Post by esymon on Feb 1, 2021 6:10:31 GMT
I'm having issues with MD82F,MD 82 and MD83, these aircraft will not show up on my game.
i have insured that the files are all unzipped and installed as it is written
i have deleted all said original files that the aircraft came from after adding it.
ive tried uninstalls and re installs and the aircraft will still not show up.
i believe the acg files are correct. here they are:
MD-82F
/HJG MD-82SF (FREIGHTER CONVERSION) V1.0
//FS2004
//JANUARY 14TH 2014
[fltsim.0]
title=HJG MD-82SF Everts Air Cargo 2014
sim=MD-82SF
model=freighter02
panel=
sound=
texture=everts_air_cargo_2013_82sf_n73444
kb_checklists=
atc_id=N73444
atc_airline=EVERTS
atc_flight_number=821
atc_heavy=0
ui_manufacturer=McDonnell Douglas
ui_type=MD-82SF
ui_variation=Everts Air Cargo (2014)
ui_typerole=Commercial Airliner
ui_createdby=Historic Jetliners Group
description=HJG MD-82SF v1.0 repaint by Tony MADGE. 3D model editing by Nick BOTAMER & Paul HAAK
[fltsim.1] // Change "xx" to next number in sequence starting from 0
title=MD-82SF Aeronaves TSM (basic livery) 2015
sim=MD-82SF
model=freighter02
panel=
sound=
texture=aeronaves_tsm_2015_82sf_xa-utx
kb_checklists=
kb_reference=
atc_id=XA-UTX
atc_airline=AERONAVES
atc_flight_number=820
atc_heavy=0
atc_parking_codes=VTM
atc_parking_types=CARGO
ui_manufacturer=McDonnell Douglas
ui_type=MD-82SF
ui_variation=Aeronaves TSM - basic livery (2015)
ui_typerole=Commercial Airliner
ui_createdby=Historic Jetliners Group
description=HJG MD-81 v1.1 repaint by Erik INGRAM
[GENERAL]
atc_type=MCDONNELDOUGLAS
atc_model=MD80
Editable=0
performance=Maximum Ramp Weight: 150,500 lb / 68,409 kg\nMaximum Takeoff Weight: 149,500 lb / 67,954 kg\nMaximum Landing Weight: 130,000 lb / 59,090 kg\nMaximum Zero Fuel Weight: 122,000 lb / 55,4545 kg\nOperating Empty Weight: 75,400 lb / 34,201 kg\nMaximum Payload: 46,600 lb / 21,137 kg\n
[VIEWS]
eyepoint = 52.70,-1.887,5.255 //cockpit View Viewpoint
[FORCEFEEDBACK]
stick_shaker_magnitude = 0
stick_shaker_direction = 0
stick_shaker_period = 0
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.2
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[FLIGHT_TUNING]
elevator_effectiveness =1.0
aileron_effectiveness =1.0
rudder_effectiveness =1.1
elevator_trim_effectiveness =0.90
aileron_trim_effectiveness =1.0
rudder_trim_effectiveness =1.0
pitch_stability =1.50
roll_stability =1.0
yaw_stability =1.1
cruise_lift_scalar =1.30
parasite_drag_scalar =1.0
induced_drag_scalar =1.0
[WEIGHT_AND_BALANCE]
max_gross_weight = 150500
empty_weight = 75400
reference_datum_position = 6.0,
Md82
//HJG MD-82 V1.1
//FS2004
//NOVEMBER 24TH 2011
[fltsim.0]
title=HJG MD-83 Alaska Airlines '2008'
sim=MD-83
model=02
panel=
sound=
texture=as_2008_83_n972as
kb_checklists=
kb_reference=
atc_id=N972AS
atc_airline=ALASKA
atc_flight_number=732
atc_heavy=0
ui_manufacturer=McDonnell Douglas
ui_type=MD-83
ui_variation=Alaska Airlines '2008'
description=HJG MD-80 v1
[fltsim.1]
TITLE=HJG MD-83 TWA 1998
SIM=MD-80
MODEL=02
PANEL=
SOUND=
TEXTURE=hjg_md83_twa_n9627r_1998
KB_CHECKLISTS=
KB_REFERENCE=
ATC_ID=N9627R
ATC_AIRLINE=TWA
ATC_FLIGHT_NUMBER=034
ATC_HEAVY=0
UI_MANUFACTURER=MCDONNELL DOUGLAS
UI_TYPE=MD-83
UI_VARIATION=TWA 1998
DESCRIPTION=HJG MD-80
[GENERAL]
atc_type=MCDONNELDOUGLAS
atc_model=MD80
Editable=0
performance=Maximum Ramp Weight: 150,500 lb / 68,409 kg\nMaximum Takeoff Weight: 149,500 lb / 67,954 kg\nMaximum Landing Weight: 130,000 lb / 59,090 kg\nMaximum Zero Fuel Weight: 122,000 lb / 55,4545 kg\nOperating Empty Weight: 78,564 lb / 35,710 kg\nMaximum Payload: 41,458 lb / 18,844 kg\n
[VIEWS]
eyepoint = 52.70,-1.887,5.255 //cockpit View Viewpoint
[FORCEFEEDBACK]
stick_shaker_magnitude = 0
stick_shaker_direction = 0
stick_shaker_period = 0
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.2
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[FLIGHT_TUNING]
elevator_effectiveness =1.0
aileron_effectiveness =1.0
rudder_effectiveness =1.1
elevator_trim_effectiveness =0.90
aileron_trim_effectiveness =1.0
rudder_trim_effectiveness =1.0
pitch_stability =1.50
roll_stability =1.0
yaw_stability =1.1
cruise_lift_scalar =1.4
parasite_drag_scalar =1.0
induced_drag_scalar =1.0
[WEIGHT_AND_BALANCE]
max_gross_weight = 149500
empty_weight = 78000
reference_datum_position = 6.0, 0.0, 0.0
empty_weight_CG_position = -3.0, 0.0, 0.0
empty_weight_pitch_MOI = 3661351.0
empty_weight_roll_MOI = 822918.0
empty_weight_yaw_MOI = 3924730.0
empty_weight_coupled_MOI = 0.0
max_number_of_stations = 20
station_load.0 = " 380, 52.70, 0.0, 0.0, Pilot (2)"
station_load.1 = " 190, 50.25, 0.0, 0.0, Observer (1)"
station_load.2 = " 380, 42.60, 0.0, 0.0, F/A (2)"
station_load.3 = " 190, -30.00, 0.0, 0.0, F/A (1)"
station_load.4 = " 380, -40.00, 0.0, 0.0, F/A (2)"
station_load.5 = "3040, 33.70, 0.0, 0.0, First (16)"
station_load.6 = "5700, 23.16, 0.0, 0.0, Coach A(30)"
station_load.7 = "5700, 9.50, 0.0, 0.0, Coach B(30)"
station_load.8 = "5700, -4.20, 0.0, 0.0, Coach C(30)"
station_load.9 = "4750, -17.40, 0.0, 0.0, Coach D(25)"
station_load.10 = "3420, -31.60, 0.0, 0.0, Coach E(18)"
station_load.11 = "2660, 31.70, 0.0, 0.0, Fwd Cargo"
station_load.12 = "2660, 9.30. 0.0, 0.0, Mid Cargo"
station_load.13 = "2660, -31.70, 0.0, 0.0, Aft Cargo"
[FUEL]
Center1 = -1.67, 0.0, 0.00, 3074.0, 10.7
LeftMain = -7.25, -18.0, 0.00, 1383.0, 7.7
RightMain = -7.25, 18.0, 0.00, 1383.0, 7.7
fuel_type = 2.00
number_of_tank_selectors = 1
electric_pump = 0
[GENERALENGINEDATA]
engine_type = 1
Engine.0 = -48.800, -8.000, 2.680
