[fltsim.0]
title=Angel 44
sim=angel44
model=
panel=
sound=
texture=1
panel_alias = 
sound_alias = 
kb_checklists=
kb_reference=
atc_id=NTEP
ui_manufacturer=Angel
ui_type=44
ui_variation=Private
description=Enter your description here.
atc_heavy=0
atc_airline=
atc_flight_number=
atc_id_color=0x00000000
atc_parking_types=RAMP
atc_id_font=Verdana,-11,1,600,0
visual_damage=0

[General]
atc_type=Angel 
atc_model=44 
editable=1 
performance=Range 800 to 1,000 miles.
Category=airplane

[weight_and_balance]

// ACM V2.5
max_gross_weight = 5800.00
empty_weight = 3880.00
reference_datum_position = 0.00, 0.00, 0.00
empty_weight_CG_position = 0.00, 0.00, 0.00
empty_weight_pitch_MOI = 4000.00
empty_weight_roll_MOI = 4000.00
empty_weight_yaw_MOI = 5000.00
empty_weight_coupled_MOI = 0.00
CG_forward_limit = 0.00
CG_aft_limit = 1.00
max_number_of_stations = 0


[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -1.1, -20.2, 1.3, fx_navred
light.1 = 3, -1.1, 20.2, 1.3, fx_navgre
light.2 = 3, -15.4, 0, 1.8, fx_navwhi
light.3 = 2, -1.40, -20.2, 1.3, fx_strobe
light.4 = 2, -1.40, 20.2, 1.3, fx_strobe
light.5 = 4,  8.59,  0.00, 2.96, fx_vclight

[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 0.90
min_throttle_limit = -0.25
engine.0 = -4.60,-5.60, 1.00 
engine.1 = -4.60, 5.60, 1.00 

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_154, 1
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

LeftMain = 3.00, -4.00, 0.00, 111.00, 0.00
RightMain = 3.00, 4.00, 0.00, 111.00, 0.00

[contact_points]
static_pitch = 0.00
static_cg_height = 3.20
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 7

point.0 = 1, 15.50, 0.00, -3.20, 2000.00, 0.00, 0.70, 40.00, 0.20, 2.50, 0.90, 3.00, 3.00, 0.00, 0.00, 0.00
point.1 = 1, -1.00, -6.20, -3.30, 2000.00, 1.00, 0.90, 0.00, 0.30, 2.50, 0.90, 4.00, 4.00, 2.00, 0.00, 0.00
point.2 = 1, -1.00, 6.20, -3.30, 2000.00, 2.00, 0.90, 0.00, 0.30, 2.50, 0.90, 4.00, 4.00, 3.00, 0.00, 0.00

point.3 = 2, -0.30, -20.00, 1.30, 800.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 5.00, 0.00, 0.00
point.4 = 2, -0.30, 20.00, 1.30, 800.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 6.00, 0.00, 0.00
point.5 = 2, -13.30, 0.00, 0.90, 800.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 9.00, 0.00, 0.00
point.6 = 2, 16.40, 0.00, -0.20, 800.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 4.00, 0.00, 0.00

[keyboard_response]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250

[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 5000
stick_shaker_direction = 0
stick_shaker_period = 111111

