[fltsim.0] title=ALPHA Swift FR5 sim=alpha_fr5 model= panel= sound= texture= KB_checklists=fr5_check kb_reference= ui_manufacturer=ALPHA ui_type=Supermarine Swift FR.5 ui_variation=FR.5 atc_id_color=0x00000000 atc_heavy=0 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 atc_id= atc_airline= atc_flight_number= atc_parking_types=MIL_COMBAT description=© AlphaSim 2006\n\nThe Supermarine Swift was the first British production aircraft to have swept wings and tailplanes. Essentially a revision of the Supermarine Attacker, the type evolved through several marques, eventually arriving at the FR.5, which was the most numerous. Incorporating tricycle gear and an afterburning engine, this aircraft held the world speed record for a scant 24 hours, when it was again broken by the Douglas F4D Skyray. The FR.5 utilised a "sawtooth" leading edge on the main wing (adding stability at high angles of attack) and remained operational until the summer of 1961. A later development, the FR.7, was adapted to the reconnaissance role, with a dozen of these being produced. [fltsim.1] title=ALPHA Swift FR5 longrange sim=alpha_fr5 model=1 panel= sound= texture= KB_checklists=fr5_check kb_reference= ui_manufacturer=ALPHA ui_type=Supermarine Swift FR.5 ui_variation=FR.5, long range atc_id_color=0x00000000 atc_heavy=0 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 atc_id= atc_airline= atc_flight_number= atc_parking_types=MIL_COMBAT description=© AlphaSim 2006\n\nThe Supermarine Swift was the first British production aircraft to have swept wings and tailplanes. Essentially a revision of the Supermarine Attacker, the type evolved through several marques, eventually arriving at the FR.5, which was the most numerous. Incorporating tricycle gear and an afterburning engine, this aircraft held the world speed record for a scant 24 hours, when it was again broken by the Douglas F4D Skyray. The FR.5 utilised a "sawtooth" leading edge on the main wing (adding stability at high angles of attack) and remained operational until the summer of 1961. A later development, the FR.7, was adapted to the reconnaissance role, with a dozen of these being produced. [General] performance=Model: AlphaSim\nPanel: P Perrott\nGauges: H Pralle\nTextures: G Flores\nFlight Model: J. McDaniel\n\nFirst flight: 25 August 1952 \nWingspan: 32 feet 4 inches \nLength: 42 feet 3 inches \nHeight: 13 feet 6 inches\nEmpty weight: 13,435 pounds \nMaximum weight: 21,400 pounds \nMax speed: 717 mph \nCeiling: 45,800 feet \nPower plant: Rolls-Royce Avon 114, 9450-lbf\nRange: 630 miles\nAccommodation: One pilot\nArmament: Two 30 mm cannon editable=1 atc_type= atc_model= [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -5.61, -15.65, -0.96, fx_navred light.1 = 3, -5.61, 15.65, -0.96, fx_navgre light.2 = 3, -19.72, 0.0, 1.51, fx_navwhi light.3 = 4, 10.77, 0.0, 2.36, fx_vclight //afterburner light.17=9, -19.00, 0.00, 0.00, fx_Bob_both_smaller_blue light.18=9, -21.50, 0.00, -0.50, fx_Bshort_Burnerflame [smokesystem] smoke.0 = 0.0, -30.00, 0.00, fx_smoke_f6 [weight_and_balance] max_gross_weight = 21400 empty_weight = 13435 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 28494 empty_weight_roll_MOI = 11585 empty_weight_yaw_MOI = 23848 empty_weight_coupled_MOI = 0 CG_forward_limit = 0.00 CG_aft_limit = 1.00 max_number_of_stations = 0 [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 1.0 min_throttle_limit = 0.00 engine.0 = -20.00, 0.00, 0.00 [TurbineEngineData] fuel_flow_gain=0.90 inlet_area=5.80 rated_N2_rpm=12000.00 static_thrust=9450.00 afterburner_available=1 reverser_available=0.00 [Reference Speeds] flaps_up_stall_speed=114.00 full_flaps_stall_speed=96.00 cruise_speed=450.00 //knots over the ground at 36,000 ft. (264 indicated) max_indicated_speed=820 