[fltsim.0]
title=Boeing B-9
sim=Boeing_B9
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=N36644
ui_manufacturer="Boeing"
ui_type="B-9"
ui_variation="UAAC"
ui_typerole="Twin Engine Bomber"
ui_createdby=
description="The Boeing B-9 was the first all metal bomber produced for the USAAC. It was faster than the current fighters and easily won combat competitions. It did suffer from visibility problems for the pilot and still had open cockpits. Only a few were produced before it was replaced by the more sleek Martin B-10 and the later Douglas B-18.
atc_id_color=0x00000000
atc_heavy=0
atc_id_font=Verdana,-11,1,600,0
visual_damage=0
[General]
atc_type=Boeing
atc_model=B-9
editable=0
performance="Cruise speed\n165 mph 143 kts 265 km/hr\n\nEngines\nTwo Pratt & Whitney R-1860-11 Hornets\n\nMaximum range\n540miles 470nmi 869 km\n\nService ceiling\n20,750 ft 6325 m\n\n\Empty Weight 8941 lb \n\nMaximum gross weight\n14320 lb \n\nLength\n52 ft\n\nWingspan\n76 ft 10in\n\nHeight\n12 ft \n\nMax speed\n188 mph\n\n\Designer Paul Clawson 9/2011"
Category = airplane
[CameraDefinition.0]
Title = "Tail"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = 0, 7.5, -30.0
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 15.8, 1.3, 0.0
InitialPbh = 8, 0, 270
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
[CameraDefinition.2]
Title = "Left Wing"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -15.8, 1.3, 0.0
InitialPbh = 8, 0, 90
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum
[weight_and_balance]
// ACM V2.5
max_gross_weight = 26200
empty_weight = 16145
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI = 69699.03
empty_weight_roll_MOI = 61179.1
empty_weight_yaw_MOI = 131797.97
empty_weight_coupled_MOI = 0
max_number_of_stations = 4
station_load.0 = 170, 6.81, -2, 1.52
station_load.1 = 170, 1.47, 2, 1.52
station_load.2 = 170, -15.44, 0, 2.29
station_load.3 = 170, 12.17, 0, 1.45
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -0.598, -36.804, 2.024, fx_navredm ,
light.1 = 3, -0.598, 36.804, 2.024, fx_navgrem ,
light.2 = 3, -38.24, 0.00, 11.993, fx_navwhi ,
//light.3 = 1, -36.80, 0.00, 6.25, fx_beaconh ,
//light.4 = 4, 1.0, 0.00, 3.15, fx_vclighth,
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 1.0
min_throttle_limit = 0.0
master_ignition_switch = 1
engine.0 = 7.27, -9.02, -1.80,
engine.1 = 7.27, 9.02, -1.80,
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
startup = fx_engstrt_jenny
windshield_rain_effect_available = 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 2
electric_pump = 1
Center1 = 0, 0, -2.7, 200, 0
LeftMain = 0, -6.7, -3, 202, 0
RightMain = 0, 6.7, -3, 202, 0
[contact_points]
static_pitch = 9.5
static_cg_height = 8.3
tailwheel_lock = 1
gear_system_type = 1
max_number_of_points = 7
point.0 = 1, -39.3998, 0, -2.6, 1200, 0, 0.7, 30, 0.2, 2.5, 0.695, 0, 0, 0, 0, 0
point.1 = 1, 0.4582, -9.25, -9.2, 1600, 1, 1.8, 0, 0.39, 1.25, 0.8, 5, 5, 3, 166, 166
point.2 = 1, 0.5483, 9.25, -9.2, 1600, 2, 1.8, 0, 0.39, 1.25, 0.8, 5, 5, 2, 166, 166
point.3 = 2, -3.2446, -35.8092, -0.6585, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -3.2121, 35.6627, -0.7157, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -43.0695, 0, -0.0422, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 13.5127, 0, -1.9086, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
[keyboard_response]
elevator = 200, 1000
aileron = 200, 1000
rudder = 200, 1000
[forcefeedback]
ground_bumps_magnitude1 = 2600
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.6
ground_bumps_magnitude2 = 1200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.085
ground_bumps_slope2 = 0.65
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 3500000
[airplane_geometry]
wing_area = 987.0
wing_span = 76.94
wing_root_chord = 16.79
wing_dihedral = 3
wing_incidence = 2.0
wing_twist = -1.0
oswald_efficiency_factor = 0.60
wing_winglets_flag = 0
wing_sweep = 5
wing_pos_apex_lon = 3.35
wing_pos_apex_vert = 0
htail_area = 95.8
htail_span = 25.75
htail_pos_lon = -31.72
htail_pos_vert = 0.97
htail_incidence = -1.0
htail_sweep = 27