[airplane_geometry]
//ACM_AREAW1// 0,0,0,2.4384,0.7789,0.7789,0.0408,2.3573,1.5578,1.5578
//ACM_AREAW2// 0.0816,2.2762,2.3366,2.3366,0.1224,2.1951,3.1157,3.1157,0.1632,2.1140
//ACM_AREAW3// 3.8945,3.8945,0.2040,2.0329,4.6735,4.6735,0.2449,1.9517,5.4524,5.4524
//ACM_AREAW4// 0.2856,1.8707,6.2314,6.2314,0.3264,1.7896,7.0103,7.0103,0.3673,1.7085
//ACM_AREAH1// 0,0,0,1.6255,0.2709,0.2709,0.0237,1.5680,0.5418,0.5418
//ACM_AREAH2// 0.0474,1.5104,0.8127,0.8127,0.0711,1.4528,1.0837,1.0837,0.0948,1.3952
//ACM_AREAH3// 1.3546,1.3546,0.1185,1.3377,1.6255,1.6255,0.1422,1.2801,1.8965,1.8965
//ACM_AREAH4// 0.1659,1.2225,2.1674,2.1674,0.1896,1.1649,2.4384,2.4384,0.2133,1.1074
//ACM_AREAV1// 0.0735,0.0735,-1.7281,2.3407,0.2478,0.2478,-0.7641,2.4122,0.3853,0.3853
//ACM_AREAV2// 0.1815,2.4470,0.5780,0.5780,0.5204,2.4818,0.7523,0.7523,0.6939,2.4981
//ACM_AREAV3// 0.9449,0.9449,0.8674,2.5880,1.1560,1.1560,1.0409,2.6412,1.3487,1.3487
//ACM_AREAV4// 1.2143,2.6760,1.5597,1.5597,1.3878,2.7291,1.7340,1.7340,1.5613,2.7822
//ACM_CAREAW1// 3.5051,3.5051,1.4027,1.8904,3.8945,3.8945,1.4233,1.8866,4.2841,4.2841
//ACM_CAREAW2// 1.4436,1.8825,4.6735,4.6735,1.4641,1.8786,5.0630,5.0630,1.4845,1.8746
//ACM_CAREAW3// 5.4524,5.4524,1.5048,1.8707,5.8420,5.8420,1.5253,1.8667,6.2314,6.2314
//ACM_CAREAW4// 1.5456,1.8626,6.6209,6.6209,1.5661,1.8587,7.0103,7.0103,1.5865,1.8547
//ACM_CAREAH1// 0,0,1.1069,1.6255,0.2893,0.2893,1.0938,1.6086,0.5786,0.5786
//ACM_CAREAH2// 1.0808,1.5917,0.8311,0.8311,1.1045,1.5747,1.0837,1.0837,1.1098,1.5578
//ACM_CAREAH3// 1.3546,1.3546,1.1151,1.5409,1.6255,1.6255,1.1020,1.5239,1.8965,1.8965
//ACM_CAREAH4// 1.1441,1.5070,2.1674,2.1674,1.1127,1.4901,2.5854,2.5854,0.7135,1.4731
//ACM_CAREAV1// 0,0,0.4335,1.3005,0.1926,0.1926,0.6070,1.4046,0.3853,0.3853
//ACM_CAREAV2// 0.7804,1.5087,0.5780,0.5780,0.9539,1.6129,0.7706,0.7706,1.1274,1.7170
//ACM_CAREAV3// 0.9633,0.9633,1.3009,1.8211,1.1560,1.1560,1.4744,1.9252,1.3487,1.3487
//ACM_CAREAV4// 1.6479,2.0294,1.5413,1.5413,1.8213,2.1335,1.7340,1.7340,1.9948,2.2376
wing_area = 220.00
wing_span = 40.00
wing_root_chord = 7.60
wing_dihedral = 5.00
wing_incidence = -1.00
wing_twist = -1.00
oswald_efficiency_factor = 0.80
wing_winglets_flag = 0
wing_sweep = 14.00
wing_pos_apex_lon = 4.50
wing_pos_apex_vert = -0.20
htail_area = 66.00
htail_span = 17.00
htail_pos_lon = -10.40
htail_pos_vert = 2.30
htail_incidence = 0.00
htail_sweep = 14.00
vtail_area = 35.00
vtail_span = 5.50
vtail_sweep = 42.00
vtail_pos_lon = -7.60
vtail_pos_vert = 2.80
elevator_area = 26.00
aileron_area = 10.00
rudder_area = 10.00
elevator_up_limit = 17.00
elevator_down_limit = 15.00
aileron_up_limit = 30.00
aileron_down_limit = 30.00
rudder_limit = 30.00
elevator_trim_limit = 15.00
spoiler_limit = 0.00
aileron_to_spoileron_gain = 0.00
spoiler_handle_available = 0
min_ailerons_for_spoilerons = 0.00
min_flaps_for_spoilerons = 0.00
spoilerons_available = 0
auto_spoiler_available=0
positive_g_limit_flaps_up=3.00
positive_g_limit_flaps_down=2.00
negative_g_limit_flaps_up=-2.00
negative_g_limit_flaps_down=-2.00