max_mach=1.20 max_level_speed=737 mph (649 knots) //indicated at 5,000 feet. [effects] windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 electric_pump = 1 Center1 = 2, 0, 0, 300, 3 Center2 = -2, 0, 0, 250, 3 [contact_points] static_pitch = -1.59 static_cg_height = 5.29 tailwheel_lock = 0 gear_system_type = 1 max_number_of_points = 7 point.0 =1, 13.10, 0.00, -5.15, 3000.00, 0.00, 0.80, 25.00, 0.13, 3.50, 0.85, 5.00, 5.00, 0.00, 250.00, 230.00 point.1 =1, -1.00, -7.60, -5.80, 3000.00, 1.00, 1.15, 0.00, 0.45, 2.50, 0.80, 5.00, 5.00, 2.00, 250.00, 230.00 point.2 =1, -1.00, 7.60, -5.80, 3000.00, 2.00, 1.15, 0.00, 0.45, 2.50, 0.80, 5.00, 5.00, 3.00, 250.00, 230.00 point.3 =2, -10.00, -16.03, -1.06, 1500.00, 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, -10.00, 16.03, -1.06, 1500.00, 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, -20.00, 0.00, -1.10, 1500.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 5.00, 9.00, 0.00, 0.00 point.6 =2, 20.60, 0.00, 0.60, 1500.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00 [keyboard_response] elevator = 150.00, 250.00 aileron = 150.00, 150.00 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 = 327.70 wing_span = 32.33 wing_root_chord = 13.50 wing_dihedral = 1.00 wing_incidence = 0.00 wing_twist = 0.00 oswald_efficiency_factor = 0.85 wing_winglets_flag = 0 wing_sweep = 50.00 wing_pos_apex_lon = 8.00 wing_pos_apex_vert = -0.80 htail_area = 40.00 htail_span = 13.00 htail_pos_lon = -13.30 htail_pos_vert = 1.50 htail_incidence = -1.00 htail_sweep = 50.00 vtail_area = 19.14 vtail_span = 5.46 vtail_sweep = 45.00 vtail_pos_lon = -11.00 vtail_pos_vert = 2.50 elevator_area = 12.00 aileron_area = 33.00 rudder_area = 9.50 elevator_up_limit = 14.00 elevator_down_limit = 11.00 aileron_up_limit = 20.00 aileron_down_limit = 15.00 rudder_limit = 30.00 elevator_trim_limit = 18.00 spoiler_limit = 0.00 aileron_to_spoileron_gain = 0.00 spoiler_handle_available = 0 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 = 400 engine_generator_map = 1 electric_always_available = 1 [exits] number_of_exits=1 exit_rate.0=0.5 [TailHook] tailhook_length = 3 tailhook_position = -15, 0, -2.00 cable_force_adjust = 1 [Views] eyepoint=9.5, 0.00, 2.80 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 autothrottle_arming_required= 0 autothrottle_max_rpm = 100 autothrottle_takeoff_ga= 0 pitch_takeoff_ga=8 ; max_pitch=10.0 max_pitch_acceleration=0.8 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.2 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.5 max_bank_velocity=2.00 max_throttle_rate=0.10 nav_proportional_control=11.00 nav_integrator_control=0.20 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 [direction_indicators] direction_indicator.0=3,0 [brakes] toe_brakes_scale=1.09 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=1 flap_limit_power=25 flap_limit_idle=5 [hydraulic_system] electric_pumps=1 engine_map=1 normal_pressure=3000.00 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.11 ;Percent per second [jet_engine] thrust_scalar=1.000 [flight_tuning] cruise_lift_scalar=1.00 pitch_stability=1.00 roll_stability=1.00 yaw_stability=1.00 parasite_drag_scalar=1.00 induced_drag_scalar=1.00 elevator_effectiveness=1.00 aileron_effectiveness=1.00 rudder_effectiveness=1.00 elevator_trim_effectiveness=1.00 aileron_trim_effectiveness=1.00 rudder_trim_effectiveness=1.00 [Radios] Audio.1=1 Com.1=1,0 Com.2=0,0 Nav.1=1,0,1 Nav.2=0,0,0 Adf.1=1,0 Transponder.1=1 Marker.1=1 [Flaps.0] type= 1 span-outboard= 0.50 extending-time= 5.00 system_type= 1 damaging-speed= 255.00 blowout-speed= 300.00 flaps-position.0= 0.00, 0.00 flaps-position.1= 15.00, 0.00 flaps-position.2= 30.00, 0.00 flaps-position.3= 45.00, 0.00 flaps-position.4= 100.00, 0.00