[fltsim.0] title=B-25H 498th BS sim=B25H model= panel= sound= texture= description=B-25H of the 498th Bomb Squadron "Flying Falcons" atc_id= atc_airline= atc_flight_number= atc_parking_types=GATE,RAMP ui_manufacturer=North American ui_type=B-25H ui_variation=Flying Falcons atc_heavy=0 atc_id_color=0000000000 visual_damage=0 description= [WEIGHT_AND_BALANCE] empty_weight = 19480 // (pounds) reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -1.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = 170, 12.0, -4.0, 2.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.0 = 170, 12.0, 4.0, 2.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 50000 //slug-ft^2 empty_weight_roll_MOI = 59000 //slug-ft^2 empty_weight_yaw_MOI = 130000 //slug-ft^2 empty_weight_coupled_MOI=0.000000 max_gross_weight=29475.000000 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 2.0 aileron_effectiveness = 2.0 rudder_effectiveness = 1.7 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 = 1.5 cylinder_displacement=185.930000 compression_ratio=6.850000 number_of_cylinders=14 max_rated_rpm=2600.000000 max_rated_hp=1700.000000 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.035000 turbocharged=1 max_design_mp=44.299999 min_design_mp=1.000000 critical_altitude=17000.000000 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] thrust_scalar = 1.0 propeller_type=0 propeller_diameter=12.583000 propeller_blades=3 propeller_moi=52.300000 beta_max=49.000000 beta_min=18.000000 min_gov_rpm=1400.000000 prop_tc=0.010000 gear_reduction_ratio=1.780000 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=0.000000 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [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, 15.84, 0.00, -7.90, 1400, 0, 1.50, 45.0, 0.46, 2.5, 0.70, 6.0, 7.0, 0 point.1=1, -1.82, -9.23, -8.00, 2000, 1, 2.50, 0.0, 1.06, 2.5, 0.86, 7.5, 8.5, 2 point.2=1, -1.82, 9.23, -8.00, 2000, 2, 2.50, 0.0, 1.06, 2.5, 0.86, 7.0, 8.0, 3 point.3=2, 0.00, -55.83, 1.00, 800, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5 point.4=2, 0.00, 55.83, 1.00, 800, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6 point.5=2, -39.58, 0.00, -2.83, 800, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9 point.6=2, 17.16, 0.00, -4.83, 800, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4 static_cg_height = 6.88 //(feet) altitude of CG when at rest (altitude when loaded on ground) static_pitch = 1.28 //degrees (pitch when loaded on ground) gear_system_type=0 [Views] eyepoint= 10.00, -1.00, 3.22 //(feet) longitudinal, lateral, vertical distance from reference datum [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 [General] performance=Speed: 272 mph @ 13000 ft\nInitial climb: 860 ft\/min\nRange: 1350 miles [fuel] Center1=-2.310000,0.000000,1.200000,215.000000,0.000000 LeftMain=-2.310000,-4.950000,0.820000,335.000000,0.000000 RightMain=-2.310000,4.950000,0.820000,335.000000,0.000000 External1=-2.310000,0.000000,-1.200000,335.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=610.000000 wing_span=67.583333 wing_root_chord=9.666667 wing_dihedral=0.000000 wing_incidence=1.999512 wing_twist=-1.994019 oswald_efficiency_factor=0.904545 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=140.000000 htail_span=43.000000 htail_pos_lon=-26.666667 htail_pos_vert=0.000000 htail_incidence=1.999512 htail_sweep=0.000000 vtail_area=220.000000 vtail_span=16.911535 vtail_sweep=0.000000 vtail_pos_lon=-38.750000 vtail_pos_vert=7.166667 elevator_area=94.410000 aileron_area=80.250000 rudder_area=39.490000 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=5156.620156 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [brakes] toe_brakes_scale=0.488296 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 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=15.000035,0.000000 flaps-position.2=30.000070,0.000000 flaps-position.3=45.000105,0.000000 [GeneralEngineData] engine_type=0 Engine.0=8.166667,-9.250000,0.000000 Engine.1=8.166667,9.250000,0.000000 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=110.000000 full_flaps_stall_speed=88.000000 cruise_speed=206.815742 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=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=90.000000 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 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=6.930556 [stall_warning] type=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0