[fltsim.0] title=ALPHA P-47D Thunderbolt RB1 sim=P-47D model=RB2 panel=RB sound= texture=RB1 kb_checklists= description=© ALPHA Simulations 2004\n\nP-47D Thunderbolt\n\n ui_manufacturer=ALPHA ui_type=P-47D Thunderbolt ui_variation=1. 'Razorback', 72nd FG, 82nd FS atc_id_color=0000000000 visual_damage=0 atc_heavy=0 atc_id=P47D atc_airline= atc_flight_number= [fltsim.1] title=ALPHA P-47D Thunderbolt RB4 sim=P-47D model=RB1 panel=RB sound= texture=RB4 kb_checklists= description=© ALPHA Simulations 2004\n\nP-47D Thunderbolt\n\n ui_manufacturer=ALPHA ui_type=P-47D Thunderbolt ui_variation=2. 'Razorback', 19th FS, 318th FG, Saipan, Marianas, 1944 atc_id_color=0000000000 visual_damage=0 atc_heavy=0 atc_id=P47D atc_airline= atc_flight_number= [fltsim.2] title=ALPHA P-47D Thunderbolt RB3 sim=P-47D model=RB1 panel=RB sound= texture=RB3 kb_checklists= description=© ALPHA Simulations 2004\n\nP-47D Thunderbolt\n\n ui_manufacturer=ALPHA ui_type=P-47D Thunderbolt ui_variation=3. 'Razorback', 73 OTU, Fayid, Egypt, 1944 atc_id_color=0000000000 visual_damage=0 atc_heavy=0 atc_id=P47D atc_airline= atc_flight_number= [fltsim.3] title=ALPHA P-47D Thunderbolt RB2 sim=P-47D model=RB1 panel=RB sound= texture=RB2 kb_checklists= description=© ALPHA Simulations 2004\n\nP-47D Thunderbolt\n\n ui_manufacturer=ALPHA ui_type=P-47D Thunderbolt ui_variation=4. 'Razorback', 61st FS, 56th FG Halesworth, March 1944 atc_id_color=0000000000 visual_damage=0 atc_heavy=0 atc_id=P47D atc_airline= atc_flight_number= [fltsim.4] title=ALPHA P-47D Thunderbolt BT1 sim=P-47D model=BT panel=BT sound= texture=BT1 kb_checklists= description=© ALPHA Simulations 2004\n\nP-47D Thunderbolt\n\n ui_manufacturer=ALPHA ui_type=P-47D Thunderbolt ui_variation=5. 'Bubble-Top', 350 FG, 346 FS atc_id_color=0000000000 visual_damage=0 atc_heavy=0 atc_id=P47D atc_airline= atc_flight_number= [fltsim.5] title=ALPHA P-47D Thunderbolt BT2 sim=P-47D model=BT panel=BT sound= texture=BT2 kb_checklists= description=© ALPHA Simulations 2004\n\nP-47D Thunderbolt\n\n ui_manufacturer=ALPHA ui_type=P-47D Thunderbolt ui_variation=6. 'Bubble-Top', 365th FG, Azeville (A-7) France, July 1944 atc_id_color=0000000000 visual_damage=0 atc_heavy=0 atc_id=P47D atc_airline= atc_flight_number= [fltsim.6] title=ALPHA P-47D Thunderbolt BT3 sim=P-47D model=BT panel=BT sound= texture=BT3 kb_checklists= description=© ALPHA Simulations 2004\n\nP-47D Thunderbolt\n\n ui_manufacturer=ALPHA ui_type=P-47D Thunderbolt ui_variation=7. 'Bubble-Top', 392nd FS, 367th FG, Spring of 45, France. atc_id_color=0000000000 visual_damage=0 atc_heavy=0 atc_id=P47D atc_airline= atc_flight_number= [General] performance=Model Designer: Chris Lampard\nPanel: Phil Perrott\nFlight model: Jay McDaniel\nTextures: C Lampard & D Swart\n\nEmpty weight: 9950 lbs\nLoaded weight: 17500 lbs\nWingspan: 40 ft 9 in\nLength: 36 ft 2 in\nPower: Pratt & Whitney R-2800-59W with 2000 HP\nInitial climb: 3100 fpm\nTop speed, SL: 314 mph\nTop speed, 25000 ft: 420 mph\nArmament: Eight .50 caliber guns, up to 2500 lbs. of external stores. editable=1 atc_type= atc_model= [weight_and_balance] // ACM V2.3 max_gross_weight = 