[fltsim.0] title=Civil Aviation Flying Unit sim=civiloxford model= panel= sound= texture= KB_checklists=Airspeedoxford_check kb_reference=Airspeedoxford_ref atc_id=GAJX1 ui_manufacturer=Airspeed ui_type=Oxford ui_variation=Civil Aviation Flying Unit description=The Airspeed Oxford was a ww11 military trainer which was derived from the airspeed envoy.The Pioneer aviator Amy Johnson tragically lost her life in an Oxford after crashing into the river Thames estuary in January, 1941.This particular colour scheme was used by The Ministry of Civil Aviation Flying Unit at Gatwick. atc_heavy=0 atc_airline=Airforce atc_flight_number= [General] atc_type=Airspeed atc_model=Oxford editable=1 performance=Max speed\n182 mph 291 km\/h @ 19,200 ft\n\nEngine\nradial air-cooled Armstrong Siddeley Cheetah X\n\nMax Weight\n7,600 lb 3,450 kg\n\nCeiling\n19,200 ft\n\nMax climb rate\n930 ft\/min \/min\n\nRange\n550 miles 885 km [WEIGHT_AND_BALANCE] max_gross_weight = 8000.000 empty_weight = 5670.000 reference_datum_position = 19.250, 0.000, 0.000 empty_weight_CG_position = -20.900, 0.000, 0.000 max_number_of_stations =50 station_load.0 =170.000000, -5.400000, -2.000000, 0.000000, Pilot station_load.1 =170.000000, -5.400000, 2.000000, 0.000000, Co-Pilot station_load.2 =680.000000, -14.200000, 0.000000, 0.000000, Passenger Row 1 station_load.3 =680.000000, -17.400000, 0.000000, 0.000000, Passenger Row 2 station_load.4 =680.000000, -20.700000, 0.000000, 0.000000, Passenger Row 3 station_load.5 =680.000000, -23.900000, 0.000000, 0.000000, Passenger Row 4 station_load.6 =510.000000, -27.200000, 0.000000, 0.000000, Passenger Row 5 station_load.7 =510.000000, -30.400000, 0.000000, 0.000000, Passenger Row 6 station_load.8 =340.000000, -33.700000, 0.000000, 0.000000, Passenger Row 7 station_load.9 =340.000000, -36.900000, 0.000000, 0.000000, Passenger Row 8 station_load.10 =500.000000, -23.800000, 0.000000, 0.000000, Forward Baggage station_load.11 =100.000000, -45.500000, 0.000000, 0.000000, Rear Cargo ;Moments of Inertia empty_weight_pitch_MOI = 69699.030 empty_weight_roll_MOI = 61179.100 empty_weight_yaw_MOI = 131797.970 empty_weight_coupled_MOI = 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.000 induced_drag_scalar =1.000 elevator_effectiveness =1.000 aileron_effectiveness =1.000 rudder_effectiveness =1.000 pitch_stability =1.000 roll_stability =1.000 yaw_stability =1.000 elevator_trim_effectiveness =1.000 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =1.000 p_factor_on_yaw = -0.3 torque_on_roll = -0.3 gyro_precession_on_yaw = 0.0 gyro_precession_on_pitch = 1.0 [GeneralEngineData] engine_type = 0 Engine.0 = -15.950, -7.100, -1.800 Engine.1 = -15.950, 7.100, -1.800 fuel_flow_scalar= 1.000 min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser master_ignition_switch = 1 //Master Ignition Switch [piston_engine] power_scalar =1.000 cylinder_displacement= 130.710 compression_ratio= 6.700 number_of_cylinders= 14 max_rated_rpm= 2700.000 max_rated_hp= 1200.000 fuel_metering_type= 1 cooling_type= 0 normalized_starter_torque= 0.300 turbocharged= 1 max_design_mp= 47.000 min_design_mp= 10.000 critical_altitude= 7000.000 emergency_boost_type= 0 emergency_boost_mp_offset= 0.000 emergency_boost_gain_offset= 0.000 fuel_air_auto_mixture= 1 auto_ignition= 1 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 [propeller] thrust_scalar =0.571 propeller_type= 0 propeller_diameter= 11.530 propeller_blades= 3 propeller_moi= 40.200 beta_max= 30.000 beta_min= 18.000 min_gov_rpm= 1400.000 prop_tc= 0.100 gear_reduction_ratio= 1.778 fixed_pitch_beta= 0.000 low_speed_theory_limit= 80.000 prop_sync_available= 1 prop_deice_available= 1 prop_feathering_available= 1 prop_auto_feathering_available= 0 min_rpm_for_feather= 700.000 beta_feather= 89.500 power_absorbed_cf= 0.900 defeathering_accumulators_available= 0 prop_reverse_available= 0.000 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 feathering_switches = 1 //Switches which invoke feathering //0 Class //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 [contact_points] point.0= 1.000, -56.000, 0.000, 2.900, 1200.000, 0.000, 0.600, 