Engine.1 = -48.800, 8.000, 2.680
fuel_flow_scalar = 0.9120
min_throttle_limit = -0.49
[TURBINEENGINEDATA]
fuel_flow_gain = 0.00300
inlet_area = 26.7
rated_N2_rpm = 29920
static_thrust = 20000
afterburner_available = 0
reverser_available = 1
[JET_ENGINE]
thrust_scalar =1.0
[AIRPLANE_GEOMETRY]
wing_area = 1209.0
wing_span = 107.8
wing_root_chord = 21.3
wing_dihedral = 3.0
wing_incidence = 1.0
wing_twist = -0.5
oswald_efficiency_factor = 0.80
wing_winglets_flag = 0
wing_sweep = 24
wing_pos_apex_lon = 9.575
wing_pos_apex_vert = 0.0
htail_area = 275.6
htail_span = 36.85
htail_pos_lon = -55.22
htail_pos_vert = 20.00
htail_incidence = 0
htail_sweep = 36
vtail_area = 161
vtail_span = 14
vtail_sweep = 44
vtail_pos_lon = -44.30
vtail_pos_vert = 8.570
elevator_area = 95.8
aileron_area = 38.0
rudder_area = 65.3
elevator_up_limit = 22.5
elevator_down_limit = 19.5
aileron_up_limit = 20.0
aileron_down_limit = 20.0
rudder_limit = 26.0
elevator_trim_limit = 12.0
spoiler_limit = 45
spoilerons_available = 1
aileron_to_spoileron_gain = 2
min_ailerons_for_spoilerons = 10
min_flaps_for_spoilerons = 0
[REFERENCE SPEEDS]
flaps_up_stall_speed = 130
full_flaps_stall_speed = 110
cruise_speed = 467
max_indicated_speed = 350
max_mach = 0.84
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[CONTACT_POINTS]
// Gear 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
point.0 = 1, 57.000, 0.000, -7.350, 2500.0, 0, 1.08, 55.0, 1.20, 1.30, 0.66, 15.00, 8.00, 0, 250.0, 300.0
point.1 = 1, -15.250, -8.350, -8.350, 2500.0, 1, 1.75, 0.0, 0.75, 1.50, 0.70, 15.00, 8.00, 2, 250.0, 300.0
point.2 = 1, -15.250, 8.350, -8.350, 2500.0, 2, 1.75, 0.0, 0.75, 1.50, 0.70, 15.00, 8.00, 3, 250.0, 300.0
// Scrapes 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
point.3 = 2, 57.200, 0.000, 0.000, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.4 = 2, 52.700, 0.000, -3.000, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.5 = 2, 0.000, 0.000, -3.250, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.6 = 2, -38.800, 0.000, -2.250, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.7 = 2, -57.550, 0.000, 5.250, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.8 = 2, -18.750, -43.750, 0.400, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 5, 0,0, 0.0
point.9 = 2, -18.750, 43.750, 0.400, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 6, 0,0, 0.0
// LL 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
point.10 = 5, -18.590, -43.151, 0.475, 2500.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 4.00, 4.00, 0, 350.0, 400.0
point.11 = 5, -18.590, 43.151, 0.475, 2500.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 4.00, 4.00, 0, 350.0, 400.0
max_number_of_points = 15
static_pitch = -0.35
static_cg_height = 7.5
gear_system_type = 1
[FLAPS.0]
type = 2
span-outboard = 0.96
extending-time = 15
flaps-position.0 = 0
flaps-position.1 = 1
flaps-position.2 = 1
flaps-position.3 = 1
flaps-position.4 = 1
flaps-position.5 = 1
damaging-speed = 300
blowout-speed = 350
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar = 1.0
system_type = 1
[FLAPS.1]
type = 1
span-outboard = 0.60
extending-time = 30
flaps-position.0 = 0
flaps-position.1 = 1
flaps-position.2 = 5
flaps-position.3 = 15
flaps-position.4 = 25
flaps-position.5 = 40
damaging-speed = 300
blowout-speed = 350
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar = 1.0
system_type = 1
[ELECTRICAL]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 65
electric_always_available = 0
flap_motor = 0, 5, 17.0
gear_motor = 0, 5, 17.0
autopilot = 0, 5, 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5, 17.0
pitot_heat = 0, 2, 17.0
additional_system = 0, 20, 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
starter2 = 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
standby_vacuum = 0, 5, 17.0
hydraulic_pump = 0, 2, 17.0
fuel_transfer_pump = 0, 5, 17.0
light_recognition = 0, 5, 17.0
light_wing = 0, 5, 17.0
light_logo = 0, 5, 17.0
[PITOT STATIC]
vertical_speed_time_constant = 1
[EXITS]
number_of_exits = 2
exit_rate.0 = 0.25
exit_rate.1 = 0.15
[KEYBOARD_RESPONSE]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[DIRECTION_INDICATORS]
direction_indicator.0 = 3,0
[AUTOPILOT]
autopilot_available =1
flight_director_available =1
default_vertical_speed =0.00
autothrottle_available =1
autothrottle_arming_required =1
autothrottle_takeoff_ga =1
autothrottle_max_rpm =95
pitch_takeoff_ga =8
use_no_default_pitch =1
use_no_default_bank =1
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 =20
max_bank_acceleration =1.8
max_bank_velocity =3
max_throttle_rate =0.1
nav_proportional_control =15
nav_integrator_control =0.1
nav_integrator_boundary =3.5
nav_derivative_control =0.03
nav_derivative_boundary =0.35
gs_proportional_control =15
gs_integrator_control =0.3
gs_derivative_control =0
gs_integrator_boundary =0.7
gs_derivative_boundary =0
yaw_damper_gain =1
[RADIOS]
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
[EFFECTS]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 =3, -24.437000, -52.439000, 0.661000, fx_navredm
light.1 =3, -24.681000, -52.556000, 0.661000, fx_navredm
light.2 =3, -28.713000, -52.864000, 0.637000, fx_navwhih
light.3 =2, -24.927000, -52.745000, 0.661000, fx_strobeh
light.4 =2, -28.778000, -52.739000, 0.637000, fx_strobeh
light.5 =3, -24.437000, 52.439000, 0.661000, fx_navgrem
light.6 =3, -24.681000, 52.556000, 0.661000, fx_navgrem
light.7 =3, -28.713000, 52.864000, 0.637000, fx_navwhih
light.8 =2, -24.927000, 52.745000, 0.661000, fx_strobeh