[electrical]
flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 5 , 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2 , 17.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 17.0
light_nav          = 0, 5 , 17.0
light_beacon       = 0, 5 , 17.0
light_landing      = 0, 5 , 17.0
light_taxi         = 0, 5 , 17.0
light_strobe       = 0, 5 , 17.0
light_panel        = 0, 5 , 17.0

[flight_tuning]
cruise_lift_scalar=1.00 
parasite_drag_scalar=1.00 
induced_drag_scalar=1.00 
elevator_effectiveness=1.00 
aileron_effectiveness=1.00 
rudder_effectiveness=1.00 
pitch_stability=1.00 
roll_stability=1.00 
yaw_stability=1.00 
elevator_trim_effectiveness=1.00 
aileron_trim_effectiveness=1.00 
rudder_trim_effectiveness=1.00 

[piston_engine]
power_scalar=1.00 
cylinder_displacement= 95.00 
compression_ratio= 8.00 
number_of_cylinders= 6
max_rated_rpm= 2700.00
max_rated_hp= 300.00
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.30
turbocharged= 1
max_design_mp= 40.00
min_design_mp= 1.00
critical_altitude= 7000.00
emergency_boost_type= 0
emergency_boost_mp_offset= 0.00
emergency_boost_gain_offset= 0.00
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.00 
idle_rpm_mechanical_efficiency_scalar=1.00
max_rpm_friction_scalar=1.00
idle_rpm_friction_scalar=1.00

[propeller]
thrust_scalar=1.00
propeller_type= 0
propeller_diameter= 6.20
propeller_blades= 3
propeller_moi= 6.00
beta_max= 45.00
beta_min= 15.00
min_gov_rpm= 1500.00
prop_tc= 0.10
gear_reduction_ratio= 1.10
fixed_pitch_beta= 0.00
low_speed_theory_limit= 80.00
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 0
min_rpm_for_feather= 700.00
beta_feather= 82.50
power_absorbed_cf= 0.90
defeathering_accumulators_available= 0
prop_reverse_available= 0.00
minimum_on_ground_beta= 0.00
minimum_reverse_beta= 0.00

[pitot_static]
vertical_speed_time_constant = 1.0              //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.00

[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second

[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 
Transponder.1=1 
Marker.1=1 

[Views]
eyepoint=7.85, -0.88, 2.49 //Longitudinal, Lateral, Vertical (feet)

[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=3,0 

[Reference Speeds]
flaps_up_stall_speed= 70.00 
full_flaps_stall_speed= 58.00 
cruise_speed= 220.00		//knots over the ground at 7,000 ft. (199 indicated) 
max_indicated_speed=280.00
max_level_speed=260		//knots over the ground at 7,000 ft.

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=700.0
autothrottle_available=0
pitch_takeoff_ga=8.00
max_pitch=10.00
max_pitch_acceleration=1.00
max_pitch_velocity_lo_alt=2.00
max_pitch_velocity_hi_alt=1.50
max_pitch_velocity_lo_alt_breakpoint=20000.00
max_pitch_velocity_hi_alt_breakpoint=28000.00
max_bank=25.00
max_bank_acceleration=1.80
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain=0.00

[brakes]
toe_brakes_scale=1.00
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.10
flap_limit_power=0.00
flap_limit_idle=31.50

[hydraulic_system]
normal_pressure=0.00

[stall_warning]
type=1
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[Flaps.0]
type= 1
span-outboard= 0.80
extending-time= 4.00
system_type= 0
damaging-speed= 150.00
blowout-speed= 250.00
lift_scalar= 1.00
drag_scalar= 1.00
pitch_scalar= 1.00
flaps-position.0= 0.00, 0.00
flaps-position.1= 10.00, 0.00
flaps-position.2= 20.00, 0.00
flaps-position.3= 30.00, 0.00
flaps-position.4= 35.00, 0.00

[vacuum_system]
max_pressure=5.15
vacuum_type=1
electric_backup_pressure=4.90
engine_map=1,1,0,0

[pneumatic_system]
max_pressure=0.00
bleed_air_scalar=0.00

[deice_system]
structural_deice_type=2