[fltsim.0]
title = Fairchild 71 Usine-Gnome & Rhone
sim = FC-2W2
model = 5
panel =
sound =
texture = 
panel_alias =
sound_alias =
kb_checklists =
kb_reference =
atc_id = N2K
atc_id_color =
atc_parking_types =
atc_parking_code =
atc_airline=
atc_flight_number=
ui_manufacturer = Fairchild
ui_type = 71
ui_variation =  Usine-Gnome & Rhone
description = N5K (c/n 675) was used for flying sight seeing tours out of Lodi, California and the surrounding area. It is an example of the typical Fairchild 71 as delivered from the factory.
visual_damage = 0

[fltsim.1]
title = Dewoitine Fairchild 71
sim = FC-2W2
model = 5
panel =
sound =
texture =1
panel_alias =
sound_alias =
kb_checklists =
kb_reference =
atc_id = NC13902
atc_id_color =
atc_parking_types =
atc_parking_code =
atc_airline=
atc_flight_number=
ui_manufacturer = Fairchild
ui_type = 71
ui_variation =Usine Dewoitine
description = Dick Kerr selected this Fairchild 71 (c/n 801) as his photo survey plane to take to Saudia Arabia in the 1934 aerial geological reconnaissance for Standard Oil of California (Socal).   A Fairchild 71 with similiar markings is on display at the Edmonton Aviation Heritage Museum; it was used in the filming of the movie “Captains of the Clouds” featuring James Cagney and Dennis Morgan.
visual_damage = 0

[fltsim.2]
title =  Fairchild 71 Usine MESSIER
sim = FC-2W2
model = 5
panel =
sound =
texture = 2
panel_alias =
sound_alias =
kb_checklists =
kb_reference =
atc_id = NC 9798
atc_id_color =
atc_parking_types =
atc_parking_code =
atc_airline=
atc_flight_number=
ui_manufacturer = Fairchild
ui_type = 71
ui_variation = Usine MESSIER
description = NC 9798 (C/n 619), was delivered to Pan Am in March 1929. Pan Am assigned this Fairchild 71 to PANAGRA, with the fleet number P6. The ultimate fate of this Fairchild 71 is not known.
visual_damage = 0

[General]
atc_type =
atc_model =
performance =Maximum Speed\n133 mph\n\nCruise Speed\n\108 mph\n\nStall Speed\n\n55 mph\n\nClimb\n\n875 fpm at 71 mph\n\nEmpty Weight\n\n2818 lbs\n\Engine\n\n420 Hp Pratt & Whitney Wasp B 
editable = 0  
prop_anim_ratio = 1
Category=airplane

[pitot_static]
vertical_speed_time_constant = 2
pitot_heat=1.000000

[WEIGHT_AND_BALANCE]
max_gross_weight =5500
empty_weight =2818

reference_datum_position = 0, 0, 0
empty_weight_CG_position  = 0.000, 0.000, 0.000
CG_forward_limit = 0
CG_aft_limit = 1


empty_weight_pitch_MOI =12600
empty_weight_roll_MOI =10000
empty_weight_yaw_MOI =13500
empty_weight_coupled_MOI =0.0

max_number_of_stations = 7
station_load.0 = 170,  1,    0,   0 // Pilot
station_load.1 = 150, -2,   -1.5, 0 // Lt fwd Passenger
station_load.2 = 150, -2,    1.5, 0 // Rt fwd Passenger
station_load.3 = 150, -4.5, -1.5, 0 // Lt middle passenger
station_load.4 = 150, -4.5,  1.5, 0 // Rt middle passenger
station_load.5 = 150, -7,   -1.5, 0 // Lt aft passenger
station_load.6 = 150, -7,    1.5, 0 // Rt aft passenger

[flight_tuning]
cruise_lift_scalar =1.10
parasite_drag_scalar =1.3
induced_drag_scalar =1.0
elevator_effectiveness =1.0
aileron_effectiveness =1.0
rudder_effectiveness =1.0
pitch_stability =1.5
roll_stability =1.5
yaw_stability =1.0
elevator_trim_effectiveness =1.0
aileron_trim_effectiveness =1.0
rudder_trim_effectiveness =1.0
hi_alpha_on_roll =1.0
hi_alpha_on_yaw =1.0
p_factor_on_yaw =1.60
torque_on_roll =1.50
gyro_precession_on_roll =1.0
gyro_precession_on_yaw =1.0