light.9 =2, -28.778000, 52.739000, 0.637000, fx_strobeh
light.10 =1, -6.250000, 0.379000, 8.575000, fx_beaconb
light.11 =1, -15.982000, 0.375000, -4.083000, fx_beaconh
light.12 =4, 58.598000, -1.875000, 4.000000, fx_vclight
light.13 =4, 58.598000, 1.875000, 4.000000, fx_vclight
[TAILHOOK]
tailhook_length = 1
tailhook_position = 0,0,0
cable_force_adjust = 0.00001
[FOLDING_WINGS]
wing_fold_system_type = 4
fold_rates = 0.25, 0.25
[brakes]
toe_brakes_scale=1.00
parking_brake=1
[gear_warning_system]
gear_warning_available = 1
pct_throttle_limit = 0.10
flap_limit_power = 25.0
flap_limit_idle = 15.0
[hydraulic_system]
electric_pumps = 1
engine_map = 1,1,0,0
normal_pressure = 3000.0
[stall_warning]
type = 1
[attitude_indicators]
attitude_indicator.0 = 1
[turn_indicators]
turn_indicator.0 = 1,0
[SMOKESYSTEM]
smoke.0= 2.4, -41.9, -8.4, fx_hjg_dc9_smoke.fx
smoke.1= 2.4, -41.9, 8.4, fx_hjg_dc9_smoke.fx
[deice_system]
structural_deice_type = 1
[vacuum_system]
max_pressure = 5.15
vacuum_type = 2
[pneumatic_system]
max_pressure = 18.0
bleed_air_scalar = 1.0
MD83:
//HJG MD-83 V1.1
//FS2004
//NOVEMBER 24TH 2011
[fltsim.0]
title=HJG MD-83 Alaska Airlines '2008'
sim=MD-83
model=02
panel=
sound=
texture=as_2008_83_n972as
kb_checklists=
kb_reference=
atc_id=N972AS
atc_airline=ALASKA
atc_flight_number=732
atc_heavy=0
ui_manufacturer=McDonnell Douglas
ui_type=MD-83
ui_variation=Alaska Airlines '2008'
description=HJG MD-80 v1
[fltsim.1]
TITLE=HJG MD-83 TWA 1998
SIM=MD-80
MODEL=02
PANEL=
SOUND=
TEXTURE=hjg_md83_twa_n9627r_1998
KB_CHECKLISTS=
KB_REFERENCE=
ATC_ID=N9627R
ATC_AIRLINE=TWA
ATC_FLIGHT_NUMBER=034
ATC_HEAVY=0
UI_MANUFACTURER=MCDONNELL DOUGLAS
UI_TYPE=MD-83
UI_VARIATION=TWA 1998
DESCRIPTION=HJG MD-80
[fltsim.2]
title=HJG MD-83 Jetsgo 2005
sim=MD-80
model=02
panel=
sound=
texture=hjg_md83_jetsgo_c-fkly_2005
kb_checklists=
kb_reference=
atc_id=C-FKLY
atc_airline=JETSGO
atc_flight_number=732
atc_heavy=0
ui_manufacturer=McDonnell Douglas
ui_type=MD-81
ui_variation=Jetsgo 2005
description=HJG MD-83
[GENERAL]
atc_type=MCDONNELDOUGLAS
atc_model=MD80
Editable=0
performance=Maximum Ramp Weight: 161,000 lb / 73,181 kg\nMaximum Takeoff Weight: 160,000 lb / 72,727 kg\nMaximum Landing Weight: 139,500 lb / 64,409 kg\nMaximum Zero Fuel Weight: 122,000 lb / 55,454 kg\nOperating Empty Weight: 89,000 lb / 40,454 kg\nMaximum Payload: 41,280 lb / 18,763 kg\n
[VIEWS]
eyepoint = 52.70,-1.887,5.255 //cockpit View Viewpoint
[FORCEFEEDBACK]
stick_shaker_magnitude = 0
stick_shaker_direction = 0
stick_shaker_period = 0
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.2
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[FLIGHT_TUNING]
elevator_effectiveness =1.0
aileron_effectiveness =1.0
rudder_effectiveness =1.1
elevator_trim_effectiveness =0.90
aileron_trim_effectiveness =1.0
rudder_trim_effectiveness =1.0
pitch_stability =1.50
roll_stability =1.0
yaw_stability =1.1
cruise_lift_scalar =1.4
parasite_drag_scalar =1.0
induced_drag_scalar =1.0
[WEIGHT_AND_BALANCE]
max_gross_weight = 160000
empty_weight = 79700
reference_datum_position = 6.0, 0.0, 0.0
empty_weight_CG_position = -3.0, 0.0, 0.0
empty_weight_pitch_MOI = 3716883.0
empty_weight_roll_MOI = 845419.0
empty_weight_yaw_MOI = 4014369.0
empty_weight_coupled_MOI = 0.0
max_number_of_stations = 20
station_load.0 = " 380, 52.70, 0.0, 0.0, Pilot (2)"
station_load.1 = " 190, 50.25, 0.0, 0.0, Observer (1)"
station_load.2 = " 380, 42.60, 0.0, 0.0, F/A (2)"
station_load.3 = " 190, -30.00, 0.0, 0.0, F/A (1)"
station_load.4 = " 380, -40.00, 0.0, 0.0, F/A (2)"
station_load.5 = "3040, 33.70, 0.0, 0.0, First (16)"
station_load.6 = "5700, 23.16, 0.0, 0.0, Coach A(30)"
station_load.7 = "5700, 9.50, 0.0, 0.0, Coach B(30)"
station_load.8 = "5700, -4.20, 0.0, 0.0, Coach C(30)"
station_load.9 = "4750, -17.40, 0.0, 0.0, Coach D(25)"
station_load.10 = "3420, -31.60, 0.0, 0.0, Coach E(18)"
station_load.11 = "4826, 31.70, 0.0, 0.0, Fwd Cargo"
station_load.12 = "4826, 9.30, 0.0, 0.0, Mid Cargo"
station_load.13 = "4826, -31.70, 0.0, 0.0, Aft Cargo"
[FUEL]
Center1 = -1.67, 0.0, 0.00, 3457.0, 10.7
LeftMain = -7.25, -18.0, 0.00, 1766.0, 7.7
RightMain = -7.25, 18.0, 0.00, 1766.0, 7.7
fuel_type = 2.00
number_of_tank_selectors = 1
electric_pump = 0
[GENERALENGINEDATA]
engine_type = 1
Engine.0 = -48.800, -8.000, 2.680
Engine.1 = -48.800, 8.000, 2.680
fuel_flow_scalar = 0.9120
min_throttle_limit = -0.49
[TURBINEENGINEDATA]
fuel_flow_gain = 0.00300
inlet_area = 26.7
rated_N2_rpm = 29920
static_thrust = 21000
afterburner_available = 0
reverser_available = 1
[JET_ENGINE]
thrust_scalar =1.0
[AIRPLANE_GEOMETRY]
wing_area = 1209.0
wing_span = 107.8
wing_root_chord = 21.3
wing_dihedral = 3.0
wing_incidence = 1.0
wing_twist = -0.5
oswald_efficiency_factor = 0.80
wing_winglets_flag = 0
wing_sweep = 24
wing_pos_apex_lon = 9.575
wing_pos_apex_vert = 0.0
htail_area = 275.6
htail_span = 36.85
htail_pos_lon = -55.22
htail_pos_vert = 20.00
htail_incidence = 0
htail_sweep = 36
vtail_area = 161
vtail_span = 14
vtail_sweep = 44
vtail_pos_lon = -44.30
vtail_pos_vert = 8.570
elevator_area = 95.8
aileron_area = 38.0
rudder_area = 65.3
elevator_up_limit = 22.5
elevator_down_limit = 19.5
aileron_up_limit = 20.0
aileron_down_limit = 20.0
rudder_limit = 26.0
elevator_trim_limit = 12.0
spoiler_limit = 45
spoilerons_available = 1
aileron_to_spoileron_gain = 2
min_ailerons_for_spoilerons = 10
min_flaps_for_spoilerons = 0
[REFERENCE SPEEDS]
flaps_up_stall_speed = 130
full_flaps_stall_speed = 110
cruise_speed = 467
max_indicated_speed = 350
