// DHC-6 100er WHEELS V3.1 020308 Stefan Hoffmann
//Realistic PT6A engine and propeller modelling for v3.11 by John Loehr 

[FLTSIM.0]
title=Antonov An-28
sim=An28
model=
panel=
sound=
texture=AERO
kb_checklists=An28_check
kb_reference=
atc_id=0210
ui_manufacturer="Antonov"
ui_type="An-28"
ui_variation="Aeroflot"
ui_typerole="Twin Engine TurboProp"
ui_createdby="RK"
description= The AN-28 was developed in 1960 in order to replace the old AN-2 for regional airlines. In 1978 the decision to transfer serial production to the Polish company PZL-MIELEC was taken. Most of the AN-28 fleet was supplied to the Soviet Union for use in the country’s northern and far eastern regions and Central Asia. Its short take-off and landing distance, rapid ascent and ability to operate in mountainous areas and low temperatures are some of the main basic characteristics of the AN-28. The aircraft is an ideal choice today, combining simple and safe navigation, powerful landing gear, autonomous engine ignition, reverse and effective navigation equipment, an anti-ice system for the wings, fins, engines and propellers and high lift devices, which make for low landing speeds to allow take-off and landing on airstrips up to 500 meters long. These unique characteristics and technical specifications of the AN-28 make it an invaluable and indispensable aircraft for use across Russia’s far-flung regions.
visual_damage=0
atc_heavy=0
atc_parking_types=RAMP,MIL_CARGO,MIL_COMBAT
atc_parking_codes=
prop_anim_ratio=-1.76

[FLTSIM.1]
title=Antonov An-28A Alrosa
sim=An28
model=
panel=
sound=
texture=ALR
kb_checklists=An28_check
kb_reference=
atc_id=0210
ui_manufacturer="Antonov"
ui_type="An-28B"
ui_variation="Alrosa"
ui_typerole="Twin Engine TurboProp"
ui_createdby="RK"
description= The AN-28 was developed in 1960 in order to replace the old AN-2 for regional airlines. In 1978 the decision to transfer serial production to the Polish company PZL-MIELEC was taken. Most of the AN-28 fleet was supplied to the Soviet Union for use in the country’s northern and far eastern regions and Central Asia. Its short take-off and landing distance, rapid ascent and ability to operate in mountainous areas and low temperatures are some of the main basic characteristics of the AN-28. The aircraft is an ideal choice today, combining simple and safe navigation, powerful landing gear, autonomous engine ignition, reverse and effective navigation equipment, an anti-ice system for the wings, fins, engines and propellers and high lift devices, which make for low landing speeds to allow take-off and landing on airstrips up to 500 meters long. These unique characteristics and technical specifications of the AN-28 make it an invaluable and indispensable aircraft for use across Russia’s far-flung regions.
visual_damage=0
atc_heavy=0
atc_parking_types=RAMP,MIL_CARGO,MIL_COMBAT
atc_parking_codes=
prop_anim_ratio=-1.76


[FLTSIM.2]
title=PZL An28 MARYNARKA RP
sim=An28
model=CIV
panel=
sound=
texture=NAV
kb_checklists=An28_check
kb_reference=
atc_id=0210
ui_manufacturer="PZL"
ui_type="An-28B Bryza"
ui_variation="Marynarka RP"
ui_typerole="Twin Engine TurboProp"
ui_createdby="RK"
description= The AN-28 was developed in 1960 in order to replace the old AN-2 for regional airlines. In 1978 the decision to transfer serial production to the Polish company PZL-MIELEC was taken. Most of the AN-28 fleet was supplied to the Soviet Union for use in the country’s northern and far eastern regions and Central Asia. Its short take-off and landing distance, rapid ascent and ability to operate in mountainous areas and low temperatures are some of the main basic characteristics of the AN-28. The aircraft is an ideal choice today, combining simple and safe navigation, powerful landing gear, autonomous engine ignition, reverse and effective navigation equipment, an anti-ice system for the wings, fins, engines and propellers and high lift devices, which make for low landing speeds to allow take-off and landing on airstrips up to 500 meters long. These unique characteristics and technical specifications of the AN-28 make it an invaluable and indispensable aircraft for use across Russia’s far-flung regions.
visual_damage=0
atc_heavy=0
atc_parking_types=RAMP,MIL_CARGO,MIL_COMBAT
atc_parking_codes=
prop_anim_ratio=-1.76

