[fltsim.0] title=OV-10A sim=OV-10A model= panel= sound= texture= kb_checklists= kb_reference= atc_id_color=0x00ffffff atc_id=14649 ui_manufacturer=North American Rockwell ui_type=OV-10A ui_variation=20th TASS ,Danang, South Viet Nam 1969 visual_damage=1 ui_createdby="Piglet's Peculiar Planes" description=Twin Turboprop FAC\/COIN aircraft designed in late '60's for USAF, and also USMC and Navy. Also used by Morocco, Thailand, Columbia, Indonesia, Venezuela, and the Philippines. atc_heavy=0 atc_airline= atc_flight_number= atc_id_font=Verdana,-11,1,600,0 prop_anim_ratio = 1.72 [fltsim.1] title=OV-10A_USMC sim=OV-10A model= panel= sound= texture=usmc kb_checklists= kb_reference= atc_id_color=0x00ffffff atc_id=55417 ui_manufacturer=North American Rockwell ui_type=OV-10A ui_variation=VMO 2 USMC,Danang, South Viet Nam 1970 visual_damage=1 ui_createdby="Piglet's Peculiar Planes" description=Twin Turboprop FAC\/COIN aircraft designed in late '60's for USAF, and also USMC and Navy. This one is in markings for 20th TASS, Danang, South Viet Nam, 1970 atc_heavy=0 atc_airline= atc_flight_number= atc_id_font=Verdana,-11,1,600,0 prop_anim_ratio = 1.72 [fltsim.2] title=OV-10A_USN sim=OV-10A model= panel= sound= texture=usn kb_checklists= kb_reference= atc_id_color=0x00ffffff atc_id=55494 ui_manufacturer=North American Rockwell ui_type=OV-10A ui_variation=VAL-4 USN, Bien Thuy, South Viet Nam 1971 visual_damage=1 ui_createdby="Piglet's Peculiar Planes" prop_anim_ratio = 1.72 description=Twin Turboprop FAC\/COIN aircraft designed in late '60's for USAF, and also USMC and Navy. This one is in markings for 20th TASS, Danang, South Viet Nam, 1970 atc_heavy=0 atc_airline= atc_flight_number= atc_id_font=Verdana,-11,1,600,0 [fltsim.3] title=OV-10A_MAF sim=OV-10A model=maf panel= sound= texture=maf kb_checklists= kb_reference= atc_id_color=0x00ffffff atc_id=55404 ui_manufacturer=North American Rockwell ui_type=OV-10A ui_variation=Moroccan Air Force 1980's visual_damage=1 ui_createdby="Piglet's Peculiar Planes" description=Twin Turboprop FAC\/COIN aircraft designed in late '60's for USAF, and also USMC and Navy. Also used by Morocco, Thailand, Columbia, Indonesia, Venezuela, and the Philippines. atc_heavy=0 atc_airline= atc_flight_number= atc_id_font=Verdana,-11,1,600,0 prop_anim_ratio = 1.72 [fltsim.4] title=OV-10E_VAF sim=OV-10A model=vaf panel= sound= texture=vaf kb_checklists= kb_reference= atc_id_color=0x00ffffff atc_id=0016 ui_manufacturer=North American Rockwell ui_type=OV-10E ui_variation=40 Squadron, Barcelona,Venezuelan Air Force 1973 visual_damage=1 ui_createdby="Piglet's Peculiar Planes" description=Twin Turboprop FAC\/COIN aircraft designed in late '60's for USAF, and also USMC and Navy. Also used by Morocco, Thailand, Columbia, Indonesia, Venezuela, and the Philippines. atc_heavy=0 atc_airline= atc_flight_number= atc_id_font=Verdana,-11,1,600,0 prop_anim_ratio = 1.72 [fltsim.5] title=OV-10F_IAF sim=OV-10A model=iaf panel= sound= texture=iaf kb_checklists= kb_reference= atc_id_color=0x00ffffff atc_id=0016 ui_manufacturer=North American Rockwell ui_type=OV-10F ui_variation=3 Squadron, Baucou,Indonesian Air Force 1981 visual_damage=1 ui_createdby="Piglet's Peculiar Planes" description=Twin