[fltsim.0] title=MAI P3 HN sim=AI_P3 model= panel= sound= texture=HN atc_id= atc_airline=NAVY atc_flight_number=4513 atc_parking_codes=P3,M002 atc_parking_types=MIL_CARGO ui_manufacturer=Lockheed ui_type=P3 ui_variation=Hellenic Navy description= atc_heavy=0 [General] atc_type=LOCKHEED atc_model=P3 editable=0 performance=Enter your performance information here. [weight_and_balance] // ACM V2.5 max_gross_weight = 15000 empty_weight = 9090 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 30000 empty_weight_roll_MOI = 18200 empty_weight_yaw_MOI = 36500 empty_weight_coupled_MOI = 0 max_number_of_stations = 6 station_load.0 = 170, 5.0, -2.0, 0.0 station_load.1 = 170, 5.0, 2.0, 0.0 station_load.2 = 170, -2.1, -2.0, 0.0 station_load.3 = 170, -2.1, 2.0, 0.0 station_load.4 = 170, -5.3, -2.0, 0.0 station_load.5 = 170, -5.3, 2.0, 0.0 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, 1.10, -50.12, 2.03, fx_navredh , light.1 = 3, 1.10, 50.12, 2.03, fx_navgreh , light.2 = 3, -60.96, 0, 6.9, fx_navwhih light.3 = 2, 0.87, -50.17, 2.03, fx_strobeh , light.4 = 2, 0.87, 50.17, 2.03, fx_strobeh , light.5 = 1, -53.41, 0.00, 25.15, fx_beaconh , light.6 = 1, -6.50, 0.00, -3.30, fx_beaconh , light.7 = 4, 35.64, 0.00, 6.81, fx_vclighth , [GeneralEngineData] engine_type = 5 Engine.0 = 9.000, -21.000, 1.500 Engine.1 = 10.000, -16.000, 0.000 fuel_flow_scalar = 1.000 min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser Engine.2= 10.000, 16.000, 0.000 Engine.3= 9.000, 21.000, 1.500 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 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 LeftMain = 0, -14.5, -1, 190, 0 LeftAux = 0, -6, -1.5, 79.5, 0 RightMain = 0, 14.5, -1, 190, 0 RightAux = 0, 6, -1.5, 79.5, 0 [contact_points] static_pitch = -1 static_cg_height = 8.7 tailwheel_lock = 0 gear_system_type = 1 max_number_of_points = 7 point.0 = 1, 13.00, 0.00,-8.2, 3000, 0, 0.596, 39.9, 0.296, 2.5, 0.9516, 4.8, 4.8, 0, 0.0, 0.0 point.1 = 1, -2.67, -8.58, -8.8, 5000, 1, 0.596, 0, 0.642, 2.5, 0.8152, 4.5, 5.2, 2, 0, 0 point.2 = 1, -2.67, 8.58, -8.8, 5000, 2, 0.596, 0, 0.642, 2.5, 0.8152, 4.8, 4.9, 3, 0, 0 point.3 = 2, -3.33, -23.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4 = 2, -3.33, 23.92, -3.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5 = 2, -22.67, 0.00, 0.00, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6 = 2, 23.08, 0.00, -1.50, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 [keyboard_response] elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [forcefeedback] gear_bump_nose_magnitude = 3000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2700 gear_bump_left_direction = 9000 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2700 gear_bump_right_direction = 27000 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1300 ground_bumps_angle1 = 08900 ground_bumps_intercept1 = 3.0 ground_bumps_slope1 = 0.20 ground_bumps_magnitude2 = 200 ground_bumps_angle2 = 09100 ground_bumps_intercept2 = 1.075 ground_bumps_slope2 = 0.035 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 stick_shaker_magnitude = 5000 stick_shaker_direction = 0 stick_shaker_period = 111111 [airplane_geometry] //ACM_AREAW1// 0,0,0,1.6459,0.9685,0.9685,0.0169,1.5805,1.9371,1.9371 //ACM_AREAW2// 0.0338,1.5151,2.9057,2.9057,0.0507,1.4497,3.8743,3.8743,0.0676,1.3843 //ACM_AREAW3// 4.8429,4.8429,0.0845,1.3189,5.8115,5.8115,0.1014,1.2535,6.7801,6.7801 //ACM_AREAW4// 0.1183,1.1881,7.7486,7.7486,0.1352,1.1228,8.7172,8.7172,0.1521,1.0574 //ACM_AREAH1// 0,0,0,1.7475,0.2912,0.2912,0.1060,1.7661,0.5825,0.5825 //ACM_AREAH2// 0.2120,1.7847,0.8737,0.8737,0.3180,1.8034,1.1650,1.1650,0.4240,1.8220 //ACM_AREAH3// 1.4562,1.4562,0.5300,1.8406,1.7475,1.7475,0.6360,1.8593,2.0387,2.0387 //ACM_AREAH4// 0.7420,1.8779,2.3300,2.3300,0.8480,1.8965,2.6212,2.6212,0.9540,1.9152 //ACM_AREAV1// 0,0,0,2.2555,0.2506,0.2506,0.2102,2.2853,0.5012,0.5012 //ACM_AREAV2// 0.4205,2.3152,0.7518,0.7518,0.6308,2.3450,1.0024,1.0024,0.8411,2.3749 //ACM_AREAV3// 1.2530,1.2530,1.0514,2.4047,1.5036,1.5036,1.2617,2.4346,1.7542,1.7542 //ACM_AREAV4// 1.4720,2.4644,2.0049,2.0049,1.6823,2.4943,2.2555,2.2555,1.8926,2.5241 //ACM_CAREAW1// 