[fltsim.0] title=Canberra Armed sim=Canberra Armed model= panel= sound= texture= kb_checklists= title=GAF_Canberra-Armed_(Vietnam) 1967-72 sim=Canberra visual_damage=1 model=GAF_RAAFarmed panel= sound= texture= atc_heavy=0 atc_id=MP234 atc_airline=Air Force atc_flight_number=MP234 atc_parking_codes=ASY ui_manufacturer=GAF Australia ui_type="Canberra B.MK20" ui_variation=RAAF No.2 Sqn Armed (1967-1972) description= First flight 24/07/56. Delivered 17/09/56. Served with 2 Sqn in Vietnam as part of USAF 35th Tactical Fighter Wing. Arrived at Phan Rang Air Base 16/04/67 after a 2 hour flight from Butterworth, Malaysia. On 09/02/71 WGCDR John Downing and SQNLDR B A Johnson were providing close air support for troops engaging the enemy. On the last of 5 bombing runs the aircraft was hit in the nose by shrapnel from one of its own bombs, the bomb fragment narrowly missed the crew, partially severed the elevator cables and embedding itself in the IFF panel. Their actions that day saw Downing and Johnson awarded the American DFC. On 07/04/71, this time crewed by FLTOFF S Fenton and PLTOFF P Murphy, 234 provided close air support to a US Army Infantry company in contact with a large enemy force. Despite the close proximity of friendly forces, and heavy ground fire, 6 single drop bombing runs were made without any US casualties. The enemy suffered 80 lost and retreated. [General] atc_type=GAF atc_model=CANBERRA performance=Width : 19.24m (63ft 11.5in)\nLength : 19.99m (65ft 6in)\nHeight : 4.79m (15ft 7in)\nEngines : Two RR Avon 109 Turbojets\nThrust : 7,500lbs static thrust each\nSpeed : 620mph\nService Ceiling : 45-50,000ft\nRange : 3,000 miles (with tip tanks)\nArmament : 4 x 750lb bombs (internal)\n2 x 750lb bombs (on wing pylons)\n Flight Dynamics By: David Friswell Aussim FD Build 9 - 11/17/04 01:50 PM Flight Dynamics Workbook V2.84.50 [pitot_static] vertical_speed_time_constant = 2 [WEIGHT_AND_BALANCE] max_gross_weight = 50000 empty_weight = 23246 reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 13 station_load.0 = 200, 15, 0, 1, Pilot station_load.1 = 200, 17, 0, 0, Navigator station_load.2 = 3000, 0, 0, 0, Bombbay Payload station_load.3 = 750, 0, -30, 0, Left Wingtip Payload station_load.4 = 750, 0, 30, 0, Right Wingtip Payload station_load.5 = 0, 0, 0, 0 station_load.6 = 0, 0, 0, 0 station_load.7 = 0, 0, 0, 0 station_load.8 = 0, 0, 0, 0 station_load.9 = 0, 0, 0, 0 station_load.10 = 0, 0, 0, 0 station_load.11 = 0, 0, 0, 0 station_load.12 = 0, 0, 0, 0 empty_weight_pitch_MOI = 99539 empty_weight_roll_MOI = 109552 empty_weight_yaw_MOI = 191186 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 1 rudder_effectiveness = 1 pitch_stability = 1 roll_stability = 1 yaw_stability = 1 elevator_trim_effectiveness = 1 aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1 hi_alpha_on_roll = 1 hi_alpha_on_yaw = 1 p_factor_on_yaw = 1 torque_on_roll = 1 gyro_precession_on_roll = 1 gyro_precession_on_yaw = 1 [GeneralEngineData] engine_type = 1 Engine.0 = 3.21, -16, -1.31 Engine.1 = 3.21, 16, -1.31 fuel_flow_scalar = 1 min_throttle_limit = 0 [TurbineEngineData] fuel_flow_gain = 0.001 inlet_area = 2.2169671888856 rated_N2_rpm = 7800 static_thrust = 7500 afterburner_available = 0 reverser_available = 0 [jet_engine] thrust_scalar = 1 [contact_points] max_number_of_points = 14 point.0 = 1, 10.71, -0.00, -6.29, 2000, 0, 1.442, 65, 0.4, 2.5, 0.8, 4, 4, 0, 0, 0 point.1 = 1, -2.56, -7.47, -6.27, 1574.8, 1, 1.442, 0, 0.5, 2.5, 0.9, 6.9, 6.9, 2, 0, 0 point.2 = 1, -2.53, 7.42, -6.27, 1574.8, 2, 1.442, 0, 0.5, 2.5, 0.9, 7.1, 7.1, 3, 0, 0 point.3 = 2, 24.972, 0.000, -2.571, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.4 = 2, -35.510, 0.000, 9.771, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.5 = 2, 16.890, 0.000, 3.271, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.6 = 2, 0.068, -1.525, -3.858, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.7 = 2, -0.068, 1.525, -3.858, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.8 = 2, -38.031, 0.000, 0.037, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.9 = 2, -3.617, -31.877, 1.467, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.10 = 2, -3.760, 31.848, 1.445, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.11 = 2, -5.023, 10.665, -2.040, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.12 = 2, -5.021, -10.685, -2.027, 1800, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0 point.13 = 5.000, 0.0, 0.0, 0.0, 0, 0, 0.0, 