Turboprop FAC\/COIN aircraft designed in late '60's for USAF, and also USMC and Navy. Also used by Morocco, Thailand, Columbia, Indonesia, Venezuela, and the Philippines. atc_heavy=0 atc_airline= atc_flight_number= atc_id_font=Verdana,-11,1,600,0 prop_anim_ratio = 1.72 [General] atc_type= North American atc_model=Bronco editable=1 performance= Category=airplane [weight_and_balance] // ACM V2.5 max_gross_weight =14000.0 empty_weight =7369.00000 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0.000, 0.000, 0.000 empty_weight_pitch_MOI =14556.00000 empty_weight_roll_MOI =6305.00000 empty_weight_yaw_MOI =15312.00000 empty_weight_coupled_MOI =0.00000 CG_forward_limit = 0.000 CG_aft_limit = 1.000 max_number_of_stations =0 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, 0.84, -19.85, 1.56, fx_navred light.1 = 3, -23.56, -7.07, 6.46, fx_navwhi light.2 = 3, 0.84, 19.79, 1.56, fx_navgre light.3 = 1, -19.37, 0.03, 6.99, fx_beacon light.4 = 1, 3.72, 0, -2.65, fx_beacon light.5 = 8, 9.50, 0, 0.53, fx_vclight_deepred light.6 = 8, 5.88, 0, 0.57, fx_vclight_deepred [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type =5 fuel_flow_scalar =1.00000 min_throttle_limit = -0.250000 engine.0 =3.800, -7.200, 0.000 engine.1 =3.800, 7.200, 0.000 [smokesystem] smoke.0 = 0.11, -1.90, -8.36, fx_smoke_w [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 = 0.000, -6.000, 1.000, 123.500, 3.000 RightMain = 0.000, 6.000, 1.000, 123.500, 3.000 External1 = 0.000, 0.000, -3.460, 150.000, 0.000 [contact_points] static_pitch = -3.360 static_cg_height = 7.000 tailwheel_lock =0 gear_system_type =1 max_number_of_points =8 point.0= 1, 10.194, 0.000, -6.252, 2000, 0, 0.900, 45.000, 0.250, 2.500, 0.900, 6.000, 9.000, 0 point.1= 1, -1.455, -7.624, -6.993, 2500, 1, 1.150, 0.000, 1.000, 1.300, 0.900, 7.000, 10.000, 2 point.2= 1, -1.409, 7.624, -6.998, 2500, 2, 1.150, 0.000, 1.000, 1.300, 0.900, 7.000, 10.000, 3 point.3= 2, 0.000, -19.777, 0.998, 787, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5 point.4= 2, 0.000, 19.777, 0.998, 787, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6 point.5= 2, -18.952, 0.000, 0.046, 787, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9 point.6= 2, 4.677, 0.000, -3.048, 787, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4 point.7= 5, -3.900, 0.000, 0.000, 1600, 0, 0.000, 50.000, 0.000, 0.000, 1.000, 1.000, 1.200, 0 [keyboard_response] elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [airplane_geometry] wing_area =291.00000 wing_span =40.00000 wing_root_chord =7.50000 wing_dihedral =0.00000 wing_incidence =0.00000 wing_twist =0.00000 oswald_efficiency_factor =0.70000 wing_winglets_flag =0 wing_sweep =0.00000 wing_pos_apex_lon =1.81933 wing_pos_apex_vert =1.50000 htail_area =70.00000 htail_span =14.00000 htail_pos_lon =-21.50000 htail_pos_vert =7.20000 htail_incidence =0.00000 htail_sweep =0.00000 vtail_area =64.00000 vtail_span =8.00000 vtail_sweep =30.00000 vtail_pos_lon =-20.50000 vtail_pos_vert =4.10000 elevator_area =22.75000 aileron_area =16.30000 rudder_area =24.00000 elevator_up_limit =17.00000 elevator_down_limit =18.00000 aileron_up_limit =18.00000 aileron_down_limit =18.00000 rudder_limit =30.00000 elevator_trim_limit =15.00000 spoiler_limit =90.00000 aileron_to_spoileron_gain =4.00000 spoiler_handle_available =0 min_ailerons_for_spoilerons =0.00000 min_flaps_for_spoilerons =0.00000 spoilerons_available =1 auto_spoiler_available=0 positive_g_limit_flaps_up=6.00000 negative_g_limit_flaps_up=-4.80000 positive_g_limit_flaps_down=4.20000 negative_g_limit_flaps_down=-3.60000 load_safety_factor=1.00000 spoiler_extension_time=0.000000 [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, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 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 [exits] number_of_exits = 3 exit_rate.0 = 0.8 ;Percent per second exit_rate.1 = 0.8 ;Percent per second exit_rate.2 = 0.8 [flight_tuning] cruise_lift_scalar=1.00000 parasite_drag_scalar=1.00000 induced_drag_scalar=1.00000 elevator_effectiveness=1.00000 aileron_effectiveness=1.00000 rudder_effectiveness=1.00000 pitch_stability=1.00000 roll_stability=1.00000 yaw_stability=1.00000 elevator_trim_effectiveness=1.00000 aileron_trim_effectiveness=1.00000 rudder_trim_effectiveness=1.00000 hi_alpha_on_roll=1.00000 hi_alpha_on_yaw=1.00000 p_factor_on_yaw=0.00000 torque_on_roll=0.00000 gyro_precession_on_roll=0.00000 gyro_precession_on_yaw=0.00000 [propeller] thrust_scalar=1.00000 propeller_type=0 propeller_diameter=9.00000 propeller_blades=3 propeller_moi=11.22477 beta_max=45.00000 beta_min=15.20000 min_gov_rpm=22500.00000 prop_tc=0.01000 gear_reduction_ratio=7.06000 fixed_pitch_beta=0.00000 low_speed_theory_limit=80.00000 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=1 min_rpm_for_feather=700.00000 beta_feather=79.30000 power_absorbed_cf=0.90000 defeathering_accumulators_available=0 prop_reverse_available=1 minimum_on_ground_beta=1.00000 minimum_reverse_beta=-14.00000 //rotation=1,-1 //Engine 1,2,3,... Rotation direction. 1 = CW, -1 = CCW [TurbineEngineData] fuel_flow_gain=0.01100 inlet_area=1.20000 rated_N2_rpm=15000.00000 static_thrust=150.00000 afterburner_available=0 reverser_available=0 [turboprop_engine] power_scalar=1.00000 maximum_torque=1767.43805 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [Views] eyepoint=8.94, 0.00, 1.81 [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 [Reference Speeds] flaps_up_stall_speed=95.99996 full_flaps_stall_speed=76.79997 cruise_speed=200.00000 max_indicated_speed=400.00000 max_mach=0.58000 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.00000 autothrottle_available=0 pitch_takeoff_ga=8.00000 max_pitch=10.00000 max_pitch_acceleration=1.00000 max_pitch_velocity_lo_alt=2.00000 max_pitch_velocity_hi_alt=1.50000 max_pitch_velocity_lo_alt_breakpoint=20000.00000 max_pitch_velocity_hi_alt_breakpoint=28000.00000 max_bank=25.00000 max_bank_acceleration=1.80000 max_bank_velocity=3.00000 max_throttle_rate=0.10000 nav_proportional_control=9.00000 nav_integrator_control=0.25000 nav_derivative_control=0.00000 nav_integrator_boundary=2.50000 nav_derivative_boundary=0.00000 gs_proportional_control=9.52000 gs_integrator_control=0.26000 gs_derivative_control=0.00000 gs_integrator_boundary=0.70000 gs_derivative_boundary=0.00000 yaw_damper_gain=0.00000 autothrottle_arming_required=0 default_pitch_mode=0 default_bank_mode=0 use_no_default_bank=1 use_no_default_pitch=1 autothrottle_takeoff_ga=1.00000 