[FLTSIM.3]
title=PZL M28B Bryza-1R
sim=An28
model=ENG
panel=
sound=
texture=ENG
kb_checklists=An28_check
kb_reference=
atc_id=0210
ui_manufacturer="PZL"
ui_type="M28B"
ui_variation="Bryza-1R"
ui_typerole="Twin Engine TurboProp"
ui_createdby="RK"
description= The AN-28 was developed in 1960 in order to replace the old AN-2 for regional airlines. In 1978 the decision to transfer serial production to the Polish company PZL-MIELEC was taken. Most of the AN-28 fleet was supplied to the Soviet Union for use in the country’s northern and far eastern regions and Central Asia. Its short take-off and landing distance, rapid ascent and ability to operate in mountainous areas and low temperatures are some of the main basic characteristics of the AN-28. The aircraft is an ideal choice today, combining simple and safe navigation, powerful landing gear, autonomous engine ignition, reverse and effective navigation equipment, an anti-ice system for the wings, fins, engines and propellers and high lift devices, which make for low landing speeds to allow take-off and landing on airstrips up to 500 meters long. These unique characteristics and technical specifications of the AN-28 make it an invaluable and indispensable aircraft for use across Russia’s far-flung regions.
visual_damage=0
atc_heavy=0
atc_parking_types=RAMP,MIL_CARGO,MIL_COMBAT
atc_parking_codes=
prop_anim_ratio=-1.76

[FLTSIM.4]
title=PZL An28 BLUE WING
sim=An28
model=CIV
panel=
sound=
texture=BLW
kb_checklists=An28_check
kb_reference=
atc_id=0074
ui_manufacturer="PZL"
ui_type="An-28"
ui_variation="Blue Wing"
ui_typerole="Twin Engine TurboProp"
ui_createdby="RK"
description= The AN-28 was developed in 1960 in order to replace the old AN-2 for regional airlines. In 1978 the decision to transfer serial production to the Polish company PZL-MIELEC was taken. Most of the AN-28 fleet was supplied to the Soviet Union for use in the country’s northern and far eastern regions and Central Asia. Its short take-off and landing distance, rapid ascent and ability to operate in mountainous areas and low temperatures are some of the main basic characteristics of the AN-28. The aircraft is an ideal choice today, combining simple and safe navigation, powerful landing gear, autonomous engine ignition, reverse and effective navigation equipment, an anti-ice system for the wings, fins, engines and propellers and high lift devices, which make for low landing speeds to allow take-off and landing on airstrips up to 500 meters long. These unique characteristics and technical specifications of the AN-28 make it an invaluable and indispensable aircraft for use across Russia’s far-flung regions.
visual_damage=0
atc_heavy=0
atc_parking_types=RAMP,MIL_CARGO,MIL_COMBAT
atc_parking_codes=
prop_anim_ratio=-1.76


[FLTSIM.5]
title=PZL An28 SKYDIVE
sim=An28
model=CIV
panel=
sound=
texture=SKY
kb_checklists=An28_check
kb_reference=
atc_id=0074
ui_manufacturer="PZL"
ui_type="An-28"
ui_variation="Sky Dive"
ui_typerole="Twin Engine TurboProp"
ui_createdby="RK"
description= The AN-28 was developed in 1960 in order to replace the old AN-2 for regional airlines. In 1978 the decision to transfer serial production to the Polish company PZL-MIELEC was taken. Most of the AN-28 fleet was supplied to the Soviet Union for use in the country’s northern and far eastern regions and Central Asia. Its short take-off and landing distance, rapid ascent and ability to operate in mountainous areas and low temperatures are some of the main basic characteristics of the AN-28. The aircraft is an ideal choice today, combining simple and safe navigation, powerful landing gear, autonomous engine ignition, reverse and effective navigation equipment, an anti-ice system for the wings, fins, engines and propellers and high lift devices, which make for low landing speeds to allow take-off and landing on airstrips up to 500 meters long. These unique characteristics and technical specifications of the AN-28 make it an invaluable and indispensable aircraft for use across Russia’s far-flung regions.
visual_damage=0
atc_heavy=0
atc_parking_types=RAMP,MIL_CARGO,MIL_COMBAT
atc_parking_codes=
prop_anim_ratio=-1.76

[FLTSIM.6]
title=PZL An28 DIJBUTI AIR FORCES
sim=An28
model=CIV
panel=
sound=
texture=DIJ
kb_checklists=An28_check
kb_reference=
atc_id=0074
ui_manufacturer="PZL"
ui_type="An-28"
ui_variation="DIJBUTI AIR FORCES"
ui_typerole="Twin Engine TurboProp"
ui_createdby="RK"
description= The AN-28 was developed in 1960 in order to replace the old AN-2 for regional airlines. In 1978 the decision to transfer serial production to the Polish company PZL-MIELEC was taken. Most of the AN-28 fleet was supplied to the Soviet Union for use in the country’s northern and far eastern regions and Central Asia. Its short take-off and landing distance, rapid ascent and ability to operate in mountainous areas and low temperatures are some of the main basic characteristics of the AN-28. The aircraft is an ideal choice today, combining simple and safe navigation, powerful landing gear, autonomous engine ignition, reverse and effective navigation equipment, an anti-ice system for the wings, fins, engines and propellers and high lift devices, which make for low landing speeds to allow take-off and landing on airstrips up to 500 meters long. These unique characteristics and technical specifications of the AN-28 make it an invaluable and indispensable aircraft for use across Russia’s far-flung regions.
visual_damage=0
atc_heavy=0
atc_parking_types=RAMP,MIL_CARGO,MIL_COMBAT
atc_parking_codes=
prop_anim_ratio=-1.76


