[fltsim.0] title=Antonov An26 UA NAVY sim=An26 model= panel= sound= texture= prop_anim_ratio=-1.4 ui_manufacturer=Antonov ui_type=An26 ui_variation=Ua NAVI atc_id=UA40 atc_airline=UA NAVI atc_flight_number=UA40 visual_damage=1 description=Antonov An 26 light military transport Ukraine Navy SAR [fltsim.1] title=Antonov An26 Luftwaffe sim=An26 model= panel= sound= texture=1 prop_anim_ratio=-1.4 ui_manufacturer=Antonov ui_type=An26 ui_variation=Luftwaffe atc_id=5209 atc_airline=Luftwaffe atc_flight_number=5209 visual_damage=1 description=Antonov An 26 light military transport Luftwaffe [fltsim.2] title=Antonov An26 UN sim=An26 model= panel= sound= texture=2 prop_anim_ratio=-1.4 ui_manufacturer=Antonov ui_type=An26 ui_variation=UN atc_id=UNO962 atc_airline=UN atc_flight_number=UNO962 visual_damage=1 description=Antonov An 26 light military transport United Nations [fltsim.3] title=Antonov An26 Russian Ministry of Emergency (MChS) sim=An26 model= panel= sound= texture=3 prop_anim_ratio=-1.4 ui_manufacturer=Antonov ui_type=An26 ui_variation=Ru MCS atc_id=RA76314 atc_airline=MCS atc_flight_number=RA76314 visual_damage=1 description=Antonov An 26 Light transport Russian Ministry of Emergency (MChS) [General] atc_type=Antonov atc_model=An26 editable=0 performance=Antonov KB -1969, Crew 4 man, 2 Turboprop AI-24T 2075kW, weight 15020 starting weights 24000kg, loading 5500kg, speed 240mph, max 270, height 8100m, range 900-2250km, (C) 2002- Vladimir Zhyhulskiy: zh@selena.Kherson.ua [WEIGHT_AND_BALANCE] max_gross_weight=15000 // (pounds) empty_weight=9090 // (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=170, 5.0, -2.0, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, 5.0, 2.0, 0.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=170, -2.1, -2.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=170, -2.1, 2.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=170, -5.3, -2.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5=170, -5.3, 2.0, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=30000 empty_weight_roll_MOI=18200 empty_weight_yaw_MOI=36500 empty_weight_coupled_MOI=0.0 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=0.75 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.4 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=0.9 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [GeneralEngineData] engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-8.3, -4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-8.3, 4.8, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency [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=28920 //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=4270 //Maximum torque available (ft-lbs) [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 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 //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) [contact_points] point.0=1, 28.00, 0.00, -7.2, 1181, 0, 0.596, 39.9, 0.296, 2.5, 0.9516, 4.8, 4.8, 0, 0.0, 0.0 point.1=1, -1.67, -8.58, -7.2, 1574, 1, 0.596, 0.0, 0.642, 2.5, 0.8152, 4.5, 5.2, 2, 0.0, 0.0 point.2=1, -1.67, 8.58, -7.2, 1574, 2, 0.596, 0.0, 0.642, 2.5, 0.8152, 4.8, 4.9, 3, 0.0, 0.0 point.3=2, -3.33, -23.92, -6.00, 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, -6.00, 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, 6.00, 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, -3.50, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 static_pitch=-0 static_cg_height=6.6 [Views] eyepoint=4.54, -1.20, 3.25 [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 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator=150, 250 aileron=150, 250 rudder=150, 250 [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [SMOKESYSTEM] smoke.0=-3.400,-44.00,-10.48, fx_smoke_rx \\smoke.1=-3.200,-55.00,0.00, fx_smoke_rx smoke.2=-3.400,-44.00,10.48, fx_smoke_rx [fuel] LeftMain=0.0, -14.5, -1.0, 290.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftAux=0.0, -6.0, -1.5, 109.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=0.0, 14.5, -1.0, 290.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightAux=0.0, 6.0, -1.5, 109.5, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [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) [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=0 pitch_takeoff_ga=8.000000 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 4.1, -44.5, 4.6, fx_navred , light.1=3, 4.1, 44.5, 4.6, fx_navgre , light.2=2, 4.1, 44.5, 4.6, fx_strobe , light.3=2, 4.1, -44.5, 4.6, fx_strobe , light.4=1, -26.9, 0.00, 9.5, fx_beacon , light.5=1, -2.1, 0.00, -3.7, fx_beacon , light.6=4, -16, 1.5, -1.5, fx_vclight light.7=4, -3, -2.00, -1.3, fx_vclight light.8=4, -8, 2.00, -1.2, fx_vclight light.9=4, -10, -2.00, -1.40, fx_vclight light.10=4, -16, -1.5, -1.2, fx_vclight light11=4, -3, 2.00, -1.3, fx_vclight light.12=4, -8, -2.00, -1.2, fx_vclight light.13=4, -10, 2.00, -1.20, fx_vclight light.10=4, 16, -1.5, -1.5, fx_vclight light11=4, 18, -1.00, -1.2, fx_vclight light.12=4, 6, -1.00, -1.4, fx_vclight light.13=4, 20, -1.00, -1.3, fx_vclight light.14=4, 17, -1.00, -0.5, fx_vclight [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [airplane_geometry] wing_area=310.000000 wing_span=57.166667 wing_root_chord=5.416667 wing_dihedral=5.998535 wing_incidence=0.999756 wing_twist=-1.499634 oswald_efficiency_factor=0.517744 wing_winglets_flag=1 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=67.000000 htail_span=17.166667 htail_pos_lon=-24.583333 htail_pos_vert=0.000000 htail_incidence=0.499878 htail_sweep=0.000000 vtail_area=42.000000 vtail_span=7.389181 vtail_sweep=0.000000 vtail_pos_lon=-20.500000 vtail_pos_vert=4.083333 elevator_area=16.985000 aileron_area=13.477000 rudder_area=7.275000 elevator_up_limit=16.999658 elevator_down_limit=15.498508 aileron_up_limit=18.002334 aileron_down_limit=18.002334 rudder_limit=30.000070 elevator_trim_limit=15.000035 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 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 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
