[fltsim.0]
title=PC7 Trainer
sim=PC7 Trainer
model=
panel=
sound=
texture=
kb_checklists=PC7_checklist
kb_reference=specs
description=Notes Aircraft Pilatus P.C.7 Mk II Astra is a single engine turboprop, all metal, low-wing, two-seat training aircraft from the South African Airforce. \nModel: Thinus Pretorius\nAerodyn.: Dr. J. v. Kampen (c) 2008
ui_manufacturer=Pilatus
ui_type=PC7 Astra Mk. 2
ui_variation=Trainer
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
visual_damage=1
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
atc_parking_types=MIL_COMBAT

[fltsim.1]
title=PC7 Silver Falcons
sim=PC7 Silver Falcons
model=1
panel=
sound=
texture=1
kb_checklists=PC7_checklist
kb_reference=specs
description=Notes The Aircraft is depicted as Silver Falcon 1 of the South African Airforce. Pilatus P.C.7 Mk II Astra is a single engine turboprop, all metal, low-wing, two-seat training aircraft. \nModel: Thinus Pretorius\nAerodyn.: Dr. J. v. Kampen (c) 2008
ui_manufacturer=Pilatus
ui_type=PC7 Astra Mk. 2
ui_variation=Silver Falcon 1
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
visual_damage=1
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
atc_parking_types=MIL_COMBAT

[fltsim.2]
title=PC7 Silver Falcon2
sim=PC7 Silver Falcons
model=1
panel=
sound=
texture=2
kb_checklists=PC7_checklist
kb_reference=specs
description=Notes 9A:The Aircraft is depicted as Silver Falcon 2 of the South African Airforce. Pilatus P.C.7 Mk II Astra is a single engine turboprop, all metal, low-wing, two-seat training aircraft. \nModel: Thinus Pretorius\nAerodyn.: Dr. J. v. Kampen (c) 2008
ui_manufacturer=Pilatus
ui_type=PC7 Astra Mk. 2
ui_variation=Silver Falcon2
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
visual_damage=1
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
atc_parking_types=MIL_COMBAT

[fltsim.3]
title=PC7 Silver Falcon3
sim=PC7 Silver Falcons
model=1
panel=
sound=
texture=3
kb_checklists=PC7_checklist
kb_reference=specs
description=Notes 7A The Aircraft is depicted as Silver Falcon 3 of the South African Airforce. Pilatus P.C.7 Mk II Astra is a single engine turboprop, all metal, low-wing, two-seat training aircraft. \nModel: Thinus Pretorius\nAerodyn.: Dr. J. v. Kampen (c) 2008
ui_manufacturer=Pilatus
ui_type=PC7 Astra Mk. 2
ui_variation=Silver Falcon3
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
visual_damage=1
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
atc_parking_types=MIL_COMBAT

[fltsim.4]
title=PC7 Silver Falcons4
sim=PC7 Silver Falcons
model=1
panel=
sound=
texture=4
kb_checklists=PC7_checklist
kb_reference=specs
description=Notes The Aircraft is depicted as Basic Trainer of the South African Airforce. Pilatus P.C.7 Mk II Astra is a single engine turboprop, all metal, low-wing, two-seat training aircraft. \nModel: Thinus Pretorius\nAerodyn.: Dr. J. v. Kampen (c) 2008
ui_manufacturer=Pilatus
ui_type=PC7 Astra Mk. 2
ui_variation=Silver Falcon4
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
visual_damage=1
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
atc_parking_types=MIL_COMBAT

[fltsim.5]
title=PC7 Solo
sim=PC7 Trainer
model=solo
panel=
sound=
texture=
kb_checklists=PC7_checklist
kb_reference=specs
description=Notes Aircraft Pilatus P.C.7 Mk II Astra is a single engine turboprop, all metal, low-wing, two-seat training aircraft from the South African Airforce. \nModel: Thinus Pretorius\nAerodyn.: Dr. J. v. Kampen (c) 2008
ui_manufacturer=Pilatus
ui_type=PC7 Astra Mk. 2
ui_variation=Solo
atc_heavy=0
atc_id=
atc_airline=
atc_flight_number=
visual_damage=1
atc_id_color=0x00000000
atc_id_font=Verdana,-11,1,600,0
atc_parking_types=MIL_COMBAT