[FLTSIM.7]
title=PZL An28 PERU NAVAL AIR FORCES
sim=An28
model=CIV
panel=
sound=
texture=PER
kb_checklists=An28_check
kb_reference=
atc_id=0074
ui_manufacturer="PZL"
ui_type="An-28"
ui_variation="PERU ARMED FORCSE - BAT 811"
ui_typerole="Twin Engine TurboProp"
ui_createdby="RK"
description= The AN-28 was developed in 1960 in order to replace the old AN-2 for regional airlines. In 1978 the decision to transfer serial production to the Polish company PZL-MIELEC was taken. Most of the AN-28 fleet was supplied to the Soviet Union for use in the country’s northern and far eastern regions and Central Asia. Its short take-off and landing distance, rapid ascent and ability to operate in mountainous areas and low temperatures are some of the main basic characteristics of the AN-28. The aircraft is an ideal choice today, combining simple and safe navigation, powerful landing gear, autonomous engine ignition, reverse and effective navigation equipment, an anti-ice system for the wings, fins, engines and propellers and high lift devices, which make for low landing speeds to allow take-off and landing on airstrips up to 500 meters long. These unique characteristics and technical specifications of the AN-28 make it an invaluable and indispensable aircraft for use across Russia’s far-flung regions.
visual_damage=0
atc_heavy=0
atc_parking_types=RAMP,MIL_CARGO,MIL_COMBAT
atc_parking_codes=
prop_anim_ratio=-1.76


[FLTSIM.8]
title=PZL An28 GEORGIAN AIR FORCES
sim=An28
model=CIV
panel=
sound=
texture=GEO
kb_checklists=An28_check
kb_reference=
atc_id=0074
ui_manufacturer="PZL"
ui_type="An-28"
ui_variation="GEORGIAN AIR FORCES"
ui_typerole="Twin Engine TurboProp"
ui_createdby="RK"
description= The AN-28 was developed in 1960 in order to replace the old AN-2 for regional airlines. In 1978 the decision to transfer serial production to the Polish company PZL-MIELEC was taken. Most of the AN-28 fleet was supplied to the Soviet Union for use in the country’s northern and far eastern regions and Central Asia. Its short take-off and landing distance, rapid ascent and ability to operate in mountainous areas and low temperatures are some of the main basic characteristics of the AN-28. The aircraft is an ideal choice today, combining simple and safe navigation, powerful landing gear, autonomous engine ignition, reverse and effective navigation equipment, an anti-ice system for the wings, fins, engines and propellers and high lift devices, which make for low landing speeds to allow take-off and landing on airstrips up to 500 meters long. These unique characteristics and technical specifications of the AN-28 make it an invaluable and indispensable aircraft for use across Russia’s far-flung regions.
visual_damage=0
atc_heavy=0
atc_parking_types=RAMP,MIL_CARGO,MIL_COMBAT
atc_parking_codes=
prop_anim_ratio=-1.76



[GENERAL]
atc_type=Antonow
atc_model=An28
performance=Max cruise speed: 260 mph\nRange: 540-1460 nm\nCeiling: 28,000 ft\nMax weight: 13,000 lbs\nPassenger: 18
category=airplane

[PITOT STATIC]
vertical_speed_time_constant=2.0
pitot_heat=1.0

[CameraDefinition.0]
Title = "Right Wing"
Guid = {E8675708-99D3-11DC-8F84-EECB55D89593}
Description = 
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.9
ShowWeather = Yes
InitialXyz = 20.0, -1.45, -1.7
InitialPbh = 8, 0, 270
XyzAdjust = TRUE
Category=Aircraft
ClipMode=Minimum

[CameraDefinition.1]
Title = "Left Engine"
Guid = {ed46e426-b8a1-44e0-99ff-37f701a79fe9}
Description =
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.50
ShowWeather = Yes
InitialXyz = -4.0, -0.70, -1.8
InitialPbh = 4, 0, 15
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.2]
Title = "Tail"
Guid = {b2a70645-cc8b-420d-bd79-9bf8d6774cbe}
Description =
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 0, 1.55, -7.5
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum

[CameraDefinition.3]
Title = "Landing Gear"
Guid = {38daf937-ced1-4194-84a3-2dba888dc269}
Description = 
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz =  -1.5, -1.10, -4.3
InitialPbh =  10, 0, 2
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.4]
Title = "Nose"
Guid = {ea126881-0ec6-40cf-b3ef-7651a2a92af3}
Description = 
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .5
ShowWeather = Yes
InitialXyz = 0, 0.20, 9.2
InitialPbh = 12, 0, 180
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum

