[fltsim.0] title=P-51D Taiwan 7 FS 3 FG sim=P51d model= panel= sound= texture= checklists=P51d_CHECK description=The P-51D Mustang's outstanding qualities made it the leading US fighter in WW II. The P-51D combined contemporary aerodynamics, structural and system advance, exceptional fuel capacity and low drag.\nWing span: 37 ft 0.25"\nLength: 32 ft 3"\nHeight: 13 ft 8"\Model by Andrew C Wai, modified by Robert Hawk & Will Guillermo, Repaint by Alejandro Hurtado\nThis Mustang is the No. 633 of the 7 Fighter Squadron, 3 Fighter Group, in June 1945. ui_manufacturer=North American ui_type=P-51 Mustang ui_variation=Taiwan 7 FS 3 FG atc_heavy=0 atc_id=703 atc_airline=NORTH AMERICAN atc_flight_number=3 [WEIGHT_AND_BALANCE] empty_weight =7598.000 // (pounds) 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 = 50 station_load.0 = 170, -2.0, 0.0, 2.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 8185.0 empty_weight_roll_MOI = 4736.0 empty_weight_yaw_MOI = 10026.0 empty_weight_coupled_MOI=0.000000 max_gross_weight=9212.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.0 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [GeneralEngineData] engine_type=0 Engine.0=9.250, 0.000, 0.000 fuel_flow_scalar=1.000 min_throttle_limit=0.000000 [piston_engine] cylinder_displacement=137.500 compression_ratio=6.000 number_of_cylinders=12 max_rated_rpm=3000.000 max_rated_hp=1590.000 fuel_metering_type=2 cooling_type=1 normalized_starter_torque=0.025 turbocharged=1 max_design_mp=61.000 min_design_mp=1.000 critical_altitude=25000.000 emergency_boost_type=3 emergency_boost_mp_offset=6.000 emergency_boost_gain_offset=0.528 fuel_air_auto_mixture=1 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [propeller] propeller_type=0 propeller_diameter=11.167 propeller_blades=4 propeller_moi=58.000 beta_max=65.000 beta_min=23.000 min_gov_rpm=1800.000 prop_tc=0.010 gear_reduction_ratio=2.088 fixed_pitch_beta=20.000 low_speed_theory_limit=80.000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000 beta_feather=0.000 power_absorbed_cf=0.000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000 minimum_reverse_beta=0.000 [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.11 ;Percent per second [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [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) point.0=1.0,-17.00, 0.00, -2.30, 3200, 0, 0.59,180.0, 0.40, 2.5, 0.80, 7.5, 5.00, 0, 0, 135 point.1=1.0, 1.80,-7.93, -7.10, 2200, 1, 0.59, 0.0, 0.50, 2.5, 0.83, 8.0, 8.00, 2, 0, 135 point.2=1.0, 1.80, 7.93, -7.10, 2200, 2, 0.59, 0.0, 0.50, 2.5, 0.83, 8.0, 8.00, 3, 0, 135 point.3=2.0, 0.00,-18.5, 0.00, 1200, 0, 0.00, 0.00, 0.00, 0.0, 0.00, 0.0, 0.00, 5 point.4=2.0, 0.00, 18.5, 0.00, 1200, 0, 0.00, 0.00, 0.00, 0.0, 0.00, 0.0, 0.00, 6 point.5=2.0,-20.51, 0.00, 0.00, 2400, 0, 0.00, 0.00, 0.00, 0.0, 0.00, 0.0, 0.00, 9 point.6=2.0, 12.24, 0.00, 0.00, 1200, 0, 0.00, 0.00, 0.00, 0.0, 0.00, 0.0, 0.00, 4 static_pitch= 15.0 //degrees (pitch when loaded on ground) static_cg_height=6.4 //(feet) altitude of CG when at rest (altitude when loaded on ground) gear_system_type=1 [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=175 // KIAS blowout-speed=265 // KIAS [Views] eyepoint=-2.70,0.00,2.53 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.5, -18.3, -0.8, fx_navred light.1=3, 0.5, 18.3, -0.8, fx_navgre light.2=4, -2.24, 0.00, 2.20, fx_vclight panel=0.00, 0.50, -0.8, fx_vclight [General] performance=Max speed at altitude: 437 mph (703 km\/h) @25,000 ft (7,620 m)\nCeiling: 41,900 ft (12,780 m)\nClimb rate: 20,000 ft in 7min 18 sec\nRange: 1,300 mile, with drop tanks: 2,080 mile.\nEngine: Rolls-Royce Merlin V-12 1695 hp\n6 0.5" machine guns\nExternal bomb and rocket load of 2000 lbs \nEmpty: 6840 lbs\nMax take off: 12,100 lbs [fuel] Center1=-3.000000,0.000000,0.000000,85.000000,0.000000 LeftMain=0.000000,-5.100000,0.000000,92.000000,0.000000 RightMain=0.000000,5.100000,0.000000,92.000000,0.000000 External1=0.000000,-7.000000,-2.000000,75.000000,0.000000 External2=0.000000,7.000000,-2.000000,75.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=227.000000 wing_span=37.000000 wing_root_chord=6.166667 wing_dihedral=4.998779 wing_incidence=0.450439 wing_twist=0.000000 oswald_efficiency_factor=1.281117 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=28.000000 htail_span=13.166667 htail_pos_lon=-15.916667 htail_pos_vert=0.000000 htail_incidence=1.999512 htail_sweep=0.000000 vtail_area=10.000000 vtail_span=3.605551 vtail_sweep=0.000000 vtail_pos_lon=-17.500000 vtail_pos_vert=3.166667 elevator_area=13.260000 aileron_area=18.900000 rudder_area=8.230000 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=0.572958 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=1.000000 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [GeneralEngineData] engine_type=0 Engine.0=9.250, 0.000, 0.000 fuel_flow_scalar=1.000 [Reference Speeds] flaps_up_stall_speed=69.000 full_flaps_stall_speed=55.200 cruise_speed=293.002 max_indicated_speed=439.132813 [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 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 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