max_mach = 0.84
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[CONTACT_POINTS]
// Gear 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
point.0 = 1, 57.000, 0.000, -7.350, 2500.0, 0, 1.08, 55.0, 1.20, 1.30, 0.66, 15.00, 8.00, 0, 250.0, 300.0
point.1 = 1, -15.250, -8.350, -8.350, 2500.0, 1, 1.75, 0.0, 0.75, 1.50, 0.70, 15.00, 8.00, 2, 250.0, 300.0
point.2 = 1, -15.250, 8.350, -8.350, 2500.0, 2, 1.75, 0.0, 0.75, 1.50, 0.70, 15.00, 8.00, 3, 250.0, 300.0
// Scrapes 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
point.3 = 2, 57.200, 0.000, 0.000, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.4 = 2, 52.700, 0.000, -3.000, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.5 = 2, 0.000, 0.000, -3.250, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.6 = 2, -38.800, 0.000, -2.250, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.7 = 2, -57.550, 0.000, 5.250, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.8 = 2, -18.750, -43.750, 0.400, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 5, 0,0, 0.0
point.9 = 2, -18.750, 43.750, 0.400, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 6, 0,0, 0.0
// LL 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
point.10 = 5, -18.590, -43.151, 0.475, 2500.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 4.00, 4.00, 0, 350.0, 400.0
point.11 = 5, -18.590, 43.151, 0.475, 2500.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 4.00, 4.00, 0, 350.0, 400.0
max_number_of_points = 15
static_pitch = -0.35
static_cg_height = 7.5
gear_system_type = 1
[FLAPS.0]
type = 2
span-outboard = 0.96
extending-time = 15
flaps-position.0 = 0
flaps-position.1 = 1
flaps-position.2 = 1
flaps-position.3 = 1
flaps-position.4 = 1
flaps-position.5 = 1
damaging-speed = 300
blowout-speed = 350
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar = 1.0
system_type = 1
[FLAPS.1]
type = 1
span-outboard = 0.60
extending-time = 30
flaps-position.0 = 0
flaps-position.1 = 1
flaps-position.2 = 5
flaps-position.3 = 15
flaps-position.4 = 25
flaps-position.5 = 40
damaging-speed = 300
blowout-speed = 350
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar = 1.0
system_type = 1
[ELECTRICAL]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 65
electric_always_available = 0
flap_motor = 0, 5, 17.0
gear_motor = 0, 5, 17.0
autopilot = 0, 5, 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5, 17.0
pitot_heat = 0, 2, 17.0
additional_system = 0, 20, 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
starter2 = 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
standby_vacuum = 0, 5, 17.0
hydraulic_pump = 0, 2, 17.0
fuel_transfer_pump = 0, 5, 17.0
light_recognition = 0, 5, 17.0
light_wing = 0, 5, 17.0
light_logo = 0, 5, 17.0
[PITOT STATIC]
vertical_speed_time_constant = 1
[EXITS]
number_of_exits = 2
exit_rate.0 = 0.25
exit_rate.1 = 0.15
[KEYBOARD_RESPONSE]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[DIRECTION_INDICATORS]
direction_indicator.0 = 3,0
[AUTOPILOT]
autopilot_available =1
flight_director_available =1
default_vertical_speed =0.00
autothrottle_available =1
autothrottle_arming_required =1
autothrottle_takeoff_ga =1
autothrottle_max_rpm =95
pitch_takeoff_ga =8
use_no_default_pitch =1
use_no_default_bank =1
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 =20
max_bank_acceleration =1.8
max_bank_velocity =3
max_throttle_rate =0.1
nav_proportional_control =15
nav_integrator_control =0.1
nav_integrator_boundary =3.5
nav_derivative_control =0.03
nav_derivative_boundary =0.35
gs_proportional_control =15
gs_integrator_control =0.3
gs_derivative_control =0
gs_integrator_boundary =0.7
gs_derivative_boundary =0
yaw_damper_gain =1
[RADIOS]
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
[EFFECTS]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 =3, -24.437000, -52.439000, 0.661000, fx_navredm
light.1 =3, -24.681000, -52.556000, 0.661000, fx_navredm
light.2 =3, -28.713000, -52.864000, 0.637000, fx_navwhih
light.3 =2, -24.927000, -52.745000, 0.661000, fx_strobeh
light.4 =2, -28.778000, -52.739000, 0.637000, fx_strobeh
light.5 =3, -24.437000, 52.439000, 0.661000, fx_navgrem
light.6 =3, -24.681000, 52.556000, 0.661000, fx_navgrem
light.7 =3, -28.713000, 52.864000, 0.637000, fx_navwhih
light.8 =2, -24.927000, 52.745000, 0.661000, fx_strobeh
light.9 =2, -28.778000, 52.739000, 0.637000, fx_strobeh
light.10 =1, -6.250000, 0.379000, 8.575000, fx_beaconb
light.11 =1, -15.982000, 0.375000, -4.083000, fx_beaconh
light.12 =4, 58.598000, -1.875000, 4.000000, fx_vclight
light.13 =4, 58.598000, 1.875000, 4.000000, fx_vclight
[TAILHOOK]
tailhook_length = 1
tailhook_position = 0,0,0
cable_force_adjust = 0.00001
[FOLDING_WINGS]
wing_fold_system_type = 4
fold_rates = 0.25, 0.25
[brakes]
toe_brakes_scale=1.00
parking_brake=1
[gear_warning_system]
gear_warning_available = 1
pct_throttle_limit = 0.10
flap_limit_power = 25.0
flap_limit_idle = 15.0
[hydraulic_system]
electric_pumps = 1
engine_map = 1,1,0,0
normal_pressure = 3000.0
[stall_warning]
type = 1
[attitude_indicators]
attitude_indicator.0 = 1
[turn_indicators]
turn_indicator.0 = 1,0
[SMOKESYSTEM]
smoke.0= 2.4, -41.9, -8.4, fx_hjg_dc9_smoke.fx
smoke.1= 2.4, -41.9, 8.4, fx_hjg_dc9_smoke.fx
[deice_system]
structural_deice_type = 1
[vacuum_system]
max_pressure = 5.15
vacuum_type = 2
[pneumatic_system]
max_pressure = 18.0
bleed_air_scalar = 1.0
i have insured that the files are all unzipped and installed as it is written
i have deleted all said original files that the aircraft came from after adding it.
