[fltsim.0] title=IFDG A318-111 Air France Retro sim=A318_CFM_IFDG_011 model=CFM panel= sound= texture= kb_checklists= kb_reference= atc_id=F-GUGE atc_airline=Air France atc_flight_number=1263 atc_heavy=0 ui_manufacturer=Airbus ui_type=A318-111 ui_variation= Air France Retro description= "Model, FDE, Master texture by iFDG. AF Retro textures by Stephane Moine" atc_id_color=0x00ff00ff visual_damage=0 prop_anim_ratio=1.72 atc_parking_types=GATE,RAMP atc_parking_codes=AFR atc_id_font=Verdana,-11,1,600,0 [General] atc_type=Airbus atc_model=A318 editable=1 performance=Engines\nCFM56-5B9/P rated at 23,300 lbs\n\nTypical Cruise Speed\n0.78 Mach at 35,000 ft\n\nMax Speed\nVmo 350 kts Mmo 0.82 Mach\n\nRange(150 pax)\n2,900 nm (5,374 km)\n\nMax Fuel\n42,230 lbs (6,303 US gal)\n\nMax Takeoff Weight\n162,040 lbs\n\nMax Gross Weight (taxi weight)\n162,900 lbs\n\nMax Payload\n42,370 lbs guid=e76d55c4c6489c3d60a64b2ef2de549a [pitot_static] vertical_speed_time_constant = 1 [weight_and_balance] // ACM V2.5 max_gross_weight = 146400 empty_weight = 84600 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 1114620 empty_weight_roll_MOI = 566559 empty_weight_yaw_MOI = 1272194 empty_weight_coupled_MOI = 0 max_number_of_stations = 6 station_load.0 = 450, 34.90, 0.0, 4.31, Pilots station_load.1 = 114, 0.0, 0.0, 0.0, Meals station_load.2 = 3344, 0.0, 0.0, 0.0, Baggage station_load.3 = 200, 0.0, 0.0, 0.0, Mail and Cargo station_load.4 = 1700, 0.0, 0.0, 0.0, First Class+FA station_load.5 = 10200, 0, 0, 0, Couch [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.1 = 3, -59.40, 0, 5.07, iFDG_A320_whitenav light.2 = 2, -59.40, 0, 5.07, iFDG_A320_whitestrobe_tail light.3 = 2, -15.45, -54.68, 4.36, iFDG_A320_whitestrobe, light.4 = 2, -15.45, 54.68, 4.36, iFDG_A320_whitestrobe, light.5 = 1, 3.070, 0, 9.00, iFDG_A320_redbeacon_top, light.6 = 1, 6.381, 0, -5.10, iFDG_A320_redbeacon_bottom, light.7 = 5, 19.88, 6.463, 1.93, iFDG_A320_inspection, light.8 = 5, 19.88, -6.463, 1.93, iFDG_A320_inspection, [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 1 min_throttle_limit = -0.269958 engine.0 = 12, -19, -4.96, engine.1 = 12, 19, -4.96, [smokesystem] smoke.0 = 0.80052, -18.00157, 43.23110, iFDG_A320_flap smoke.1 = 0.80052, -18.00157, -43.23110, iFDG_A320_flap [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = ifdg_a320_touchdown, 1 windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 3 electric_pump = 1 Center1 = 0, 0, -4.11, 2179, 6.5 LeftMain = -4, -19.01, -0.82, 2062, 7.8 RightMain = -4, 19.01, -0.82, 2062, 7.8 [contact_points] static_pitch = 1.69 static_cg_height = 10.2 tailwheel_lock = 0 gear_system_type = 1 max_number_of_points = 12 point.0 = 1, 26.3749, 0, -11.35, 1574.8, 0, 1.68, 65, 1.33, 1.9, 0.7, 9, 9.4, 0, 0, 0 point.1 = 1, -6.4, -12, -11.5, 1574.803, 1, 1.68, 0, 1.2, 2.1, 0.4, 11.7, 13, 2, 0, 0 point.2 = 1, -6.4, 12, -11.5, 1574.803, 2, 1.68, 0, 1.2, 2.1, 0.4, 10.2, 12.9, 3, 0, 0 point.3 = 2, 9.5, -19, -8.9019, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.4 = 2, -16.3239, -54.1926, 2.2783, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.5 = 2, 9.5, 19, -8.9019, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 point.6 = 2, -16.1935, 55.3538, 2.2867, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.7 = 2, -28.5973, 