electric_always_available = 0 [Radios] // Radio Type = available, 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 [gear_warning_system] gear_warning_available = 0 [hydraulic_system] normal_pressure = 3000 //PSI electric_pumps = 1 //electric pumps engine_map = 1,0,0,0 // pumps [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI [direction_indicators] direction_indicator.0 = 3,0 //3=Electro-Mag Slaved Compass, 0=NA [attitude_indicators] attitude_indicator.0 = 0 //0=None [turn_indicators] turn_indicator.0 = 1,0 //1=Electric Gyro [stall_warning] type = 0 [exits] number_of_exits=1 exit_rate.0=0.4 //Percent per second [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1000.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm = 90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8.0 max_pitch=12.0 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=2.8 max_bank_velocity=4.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain = 0.0 [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 = 50.000, 150.000 aileron = 50.000, 150.000 rudder = 50.000, 150.000 ;[forcefeedback] //Note: FF does NOT work well in FS9 ;gear_bump_nose_magnitude = 3000.000 // 0 - 10000 ;gear_bump_nose_direction = 18000.000 //0 - 35999 degrees ;gear_bump_nose_duration = 250000.000 //in microseconds ;gear_bump_left_magnitude = 2700.000 // 0 - 10000 ;gear_bump_left_direction = 35500.000 // 0 - 35999 degrees ;gear_bump_left_duration = 250000.000 //in microseconds ;gear_bump_right_magnitude = 2700.000 // 0 - 10000 ;gear_bump_right_direction = 500.000 //0 - 35999 degrees ;gear_bump_right_duration = 250000.000 //in microseconds ;ground_bumps_magnitude1 = 1300.000 //0 - 10000 ;ground_bumps_angle1 = 8900.000 //0 - 35999 degrees ;ground_bumps_intercept1 = 3.000 ;ground_bumps_slope1 = 0.200 ;ground_bumps_magnitude2 = 200.000 //0 - 10000 ;ground_bumps_angle2 = 9100.000 //0 - 35999 degrees ;ground_bumps_intercept2 = 1.075 ;ground_bumps_slope2 = 0.035 ;crash_magnitude1 = 10000.000 //0 - 10000 ;crash_direction1 = 1000.000 // 0 - 35999 degrees ;crash_magnitude2 = 10000.000 //0 - 10000 ;crash_direction2 = 9000.000 //0 - 35999 degrees ;crash_period2 = 75000.000 //in microseconds ;crash_duration2 = 2500000.000 //in microseconds