[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