autothrottle_max_rpm=90.00000 [Flaps.0] type= 1 system_type=1 span-outboard= 0.700 extending-time= 8.0 damaging-speed=175.0 blowout-speed=200.0 flaps-position.0=0.00, 360.0 flaps-position.1=10.00, 337.5 flaps-position.2=20.00, 315.0 flaps-position.3=30.00, 292.5 flaps-position.4=50.00, 270.0 lift_scalar=1.00 drag_scalar=0.00 pitch_scalar=0.00 [brakes] toe_brakes_scale=1.00000 parking_brake=1 auto_brakes=0 hydraulic_system_scalar=0.00000 differential_braking_scale=0.00000 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.09998 flap_limit_power=30.02299 flap_limit_idle=15.01149 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.00000 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [flaps.1] type= 2 system_type=1 span-outboard= 0.500 extending-time= 8.0 damaging-speed=175.0 blowout-speed=200.0 flaps-position.0=0.00 flaps-position.1=1.00 flaps-position.2=20.00 flaps-position.3=30.00 flaps-position.4=40.00 lift_scalar=0.00 drag_scalar=0.00 pitch_scalar=1.00 [flaps.2] type= 2 system_type=1 span-outboard= 0.500 extending-time= 8.0 damaging-speed=175.0 blowout-speed=200.0 flaps-position.0=0.00 flaps-position.1=1.00 flaps-position.2=20.00 flaps-position.3=30.00 flaps-position.4=40.00 lift_scalar=0.00 drag_scalar=1.00 pitch_scalar=0.00 [AirWrench] Aircraft_Length=40.00000 Vmax_sl=323.36890 Vmax_ca=404.95913 V_rc=139.12918 Climb_Rate=2000.00000 Climb_Weight=10000.00000 Max_gforce=6.00000 Emergency_hp=0.00000 VSI_Weight=10000.00000 nose_position_lon=13.00000 ActualIncidence=1.00000 ActualTwist=-1.50000 ActualTailIncidence=0.50000 Aircraft_Type=1 FlowCorrection=1.00000 Power_Calibration=1.00000 JetAltitude=0.00000 turboprop_critical_altitude=25000.00000 target_roll_Vopt=230.15580 target_roll_rate=60.00000 pitch_damping=1.00000 yaw_damping=1.00000 elevator_scalar=1.00000 rudder_scalar=2.00000 dihedral_scalar=0.00000 Elevator_FF=50.00000 Aileron_FF=-60.00000 Roll_Response=9.00000 Adverse_Yaw=100.00000 Control_Response=70.00000 V_Max_Control=400.00000 V_Zero_Control=450.00000 Spin_Stability=50.00000 Stall_Stability=80.00000 ClAoA_S0=1.00000 ClAoA_S1=1.00000 ClAoA_S2=1.00000 Elevator_Propwash=1.00000 Rudder_Propwash=2.00000 spoiler_time=0.00000 afterburner_thrust=75.00000 mach_scale=1.00000 prop_design_altitude=5000.00000 protect_airfile=0 spoiler_type=0 spoiler_cd=0.00000 spoiler_cl=0.00000 spoiler_cm=0.00000 flaps_type=3 flaps_cd_scalar=0.90440 flaps_cm_scalar=0.14000 vfe_enabled=1 gear_cd_scalar=0.15000 gear_cm_scalar=-0.02000 cylinder_head_temperature=501.00000 exhaust_gas_temperature=1077.00000 fuel_pressure=16.50000 oil_pressure=125.00000 oil_temperature=141.00000 radiator_temperature=211.00000 exhaust_pressure_ratio=1.40000 interstage_turbine_temperature=1904.00000 knots_flag=1 cfs1_flag=0 cfs2_flag=0 ai_flag=0 fs8_flag=1 laminar_flow=1 edit_tp_torque=0 direct_edit_mach=0 fixed_wing_pos=0 AirWrenchVersion=1.01.39 ReheatCutoff=1.20000 OptimumMach=0.90000 weathervane=1.00000 critical_mach_number=0.80000 max_mach_cd0=60 mach_slope=1.00000 direct_edit_drag=0 direct_edit_2dtab=0 range_est_alt=0.00000 range_est_rpm=0.00000 range_est_mp=29.92000 range_est_fuel=397.00000 [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=0.150000 [deice_system] structural_deice_type=0