17500.00 empty_weight = 9950.00 reference_datum_position = 0.00, 0.00, 0.00 empty_weight_CG_position = 0.00, 0.00, 0.00 empty_weight_pitch_MOI = 16339.00 empty_weight_roll_MOI = 9959.00 empty_weight_yaw_MOI = 29406.00 empty_weight_coupled_MOI = 0.00 max_number_of_stations = 1 station_load.0 =180.00, -4.17, 0.00, 1.44, Pilot CG_forward_limit= 0.00 CG_aft_limit= 1.00 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 4, -3.14, 0, 2.36, fx_vclight [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 0 fuel_flow_scalar = 1.00 engine.0 = 10.20, 0.00, 0.00 min_throttle_limit=0.00 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 number_of_tank_selectors =1 Center1 = 0.00, 0.00, 0.00, 305.00, 0.00 external1=0.00, -10.0, -2.0, 150.00, 0.00 external2=0.00, 10.0, -2.0, 150.00, 0.00 electric_pump=1 [contact_points] static_pitch = 13.860 static_cg_height = 6.960 max_number_of_points = 7 point.0 = 1, -19.00, 0.00, -2.7, 1574.80, 0.00, 0.70, 40.98, 0.20, 2.50, 0.87, 7.00, 5.00, 0.00, 0.00, 0.00 point.1 = 1, 2.20, -8.03, -8.0, 2000.00, 1.00, 1.40, 0.00, 0.60, 2.50, 0.80, 8.00, 6.00, 2.00, 0.00, 0.00 point.2 = 1, 2.20, 8.03, -8.0, 2000.00, 2.00, 1.40, 0.00, 0.60, 2.50, 0.80, 6.00, 8.00, 3.00, 0.00, 0.00 point.3 = 2, 0.00, -20.40, 0.20, 2175.54, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00 point.4 = 2, 0.00, 20.40, 0.20, 2175.54, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00 point.5 = 2, -23.63, 0.00, 0.30, 2175.54, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00 point.6 = 2, 10.40, 0.00, -6.50, 1574.80, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00 gear_system_type=1 [keyboard_response] elevator = 150.00, 250.00 aileron = 150.00, 250.00 rudder = 150.00, 250.00 [forcefeedback] gear_bump_nose_magnitude = 1000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2000 gear_bump_right_direction = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 450 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.075 ground_bumps_slope2 = 1 crash_magnitude1 = 2000 crash_direction1 = 1000 crash_magnitude2 = 2000 crash_direction2 = 9000 crash_period2 = 7500 crash_duration2 = 2500000 stick_shaker_magnitude = 2000 stick_shaker_direction = 0 stick_shaker_period = 111111 [airplane_geometry] wing_area = 300.00 wing_span = 40.75 wing_root_chord = 9.60 wing_dihedral = 5.00 wing_incidence = 0.00 wing_twist = 0.00 oswald_efficiency_factor = 0.80 wing_winglets_flag = 0 wing_sweep = 3.00 wing_pos_apex_lon = 2.80 wing_pos_apex_vert = -1.50 htail_area = 37.00 htail_span = 16.14 htail_pos_lon = -18.60 htail_pos_vert = 1.30 htail_incidence = -0.35 htail_sweep = 18.00 vtail_area = 22.00 vtail_span = 5.10 vtail_sweep = 26.00 vtail_pos_lon = -17.80 vtail_pos_vert = 2.10 elevator_area = 20.70 aileron_area = 21.70 rudder_area = 14.10 elevator_up_limit = 28.00 elevator_down_limit = 23.00 aileron_up_limit = 20.00 aileron_down_limit = 15.00 rudder_limit = 28.00 elevator_trim_limit = 18.00 spoiler_limit = 0.00 aileron_to_spoileron_gain = 0.00 min_ailerons_for_spoilerons = 0.00 min_flaps_for_spoilerons = 0.00 spoilerons_available = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 