4.3586,4.3586,0.8990,1.2282,4.8429,4.8429,0.9074,1.2202,5.3272,5.3272 //ACM_CAREAW2// 0.9159,1.2122,5.8115,5.8115,0.9244,1.2042,6.2958,6.2958,0.9328,1.1962 //ACM_CAREAW3// 6.7801,6.7801,0.9413,1.1881,7.2644,7.2644,0.9497,1.1801,7.7486,7.7486 //ACM_CAREAW4// 0.9582,1.1721,8.2329,8.2329,0.9666,1.1641,8.7172,8.7172,0.9751,1.1561 //ACM_CAREAH1// 0,0,0.8737,1.7475,0.2912,0.2912,0.9797,1.8098,0.5825,0.5825 //ACM_CAREAH2// 1.0857,1.8721,0.8737,0.8737,1.1917,1.9344,1.1650,1.1650,1.2977,1.9967 //ACM_CAREAH3// 1.4562,1.4562,1.4037,2.0591,1.7475,1.7475,1.5098,2.1214,2.0387,2.0387 //ACM_CAREAH4// 1.6158,2.1837,2.3300,2.3300,1.7218,2.2460,2.6212,2.6212,1.8278,2.3083 //ACM_CAREAV1// 0,0,0.5638,1.6916,0.2506,0.2506,0.7741,1.8117,0.5012,0.5012 //ACM_CAREAV2// 0.9844,1.9317,0.7518,0.7518,1.1947,2.0518,1.0024,1.0024,1.4050,2.1719 //ACM_CAREAV3// 1.2530,1.2530,1.6153,2.2919,1.5036,1.5036,1.8256,2.4120,1.7542,1.7542 //ACM_CAREAV4// 2.0359,2.5321,2.0049,2.0049,2.2461,2.6521,2.2555,2.2555,2.4564,2.7722 wing_area = 310.0 wing_span = 57.2 wing_root_chord = 5.4 wing_dihedral = 6.0 wing_incidence = 1.0 wing_twist = -1.5 oswald_efficiency_factor = 0.7 wing_winglets_flag = 1 wing_sweep = 1.0 wing_pos_apex_lon = 2.1 wing_pos_apex_vert = 0.0 htail_area = 67.0 htail_span = 17.2 htail_pos_lon = -22.6 htail_pos_vert = 0.0 htail_incidence = 0.5 htail_sweep = 20.0 vtail_area = 42.0 vtail_span = 7.4 vtail_sweep = 40.0 vtail_pos_lon = -20.5 vtail_pos_vert = 4.1 elevator_area = 17.0 aileron_area = 13.5 rudder_area = 7.3 elevator_up_limit = 17.0 elevator_down_limit = 15.5 aileron_up_limit = 18.0 aileron_down_limit = 18.0 rudder_limit = 30.0 elevator_trim_limit = 15.0 spoiler_limit = 60.0 aileron_to_spoileron_gain = 0 spoiler_handle_available = 1 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 spoilerons_available = 0 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 engine_generator_map = 1,1 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 5, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 2, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 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 [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 [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=8.8 //Propeller Diameter, (feet) propeller_blades=4 //Number of propeller blades propeller_moi=24 //Propeller moment of inertia beta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=15.2 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=25520 //Miminum governed RPM prop_tc=0.004 //Prop time-constant gear_reduction_ratio=17.6 //Propeller gear reduction ratio fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=700 //Minimum RPM for prop feathering beta_feather=79.3 //Feathering pitch angle (degrees) power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=1.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=-14.0 //Minimum pitch angle in reverse, (degrees) [TurbineEngineData] fuel_flow_gain=0.011 //Gain on fuel flow inlet_area=1.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=158 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar=1.0 //Scalar on Turboprop power maximum_torque=3270 //Maximum torque available (ft-lbs) [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 0.0 //Flap angle that activates warning at idle flap_limit_power = 16.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 1.0 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint=4.54, -1.20, 3.25 [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.5 // 0.0 .. 1.0 extending-time = 5 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 20 // degrees flaps-position.2 = 40 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type = 4 direction_indicator.0=3,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=1,0 [Reference Speeds] flaps_up_stall_speed=96.0 //Knots True (KTAS) full_flaps_stall_speed=76.8 //Knots True (KTAS) cruise_speed=315.0 //Knots True (KTAS) max_mach = 0.58 max_indicated_speed=259.000000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=0 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 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 = 1.0 pitch_takeoff_ga=8.000000 [stall_warning] type=1