0.0, 0.0, 0.0, 0.00, 3.00, 3.00, 0, 0.0, 0.0 static_pitch = 0.0863 //degrees (pitch when loaded on ground) static_cg_height=6.279 //feet, altitude of CG when at rest on the ground gear_system_type = 1 [Views] eyepoint= 17.0, -0.9, 1.85 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 3 flaps-position.0 = 0 flaps-position.1 = 25, 185 flaps-position.2 =60, 170 damaging-speed = 195 blowout-speed = 212 system_type = 1 lift_scalar = 1 drag_scalar = 1 pitch_scalar = 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 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 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 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 light_panel = 0, 5, 17 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, -18.26, 0, 2.65, fx_navred light.1 = 2, -18.26, 0, 2.65, fx_strobe light.2 = 3, -20.96, 0, -2.95, fx_navred light.3 = 2, -20.96, 0, -2.95, fx_strobe light.4 = 3, -0.4, -30.1, 1.9, fx_navred light.5 = 3, -0.4, 30.25, 1.9, fx_navgre light.6 = 3, -37.52, 0, 2.58, fx_navwhi light.7 = 4, 10, -0.41, 1.95, fx_vclight [keyboard_response] elevator = 400, 500 aileron = 450, 1000 rudder = 400, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 1 exit_rate.0 = 0.4 [folding_wings] wing_fold_system_type = 4 fold_rates = 0.12, 0.11 [TailHook] tailhook_length = 4 tailhook_position = -15, 0, -1 cable_force_adjust = 1 [SMOKESYSTEM] smoke.1= 4.00, -31.70, 9.60, PSS_smokeyvl smoke.2= 4.00, -31.70, -9.60, PSS_smokeyvr //[SMOKESYSTEM] //smoke.1= -1.31, -15.21, -10, fx_smoke_rx //smoke.2= -1.31, 4.00, 10, fx_smkpuff_m //smoke.3= -1.31, -15.21, 10, fx_smoke_rx //smoke.4= -1.31, 4.00, -10, fx_smkpuff_m [EFFECTS] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s,1 [autopilot] autopilot_available = 1 flight_director_available = 0 default_vertical_speed = 1000 autothrottle_available = 0 autothrottle_arming_required = 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8 max_pitch_velocity_hi_alt = 1.5 max_pitch_velocity_lo_alt_breakpoint = 20000 max_pitch_velocity_hi_alt_breakpoint = 28000 max_pitch = 10 max_pitch_acceleration = 1 max_pitch_velocity_lo_alt = 2 max_bank= 25 max_bank_acceleration = 1.8 max_bank_velocity = 3 max_throttle_rate = 0.1 nav_proportional_control = 9 nav_integrator_control = 0.25 nav_derivative_control = 0 nav_integrator_boundary = 2.5 nav_derivative_boundary = 0 gs_proportional_control = 9.52 gs_integrator_control = 0.26 gs_derivative_control = 0 gs_integrator_boundary = 0.7 gs_derivative_boundary = 0 yaw_damper_gain = 0 [fuel] Center1 = 4, 0, 0.5, 550, 0 Center2 = 0, 0, 0.5, 550, 0 Center3 = -2, 0, 0.5, 550, 0 LeftMain = 0, -10, 0, 540.4, 0 RightMain = 0, 10, 0, 540.4, 0 fuel_type = 2 number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area = 960.3 wing_span = 64 wing_root_chord = 15.0046875 wing_dihedral = 3 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.89617931313337 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 3.751171875 wing_pos_apex_vert = 0 htail_area = 135.4 htail_span = 26.2 htail_pos_lon = -39.8 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 75.6 vtail_span = 11.8 vtail_sweep = 0 vtail_pos_lon = -39.1 vtail_pos_vert = 0 elevator_area = 87.5 aileron_area = 69.1 rudder_area = 45.5 elevator_up_limit = 30 elevator_down_limit = 30 aileron_up_limit = 25 aileron_down_limit = 15 rudder_limit = 30 elevator_trim_limit = 20 spoiler_limit = 60 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 [Reference Speeds] flaps_up_stall_speed = 83.4 full_flaps_stall_speed = 66.9 cruise_speed = 282 max_indicated_speed = 565 max_mach = 0.8543 [forcefeedback] gear_bump_nose_magnitude = 6000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 6000 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 6000 gear_bump_right_direction = 500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 3250 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5 ground_bumps_slope1 = 0.48 ground_bumps_magnitude2 = 750 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 = 75000 crash_duration2 = 2500000 stick_shaker_magnitude = 5000 stick_shaker_direction = 0 stick_shaker_period = 111111 [gear_warning_system] gear_warning_available = 1 pct_throttle_limit = 0.1 flap_limit_idle = 45 flap_limit_power = 22.5 [brakes] toe_brakes_scale = 0.640888698995941 parking_brake = 1 [stall_warning] type = 1 [hydraulic_system] electric_pumps = 0 engine_map = 1, 1, 0, 0 normal_pressure = 1250 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0