ive tried uninstalls and re installs and the aircraft will still not show up.
i believe the acg files are correct. here they are:
MD-82F
/HJG MD-82SF (FREIGHTER CONVERSION) V1.0
//FS2004
//JANUARY 14TH 2014
[fltsim.0]
title=HJG MD-82SF Everts Air Cargo 2014
sim=MD-82SF
model=freighter02
panel=
sound=
texture=everts_air_cargo_2013_82sf_n73444
kb_checklists=
atc_id=N73444
atc_airline=EVERTS
atc_flight_number=821
atc_heavy=0
ui_manufacturer=McDonnell Douglas
ui_type=MD-82SF
ui_variation=Everts Air Cargo (2014)
ui_typerole=Commercial Airliner
ui_createdby=Historic Jetliners Group
description=HJG MD-82SF v1.0 repaint by Tony MADGE. 3D model editing by Nick BOTAMER & Paul HAAK
[fltsim.1] // Change "xx" to next number in sequence starting from 0
title=MD-82SF Aeronaves TSM (basic livery) 2015
sim=MD-82SF
model=freighter02
panel=
sound=
texture=aeronaves_tsm_2015_82sf_xa-utx
kb_checklists=
kb_reference=
atc_id=XA-UTX
atc_airline=AERONAVES
atc_flight_number=820
atc_heavy=0
atc_parking_codes=VTM
atc_parking_types=CARGO
ui_manufacturer=McDonnell Douglas
ui_type=MD-82SF
ui_variation=Aeronaves TSM - basic livery (2015)
ui_typerole=Commercial Airliner
ui_createdby=Historic Jetliners Group
description=HJG MD-81 v1.1 repaint by Erik INGRAM
[GENERAL]
atc_type=MCDONNELDOUGLAS
atc_model=MD80
Editable=0
performance=Maximum Ramp Weight: 150,500 lb / 68,409 kg\nMaximum Takeoff Weight: 149,500 lb / 67,954 kg\nMaximum Landing Weight: 130,000 lb / 59,090 kg\nMaximum Zero Fuel Weight: 122,000 lb / 55,4545 kg\nOperating Empty Weight: 75,400 lb / 34,201 kg\nMaximum Payload: 46,600 lb / 21,137 kg\n
[VIEWS]
eyepoint = 52.70,-1.887,5.255 //cockpit View Viewpoint
[FORCEFEEDBACK]
stick_shaker_magnitude = 0
stick_shaker_direction = 0
stick_shaker_period = 0
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.2
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[FLIGHT_TUNING]
elevator_effectiveness =1.0
aileron_effectiveness =1.0
rudder_effectiveness =1.1
elevator_trim_effectiveness =0.90
aileron_trim_effectiveness =1.0
rudder_trim_effectiveness =1.0
pitch_stability =1.50
roll_stability =1.0
yaw_stability =1.1
cruise_lift_scalar =1.30
parasite_drag_scalar =1.0
induced_drag_scalar =1.0
[WEIGHT_AND_BALANCE]
max_gross_weight = 150500
empty_weight = 75400
reference_datum_position = 6.0,
Md82
//HJG MD-82 V1.1
//FS2004
//NOVEMBER 24TH 2011
[fltsim.0]
title=HJG MD-83 Alaska Airlines '2008'
sim=MD-83
model=02
panel=
sound=
texture=as_2008_83_n972as
kb_checklists=
kb_reference=
atc_id=N972AS
atc_airline=ALASKA
atc_flight_number=732
atc_heavy=0
ui_manufacturer=McDonnell Douglas
ui_type=MD-83
ui_variation=Alaska Airlines '2008'
description=HJG MD-80 v1
[fltsim.1]
TITLE=HJG MD-83 TWA 1998
SIM=MD-80
MODEL=02
PANEL=
SOUND=
TEXTURE=hjg_md83_twa_n9627r_1998
KB_CHECKLISTS=
KB_REFERENCE=
ATC_ID=N9627R
ATC_AIRLINE=TWA
ATC_FLIGHT_NUMBER=034
ATC_HEAVY=0
UI_MANUFACTURER=MCDONNELL DOUGLAS
UI_TYPE=MD-83
UI_VARIATION=TWA 1998
DESCRIPTION=HJG MD-80
[GENERAL]
atc_type=MCDONNELDOUGLAS
atc_model=MD80
Editable=0
performance=Maximum Ramp Weight: 150,500 lb / 68,409 kg\nMaximum Takeoff Weight: 149,500 lb / 67,954 kg\nMaximum Landing Weight: 130,000 lb / 59,090 kg\nMaximum Zero Fuel Weight: 122,000 lb / 55,4545 kg\nOperating Empty Weight: 78,564 lb / 35,710 kg\nMaximum Payload: 41,458 lb / 18,844 kg\n
[VIEWS]
eyepoint = 52.70,-1.887,5.255 //cockpit View Viewpoint
[FORCEFEEDBACK]
stick_shaker_magnitude = 0
stick_shaker_direction = 0
stick_shaker_period = 0
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.2
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[FLIGHT_TUNING]
elevator_effectiveness =1.0
aileron_effectiveness =1.0
rudder_effectiveness =1.1
elevator_trim_effectiveness =0.90
aileron_trim_effectiveness =1.0
rudder_trim_effectiveness =1.0
pitch_stability =1.50
roll_stability =1.0
yaw_stability =1.1
cruise_lift_scalar =1.4
parasite_drag_scalar =1.0
induced_drag_scalar =1.0
[WEIGHT_AND_BALANCE]
max_gross_weight = 149500
empty_weight = 78000
reference_datum_position = 6.0, 0.0, 0.0
empty_weight_CG_position = -3.0, 0.0, 0.0
empty_weight_pitch_MOI = 3661351.0
empty_weight_roll_MOI = 822918.0
empty_weight_yaw_MOI = 3924730.0
empty_weight_coupled_MOI = 0.0
max_number_of_stations = 20
station_load.0 = " 380, 52.70, 0.0, 0.0, Pilot (2)"
station_load.1 = " 190, 50.25, 0.0, 0.0, Observer (1)"
station_load.2 = " 380, 42.60, 0.0, 0.0, F/A (2)"
station_load.3 = " 190, -30.00, 0.0, 0.0, F/A (1)"
station_load.4 = " 380, -40.00, 0.0, 0.0, F/A (2)"
station_load.5 = "3040, 33.70, 0.0, 0.0, First (16)"
station_load.6 = "5700, 23.16, 0.0, 0.0, Coach A(30)"
station_load.7 = "5700, 9.50, 0.0, 0.0, Coach B(30)"
station_load.8 = "5700, -4.20, 0.0, 0.0, Coach C(30)"
station_load.9 = "4750, -17.40, 0.0, 0.0, Coach D(25)"
station_load.10 = "3420, -31.60, 0.0, 0.0, Coach E(18)"
station_load.11 = "2660, 31.70, 0.0, 0.0, Fwd Cargo"
station_load.12 = "2660, 9.30. 0.0, 0.0, Mid Cargo"
station_load.13 = "2660, -31.70, 0.0, 0.0, Aft Cargo"
[FUEL]
Center1 = -1.67, 0.0, 0.00, 3074.0, 10.7
LeftMain = -7.25, -18.0, 0.00, 1383.0, 7.7
RightMain = -7.25, 18.0, 0.00, 1383.0, 7.7
fuel_type = 2.00
number_of_tank_selectors = 1
electric_pump = 0
[GENERALENGINEDATA]
engine_type = 1
Engine.0 = -48.800, -8.000, 2.680
Engine.1 = -48.800, 8.000, 2.680
fuel_flow_scalar = 0.9120
min_throttle_limit = -0.49
[TURBINEENGINEDATA]
fuel_flow_gain = 0.00300
inlet_area = 26.7
rated_N2_rpm = 29920
static_thrust = 20000
afterburner_available = 0