0, -4.4916, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.8 = 2, -59.3886, 0, 31.7625, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.9 = 2, -61.0232, 0, 5.6366, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.10 = 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.11 = 2, 43.8139, 0, -0.2452, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 [keyboard_response] elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [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 = 10000 crash_direction1 = 1000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 7500 crash_duration2 = 2500000 stick_shaker_magnitude = 2000 stick_shaker_direction = 0 stick_shaker_period = 111111 [airplane_geometry] //ACM_AREAW1// 0,0,0,5.2041,1.8838,1.8838,0.8784,5.8225,3.7676,3.7676 //ACM_AREAW2// 1.7568,6.4408,5.6515,5.6515,2.6354,7.0591,7.5355,7.5355,3.5137,7.6771 //ACM_AREAW3// 9.4194,9.4194,4.3923,8.2953,11.3030,11.3030,5.2708,8.9138,13.1871,13.1871 //ACM_AREAW4// 6.1490,9.5319,15.0710,15.0710,7.0275,10.1503,16.9549,16.9549,7.9060,10.7686 //ACM_AREAH1// 0,0,0,4.1493,0.6915,0.6915,0.4663,4.4081,1.3831,1.3831 //ACM_AREAH2// 0.9329,4.6673,2.0745,2.0745,1.3990,4.9263,2.7662,2.7662,1.8658,5.1852 //ACM_AREAH3// 3.4577,3.4577,2.3322,5.4443,4.1493,4.1493,2.7987,5.7031,4.8407,4.8407 //ACM_AREAH4// 3.2651,5.9622,5.5324,5.5324,3.7316,6.2210,6.2238,6.2238,4.1981,6.4801 //ACM_AREAV1// 0,0,0,6.2575,0.6952,0.6952,0.4866,6.2437,1.3904,1.3904 //ACM_AREAV2// 0.9735,6.2300,2.0857,2.0857,1.4605,6.2161,2.7811,2.7811,1.9471,6.2024 //ACM_AREAV3// 3.4763,3.4763,2.4342,6.1887,4.1715,4.1715,2.9210,6.1749,4.8667,4.8667 //ACM_AREAV4// 3.4077,6.1612,5.5622,5.5622,3.8947,6.1472,6.2575,6.2575,4.3814,6.1336 //ACM_CAREAW1// 8.4771,8.4771,6.5553,7.5960,9.4194,9.4194,6.9945,7.9833,10.3613,10.3613 //ACM_CAREAW2// 7.4337,8.3704,11.3030,11.3030,7.8730,8.7574,12.2452,12.2452,8.3121,9.1449 //ACM_CAREAW3// 13.1871,13.1871,8.7511,9.5319,14.1288,14.1288,9.1906,9.9193,15.0710,15.0710 //ACM_CAREAW4// 9.6296,10.3065,16.0130,16.0130,10.0691,10.6934,16.9549,16.9549,10.5081,11.0808 //ACM_CAREAH1// 0,0,2.0745,4.1493,0.6915,0.6915,2.5411,4.5120,1.3831,1.3831 //ACM_CAREAH2// 3.0074,4.8747,2.0745,2.0745,3.4739,5.2375,2.7662,2.7662,3.9405,5.6002 //ACM_CAREAH3// 3.4577,3.4577,4.4067,5.9629,4.1493,4.1493,4.8734,6.3256,4.8407,4.8407 //ACM_CAREAH4// 5.3399,6.6883,5.5324,5.5324,5.8063,7.0510,6.2238,6.2238,6.2726,7.4137 //ACM_CAREAV1// 0,0,1.5642,4.6929,0.6952,0.6952,2.0511,4.9295,1.3904,1.3904 //ACM_CAREAV2// 2.5380,5.1662,2.0857,2.0857,3.0248,5.4025,2.7811,2.7811,3.5116,5.6392 //ACM_CAREAV3// 3.4763,3.4763,3.9985,5.8758,4.1715,4.1715,4.4854,6.1124,4.8667,4.8667 //ACM_CAREAV4// 4.9720,6.3488,5.5622,5.5622,5.4590,6.5854,6.2575,6.2575,5.9457,6.8220 wing_area = 1319.803 wing_span = 111.25 wing_root_chord = 17.05 wing_dihedral = 5.11 wing_incidence = -0.784 wing_twist = 0 oswald_efficiency_factor = 0.76 wing_winglets_flag = 1 wing_sweep = 25 wing_pos_apex_lon = 12.81 wing_pos_apex_vert = -2.05 htail_area = 333.6812 htail_span = 40.84 htail_pos_lon = -49.08 htail_pos_vert = 4.67 htail_incidence = -1 htail_sweep = 34 vtail_area = 231.4241 vtail_span = 22.97 vtail_sweep = 35 vtail_pos_lon = -46.88 vtail_pos_vert = 8.63 elevator_area = 70.5 aileron_area = 40.22 rudder_area = 56.2 elevator_up_limit = 28.0 elevator_down_limit = 20.0 