[fltsim.0]
title=Frontier Airlines Old DC-3 v2
sim=Douglas DC-3 DDA PH-DDZ
model=
panel=
sound=
texture=
checklists=ddz_check
kb_reference=DCA_ref
atc_id=N78490
atc_airline=Frontier Flight
atc_flight_number=2112
ui_manufacturer=Frontier Airlines
ui_type=DC-3
ui_variation=Old version Frontier Airlines v2
description=Douglas DC-3C Frontier Airlines version 2. Designer: Jan Visser, Flight Dynamics: Erik Ellis, Jan Visser, Roy Chaffin, Ian Ropper, & Bill Rambow

[fltsim.1]
title=Frontier Airlines New DC-3 v2
sim=Douglas DC-3 DDA PH-DDZ
model=
panel=
sound=
texture=1
checklists=ddz_check
kb_reference=DCA_ref
atc_id=N78490
atc_airline=Frontier Flight
atc_flight_number=2112
ui_manufacturer=Frontier Airlines
ui_type=DC-3
ui_variation=New version Frontier Airlines v2
description=Douglas DC-3C Frontier Airlines version 2. Designer: Jan Visser, Flight Dynamics: Erik Ellis, Jan Visser, Roy Chaffin, Ian Ropper, & Bill Rambow

[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=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[General]
atc_type=Douglas
atc_model=DC3
performance=Length: 64 ft, 5 in. Wing Span: 95 feet\nWeight: Empty\/Max: 19,300\/28,000 lbs\nPower: 2 x 1200 hp P&W R1830 Twin Wasp\nCruise Speed: 145 knots, Max : 185 knots\n\n
atc_type=DOUGLAS
atc_model=DC3

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight= 19068.000
empty_weight_roll_MOI= 70000.000
empty_weight_pitch_MOI= 203000.000
empty_weight_yaw_MOI= 290603.000
empty_weight_coupled_MOI= 0.000
max_gross_weight= 23892.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

[fuel]
LeftMain= 0.000, -16.667, 0.000, 202.000, 0.000
LeftAux= 0.000, 0.000, 0.000, 200.000, 0.000
RightMain= 0.000, 16.667, 0.000, 202.000, 0.000
RightAux= 0.000, 0.000, 0.000, 200.000, 0.000
fuel_type=1.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 1109.000
wing_span= 95.000
wing_root_chord= 11.667
wing_dihedral= 5.999
wing_incidence= 0.000
wing_twist= -1.000
oswald_efficiency_factor= 2.498
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 350.000
htail_span= 25.833
htail_pos_lon= -41.667
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 220.000
vtail_span= 16.912
vtail_sweep= 0.000
vtail_pos_lon= -34.167
vtail_pos_vert= 0.000
elevator_area= 150.500
aileron_area= 110.900
rudder_area= 52.500
elevator_up_limit= 27.502
elevator_down_limit= 20.626
aileron_up_limit= 19.481
aileron_down_limit= 14.897
rudder_limit= 23.491
elevator_trim_limit= 19.481
spoiler_limit= 59.989
spoilerons_available= 0
aileron_to_spoileron_gain= 0.000
min_ailerons_for_spoilerons= 0.000
min_flaps_for_spoilerons= 0.000

[contact_points]
point.0= 1.000, -38.417, 0.000, -0.833, 1574.803, 0.000, 0.666, 57.660, 0.195, 2.500, 0.916, 33.000, 33.000, 0.000, 0.000, 0.000
point.1= 1.000, 3.417, -9.917, -8.500, 1574.803, 1.000, 0.666, 0.000, 0.366, 2.500, 0.773, 5.000, 5.000, 2.000, 0.000, 0.000
point.2= 1.000, 3.417, 9.917, -8.500, 1574.803, 2.000, 0.666, 0.000, 0.366, 2.500, 0.773, 5.000, 5.000, 3.000, 0.000, 0.000
point.3= 2.000, -8.500, -47.500, 0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -8.500, 47.500, 0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -27.333, 0.000, 0.750, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 18.833, 0.000, -1.667, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 12.997
static_cg_height= 8.010


[GeneralEngineData]
engine_type= 0
Engine.0= 8.333, -9.167, -1.250
Engine.1= 8.333, 9.167, -1.250
fuel_flow_scalar= 1.000

[piston_engine]
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000
cylinder_displacement= 140.750
compression_ratio= 8.000
number_of_cylinders= 9
max_rated_rpm= 2708.000
max_rated_hp= 1350.000
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 1
max_design_mp= 8.000
min_design_mp= 0.000
critical_altitude= 30000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0

[propeller]
propeller_type= 0
propeller_diameter= 8.917
propeller_blades= 3
propeller_moi= 18.610
beta_max= 43.500
beta_min= 15.000
min_gov_rpm= 1400.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 20.000
low_speed_theory_limit= 80.000
prop_sync_available= 0
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather= 0.000
power_absorbed_cf= 0.000
defeathering_accumulators_available= 1
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000

[Reference Speeds]
flaps_up_stall_speed= 65.000
full_flaps_stall_speed= 52.000
cruise_speed= 166.769

[keyboard_response]
elevator=0.000000,0.000000
aileron=0.000000,0.000000
rudder=0.000000,0.000000

[Views]
eyepoint=13.994833,-2.076156,4.408629

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=700.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=1,0
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 5.000
system_type= 0
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 9.998, 0.000
flaps-position.2= 19.996, 0.000
flaps-position.3= 29.994, 0.000
flaps-position.4= 39.992, 0.000