//============================================= //======V.Zhyhulskiy - Kiev-Ukraine-02/2009 - Â.Æèãóëüñêèé =============== //============================================= [fltsim.0] title=Antonov An-12BK Kosmos Cargo AL (Russia) sim=An12BKzh model=CGR panel= sound= texture=KSM checklists= atc_id=Kosm prop_anim_ratio=-1.15 atc_airline=Kosmos atc_flight_number=1295 ui_manufacturer=Antonov ui_type=An-12BK visual_damage=1 atc_heavy=0 ui_variation=Kosmos description=Antonov An-12BK Kosmos Cargo AL (Russia) long ranger transport (autor Vladimir Zhyhulskiy - 12/2008) /============================================= [fltsim.1] title=Antonov An-12BK ATRAN Cargo AL (Russia) sim=An12BKzh model=CGR panel= sound= texture=ATR checklists= atc_id=9391 prop_anim_ratio=-1.15 atc_airline=ATRAN atc_flight_number=9391 ui_manufacturer=Antonov ui_type=An-12BK visual_damage=1 atc_heavy=0 ui_variation=ATRAN_93911 description=Antonov An-12BK ATRAN Cargo AL (Russia) long ranger transport (autor Vladimir Zhyhulskiy - 12/2008) /============================================= [fltsim.2] title=Antonov An-12B Goliaf Air Cargo AL (Sao Tome und Principe) sim=An12BKzh model=AFR panel= sound= texture=GOL checklists= atc_id=Kosm prop_anim_ratio=-1.15 atc_airline=Goliaf atc_flight_number=S9BO ui_manufacturer=Antonov ui_type=An-12BK visual_damage=1 atc_heavy=0 ui_variation=Goliaf Air description=Antonov An-12BK Goliaf Air Cargo AL (Sao Tome and Principe) long ranger transport (autor Vladimir Zhyhulskiy - 12/2008) /============================================= [fltsim.3] title=Antonov An-12BK Air Armenia Cargo AL model=CGR panel= sound= texture=ARM checklists= atc_id=Kosm prop_anim_ratio=-1.15 atc_airline=Air Armenia atc_flight_number=S9BO ui_manufacturer=Antonov ui_type=An-12BK visual_damage=1 atc_heavy=0 ui_variation=Air Armenia description=Antonov An-12BK Air Armenia Cargo AL (Armenia) long ranger transport (autor Vladimir Zhyhulskiy - 12/2008) /============================================= [fltsim.4] title=Antonov An-12BK Aeroflot Polar Cargo AL (Russia) sim=An12BKzh model=CGR panel= sound= texture=POL checklists= atc_id=Kosm prop_anim_ratio=-1.15 atc_airline=Aeroflot Polar atc_flight_number=1295 ui_manufacturer=Antonov ui_type=An-12BK visual_damage=1 atc_heavy=0 ui_variation=Aeroflot Polar description=Antonov An-12BK long ranger transport (autor Vladimir Zhyhulskiy - 2/2009, textures - Alexander Vysokovskiy) /============================================= [fltsim.5] title=Antonov An-12BK AFL Blue SU sim=An12BKzh model=CGR panel= sound= texture=11120 kb_checklists= atc_id=11120 prop_anim_ratio=-1.15 ui_manufacturer=Antonov atc_airline=ATRAN atc_flight_number=1112 ui_type=An-12BK visual_damage=1 atc_heavy=0 ui_variation=AFL Blue SU description=Antonov An-12BK 11120 (USSR) long ranger transport (autor Vladimir Zhyhulskiy - 2/2009, texture aka DIV) /============================================= [fltsim.6] title=Antonov An-12BK 11107 sim=An12BKzh model=CGR panel= sound= texture=RW checklists= atc_id=11107 prop_anim_ratio=-1.15 atc_airline=Aeroflot atc_flight_number=1107 ui_manufacturer=Antonov ui_type=An-12BK visual_damage=1 atc_heavy=0 ui_variation=Red Wings description=Antonov An-12BK AEROFLOT (USSR) long ranger transport (autor Vladimir Zhyhulskiy - 2/2009, textures Alexandr Doronin 02/2009) /============================================= [fltsim.7] title=Antonov An-12BK Aeroflot RA-11375 Cargo(Russia) sim=An12BKzh model=CGR panel= sound= texture=11375 checklists= atc_id=11868 prop_anim_ratio=-1.15 atc_airline=Aeroflot atc_flight_number=375 ui_manufacturer=Antonov ui_type=An-12BK visual_damage=1 atc_heavy=0 ui_variation=AFL Blue description=Antonov An-12BK Aeroflot Cargo AL (Russia) long ranger transport (autor Vladimir Zhyhulskiy - 2/2009, textures -aka GNOM) /============================================= [fltsim.8] title=An-12BK DONAVIA sim=An12BKzh model=CGR panel= sound= texture=DON checklists= atc_id=12974 prop_anim_ratio=-1.15 atc_airline=donavia atc_flight_number=2974 ui_manufacturer=Antonov ui_type=An-12BK visual_damage=1 atc_heavy=0 ui_variation=DonAvia description=Antonov An-12BK DonAvia Cargo Al (Russia) long ranger transport (autor Vladimir Zhyhulskiy - 2/2009, textures - aka GNOM) //============================================= //============================================= //============================================= [General] performance=Antonov An-12BK long ranger military transport atc_type=Antonov atc_model=An12 //============================================= //============================================= //============================================= [weight_and_balance] max_gross_weight=163000 empty_weight=80600 reference_datum_position=0, 0, 0 empty_weight_CG_position=0, 0, 0 empty_weight_pitch_MOI= 4700000 \\\4100000 empty_weight_roll_MOI= 6400000 \\\4400000 empty_weight_yaw_MOI= 7400000 empty_weight_coupled_MOI=0 max_number_of_stations=4 station_load.0="200, 34, -1, -4, Captain" station_load.1="200, 34, 1, -4, First Officer" station_load.2="200, 31, 2, -9, Radist" station_load.3="200, 29, 0, -7, Navigator" station_load.4="200, 25, -2, -9, Flight Engeneer" //============================================= //=================TUNING=================== //============================================= [FLIGHT_TUNING] cruise_lift_scalar=0.93 parasite_drag_scalar=0.80 induced_drag_scalar=0.93 elevator_effectiveness=1.41 aileron_effectiveness=1.40 rudder_effectiveness=1.20 pitch_stability=1.10 roll_stability=0.91 \\0.75 yaw_stability=1 \\0.87 elevator_trim_effectiveness=0.24 aileron_trim_effectiveness=1.00 rudder_trim_effectiveness=1.00 p_factor_on_yaw=1.0 torque_on_roll=1.0 gyro_precession_on_roll=1.0 gyro_precession_on_yaw=1.0 //===================// ENGINES //=================== [GeneralEngineData] engine_type=5 fuel_flow_scalar=0.64 \\\\0.47 engine.0=3.3, -33.0, 3.5 engine.1=3.3, -16.25, 3.5 engine.2=3.3, 16.25, 3.5 engine.3=3.3, 33.0, 3.5 min_throttle_limit=-0.15 [TurbineEngineData] fuel_flow_gain=0.033 \\\\0.018 inlet_area=1.0 rated_N2_rpm=27920 \\\29920 static_thrust=130 \\\158 afterburner_available=0 reverser_available=1 [turboprop_engine] power_scalar=1.27 maximum_torque=18700 \\\19600 [propeller] thrust_scalar=1.21 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=12 //Propeller Diameter, (feet) propeller_blades=4 //Number of propeller blades propeller_moi=23 //Propeller moment of inertia beta_max=50 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=8 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=25520 //Miminum governed RPM prop_tc=0.008 //Prop time-constant gear_reduction_ratio=15.4 //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=0.95 //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=-6.0 //Minimum pitch angle in reverse, (degrees) //===================FUEL===================================== [FUEL] Center1=0.00, 0.00, 0.00, 1200.0, 400.0 LeftMain=0.00,-8.5, -1.00, 2100.0, 400.0 RightMain=0.00, 8.5, -1.00, 2100.0, 400.0 LeftAux= -0.45, -20.0, -2.33, 300.00 RightAux= -0.45, 20.0, -2.33, 300.00 fuel_type=2 number_of_tank_selectors=1 electric_pump=0 //===================================================== ///================FLAPS============================== ///===================================================== [Flaps.0] type= 1 span-outboard= 0.800 extending-time= 10.000 system_type= 0 damaging-speed= 270.000 blowout-speed= 320.000 lift_scalar= 0.87 drag_scalar= 1.09 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.2= 15.000, 0.000 flaps-position.3= 25.000, 0.000 flaps-position.6= 35.000, 0.000 //============================================================== //===================CONTACT============================== //============================================================== [contact_points] //0 Class <0=none,1=wheel, 2=scrape, 3=float> //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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0 = 1.000, 34.000, 0.000, -9.90, 3000.000, 0.000, 1.500, 40.000, 0.300, 2.500, 0.700, 11.000, 11.000, 0.000, 335.000, 340.000 point.1 = 1.000, -7.000, -7.000, -9.4, 5000.000, 1.000, 2.200, 0.000, 0.300, 2.500, 0.700, 14.000, 14.000, 2.000, 335.000, 340.000 point.2 = 1.000, -7.000, 7.000, -9.4, 5000.000, 2.000, 2.200, 0.000, 0.300, 2.500, 0.700, 14.000, 14.000, 3.000, 335.000, 340.000 point.3 = 2.000, -2.970, -65.380, 9.560, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4 = 2.000, -2.970, 65.380, 9.560, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5 = 2.000, -54.750, 0.000, 8.450, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6 = 2.000, 41.270, 0.000, -1.500, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000, 0.000 point.7= 5, -20.9, -5.25, -7.30,1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 8.0, 8.2, 0, 0.0, 0.0 static_pitch = 0.95 static_cg_height = 9.45 tailwheel_lock = 0 gear_system_type = 0 max_number_of_points = 7 //============================================================== //===================LIGHTS===================================== //============================================================== [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, //7=RECOGNITION, 9=LOGO, 10=CABIN light.0=1, -20.00, 0.00, -5.80, fx_beacon , light.1 = 2, -6.1, -59.90, 6.3, ZH_strobeR , light.2 = 2,-6.1, 59.90, 6.3, ZH_strobeG , light.3 = 3, -52.60, 0.00, 27.40, fx_navred , Light.4 = 3, -62.70, 0.00, 6.30, fx_navwhi , light.5=2, -6.1, 59.90, 6.3, fx_navgre, light.6=4, 2.39, 0.00, 4.50, ZH_vcAn12 , Light.7 = 10, -12.30, -0.20, 5.1, ZH_cabin , ////SMOKE light.8= 7, -6.9, -32.8, 2, zh_An12smok, light.9= 7, -6.9, -16.8, 2, zh_An12smok, light.10= 7, -6.9, 16.8, 2, zh_An12smok, light.11=7, -6.9, 32.8, 2, zh_An12smok, //============================================= //============================================= //============================================= [brakes] toe_brakes_scale=0.91 parking_brake=1 ///============================================== ///============================================== ///================AUTO========================== ///============================================== [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_max_rpm=90 autothrottle_takeoff_ga=1 pitch_takeoff_ga=8 use_no_default_bank=1 use_no_default_pitch=1 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2 max_pitch_velocity_hi_alt=1.5 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=1.000000 default_pitch_mode=0 default_bank_mode=0 //============================================================== //===================VVVVVVVV=================================== //============================================================== [Views] eyepoint=3.85 , -2.27, 5.10 //============================================================== //====================EFFECT&ANIMATIONS========================= //============================================================== [exits] number_of_exits = 2 exit_rate.0 = 0.4 exit_rate.1 = 0.4 [TailHook] tailhook_length=1.1 ;(feet) tailhook_position=-21.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=0.9 [folding_wings] wing_fold_system_type=4 fold_rates=0.11,0.13 ;Percent per second //=================================================== [EFFECTS] wake = fx_wake water = fx_spray dirt = ZH_An12dust ///dirt = ZH_An12snow concrete = fx_sparks touchdown= fx_tchdwn, 1 startup= zh_An12start windshield_rain_effect_available = 1 //============================================================== //===================GEOMETRY=================================== //============================================================== [airplane_geometry] wing_area=3050 wing_span=144 wing_root_chord=16.60 wing_dihedral=1 wing_incidence=1 wing_twist=1 oswald_efficiency_factor=0.99 wing_winglets_flag=0 wing_sweep=0 wing_pos_apex_lon=3.6 wing_pos_apex_vert=-2 htail_area=610 htail_span=55.20 htail_pos_lon=-42.2 htail_pos_vert=-2 htail_incidence=0.0 htail_sweep=0 vtail_area=400 vtail_span=24.80 vtail_sweep=0 vtail_pos_lon=-32.68 vtail_pos_vert=-2.01 elevator_area=232 aileron_area=200 rudder_area=230 elevator_up_limit=25 elevator_down_limit=15 aileron_up_limit=25 aileron_down_limit=15 rudder_limit=31.5 elevator_trim_limit=25 spoiler_limit=45 aileron_to_spoileron_gain=0 min_ailerons_for_spoilerons=0 min_flaps_for_spoilerons=0 spoilerons_available=1 //============================================================== //===================MISK======================================= //============================================================== [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=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=2700 gear_bump_right_direction=00500 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 [keyboard_response] elevator=150, 250 aileron=150, 250 rudder=150, 250 [Reference Speeds] flaps_up_stall_speed=90.0 full_flaps_stall_speed=92.0 cruise_speed=340.0 max_indicated_speed=370.0 max_mach=0.64 //============================================= [ELECTRICAL] autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 ///==========================================END!!! [Radios] Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 0, 1 Nav.2=1, 0, 1 Adf.1=1 Transponder.1=1 Marker.1=1 [direction_indicators] direction_indicator.0=3,0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_idle=5.042029 flap_limit_power=25.496622 [brakes] toe_brakes_scale=0.48 parking_brake=1 [hydraulic_system] normal_pressure=3000.000000 electric_pumps=0 engine_map=1,1,1,1 [stall_warning] type=1 [pitot_static] vertical_speed_time_constant=1