50.000, 0.200, 2.500, 0.695, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, -18.550, -9.250, -6.500, 1600.000, 1.000, 1.350, 0.000, 0.204, 2.500, 0.686, 7.000, 9.000, 7.000, 166.000, 166.000 point.2= 1.000, -18.550, 9.250, -6.500, 1600.000, 2.000, 1.350, 0.000, 0.204, 2.500, 0.682, 7.000, 9.000, 7.000, 166.000, 166.000 point.3= 2.000, -27.000, -46.300, -0.100, 800.000, 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, -27.000, 46.300, -0.100, 800.000, 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, -61.000, 0.000, 14.000, 800.000, 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, 0.400, 0.000, -1.200, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch = 14.360 static_cg_height = 5.900 gear_system_type=0 //Hydraulic tailwheel_lock = 0 [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 = 0.3 //Brake scalar differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected [hydraulic_system] normal_pressure = 732.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint = -17.000, -0.9, 3.117 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -20.20, -27.0, 0.93, fx_navredm , light.1 = 3, -20.20, 27.0, 0.84, fx_navgrem , light.2 = 2, -20.20, -27.0, 0.93, fx_strobe, light.3 = 2, -20.20, 27.0, 0.84, fx_strobe, light.4 = 3, -44.30, 0.00, 1.80, fx_navwhi , light.5 = 4, -15.00, -1.00, 1.317, fx_vclight, [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 = 0 Adf.2 = 0 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 =200, 1000 aileron =200, 1000 rudder =200, 1000 [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=1,0 direction_indicator.1=2,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 attitude_indicator.1 = 2 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0=2,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks startup=fx_engstrt_jenny touchdown=fx_tchdwn_s, 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 25 max_generator_alternator_amps = 100 [fuel] LeftMain = -22.550, -6.700, -3.000, 202.000, 0.000 RightMain= -22.550, 6.700, -3.000, 202.000, 0.000 Center1 = -22.550, 0.000, -2.700, 200.000, 0.000 fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 2 electric_pump=1 [airplane_geometry] wing_area = 987.000 wing_span = 95.000 wing_root_chord = 12.850 wing_dihedral = 5.000 wing_incidence = 2.000 wing_twist = -1.000 oswald_efficiency_factor= 0.650 wing_winglets_flag = 0 wing_sweep = 14.500 wing_pos_apex_lon = -13.000 wing_pos_apex_vert = -2.700 htail_area = 95.800 htail_span = 28.250 htail_pos_lon = -52.700 htail_pos_vert = -52.700 htail_incidence = -1.000 htail_sweep = 27.000 vtail_area = 37.900 vtail_span = 11.490 vtail_sweep = 50.400 vtail_pos_lon = -51.400 vtail_pos_vert = 6.700 elevator_area = 83.400 aileron_area = 102.800 rudder_area = 46.700 elevator_up_limit = 30.000 elevator_down_limit = 20.000 aileron_up_limit = 27.000 aileron_down_limit = 18.000 rudder_limit = 30.000 elevator_trim_limit = 12.000 spoiler_limit = 0.000 spoilerons_available = 0 aileron_to_spoileron_gain = 0.000 min_ailerons_for_spoilerons = 0.000 min_flaps_for_spoilerons = 0.000 [Reference Speeds] flaps_up_stall_speed = 67.500 full_flaps_stall_speed = 61.500 cruise_speed = 95.000 max_indicated_speed = 224 //Red line (KIAS) [autopilot] autopilot_available= 1 flight_director_available= 0 pitch_takeoff_ga=0.0 default_vertical_speed=700.000000 autothrottle_available=0 direction_indicator=1 attitude_indicator =1 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=1.800000 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 = 0.0 default_bank_mode=2 //Default to Heading Hold [forcefeedback] ground_bumps_magnitude1=2600 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.6 ground_bumps_magnitude2=1200 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.085 ground_bumps_slope2=0.65 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=3500000 ; in microseconds [stall_warning] type=1 [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 7.000 system_type= 1 damaging-speed= 140.000 blowout-speed= 175.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 15.000, 0.000 flaps-position.2= 30.000, 0.000 flaps-position.3= 45.000, 0.000