[fltsim.0]
title = Flack-Bait B-26C Maruder
sim = fb26c
model = fb26c
panel =
sound =
texture =
panel_alias =
sound_alias =
kb_checklists = CheckList_3US_B-26G Maruder.txt
kb_reference =
atc_id = 0
atc_id_color = 0xffffffff
atc_airline =
atc_flight_number = 1
ui_manufacturer = Martin
ui_type = B-26C Maruder
ui_variation = USAAF
description = B-26C Maruder

[General]
atc_type =
atc_model =
editable = 1
performance = Weight: 26367 lbs|Power: 1920 hp|4.5g Corner speed: 226 mph|Max speed @ SL: 270 mph|Max speed: 282 mph @ 15000 ft|Climb rate: 1200 ft/min @ 170 mph|Flight Model By: Jerry Beckwith|12/9/02 09:17 PM|Flight Model Workbook V2.82.28

[pitot_static]
vertical_speed_time_constant = 2

[WEIGHT_AND_BALANCE]
max_gross_weight = 38200
empty_weight = 24767

reference_datum_position = 0, 0, 0
empty_weight_CG_position  = -0.028, 0, 0
CG_forward_limit = 0
CG_aft_limit = 1

max_number_of_stations = 8
station_load.0 = 200, 24, 0, 0, // Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 200, 13.3, 1.3, 0, //
station_load.2 = 200, 13.3, -1.3, 0, //
station_load.3 = 200, 10, 1.3, 0, //
station_load.4 = 200, 10, -1.3, 0, //
station_load.5 = 200, -16, 0, 0, //
station_load.6 = 200, -18, 0, 0, //
station_load.7 = 200, -33, 0, 0, //

empty_weight_pitch_MOI = 71127
empty_weight_roll_MOI = 75230
empty_weight_yaw_MOI = 143719
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

[GeneralEngineData]
engine_type = 0
Engine.0 = 10, -11, 0
Engine.1 = 10, 11, 0
fuel_flow_scalar = 1

[piston_engine]
power_scalar = 1
cylinder_displacement = 155.555555555556
compression_ratio = 6.7
number_of_cylinders = 18
max_rated_rpm = 2700
max_rated_hp = 1920
fuel_metering_type = 0
cooling_type = 0
normalized_starter_torque = 0.033
turbocharged = 1
max_design_mp = 52
min_design_mp = 9
critical_altitude = 15000
emergency_boost_type = 0
emergency_boost_mp_offset = 0
emergency_boost_gain_offset = 0
fuel_air_auto_mixture = 0
auto_ignition = 0
max_rpm_mechanical_efficiency_scalar = 1
idle_rpm_mechanical_efficiency_scalar = 1
max_rpm_friction_scalar = 1
idle_rpm_friction_scalar = 1
emergency_boost_duration = 300
fuel_flow_scalar=1.000000

[propeller]
thrust_scalar = 1
propeller_type = 0
propeller_diameter = 13.5
propeller_blades = 4
propeller_moi = 57.1
beta_max = 65
beta_min = 15
min_gov_rpm = 405
prop_tc = 0.01
gear_reduction_ratio = 2
fixed_pitch_beta = 20
low_speed_theory_limit = 80
prop_sync_available = 1
prop_deice_available = 1
prop_feathering_available = 1
prop_auto_feathering_available = 1
min_rpm_for_feather = 70
beta_feather = 88.5
power_absorbed_cf = 0.9
defeathering_accumulators_available = 0
prop_reverse_available = 0
minimum_on_ground_beta = 1
minimum_reverse_beta = -14
rotation = 1, 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 = 13
point.0 = 1, 16.5, 0, -7.85, 1377.953, 0, 1.375, 60, 0.316, 2.5, 0.7, 3.5, 3.5, 0, 127, 140
point.1 = 1, -1.7, -10.96, -8, 1968.504, 1, 2, 0, 0.528, 2.5, 0.73, 3.5, 3.5, 2, 127, 140
point.2 = 1, -1.7, 10.96, -8, 1968.504, 2, 2, 0, 0.528, 2.5, 0.73, 3.5, 3.5, 3, 127, 140
point.3 = 2, 22, 0, 0, 2100, 0, 0, 0, 0, 0, 0, 0, 0, 4
point.4 = 2, 5.3, 0, -4, 3000, 0, 0, 0, 0, 0, 0, 0, 0, 4
point.5 = 2, -3.07, -35.3, 4, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 5
point.6 = 2, -3.07, 35.3, 4, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 6
point.7 = 2, -28.6, 0, 14.3, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 9
point.8 = 2, 10, 10.96, -4.5, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 4
point.9 = 2, 10, -10.96, -4.5, 787.402, 0, 0, 0, 0, 0, 0, 0, 0, 4
point.10 = 2, -33, 0, -0.5, 1900, 0, 0, 0, 0, 0, 0, 0, 0, 4
point.11 = 2, -3.07, -22, 4, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 5
point.12 = 2, -3.07, 22, 4, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 6

static_pitch= 0.86
static_cg_height= 7.36


[Views]
eyepoint= -2.27, 0, 2.9

[flaps.0]       //Trailing Edge Flaps
type = 1
span-outboard = 0.5
extending-time = 5
flaps-position.0 = 0
flaps-position.1 = 7, 193
flaps-position.2 = 15, 184
flaps-position.3 = 22, 176
flaps-position.4 = 30, 168
damaging-speed = 193
blowout-speed = 209
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 = 1

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]
panel = 0, 0.35, -0.8, fx_vclight

[LSO]
LSOAdjustSpeed = 1.2

[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, 1

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8

[fuel]
LeftMain = 0, -3.33, 0, 360,  0
RightMain = 0, 3.33, 0, 360,  0
LeftAux = 0, -5, 0, 121,  0
RightAux = 0, 5, 0, 121,  0
fuel_type =  1
number_of_tank_selectors = 1

[airplane_geometry]
wing_area = 658
wing_span = 71
wing_root_chord = 12.6
wing_dihedral = 2
wing_incidence = 5
wing_twist = -1
oswald_efficiency_factor = 0.885367302431611
wing_winglets_flag = 0
wing_sweep  = 3
wing_pos_apex_lon = 3.15
wing_pos_apex_vert = 1.9
htail_area = 46.2
htail_span = 28.4
htail_pos_lon = -29.125
htail_pos_vert = 1
htail_incidence = 4
htail_sweep = 10
vtail_area = 22
vtail_span = 11
vtail_sweep = 22
vtail_pos_lon  = -32
vtail_pos_vert = 1.7
elevator_area = 30.8
aileron_area = 47.5076
rudder_area = 16.7
elevator_up_limit = 30
elevator_down_limit = 20
aileron_up_limit = 20
aileron_down_limit = 15
rudder_limit = 21
elevator_trim_limit = 18
spoiler_limit = 1
spoilerons_available = 0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0

[Reference Speeds]
flaps_up_stall_speed    = 91.2
full_flaps_stall_speed  = 78.2
cruise_speed            = 186

[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