[fltsim.0] title=Swordf01 sim=Swordf01 model= panel= sound= texture= kb_checklists= description=FS2004 Fairey Swordfish MK I\nby JRLucariny\nhttp:\/\/www.jrlucariny.com ui_manufacturer=Fairey ui_type=Swordfish ui_variation=Swordfish MK I atc_heavy=0 atc_id= atc_airline= atc_flight_number= [General] performance=General characteristics\nCrew: Three (pilot, observer, and radio operator\/rear gunner) \nLength: 35 ft 8 in (10.87 m) \nWingspan: 45 ft 6 in (13.87 m) \nHeight: 12 ft 4 in (3.76 m) \nWing area: 542 ft² (50.4 m²) \nEmpty weight: 4,195 lb (1,900 kg) \nLoaded weight: 7,720 lb (3,500 kg) \nPowerplant: 1× Bristol Pegasus IIIM.3 or XXX radial engine, 690 hp (510 kW) (750 hp (560 kW) for Pegasus XXX) \nPerformance\nMaximum speed: 138 mph (222 km\/h) at 5,000 ft (1,500 m) \nRange: 546 mi (879 km) \nFerry range: 1,025 mi (1,650 km) \nService ceiling: 19,250 ft (5,870 m) \nRate of climb: 1,220 ft\/min (6.2 m\/s) \nArmament\nGuns: * 1 × fixed, forward-firing .303 in (7.7 mm) Vickers machine gun in engine cowling \n1 × .303 in (7.7 mm) Lewis or Vickers K machine gun in rear cockpit \nRockets: 8 × "60 lb" RP-3 rocket projectiles (Mk.II and later) \nBombs: 1 × 1,670 lb (760 kg) torpedo or 1,500 lb (700 kg) mine atc_type= atc_model= [WEIGHT_AND_BALANCE] empty_weight = 4195.0 // (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 = 120, -1.5, 0.0, 1.5 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 120, -3.0, 0.0, 1.5 //Gunner Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 6668.43 //slug-ft^2 empty_weight_roll_MOI = 5725.72 //slug-ft^2 empty_weight_yaw_MOI = 10186.09 //slug-ft^2 empty_weight_coupled_MOI=0.000000 max_gross_weight=10350.000000 [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 [piston_engine] power_scalar=1.0 cylinder_displacement= 137.500 compression_ratio= 6.400 number_of_cylinders= 9 max_rated_rpm= 2475.000 max_rated_hp= 952.000 fuel_metering_type=0 cooling_type= 1 normalized_starter_torque= 0.035 turbocharged= 1 max_design_mp= 40.999999 min_design_mp= 1.000 critical_altitude= 21100.000 emergency_boost_type= 3 emergency_boost_mp_offset= 4.510 emergency_boost_gain_offset= 0.350 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=11.65 propeller_blades=3 propeller_moi=29.669868 beta_max=39.142857 beta_min=15.000000 min_gov_rpm=1400.000000 prop_tc=0.010000 gear_reduction_ratio=2.088000 fixed_pitch_beta=20.000000 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, -19.85, 0.00, -3.17, 1600, 0, 0.25, 90.0, 0.30, 2.5, 0.50, 0.0, 0.0, 0 point.1=1, 2.55, -5.25, -7.65, 2200, 1, 1.25, 0.0, 0.50, 2.5, 0.50, 0.0, 0.0, 2 point.2=1, 2.55, 5.25, -7.65, 2200, 2, 1.25, 0.0, 0.50, 2.5, 0.50, 0.0, 0.0, 3 point.3=2, 0.00, -22.70, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5 point.4=2, 0.00, 22.70, -1.25, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6 point.5=2, -25.38, 0.00, -1.66, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 9 point.6=2, 2.41, 0.00, -2.08, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4 static_pitch = 15.35 //degrees (pitch when loaded on ground) static_cg_height = 5.95 //(feet) altitude of CG when at rest (altitude when loaded on ground) [TailHook] tailhook_length=8 ;(feet) tailhook_position=-15.0, 0.0, -4.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1.0 [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.12,0.11 [Views] eyepoint=0, 0.0, 0.1 //(feet) longitudinal, lateral, vertical distance from reference datum [fuel] LeftMain=0.000000,0.000000,0.000000,100.000000,0.000000 RightMain=0.000000,0.000000,0.000000,100.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=343.000000 wing_span=45.250000 wing_root_chord=7.583333 wing_dihedral=2.598267 wing_incidence=1.697388 wing_twist=-1.983032 oswald_efficiency_factor=0.723952 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=56.000000 htail_span=12.750000 htail_pos_lon=-19.166667 htail_pos_vert=0.000000 htail_incidence=-0.988770 htail_sweep=0.000000 vtail_area=30.000000 vtail_span=6.244998 vtail_sweep=0.000000 vtail_pos_lon=-20.500000 vtail_pos_vert=1.500000 elevator_area=24.080000 aileron_area=32.400000 rudder_area=10.500000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit=23.491270 elevator_trim_limit=19.480565 spoiler_limit=59.988681 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 [Flaps.0] type=1 span-outboard=0.500000 extending-time=3.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=9.998114,0.000000 flaps-position.2=19.996227,0.000000 flaps-position.3=29.994341,0.000000 flaps-position.4=39.992454,0.000000 [GeneralEngineData] engine_type=0 Engine.0=8.450000,0.000000,0.000000 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=91.000000 full_flaps_stall_speed=72.800000 cruise_speed=138.000000 max_indicated_speed=150.000000 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000 autothrottle_available=0 pitch_takeoff_ga=8.000 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] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [direction_indicators] direction_indicator.0=1,0