vtail_area = 37.9
vtail_span = 9.26
vtail_sweep = 25
vtail_pos_lon = -33.13
vtail_pos_vert = 2.79
elevator_area = 83.4
aileron_area = 102.8
rudder_area = 46.7
elevator_up_limit = 30.0
elevator_down_limit = 20.0
aileron_up_limit = 27.0
aileron_down_limit = 18.0
rudder_limit = 30.0
elevator_trim_limit = 12.0
spoiler_limit = 0.0
aileron_to_spoileron_gain = 0
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
spoilerons_available = 0
auto_spoiler_available=0
positive_g_limit_flaps_up=0.000000
positive_g_limit_flaps_down=0.000000
negative_g_limit_flaps_up=0.000000
negative_g_limit_flaps_down=0.000000
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 25
max_generator_alternator_amps = 100
engine_generator_map = 1,1
electric_always_available = 0
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
p_factor_on_yaw = 0.5
torque_on_roll = 1.0
gyro_precession_on_yaw = 1.0
gyro_precession_on_pitch = 1.0
//[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 7 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 11 // degrees
flaps-position.2 = 23 // degrees
flaps-position.3 = 34 // degrees
flaps-position.4 = 45.0 // degrees
damaging-speed = 140 // KIAS
blowout-speed = 175 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[piston_engine]
power_scalar=1.0 //Piston power scalar
cylinder_displacement=206.7 //Cubic inches per cylinder
compression_ratio=6.7 //Compression ratio
number_of_cylinders=9 //Number of cylinders
max_rated_rpm=2700 //Max rated RPM
max_rated_hp=600 //Max rated HP
fuel_metering_type=1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3 //Starter torque factor
turbocharged=1 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=47 //Max design manifold pressure, (inHg)
min_design_mp=10 //Min design manifold pressure, (inHg)
critical_altitude=7000 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar=1.0 //Scalar on idle RPM friction
magneto_order_left_right_both = 1 //sets the order of the magneto switch direction
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=12.3 //Propeller Diameter, (feet)
propeller_blades=3 //Number of propeller blades
propeller_moi=40.2 //Propeller moment of inertia
beta_max=30.0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=18.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=1400 //Miminum governed RPM
prop_tc=0.1 //Prop time-constant
gear_reduction_ratio=1.778 //Propeller gear reduction ratio
fixed_pitch_beta=0.0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80.0 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=700.0 //Minimum RPM for prop feathering
beta_feather=89.5 //Feathering pitch angle (degrees)
power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller in feather
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=0.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0.0 //Minimum pitch angle in reverse, (degrees)
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
[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 = 0.7 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
auto_brakes = 0
[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=1.2, 0.0, 4.05
[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=1
Adf.2 = 1
Transponder.1=0
Marker.1=1
[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
[altimeters]
altimeter.0=1
altimeter.1=1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=2,0
[vacuum_system]
max_pressure=5.0 //PSI
vacuum_type=1 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi
engine_map=1,1
[pneumatic_system]
max_pressure=0.000000
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat = 1.0 //Scalar on heat effectiveness, 0 = not available
[Reference Speeds]
flaps_up_stall_speed=67.5 //Knots True (KTAS)
full_flaps_stall_speed=61.5 //Knots True (KTAS)
cruise_speed=95.0 //Knots True (KTAS)
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
[stall_warning]
type=1
stick_shaker=0
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.0 = 0.7
[deice_system]
structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots
[Flaps.0]
type=0
span-outboard=0.500000
extending-time=0.000000
system_type=0