reverser_available = 1
[JET_ENGINE]
thrust_scalar =1.0
[AIRPLANE_GEOMETRY]
wing_area = 1209.0
wing_span = 107.8
wing_root_chord = 21.3
wing_dihedral = 3.0
wing_incidence = 1.0
wing_twist = -0.5
oswald_efficiency_factor = 0.80
wing_winglets_flag = 0
wing_sweep = 24
wing_pos_apex_lon = 9.575
wing_pos_apex_vert = 0.0
htail_area = 275.6
htail_span = 36.85
htail_pos_lon = -55.22
htail_pos_vert = 20.00
htail_incidence = 0
htail_sweep = 36
vtail_area = 161
vtail_span = 14
vtail_sweep = 44
vtail_pos_lon = -44.30
vtail_pos_vert = 8.570
elevator_area = 95.8
aileron_area = 38.0
rudder_area = 65.3
elevator_up_limit = 22.5
elevator_down_limit = 19.5
aileron_up_limit = 20.0
aileron_down_limit = 20.0
rudder_limit = 26.0
elevator_trim_limit = 12.0
spoiler_limit = 45
spoilerons_available = 1
aileron_to_spoileron_gain = 2
min_ailerons_for_spoilerons = 10
min_flaps_for_spoilerons = 0
[REFERENCE SPEEDS]
flaps_up_stall_speed = 130
full_flaps_stall_speed = 110
cruise_speed = 467
max_indicated_speed = 350
max_mach = 0.84
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[CONTACT_POINTS]
// Gear 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
point.0 = 1, 57.000, 0.000, -7.350, 2500.0, 0, 1.08, 55.0, 1.20, 1.30, 0.66, 15.00, 8.00, 0, 250.0, 300.0
point.1 = 1, -15.250, -8.350, -8.350, 2500.0, 1, 1.75, 0.0, 0.75, 1.50, 0.70, 15.00, 8.00, 2, 250.0, 300.0
point.2 = 1, -15.250, 8.350, -8.350, 2500.0, 2, 1.75, 0.0, 0.75, 1.50, 0.70, 15.00, 8.00, 3, 250.0, 300.0
// Scrapes 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
point.3 = 2, 57.200, 0.000, 0.000, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.4 = 2, 52.700, 0.000, -3.000, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.5 = 2, 0.000, 0.000, -3.250, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.6 = 2, -38.800, 0.000, -2.250, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.7 = 2, -57.550, 0.000, 5.250, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.8 = 2, -18.750, -43.750, 0.400, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 5, 0,0, 0.0
point.9 = 2, -18.750, 43.750, 0.400, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 6, 0,0, 0.0
// LL 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
point.10 = 5, -18.590, -43.151, 0.475, 2500.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 4.00, 4.00, 0, 350.0, 400.0
point.11 = 5, -18.590, 43.151, 0.475, 2500.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 4.00, 4.00, 0, 350.0, 400.0
max_number_of_points = 15
static_pitch = -0.35
static_cg_height = 7.5
gear_system_type = 1
[FLAPS.0]
type = 2
span-outboard = 0.96
extending-time = 15
flaps-position.0 = 0
flaps-position.1 = 1
flaps-position.2 = 1
flaps-position.3 = 1
flaps-position.4 = 1
flaps-position.5 = 1
damaging-speed = 300
blowout-speed = 350
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar = 1.0
system_type = 1
[FLAPS.1]
type = 1
span-outboard = 0.60
extending-time = 30
flaps-position.0 = 0
flaps-position.1 = 1
flaps-position.2 = 5
flaps-position.3 = 15
flaps-position.4 = 25
flaps-position.5 = 40
damaging-speed = 300
blowout-speed = 350
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar = 1.0
system_type = 1
[ELECTRICAL]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 65
electric_always_available = 0
flap_motor = 0, 5, 17.0
gear_motor = 0, 5, 17.0
autopilot = 0, 5, 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5, 17.0
pitot_heat = 0, 2, 17.0
additional_system = 0, 20, 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
starter2 = 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
standby_vacuum = 0, 5, 17.0
hydraulic_pump = 0, 2, 17.0
fuel_transfer_pump = 0, 5, 17.0
light_recognition = 0, 5, 17.0
light_wing = 0, 5, 17.0
light_logo = 0, 5, 17.0
[PITOT STATIC]
vertical_speed_time_constant = 1
[EXITS]
number_of_exits = 2
exit_rate.0 = 0.25
exit_rate.1 = 0.15
[KEYBOARD_RESPONSE]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[DIRECTION_INDICATORS]
direction_indicator.0 = 3,0
[AUTOPILOT]
autopilot_available =1
flight_director_available =1
default_vertical_speed =0.00
autothrottle_available =1
autothrottle_arming_required =1
autothrottle_takeoff_ga =1
autothrottle_max_rpm =95
pitch_takeoff_ga =8
use_no_default_pitch =1
use_no_default_bank =1
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 =20
max_bank_acceleration =1.8
max_bank_velocity =3
max_throttle_rate =0.1
nav_proportional_control =15
nav_integrator_control =0.1
nav_integrator_boundary =3.5
nav_derivative_control =0.03
nav_derivative_boundary =0.35
gs_proportional_control =15
gs_integrator_control =0.3
gs_derivative_control =0
gs_integrator_boundary =0.7
gs_derivative_boundary =0
yaw_damper_gain =1
[RADIOS]
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
[EFFECTS]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 =3, -24.437000, -52.439000, 0.661000, fx_navredm
light.1 =3, -24.681000, -52.556000, 0.661000, fx_navredm
light.2 =3, -28.713000, -52.864000, 0.637000, fx_navwhih
light.3 =2, -24.927000, -52.745000, 0.661000, fx_strobeh
light.4 =2, -28.778000, -52.739000, 0.637000, fx_strobeh
light.5 =3, -24.437000, 52.439000, 0.661000, fx_navgrem
light.6 =3, -24.681000, 52.556000, 0.661000, fx_navgrem
light.7 =3, -28.713000, 52.864000, 0.637000, fx_navwhih
light.8 =2, -24.927000, 52.745000, 0.661000, fx_strobeh
light.9 =2, -28.778000, 52.739000, 0.637000, fx_strobeh
light.10 =1, -6.250000, 0.379000, 8.575000, fx_beaconb
light.11 =1, -15.982000, 0.375000, -4.083000, fx_beaconh