[GeneralEngineData]
engine_type =0
Engine.0 =7.600, 0.000, 0.000
fuel_flow_scalar =1.0
min_throttle_limit = 0

[piston_engine]
power_scalar =1.0
cylinder_displacement =149.11111
compression_ratio =5.25
number_of_cylinders =9
max_rated_rpm =2000
max_rated_hp =420
fuel_metering_type =1
cooling_type =0
normalized_starter_torque =0.6
turbocharged =0
max_design_mp =29.92
min_design_mp =0.0
critical_altitude =0.0
emergency_boost_type =0
emergency_boost_mp_offset =0.0
emergency_boost_gain_offset =0.0
fuel_air_auto_mixture =0
auto_ignition =0
emergency_boost_duration =0.0
max_rpm_mechanical_efficiency_scalar =1.0
idle_rpm_mechanical_efficiency_scalar =1.0
max_rpm_friction_scalar =1.0
idle_rpm_friction_scalar =1.0

[propeller]
thrust_scalar =1.0
propeller_type =1
propeller_diameter =8.67
propeller_blades =3
propeller_moi =8.0
beta_max =20.0
beta_min =18.0
min_gov_rpm =1200
prop_tc =0.010
gear_reduction_ratio =1.0
fixed_pitch_beta =19
low_speed_theory_limit =77.72098
prop_sync_available =0
prop_deice_available =1
prop_feathering_available =0
prop_auto_feathering_available =0
min_rpm_for_feather =700
beta_feather =88.50
power_absorbed_cf =0.90
defeathering_accumulators_available =0
prop_reverse_available =0
minimum_on_ground_beta =1.0
minimum_reverse_beta =-14.0
rotation = 1


[folding_wings]
wing_fold_system_type =  1
fold_rates =  0.12, 0.11

[TailHook]
tailhook_length = 0
tailhook_position = 0, 0, 0
cable_force_adjust = 1

[contact_points]
max_number_of_points =11

static_pitch= 15.342
static_cg_height= 5.741
gear_system_type =1
point.0= 1, -22.784,   0.000, -0.015, 1500, 0, 1.462, 180.000, 0.500, 2.500, 0.700, 0.000, 0.000, 7
point.1= 1,   1.462,  -3.829, -6.986, 1300, 1, 1.462,   0.000, 0.633, 2.501, 0.800, 0.000, 0.000, 2
point.2= 1,   1.462,   3.829, -6.986, 1300, 2, 1.462,   0.000, 0.633, 2.501, 0.800, 0.000, 0.000, 3
point.3= 2,   6.890,   0.000, -1.281, 3000, 0, 0.000,   0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.4= 2, -25.168,   0.000,  0.549, 3000, 0, 0.000,   0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.5= 2, -25.491,   0.000,  1.574, 700,  0, 0.000,   0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.6= 2,   0.000, -25.246,  3.843, 3000, 0, 0.000,   0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.7= 2,   0.000,  25.246,  3.843, 3000, 0, 0.000,   0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.8= 2,   3.700,   0.000, -4.000, 3000, 0, 0.000,   0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.9= 2,  -2.400,   0.000, -3.900, 3000, 0, 0.000,   0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.10= 2,  7.402,   0.000, -5.050, 50,   0, 0.000,   0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
tailwheel_lock=0


[Views]
eyepoint= 1.047, 0, 2.000


[electrical]
max_battery_voltage = 12  //24
generator_alternator_voltage = 14  //28
max_generator_alternator_amps = 160
electric_always_available = 1

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
fuel_pump = 0, 5, 17
starter1 = 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
standby_vacuum = 0, 15, 17
fuel_transfer_pump = 0, 5, 17

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 =  3,  -0.139, -24.87,  3.713,  fx_navred
light.1 =  3,  -0.139,  24.87,  3.713,  fx_navgre
light.2 =  3, -23.10,    0,     8.201,  fx_navwhi
light.3 =  4,   1.147,   0,     1.365,  fx_vclight
light.4 =  2,   4.900,   1.85, -4.45,   fx_RobJcruise
light.5 =  2,   0.15,   -1.90, -3.25,   fx_RobJcruise
light.6 =  4,  -6.411,   0.2    1.601,  fx_vclight


