[fltsim.0]
title=221A Monomail
sim=221A
model =
panel =
sound =
texture =
panel_alias =
sound_alias =
kb_checklists =
kb_reference =
atc_id =
atc_id_color =
atc_parking_types =
atc_parking_code =
atc_airline=
atc_flight_number=
prop_anim_ratio = 1.76
ui_manufacturer = Boeing Aircraft
ui_type = 221A
ui_variation = U.S. Civil Register
description = The 221A Monomail was a major advance in aircraft design, being one of the first all metal, stressed skin monoplanes built. Despite it's advances the 221A'a layout harked back to the biplane era, with the cabin forward, and open cockpit aft. Lack of a constant speed propeller prevented the Monomail's true success, as better twins were introduced by the time C-S props appeared. Only one 221A saw brief service between Chicago-Cheyenne.
visual_damage = 1
[General]
atc_type =
atc_model =
performance = + Empty Weight: 6318 lbs + Max Power: 575 Hp + Maneuver speed: 111 mph @ 4.0 g + Max speed: 158 mph @ 10000 ft + Max speed at sea-level: 158 mph + Climb rate: 1600 ft/min @ 80 mph Flight Dynamics By: Tim Piglet Conrad Piglet's Peculiar Planes FD Build 14 - 6/5/05 09:13 PM Flight Dynamics Workbook V3.00.03
editable = 1
[pitot_static]
vertical_speed_time_constant = 2
[WEIGHT_AND_BALANCE]
max_gross_weight = 8200
empty_weight = 4758
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -0.5, 0, 0
CG_forward_limit = 0
CG_aft_limit = 1
max_number_of_stations = 6
station_load.0 = 200, -9.5, 0, 1.36, Pilot
station_load.1 = 340, 4, 0, 0, Passengers/Mail
station_load.2 = 340, 2, 0, 0, Passengers/Mail
station_load.3 = 340, -2, 0, 0, Passengers/Mail
station_load.4 = 340, -4, 0, 0, Passengers/Mail
empty_weight_pitch_MOI = 17383
empty_weight_roll_MOI = 8385
empty_weight_yaw_MOI = 24201
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
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 = 0
Engine.0 = 9.97, 0, 0
fuel_flow_scalar = 1
min_throttle_limit = 0
[piston_engine]
power_scalar = 1
cylinder_displacement = 148.888888888889
compression_ratio = 6
number_of_cylinders = 9
max_rated_rpm = 1950
max_rated_hp = 575
fuel_metering_type = 1
cooling_type = 0
normalized_starter_torque = 0.07
turbocharged = 0
max_design_mp = 29
min_design_mp = 9
critical_altitude = 10000
emergency_boost_type = 0
emergency_boost_mp_offset = 0
emergency_boost_gain_offset = 0
fuel_air_auto_mixture = 0
auto_ignition = 0
emergency_boost_duration = 0
max_rpm_mechanical_efficiency_scalar = 1
idle_rpm_mechanical_efficiency_scalar = 1
max_rpm_friction_scalar = 1
idle_rpm_friction_scalar = 1
[propeller]
thrust_scalar = 1
propeller_type = 0
propeller_diameter = 10.6
propeller_blades = 2
propeller_moi = 24.9
beta_max = 65
beta_min = 15
min_gov_rpm = 292.5
prop_tc = 0.01
gear_reduction_ratio = 1
fixed_pitch_beta = 30
low_speed_theory_limit = 80
prop_sync_available = 0
prop_deice_available = 1
prop_feathering_available = 0
prop_auto_feathering_available = 0
min_rpm_for_feather = 700
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
[contact_points]
max_number_of_points = 7
point.0 = 1, -27.1002, 0, -2.9254, 1800, 0, 0.6, 45, 0.25, 2.5, 0.7, 0, 0, 0, 200, 250
point.1 = 1, 1.31, -5.23, -8.04, 1600, 1, 1.5, 0, 0.35, 3, 0.8, 5, 7, 2, 200, 250
point.2 = 1, 1.31, 5.23, -8.04, 1600, 2, 1.5, 0, 0.35, 3, 0.8, 6, 8, 3, 200, 250
point.3 = 2, -3.2457, -28.6256, -1.2986, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5
point.4 = 2, -3.3034, 29.0925, -1.3796, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6
point.5 = 2, -30.6839, 0, -0.9549, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9
point.6 = 2, 3.7858, 0, -3.6092, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4
static_pitch= 10.14
static_cg_height= 7.67
gear_system_type = 1
tailwheel_lock = 1
[Views]
eyepoint= -9.92, 0, 3.00
[flaps.0] //Trailing Edge Flaps
type = 1
span-outboard = 0.5
extending-time = 0
flaps-position.0 = 0
damaging-speed = 500
blowout-speed = 550
system_type = 4
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, -2.52, -29.33, -0.46, fx_navred
light.1 = 4, 3.54, 0, 1.02, fx_vclight_offwhi
light.2 = 4, -3.45, 0, 0.84, fx_vclight_offwhi
light.3 = 3, -2.44, 29.35, -0.53, fx_navgre
light.4 = 4, -9.34, 0, 1.58, 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, 0
Adf.1 = 1
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 = 2
exit_rate.0 = 0.8
exit_rate.1 = 0.4
[EFFECTS]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
[autopilot]
autopilot_available = 1
use_no_default_bank = 1
use_no_default_pitch = 1
flight_director_available = 0
default_vertical_speed = 1000
autothrottle_available = 0
autothrottle_arming_required = 0
autothrottle_takeoff_ga = 1
autothrottle_max_rpm = 90
pitch_takeoff_ga = 8
default_pitch_mode =0
default_bank_mode =0
max_pitch = 10
max_pitch_acceleration = 1
max_pitch_velocity_lo_alt = 2
max_pitch_velocity_hi_alt = 1.5
max_pitch_velocity_lo_alt_breakpoint = 20000
max_pitch_velocity_hi_alt_breakpoint = 28000
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 = 0
[fuel]
LeftMain = 0, -5.1, 0, 150, 0
RightMain = 0, 5.1, 0, 150, 0
fuel_type = 1
number_of_tank_selectors = 1
electric_pump=0
[airplane_geometry]
wing_area = 535
wing_span = 59.125
wing_root_chord = 9.04862579281184
wing_dihedral = 5
wing_incidence = 0
wing_twist = 0
oswald_efficiency_factor = 0.890923849632474
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 1.76215644820296
wing_pos_apex_vert = 0
htail_area = 68.51
htail_span = 13.1
htail_pos_lon = -27.43
htail_pos_vert = 0
htail_incidence = 0
htail_sweep = 0
vtail_area = 10.55
vtail_span = 6.2
vtail_sweep = 0
vtail_pos_lon = -27.43
vtail_pos_vert = 0
elevator_area = 35.56
aileron_area = 47
rudder_area = 19.83
elevator_up_limit = 30
elevator_down_limit = 20
aileron_up_limit = 15
aileron_down_limit = 15
rudder_limit = 30
elevator_trim_limit = 18
spoiler_limit = 0
spoilerons_available = 0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
[Reference Speeds]
flaps_up_stall_speed = 47.8
full_flaps_stall_speed = 47.8
cruise_speed = 117
max_indicated_speed = 152
max_mach = 0.2628
[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 = 33.75
flap_limit_power = 16.875
[brakes]
toe_brakes_scale = 0.8
parking_brake = 1
differential_braking_scale = 1.0
[stall_warning] // 0 = None, 1 = Suction, 2 = Electric.
type = 1
[hydraulic_system]
electric_pumps = 0
engine_map = 1, 0, 0, 0
normal_pressure = 1000
[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