[General]
performance=AIRCRAFT SPECIFICATION\nTwo seater trainer\nPowerplant:1 x 700 shp P& W Canada PT6A-25C\nMax speed: 350 kts (Mach 0.53)\nVno: 280 kts\nRange:1500 km\nLength:10.13 m \nWing span:10.12 m\nWeight empty:1330 kg \nMax weight: 2700 kg\nModel: Thinus Pretorius\nAerodyn.: Dr. J. v. Kampen (c) 2008 
atc_type=PILATUS 
atc_model=PC7 
editable=0 
category=airplane

[weight_and_balance]

// ACM V2.5
max_gross_weight = 5164
empty_weight = 3196
reference_datum_position = -0.1, 0, -0.1
empty_weight_CG_position = 0.02, 0, 0
empty_weight_pitch_MOI = 7500
empty_weight_roll_MOI = 2581
empty_weight_yaw_MOI = 5108
empty_weight_coupled_MOI = 0.000
CG_forward_limit = 0.300
CG_aft_limit = 0.500
max_number_of_stations = 2

station_load.0 = 160, 1.600, 0.000, 0.000
station_load.1 = 160, -3.750, 0.000, 0.000


[lights]

//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing,  6=taxi, 7=recognition, 8=wing, 9=logo, 10=cabin

light.0 = 3, 1.55, -16.706, -0.4, fx_navred
light.1 = 3, 1.55, 16.455, -0.4, fx_navgre
light.2 = 2, -0.65, 0, -2.758, fx_PC7_nav_red_flash
light.3 = 3, -18.2, 0, 0, fx_navwhi
light.4 = 6, 10.0, 1.15, 0, fx_PC7_SmokeL
light.5 = 6, 10.0, -1.15, 0, fx_PC7_SmokeR

[GeneralEngineData]

//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.0200  //FFcurve/thr!
min_throttle_limit = -0.10000
engine.0 = 7.150, 0.000, -0.20

[smokesystem]
smoke.0 = 10.5, 0,0,  fx_PC7engine

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_m, 1
startup = fx_engstrt
windshield_rain_effect_available = 1

[fuel]

//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2
number_of_tank_selectors = 1
electric_pump = 1

LeftMain = -0.12, 6, -1.8, 64.5, 1
RightMain = -0.12, -6, -1.8, 64.5, 1


[contact_points]
static_pitch = 0.260
static_cg_height = 5.350
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points =10
point.0= 1, 7.000, 0.000, -5.380, 1858, 0, 0.750, 36.500, 0.120, 2.157, 0.595, 5.000, 6.000, 0
point.1= 1, -1.651, -4.450, -5.440, 1926, 1, 0.825, 0.000, 0.288, 2.486, 0.808, 5.200, 5.000, 2
point.2= 1, -1.650, 4.450, -5.440, 1926, 2, 0.825, 0.000, 0.288, 2.486, 0.808, 5.000, 5.200, 3
point.3= 2, -15.500, 0.000, 6.000, 500, 0, 0.000, 0.000, 0.000, -1.000, 0.000, 0.000, 0.000, 9
point.4= 2, 0.000, -16.583, -0.500, 1275, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.5= 2, 9.500, 0.000, -2.300, 500, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.6= 2, 0.000, 16.583, -0.550, 1275, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.7= 2, -17.000, 0.000, -1.900, 1075, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.8= 2, -0.500, 0.000, -2.850, 500, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.9= 2, 1.083, 0.000, 0.500, 275, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4



