[fltsim.0]
title=Canberra B.2
sim=Canberra_B.2
visual_damage=1
model=
panel=
sound=
texture=
kb_checklists=
atc_heavy=0
atc_id=2504
atc_airline=Air Force
atc_flight_number=2504
atc_parking_codes=
ui_manufacturer=Rhodesian Air Force
ui_type="Canberra B.2
ui_variation=5 Sqn "late"
description=English Electric Canberra B.2 of No 5 Sqn, Rhodesian Air Force. 15 B.2's and 3 dual control T.4's were delivered to the RhAF. They were later employed with great effect during the anti guerilla war. During the early 70's several aircraft in the fleet were grounded due to cracks in the wing spar. 

[fltsim.1]
title=Canberra B.2#2
sim=Canberra_B.2
visual_damage=1
model=
panel=
sound=
texture=2
kb_checklists=
atc_heavy=0
atc_id=R2085
atc_airline=Air Force
atc_flight_number=R2085
atc_parking_codes=
ui_manufacturer=Rhodesian Air Force
ui_type="Canberra B.2
ui_variation=5 Sqn "UDI"
description=English Electric Canberra B.2 of No 5 Sqn, Rhodesian Air Force. 15 B.2's and 3 dual control T.4's were delivered to the RhAF. They were later employed with great effect during the anti guerilla war. During the early 70's several aircraft in the fleet were grounded due to cracks in the wing spar. 



[General]
atc_type=
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 = 200,  0, -30, 0, Left Wingtip Tank weight
station_load.4 = 200,  0,  30, 0, Right Wingtip Tank weight


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
parasite_drag_scalar = 1.10
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

[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= 17.5, -0.8, 1.95      //Pilotv

[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 = 150
electric_always_available = 0
flap_motor = 1, 4, 0
gear_motor = 1, 4, 0
autopilot = 0, 5, 0
avionics_bus = 0, 30, 0
avionics = 1, 5, 0
pitot_heat = 0, 5, 0
additional_system = 0, 76, 0
marker_beacon = 1, 2, 0
gear_warning = 0, 2, 0
fuel_pump = 0, 35, 0
starter1 = 0, 20, 0
light_nav = 0, 5, 0
light_beacon = 0, 5, 0
light_landing = 0, 8, 0
light_panel = 0, 5, 0


[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
light.8 =  3, 1.404, -31.202, .863,    fx_navred
light.9 =  3, 1.304, 31.202, .863,    fx_navgre


[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, 0
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_f6

[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
External1 = 0, -30, 0,   300.2,  0
External2 = 0,  30, 0,   300.2,  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 = 0.943482424063866
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 = 0
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=  3.60,  -35.70,  10.60, fx_Cansmoke_L
smoke.2=  3.60,  -35.70, -10.60, fx_Cansmoke_R