light.12 =4, 58.598000, -1.875000, 4.000000, fx_vclight
light.13 =4, 58.598000, 1.875000, 4.000000, fx_vclight
[TAILHOOK]
tailhook_length = 1
tailhook_position = 0,0,0
cable_force_adjust = 0.00001
[FOLDING_WINGS]
wing_fold_system_type = 4
fold_rates = 0.25, 0.25
[brakes]
toe_brakes_scale=1.00
parking_brake=1
[gear_warning_system]
gear_warning_available = 1
pct_throttle_limit = 0.10
flap_limit_power = 25.0
flap_limit_idle = 15.0
[hydraulic_system]
electric_pumps = 1
engine_map = 1,1,0,0
normal_pressure = 3000.0
[stall_warning]
type = 1
[attitude_indicators]
attitude_indicator.0 = 1
[turn_indicators]
turn_indicator.0 = 1,0
[SMOKESYSTEM]
smoke.0= 2.4, -41.9, -8.4, fx_hjg_dc9_smoke.fx
smoke.1= 2.4, -41.9, 8.4, fx_hjg_dc9_smoke.fx
[deice_system]
structural_deice_type = 1
[vacuum_system]
max_pressure = 5.15
vacuum_type = 2
[pneumatic_system]
max_pressure = 18.0
bleed_air_scalar = 1.0
MD83:
//HJG MD-83 V1.1
//FS2004
//NOVEMBER 24TH 2011
[fltsim.0]
title=HJG MD-83 Alaska Airlines '2008'
sim=MD-83
model=02
panel=
sound=
texture=as_2008_83_n972as
kb_checklists=
kb_reference=
atc_id=N972AS
atc_airline=ALASKA
atc_flight_number=732
atc_heavy=0
ui_manufacturer=McDonnell Douglas
ui_type=MD-83
ui_variation=Alaska Airlines '2008'
description=HJG MD-80 v1
[fltsim.1]
TITLE=HJG MD-83 TWA 1998
SIM=MD-80
MODEL=02
PANEL=
SOUND=
TEXTURE=hjg_md83_twa_n9627r_1998
KB_CHECKLISTS=
KB_REFERENCE=
ATC_ID=N9627R
ATC_AIRLINE=TWA
ATC_FLIGHT_NUMBER=034
ATC_HEAVY=0
UI_MANUFACTURER=MCDONNELL DOUGLAS
UI_TYPE=MD-83
UI_VARIATION=TWA 1998
DESCRIPTION=HJG MD-80
[fltsim.2]
title=HJG MD-83 Jetsgo 2005
sim=MD-80
model=02
panel=
sound=
texture=hjg_md83_jetsgo_c-fkly_2005
kb_checklists=
kb_reference=
atc_id=C-FKLY
atc_airline=JETSGO
atc_flight_number=732
atc_heavy=0
ui_manufacturer=McDonnell Douglas
ui_type=MD-81
ui_variation=Jetsgo 2005
description=HJG MD-83
[GENERAL]
atc_type=MCDONNELDOUGLAS
atc_model=MD80
Editable=0
performance=Maximum Ramp Weight: 161,000 lb / 73,181 kg\nMaximum Takeoff Weight: 160,000 lb / 72,727 kg\nMaximum Landing Weight: 139,500 lb / 64,409 kg\nMaximum Zero Fuel Weight: 122,000 lb / 55,454 kg\nOperating Empty Weight: 89,000 lb / 40,454 kg\nMaximum Payload: 41,280 lb / 18,763 kg\n
[VIEWS]
eyepoint = 52.70,-1.887,5.255 //cockpit View Viewpoint
[FORCEFEEDBACK]
stick_shaker_magnitude = 0
stick_shaker_direction = 0
stick_shaker_period = 0
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 35500
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.2
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 1000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
[FLIGHT_TUNING]
elevator_effectiveness =1.0
aileron_effectiveness =1.0
rudder_effectiveness =1.1
elevator_trim_effectiveness =0.90
aileron_trim_effectiveness =1.0
rudder_trim_effectiveness =1.0
pitch_stability =1.50
roll_stability =1.0
yaw_stability =1.1
cruise_lift_scalar =1.4
parasite_drag_scalar =1.0
induced_drag_scalar =1.0
[WEIGHT_AND_BALANCE]
max_gross_weight = 160000
empty_weight = 79700
reference_datum_position = 6.0, 0.0, 0.0
empty_weight_CG_position = -3.0, 0.0, 0.0
empty_weight_pitch_MOI = 3716883.0
empty_weight_roll_MOI = 845419.0
empty_weight_yaw_MOI = 4014369.0
empty_weight_coupled_MOI = 0.0
max_number_of_stations = 20
station_load.0 = " 380, 52.70, 0.0, 0.0, Pilot (2)"
station_load.1 = " 190, 50.25, 0.0, 0.0, Observer (1)"
station_load.2 = " 380, 42.60, 0.0, 0.0, F/A (2)"
station_load.3 = " 190, -30.00, 0.0, 0.0, F/A (1)"
station_load.4 = " 380, -40.00, 0.0, 0.0, F/A (2)"
station_load.5 = "3040, 33.70, 0.0, 0.0, First (16)"
station_load.6 = "5700, 23.16, 0.0, 0.0, Coach A(30)"
station_load.7 = "5700, 9.50, 0.0, 0.0, Coach B(30)"
station_load.8 = "5700, -4.20, 0.0, 0.0, Coach C(30)"
station_load.9 = "4750, -17.40, 0.0, 0.0, Coach D(25)"
station_load.10 = "3420, -31.60, 0.0, 0.0, Coach E(18)"
station_load.11 = "4826, 31.70, 0.0, 0.0, Fwd Cargo"
station_load.12 = "4826, 9.30, 0.0, 0.0, Mid Cargo"
station_load.13 = "4826, -31.70, 0.0, 0.0, Aft Cargo"
[FUEL]
Center1 = -1.67, 0.0, 0.00, 3457.0, 10.7
LeftMain = -7.25, -18.0, 0.00, 1766.0, 7.7
RightMain = -7.25, 18.0, 0.00, 1766.0, 7.7
fuel_type = 2.00
number_of_tank_selectors = 1
electric_pump = 0
[GENERALENGINEDATA]
engine_type = 1
Engine.0 = -48.800, -8.000, 2.680
Engine.1 = -48.800, 8.000, 2.680
fuel_flow_scalar = 0.9120
min_throttle_limit = -0.49
[TURBINEENGINEDATA]
fuel_flow_gain = 0.00300
inlet_area = 26.7
rated_N2_rpm = 29920
static_thrust = 21000
afterburner_available = 0
reverser_available = 1
[JET_ENGINE]
thrust_scalar =1.0
[AIRPLANE_GEOMETRY]
wing_area = 1209.0
wing_span = 107.8
wing_root_chord = 21.3
wing_dihedral = 3.0
wing_incidence = 1.0
wing_twist = -0.5
oswald_efficiency_factor = 0.80
wing_winglets_flag = 0
wing_sweep = 24
wing_pos_apex_lon = 9.575
wing_pos_apex_vert = 0.0
htail_area = 275.6
htail_span = 36.85
htail_pos_lon = -55.22
htail_pos_vert = 20.00
htail_incidence = 0
htail_sweep = 36
vtail_area = 161
vtail_span = 14
vtail_sweep = 44
vtail_pos_lon = -44.30
vtail_pos_vert = 8.570
elevator_area = 95.8
aileron_area = 38.0
rudder_area = 65.3
elevator_up_limit = 22.5
elevator_down_limit = 19.5
aileron_up_limit = 20.0
aileron_down_limit = 20.0
rudder_limit = 26.0
elevator_trim_limit = 12.0
spoiler_limit = 45
spoilerons_available = 1
aileron_to_spoileron_gain = 2
min_ailerons_for_spoilerons = 10
min_flaps_for_spoilerons = 0
[REFERENCE SPEEDS]
flaps_up_stall_speed = 130
full_flaps_stall_speed = 110
cruise_speed = 467