aileron_up_limit = 26.0 aileron_down_limit = 26.0 rudder_limit = 25.0 elevator_trim_limit = 18.5 spoiler_limit = 35.0 aileron_to_spoileron_gain = 1 spoiler_handle_available = 1 min_ailerons_for_spoilerons = 10 min_flaps_for_spoilerons = 0 spoilerons_available = 1 [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, 0, 17 avionics = 1, 0, 17 pitot_heat = 0, 2, 17 additional_system = 0, 0, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 light_nav = 0, 0, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 0, 17 [Reference Speeds] flaps_up_stall_speed=128.0 full_flaps_stall_speed=102.0 cruise_speed=455.0 max_mach = 0.82 max_indicated_speed = 350.0 [Flaps.0] type=1 span-outboard = 0.78 extending-time = 14 flaps-position.0 = 0.0, 0 flaps-position.1 = 1.0, 230 //Conf. 1 Intermediate approach flaps-position.2 = 10.0, 215 //Conf. 1+F Take off flaps-position.3 = 15.0, 200 //Conf. 2 Take off and Approach flaps-position.4 = 20.0, 185 //Conf. 3 Take off, Approach, and Landing flaps-position.5 = 40.0, 177 //Conf "Full" Landing damaging-speed = 230.0 blowout-speed = 250.0 lift_scalar = 0.347 //0.57 drag_scalar = 1.25 pitch_scalar = 0 system_type = 1 //Hydraulic [flaps.1] type=2 // 1 - tail, 2 - lead span-outboard = 0.85 extending-time = 4 flaps-position.0 = 0, 0 flaps-position.1 = 18, 230 //Conf. 1 Intermediate approach flaps-position.2 = 18, 215 //Conf. 1+F Take off flaps-position.3 = 22, 200 //Conf. 2 Take off and Approach flaps-position.4 = 22, 185 //Conf. 3 Take off, Approach, and Landing flaps-position.5 = 27, 177 //Conf "Full" Landing damaging-speed = 230 blowout-speed = 250 lift_scalar = 0.35 //0.55 drag_scalar = 0.4 pitch_scalar = 0.2 system_type = 1 //Hydraulic [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 [TurbineEngineData] fuel_flow_gain=0.004 inlet_area=24.440 rated_N2_rpm=29920 static_thrust=23300 //CFMI CFM56-5B9/P afterburner_available=0 reverser_available=1 [jet_engine] thrust_scalar=1.0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=700.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=113.000000 pitch_takeoff_ga=10.000000 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=1.8 max_bank_velocity=3.000000 max_throttle_rate=0.100000 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 = 1.00 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.125 //Percent throttle that activates warning flap_limit_idle = 5.0 //Flap angle that activates warning at idle flap_limit_power = 25.5 //Flap angle that activates warning at above idle [brakes] toe_brakes_scale=0.66 parking_brake=1 [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=43.22074,-1.723061,4.355627 ; Longitude, Latitude and Vertical position from Reference Point, (FEET) [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 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 = 2 attitude_indicator.1 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [stall_warning] type=2 [Views] eyepoint=43.22074,-1.723061,4.355627 ///(feet) longitudinal, lateral, vertical distance from reference datum3 [exits] number_of_exits = 2 exit_rate.0 = 0.2 ;Percent per second exit_rate.1 = 0.2 ;Percent per second [TailHook] tailhook_length=1 ;(feet) tailhook_position=0, 0, 0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1 [folding_wings] wing_fold_system_type=4 fold_rates=0.11,0.13