[keyboard_response]
elevator = 120, 240
aileron = 120, 240
rudder = 10, 110


[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

[airplane_geometry]
//ACM_AREAW1// 0,0,0,2.4993,0.5842,0.5842,0.0204,2.3947,1.1684,1.1684
//ACM_AREAW2// 0.0408,2.2901,1.7525,1.7525,0.0612,2.1856,2.3368,2.3368,0.0816,2.0810
//ACM_AREAW3// 2.9210,2.9210,0.1018,1.9765,3.5051,3.5051,0.1224,1.8717,4.0893,4.0893
//ACM_AREAW4// 0.1428,1.7673,4.6736,4.6736,0.1632,1.6627,5.2578,5.2578,0.1835,1.5582
//ACM_AREAH1// 0,0,0,1.1683,0.1947,0.1947,0.0170,1.1267,0.3894,0.3894
//ACM_AREAH2// 0.0340,1.0856,0.5841,0.5841,0.0511,1.0441,0.7789,0.7789,0.0680,1.0025
//ACM_AREAH3// 0.9735,0.9735,0.0851,0.9613,1.1683,1.1683,0.1022,0.9200,1.3631,1.3631
//ACM_AREAH4// 0.1190,0.8787,1.5578,1.5578,0.1360,0.8373,1.7525,1.7525,0.1533,0.7957
//ACM_AREAV1// -0.1895,-0.1895,-0.1703,1.7416,0.1703,0.1703,-0.5248,1.6818,0.3406,0.3406
//ACM_AREAV2// 0.0118,1.6409,0.5109,0.5109,0.2642,1.6188,0.6812,0.6812,0.3269,1.5779
//ACM_AREAV3// 0.8517,0.8517,0.3898,1.5750,1.0219,1.0219,0.4336,1.5532,1.1921,1.1921
//ACM_AREAV4// 0.5343,1.5123,1.3624,1.3624,0.5971,1.4903,1.6275,1.6275,0.6790,1.4305
//ACM_CAREAW1// 2.6289,2.6289,1.3414,1.8413,2.9210,2.9210,1.3516,1.8265,3.2130,3.2130
//ACM_CAREAW2// 1.3617,1.8114,3.5051,3.5051,1.3717,1.7969,3.7973,3.7973,1.3822,1.7819
//ACM_CAREAW3// 4.0893,4.0893,1.3924,1.7673,4.3814,4.3814,1.4026,1.7525,4.6736,4.6736
//ACM_CAREAW4// 1.4127,1.7378,4.9657,4.9657,1.4227,1.7230,5.2578,5.2578,1.4332,1.7079
//ACM_CAREAH1// 0,0,0.5841,1.1683,0.1947,0.1947,0.6011,1.1562,0.3894,0.3894
//ACM_CAREAH2// 0.6182,1.1440,0.5841,0.5841,0.6352,1.1318,0.7789,0.7789,0.6523,1.1196
//ACM_CAREAH3// 0.9735,0.9735,0.6693,1.1073,1.1683,1.1683,0.6862,1.0951,1.3631,1.3631
//ACM_CAREAH4// 0.7034,1.0829,1.5578,1.5578,0.7203,1.0707,1.7525,1.7525,0.7375,1.0585
//ACM_CAREAV1// 0,0,0.3831,1.1497,0.1703,0.1703,0.3892,1.0944,0.3406,0.3406
//ACM_CAREAV2// 0.3950,1.0391,0.5109,0.5109,0.4011,0.9836,0.6812,0.6812,0.4070,0.9283
//ACM_CAREAV3// 0.8517,0.8517,0.4129,0.8729,1.0219,1.0219,0.4189,0.8173,1.1921,1.1921
//ACM_CAREAV4// 0.4248,0.7620,1.3624,1.3624,0.4307,0.7067,1.5331,1.5331,0.4368,0.6514
wing_area = 192.60000
wing_span = 34.30000
wing_root_chord = 7.74000
wing_dihedral = 1.10000
wing_incidence = 0.00000
wing_twist = 0.00000
oswald_efficiency_factor = 0.84000
wing_winglets_flag = 0
wing_sweep = 3.00000
wing_pos_apex_lon = 1.6585
wing_pos_apex_vert = -2.00000
htail_area = 32.50000
htail_span = 11.50000
htail_pos_lon = -13.50000
htail_pos_vert = 0.00000
htail_incidence = -0.125
htail_sweep = 9.00000
vtail_area = 26.00000
vtail_span = 5.03000
vtail_sweep = 12.00000
vtail_pos_lon = -14.00000
vtail_pos_vert = 0.85000
elevator_area = 6.80000
aileron_area = 6.60000
rudder_area = 6.20000
elevator_up_limit = 25.00000
elevator_down_limit = 18.00000
aileron_up_limit = 25.00000
aileron_down_limit = 12.50000
rudder_limit = 16.00000
elevator_trim_limit = 18.0000
spoiler_limit = 43.00000
aileron_to_spoileron_gain = 0.00000
spoiler_handle_available = 1
min_ailerons_for_spoilerons = 0.00000
min_flaps_for_spoilerons = 0.00000
spoilerons_available = 0
auto_spoiler_available=1
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=9.690171
positive_g_limit_flaps_down=4.273504
negative_g_limit_flaps_up=-4.310897
negative_g_limit_flaps_down=-2.534188