[Radios] // availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 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 = 0.4
exit_rate.1 = 0.4

[EFFECTS]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
startup = fx_FC2W-Byrd_start
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 =1000.00000
autothrottle_available =0
autothrottle_arming_required =0
autothrottle_takeoff_ga =1.00000
autothrottle_max_rpm =90.00000
pitch_takeoff_ga =8.00000
default_pitch_mode =0
default_bank_mode =0
max_pitch =10.00000
max_pitch_acceleration =1.00000
max_pitch_velocity_lo_alt =2.00000
max_pitch_velocity_hi_alt =1.50000
max_pitch_velocity_lo_alt_breakpoint =20000.00000
max_pitch_velocity_hi_alt_breakpoint =28000.00000
max_bank=25.00000
max_bank_acceleration =1.80000
max_bank_velocity =3.00000
max_throttle_rate =0.10000
nav_proportional_control =9.00000
nav_integrator_control =0.25000
nav_derivative_control =0.00000
nav_integrator_boundary =2.50000
nav_derivative_boundary =0.00000
gs_proportional_control =9.52000
gs_integrator_control =0.26000
gs_derivative_control =0.00000
gs_integrator_boundary =0.70000
gs_derivative_boundary =0.00000
yaw_damper_gain =0.00000

[fuel]
Center1 =   0.000,  0.000, -0.100, 40.000, 0.000
LeftMain =  0.000, -2.250,  3.250, 60.000, 0.000
RightMain = 0.000,  2.250,  3.250, 60.000, 0.000
fuel_type =1
number_of_tank_selectors =1
electric_pump=0

[airplane_geometry]
wing_area =310
wing_span =50
wing_root_chord =7.0
wing_dihedral =1.5
wing_incidence =0.0
wing_twist =0.0
oswald_efficiency_factor =0.80
wing_winglets_flag =0
wing_sweep  =0.0
wing_pos_apex_lon =1.45012
wing_pos_apex_vert =0.0
htail_area =28.8
htail_span =14.0
htail_pos_lon =-25.75
htail_pos_vert =0.0
htail_incidence =0.0
htail_sweep =0.0
vtail_area =12.9
vtail_span =7.0
vtail_sweep =0.0
vtail_pos_lon  =-25.75
vtail_pos_vert =0.0
elevator_area =25.7
aileron_area =15.3
rudder_area =13.0
elevator_up_limit =30.0
elevator_down_limit =24.0
aileron_up_limit =25.0
aileron_down_limit =19.0
rudder_limit =30.0
elevator_trim_limit =18.0
spoiler_limit =0.0
spoilerons_available =0
aileron_to_spoileron_gain =0.0
min_ailerons_for_spoilerons =0.0
min_flaps_for_spoilerons =0.0
spoiler_handle_available=0
auto_spoiler_available=0
positive_g_limit_flaps_up=7.3
negative_g_limit_flaps_up=-5.84
positive_g_limit_flaps_down=5.11
negative_g_limit_flaps_down=-4.38
load_safety_factor=1.0

[Reference Speeds]
flaps_up_stall_speed    =47.79369
full_flaps_stall_speed  =47.79369
cruise_speed            =94.02322
max_indicated_speed =140.00000
max_mach =0.26000

[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 =0 //gear down and welded


[brakes]
toe_brakes_scale =0.40
parking_brake = 1
differential_braking_scale = 1

[stall_warning] //  0 = None, 1 = Suction, 2 = Electric.
type = 1
stick_shaker=1

[hydraulic_system]
electric_pumps = 0
engine_map = 1, 0, 0, 0
normal_pressure =1000.00000

[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.0 = 1.45, -25, 0, fx_smoke_w
smoke.1 = 1.45, 25, 0, fx_smoke_w



[Flaps.0]
type=0
span-outboard=0.500000
extending-time=0.000000
system_type=0
[vacuum_system]
max_pressure=5.150000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=0.150000
[deice_system]
structural_deice_type=0
