[fltsim.0] title=PR9 Canberra sim=PR9 Canberra model= panel= sound= texture= kb_checklists= title=BAC PR.9 Canberra (Photo Recon.) sim=Canberra visual_damage=1 atc_heavy=0 atc_id=XH131 atc_airline=Air Force atc_flight_number=XH131 atc_parking_codes=ASY ui_manufacturer=BAC ui_type="Canberra PR.9" ui_variation=Last Photo Recon version description=The prototype PR9 made its maiden flight on 8 July 1955. The aircraft was built under licence by Short Brothers, Belfast and in total, 23 production standard PR9s were built between 1958 and 1962. The first operational sortie was flown by an aircraft of No 58 Squadron in April 1960. The remaining PR9s serve with No 39 Squadron at RAF Marham. This squadron first received the PR9 in 1962, being equipped with 8 by Dec of that year. As the only remaining Canberra squadron in RAF service, No 39 conducts its own conversion training, for which it retains a number of T4 dual-control training aircraft. [General] atc_type=BAC atc_model=CANBERRA performance=+ Empty Weight: 26646 lbs\n+ Power: 7500 lbs thrust\n+ Maneuver speed: 208 mph @ 5.0 g\n+ Max speed: 605 mph @ 15000 ft\n+ Max speed at sea-level: 638 mph\n+ Climb rate: 5400 ft\/min @ 638 mph\n+ Vmca = 120kts IAS\n+ Stall = 80kts IAS Clean,\n+ Stall = 60kts IAS Gear\/Flaps Down\nFlight Dynamics By: David Friswell\nAussim\nFD Build 35 - 05\/01\/05 03:57 PM\nFlight Dynamics Workbook V2.84.65 [pitot_static] vertical_speed_time_constant = 2 [WEIGHT_AND_BALANCE] max_gross_weight = 50000 empty_weight = 23246 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 CG_forward_limit = 0 CG_aft_limit = 1 max_number_of_stations = 5 station_load.0 = 200, 15, 0, 1, Pilot station_load.1 = 200, 17, 0, 0, Navigator station_load.2 = 0, 0, 0, 0, Bombbay Payload station_load.3 = 0, 0, -30, 0, Left Wingtip Payload station_load.4 = 0, 0, 30, 0, Right Wingtip Payload empty_weight_pitch_MOI = 66892 empty_weight_roll_MOI = 99058 empty_weight_yaw_MOI = 152748 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1.5 parasite_drag_scalar = 0.95 induced_drag_scalar = 0.95 elevator_effectiveness = 1 aileron_effectiveness = 1 rudder_effectiveness = 1 pitch_stability = 5.0 roll_stability = 1.5 yaw_stability = 1.5 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 = 2.8069671888856 rated_N2_rpm = 7800 static_thrust = 12250 afterburner_available = 1 reverser_available = 0 [jet_engine] thrust_scalar = 1.0 [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 [contact_points] max_number_of_points = 14 point.0 = 1, 10.71, 0, -6.29, 2000, 0, 1.442, 65, 0.4, 2.5, 0.8, 4, 4, 0, 192.72, 202.4 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, 192.72, 202.4 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, 192.72, 202.4 point.3 = 2, 24.972, 0, -2.571, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.4 = 2, -35.51, 0, 9.771, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.5 = 2, 16.89, 0, 3.271, 1800, 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 point.7 = 2, -0.068, 1.525, -3.858, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.8 = 2, -38.031, 0, 0.037, 1800, 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 point.10 = 2, -3.76, 31.848, 1.445, 1800, 0, 0, 0, 0, 0, 0, 0, 0, 0 point.11 = 2, -5.023, 10.665, -2.04, 1800, 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 point.13 = 5, 0, 0, 0, 0, 0, 0, 0, 0, 0, 0, 3, 3, 0 static_pitch= 0.0863 static_cg_height= 6.279 gear_system_type = 1 [Views] eyepoint= 14.0, -.8, 3.2 //Pilot [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 60, 159 damaging-speed = 175 blowout-speed = 192 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, -20.46, 0, 2.68, fx_navred light.1 = 2, -20.46, 0, 2.68, 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, -0.88, -30.1, 1.9, fx_navred light.5 = 3, -0.88, 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 [Radios] // 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, 1 Adf.1 = 1, 0 Transponder.1 = 1 Marker.1 = 1 //[keyboard_response] //elevator = 350, 500 //aileron = 450, 1000 //rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 1 exit_rate.0 = 0.4 [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 = 2000 autothrottle_available = 1 autothrottle_arming_required = 0 autothrottle_max_rpm = 100 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 = 1 [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 = 700.3 wing_span = 67.5 wing_root_chord = 15.0046875 wing_dihedral = 3 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.943482424063866 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 = 80.8 full_flaps_stall_speed = 65.2 cruise_speed = 380 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 = 0.6 parking_brake = 1 [stall_warning] // 0 = None, 1 = Suction, 2 = Electric. type = 1 [hydraulic_system] electric_pumps = 1 engine_map = 1, 1, 0, 0 normal_pressure = 1250 [attitude_indicators] // 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] // 0=None, 1=Electric Gyro, 2=Vacuum Gyro turn_indicator.0 = 1, 0 [direction_indicators] // 0=None, 1=Vac Gyro, 2=Elec Gyro, 3=EM Slave Compass, 4=Slave to other ind direction_indicator.0 = 1, 0 [airspeed_indicators] airspeed_indicator.0 = 1, 0 [SMOKESYSTEM] smoke.1=-2.00, -11.00, 5.80, fx_flare smoke.2=-2.00, -11.00, -5.80, fx_flare smoke.3= -1.60, -22.00, 5.80, fx_smoke_w smoke.4= -1.60, -22.00, -5.80, fx_smoke_w [keyboard_response] elevator=350.000000,500.000000 aileron=450.000000,1000.000000 rudder=200.000000,1000.000000