electric_always_available = 1 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [flight_tuning] cruise_lift_scalar=1 parasite_drag_scalar=1 induced_drag_scalar=1 elevator_effectiveness=1 aileron_effectiveness=1 rudder_effectiveness=1 pitch_stability=1 roll_stability=1 yaw_stability=1 elevator_trim_effectiveness=1 aileron_trim_effectiveness=1 rudder_trim_effectiveness=1 [piston_engine] power_scalar=1 cylinder_displacement= 155.56 compression_ratio= 6.70 number_of_cylinders= 18 max_rated_rpm= 2700.00 max_rated_hp= 2000.00 fuel_metering_type= 0 cooling_type= 0 normalized_starter_torque= 0.035 turbocharged= 1 max_design_mp= 54.00 min_design_mp= 10.00 critical_altitude= 30000.00 emergency_boost_type= 1 emergency_boost_mp_offset= 5.14 emergency_boost_gain_offset= 0.59 fuel_air_auto_mixture= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar=1 idle_rpm_mechanical_efficiency_scalar=1 max_rpm_friction_scalar=1 idle_rpm_friction_scalar=1 [propeller] thrust_scalar=1 propeller_type= 0 propeller_diameter= 13.00 propeller_blades= 4 propeller_moi= 46.40 beta_max= 65.00 beta_min= 15.00 min_gov_rpm= 700.00 prop_tc= 0.010 gear_reduction_ratio= 2.00 fixed_pitch_beta= 0.00 low_speed_theory_limit= 80.00 prop_sync_available= 0 prop_deice_available= 1 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 700.00 beta_feather= 0.00 power_absorbed_cf= 0.90 defeathering_accumulators_available= 0 prop_reverse_available= 0.00 minimum_on_ground_beta= 15.00 minimum_reverse_beta= 0.00 rotation = 1 [folding_wings] wing_fold_system_type = fold_rates = , [TailHook] tailhook_length = tailhook_position = , , cable_force_adjust = 1 [Views] eyepoint=-4.15, 0.00, 3.50 //(feet) longitudinal, lateral, vertical distance from reference datum [LSO] LSOAdjustSpeed = 1.2 [exits] number_of_exits = 1 exit_rate.0 = 0.4 [brakes] toe_brakes_scale=0.54 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=30.00 flap_limit_idle=15.00 [Reference Speeds] flaps_up_stall_speed= 76.00 full_flaps_stall_speed= 70.00 cruise_speed= 250.00 //knots over the ground at 25,000 feet. (170 indicated) max_indicated_speed=450 max_level_speed=370 //knots over the ground at 25,000 feet. [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.00 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=110.00 pitch_takeoff_ga=8.00 max_pitch=10.00 max_pitch_acceleration=1.00 max_pitch_velocity_lo_alt=2.00 max_pitch_velocity_hi_alt=1.50 max_pitch_velocity_lo_alt_breakpoint=20000.00 max_pitch_velocity_hi_alt_breakpoint=28000.00 max_bank=25.00 max_bank_acceleration=1.80 max_bank_velocity=3.00 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=0.00 [hydraulic_system] electric_pumps=0 engine_map=1,0,0,0 normal_pressure=950 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1=1 Com.1=1 Com.2=1 Nav.1=1,0,1 Nav.2=1 Adf.1=1 Transponder.1=1 Marker.1=1 [Flaps.0] type= 1 span-outboard= 0.50 extending-time= 5.00 system_type= 0 damaging-speed= 182.00 blowout-speed= 197.00 lift_scalar= 1.00 drag_scalar= 1.00 pitch_scalar= 1.00 flaps-position.0= 0.00, 0.00 flaps-position.1= 10.00, 0.00 flaps-position.2= 20.00, 0.00 flaps-position.3= 30.00, 0.00 flaps-position.4= 40.00, 0.00