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
engine_generator_map = 1
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 5, 17
avionics = 1, 5, 17
pitot_heat = 0, 2, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 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

[flight_tuning]
cruise_lift_scalar  =1.00000 
pitch_stability     =1.00000 
roll_stability      =1.00000 
yaw_stability       =1.00000 
parasite_drag_scalar= 1.0000 
induced_drag_scalar = 1.0000 
elevator_effectiveness=1.00000 
aileron_effectiveness =1.00000 
rudder_effectiveness  =1.00000 
elevator_trim_effectiveness=1.00000 
aileron_trim_effectiveness =1.00000 
rudder_trim_effectiveness  =1.00000 
hi_alpha_on_roll     =1.00000
hi_alpha_on_yaw      =1.00000
p_factor_on_yaw      =1.00000
torque_on_roll       =1.00000
gyro_precession_on_roll=1.00000
gyro_precession_on_yaw =1.00000

[propeller]
thrust_scalar=1.00000 
propeller_type=0 
propeller_diameter=9.5 
propeller_blades=4 
propeller_moi=54 
beta_max=45.0000 // full power
beta_min=9.5000  // park
min_gov_rpm=24000.00000 
prop_tc=0.00800 
gear_reduction_ratio=16.0000 
fixed_pitch_beta=0.00000 
low_speed_theory_limit=65.00000  //eq.Vrot
prop_sync_available=0 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=700.00000 
beta_feather=79.80000 
power_absorbed_cf=0.90000 
defeathering_accumulators_available=0 
prop_reverse_available=0 
minimum_on_ground_beta=0.00000 
minimum_reverse_beta=0.0000 

[TurbineEngineData]
fuel_flow_gain=0.0120 
inlet_area=1.02000 
rated_N2_rpm=33000.00000 
static_thrust=192.0000   //dont change
reverser_available=0 
afterburner_available=0 

[turboprop_engine]
power_scalar=1.00000 
maximum_torque=3500 //lim M=0.6  

[pitot_static]
vertical_speed_time_constant = 1.0              //Increasing this value will cause a more instantaneous reaction in the VSI
pitot_heat=1.000000

[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 

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1 
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=1,0
[exits]
number_of_exits = 1
exit_rate.0 = 0.4                               ;Percent per second

[Reference Speeds]
flaps_up_stall_speed=57.5 //c.air
full_flaps_stall_speed=48.6 
cruise_speed=280.00000 
max_indicated_speed=360.00000
max_mach=0.54300

[autopilot]
autopilot_available=1 
flight_director_available=1 
default_vertical_speed=900 
autothrottle_available=0 
max_pitch=8
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 =1
pitch_takeoff_ga=8 
default_pitch_mode=0
default_bank_mode=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=80
use_no_default_bank=1
use_no_default_pitch=1

[stall_warning]
type=1
stick_shaker=1
[gear_warning_system]
gear_warning_available =1
pct_throttle_limit =0.10000
flap_limit_idle    =18.75000
flap_limit_power   =16.00000
[brakes]
parking_brake =1.05
toe_brakes_scale =0.98000
auto_brakes=0
hydraulic_system_scalar=0.51000
differential_braking_scale=0.00000
[hydraulic_system]
normal_pressure =3000.00000
electric_pumps  = 0         //no electric pumps
engine_map      = 1,0,0,0   //pumps on Eng1
[Radios]
// Radio Type = 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 