max_indicated_speed = 350
max_mach = 0.84
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[CONTACT_POINTS]
// Gear 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
point.0 = 1, 57.000, 0.000, -7.350, 2500.0, 0, 1.08, 55.0, 1.20, 1.30, 0.66, 15.00, 8.00, 0, 250.0, 300.0
point.1 = 1, -15.250, -8.350, -8.350, 2500.0, 1, 1.75, 0.0, 0.75, 1.50, 0.70, 15.00, 8.00, 2, 250.0, 300.0
point.2 = 1, -15.250, 8.350, -8.350, 2500.0, 2, 1.75, 0.0, 0.75, 1.50, 0.70, 15.00, 8.00, 3, 250.0, 300.0
// Scrapes 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
point.3 = 2, 57.200, 0.000, 0.000, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.4 = 2, 52.700, 0.000, -3.000, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.5 = 2, 0.000, 0.000, -3.250, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.6 = 2, -38.800, 0.000, -2.250, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.7 = 2, -57.550, 0.000, 5.250, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 4, 0,0, 0.0
point.8 = 2, -18.750, -43.750, 0.400, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 5, 0,0, 0.0
point.9 = 2, -18.750, 43.750, 0.400, 700.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.00, 0.00, 6, 0,0, 0.0
// LL 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15
point.10 = 5, -18.590, -43.151, 0.475, 2500.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 4.00, 4.00, 0, 350.0, 400.0
point.11 = 5, -18.590, 43.151, 0.475, 2500.0, 0, 0.00, 0.0, 0.00, 0.00, 0.00, 4.00, 4.00, 0, 350.0, 400.0
max_number_of_points = 15
static_pitch = -0.35
static_cg_height = 7.5
gear_system_type = 1
[FLAPS.0]
type = 2
span-outboard = 0.96
extending-time = 15
flaps-position.0 = 0
flaps-position.1 = 1
flaps-position.2 = 1
flaps-position.3 = 1
flaps-position.4 = 1
flaps-position.5 = 1
damaging-speed = 300
blowout-speed = 350
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar = 1.0
system_type = 1
[FLAPS.1]
type = 1
span-outboard = 0.60
extending-time = 30
flaps-position.0 = 0
flaps-position.1 = 1
flaps-position.2 = 5
flaps-position.3 = 15
flaps-position.4 = 25
flaps-position.5 = 40
damaging-speed = 300
blowout-speed = 350
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar = 1.0
system_type = 1
[ELECTRICAL]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 65
electric_always_available = 0
flap_motor = 0, 5, 17.0
gear_motor = 0, 5, 17.0
autopilot = 0, 5, 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5, 17.0
pitot_heat = 0, 2, 17.0
additional_system = 0, 20, 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
starter2 = 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
standby_vacuum = 0, 5, 17.0
hydraulic_pump = 0, 2, 17.0
fuel_transfer_pump = 0, 5, 17.0
light_recognition = 0, 5, 17.0
light_wing = 0, 5, 17.0
light_logo = 0, 5, 17.0
[PITOT STATIC]
vertical_speed_time_constant = 1
[EXITS]
number_of_exits = 2
exit_rate.0 = 0.25
exit_rate.1 = 0.15
[KEYBOARD_RESPONSE]
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[DIRECTION_INDICATORS]
direction_indicator.0 = 3,0
[AUTOPILOT]
autopilot_available =1
flight_director_available =1
default_vertical_speed =0.00
autothrottle_available =1
autothrottle_arming_required =1
autothrottle_takeoff_ga =1
autothrottle_max_rpm =95
pitch_takeoff_ga =8
use_no_default_pitch =1
use_no_default_bank =1
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 =20
max_bank_acceleration =1.8
max_bank_velocity =3
max_throttle_rate =0.1
nav_proportional_control =15
nav_integrator_control =0.1
nav_integrator_boundary =3.5
nav_derivative_control =0.03
nav_derivative_boundary =0.35
gs_proportional_control =15
gs_integrator_control =0.3
gs_derivative_control =0
gs_integrator_boundary =0.7
gs_derivative_boundary =0
yaw_damper_gain =1
[RADIOS]
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
[EFFECTS]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn, 1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 =3, -24.437000, -52.439000, 0.661000, fx_navredm
light.1 =3, -24.681000, -52.556000, 0.661000, fx_navredm
light.2 =3, -28.713000, -52.864000, 0.637000, fx_navwhih
light.3 =2, -24.927000, -52.745000, 0.661000, fx_strobeh
light.4 =2, -28.778000, -52.739000, 0.637000, fx_strobeh
light.5 =3, -24.437000, 52.439000, 0.661000, fx_navgrem
light.6 =3, -24.681000, 52.556000, 0.661000, fx_navgrem
light.7 =3, -28.713000, 52.864000, 0.637000, fx_navwhih
light.8 =2, -24.927000, 52.745000, 0.661000, fx_strobeh
light.9 =2, -28.778000, 52.739000, 0.637000, fx_strobeh
light.10 =1, -6.250000, 0.379000, 8.575000, fx_beaconb
light.11 =1, -15.982000, 0.375000, -4.083000, fx_beaconh
light.12 =4, 58.598000, -1.875000, 4.000000, fx_vclight
light.13 =4, 58.598000, 1.875000, 4.000000, fx_vclight
[TAILHOOK]
tailhook_length = 1
tailhook_position = 0,0,0
cable_force_adjust = 0.00001
[FOLDING_WINGS]
wing_fold_system_type = 4
fold_rates = 0.25, 0.25
[brakes]
toe_brakes_scale=1.00
parking_brake=1
[gear_warning_system]
gear_warning_available = 1
pct_throttle_limit = 0.10
flap_limit_power = 25.0
flap_limit_idle = 15.0
[hydraulic_system]
electric_pumps = 1
engine_map = 1,1,0,0
normal_pressure = 3000.0
[stall_warning]
type = 1
[attitude_indicators]
attitude_indicator.0 = 1
[turn_indicators]
turn_indicator.0 = 1,0
[SMOKESYSTEM]
smoke.0= 2.4, -41.9, -8.4, fx_hjg_dc9_smoke.fx
smoke.1= 2.4, -41.9, 8.4, fx_hjg_dc9_smoke.fx
[deice_system]
structural_deice_type = 1
[vacuum_system]
max_pressure = 5.15
vacuum_type = 2
[pneumatic_system]
max_pressure = 18.0
bleed_air_scalar = 1.0