[Flaps.0]
type= 1
system_type=0
span-outboard= 0.526
extending-time= 11
damaging-speed=240.0
blowout-speed=260.0
flaps-position.0=0.00
flaps-position.1=15.00
flaps-position.2=30.00
lift_scalar= 0.5200   //dont change
drag_scalar= 1.0000
pitch_scalar=0.985

[GPWS]
max_warning_height=250
sink_rate_fpm=-1200
excessive_sink_rate_fpm=-1500
climbout_sink_rate_fpm=-100
flap_and_gear_sink_rate_fpm=-150
[AirWrench]
Aircraft_Length=28.98000
Vmax_sl=379.75707
Vmax_ca=384.70542
V_rc=230.50103
Climb_Rate=2500.20000
Climb_Weight=3096.00000
Max_gforce=9.50000
Emergency_hp=180.00000
VSI_Weight=3416.00000
static_margin=0.09500
nose_position_lon=10.24000
ActualIncidence=1.50000
ActualTwist=-3.00000
ActualTailIncidence=-0.01000
Aircraft_Type=7
FlowCorrection=1.00000
ReheatCutoff=1.20000
OptimumMach=0.60000
Power_Calibration=1.00000
IdleRPM=0.00000
piston_research=0.00000
JetAltitude=0.00000
turboprop_critical_altitude=19964.00000
target_roll_Vopt=345.69401
target_roll_rate=53.10000
pitch_damping=1.10000
yaw_damping=0.90000
weathervane=1.00000
elevator_scalar=1.00000
aileron_scalar=1.00000
rudder_scalar=1.00000
dihedral_scalar=1.00000
sideslip_scalar=1.00000
prop_yaw_damping_scalar=1.00000
Elevator_FF=130.00000
Aileron_FF=-150.00000
Roll_Response=25.00000
Adverse_Yaw=100.00000
Control_Response=97.00000
V_Max_Control=379.75707
V_Zero_Control=759.51414
V_Max_RdrControl=379.75707
V_Zero_RdrControl=759.51414
Spin_Stability=98.00000
Roll_Off=0.00000
glide_ratio=14.12337
CritAoA=12.00000
ClAoA_k0=0.10000
ClAoA_k1=0.10000
ClAoA_k2=0.15000
ClAoA_k3=0.15000
Elevator_Propwash=1.10000
Rudder_Propwash=1.00000
afterburner_thrust=875.00000
prop_design_altitude=5000.00000
prop_material_type=1
protect_airfile=0
spoiler_type=1
spoiler_cd=0.06010
spoiler_cl=-0.02200
spoiler_cm=-0.00220
auto_flaps_enabled=0
flaps_type=1
flaps_cd_scalar=0.30700
flaps_cm_scalar=0.00500
vfe_enabled=0
gear_cd_scalar=0.38000
gear_cm_scalar=-0.00000
critical_mach_number=0.80000
max_mach_cd0=60
direct_edit_drag=0
cylinder_head_temperature=501.00000
exhaust_gas_temperature=826.00000
fuel_pressure=16.50000
oil_pressure=66.00000
oil_temperature=141.00000
radiator_temperature=211.00000
lo_rpm_friction=1.00000
hi_rpm_friction=1.00000
exhaust_pressure_ratio=1.40000
interstage_turbine_temperature=1682.00000
knots_flag=1
cfs1_flag=0
cfs2_flag=0
AI_flag=0
edit_tp_torque=1
direct_edit_mach=0
direct_edit_2dtab=0
fixed_wing_pos=1
range_est_alt=0.00000
range_est_rpm=0.00000
range_est_mp=29.92000
range_est_fuel=129.40000
contact_light_flags=0
AirWrenchVersion=1.01.64
[Views]
eyepoint=0.558657,0.000000,3.444919             //eyepoint=-0.758657,0.000000,3.344919 

[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