[CameraDefinition.5]
Title = "Front Gear"
Guid = {96bdbc9e-3437-4d4b-9167-32a5c6b2b851}
Description = 
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 0, -2.60, 0.7
InitialPbh = 0, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum

[CameraDefinition.001]
Title = "Right Seat"
Guid = {0456199A-99D4-11DC-B263-66CC55D89593}
Origin = Virtual Cockpit
MomentumEffect = Yes
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = 0.50
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz= -0.35, -0.2, 2.4
InitialPbh=6.1, 0.0, 0.0


[CameraDefinition.002]
Title = "Center Console"
Guid = {1A299EAE-99D4-11DC-B26D-B4CC55D89593}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.80
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz= 0.0, -0.4, 2.5
InitialPbh=15, 0, 0

[CameraDefinition.003]
Title = "Overhead Front"
Guid = {0879B67C-CA84-11DC-AE8E-093256D89593}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz= 0.2, -0.3, 2.2
InitialPbh= -45, 0, 0

[CameraDefinition.004]
Title = "Overhead Aft"
Guid = {882261FC-CA85-11DC-84AC-923B56D89593}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = None
SnapPbhReturn = False
PanPbhAdjust = None
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.60
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz= -0.2, -0.3, 2.2

InitialPbh= -45, 0, 0

[CameraDefinition.005]
Title = "To Cabin"
Guid = {AB2295CC-CA86-11DC-A56C-9B4056D89593}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.80
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.45, -0.3, 0.5
InitialPbh=5.0, 0.0, 180.0

[CameraDefinition.006]
Title = "From Cabin"
Guid = {78D5E1D6-CA87-11DC-9B4C-724856D89593}
Origin = Virtual Cockpit
MomentumEffect = No
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.80
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.45, -0.2, -5.0
InitialPbh=5.0, 0.0, 0.0

[WEIGHT_AND_BALANCE]
max_gross_weight=13450
empty_weight=8600
reference_datum_position     = 0.00, 0.00, 0.00
empty_weight_CG_position     = 0.00, 0.00, 0.00
max_number_of_stations=10
station_load.0 =150, 10.1, -1.4, -1.8 	// pilot              
station_load.1 =150, 10.1, 1.4, -1.8 	// co-pilot
station_load.2 =150, -1.6, 0.0, 0.1 	// front baggage
station_load.3 =450, 7.3, 0.0, -2.1 	// 3 seats of 1 row
station_load.4 =450, 4.8, 0.0, -2.1 	// 3 seats of 2 row
station_load.5 =450, 1.9, 0.0, -2.1 	// 3 seats of 3 row
station_load.6 =450, -1.1, 0.0, -2.1 	// 3 seats of 4 row
station_load.7 =450, -3.7, 0.0, -2.1 	// 3 seats of 5 row
station_load.8 =450, -5.8, 0.0, -2.1 	// 3 seats of 6 row
station_load.9 =150, -13.0, 0, -3.0 	// rear baggage
station_name.0 = "Pilot"           
station_name.1 = "Copilot" 
station_name.2 = "Front Baggage"
station_name.3 = "SEAT Row 1"
station_name.4 = "SEAT Row 2"
station_name.5 = "SEAT Row 3"
station_name.6 = "SEAT Row 4"
station_name.7 = "SEAT Row 5"
station_name.8 = "SEAT Row 6"
station_name.9 = "Rear Baggage"
empty_weight_pitch_moi=19240			//orig 19240.6 from specification (RK)
empty_weight_roll_moi=18960			//plus 5000 to beginning value
empty_weight_yaw_moi=53533			//plus 20000 to beginning value
empty_weight_coupled_moi=0.000000

[FUEL]
LeftMain  	= 0.00,-14.50, -1.00, 209.00, 4.60  	// (Gallons) equal 3832 lb useable fuel in total (RK)
RightMain 	= 0.00, 14.50, -1.00, 209.00, 4.60	// 
LeftAux 	= 0.00,-2.50, -1.00, 92.00, 2.10
RightAux	= 0.00, 2.50, -1.00, 92.00, 2.10
fuel_type = 2                                		//Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=1


[GENERALENGINEDATA]
engine_type	= 5
Engine.0	= 4.6, -8.7, 1.4
Engine.1	= 4.6, 8.7, 1.4
fuel_flow_scalar	= 1.0	//
 may be incorrect (RK)

min_throttle_limit	= -0.6	// 60% reverse thrust, orig app. 40% of full thrust (RK)	
max_contrail_temperature= -30	//by Pedro L. Mayorga
master_ignition_switch	= 2
starter_type	= 1 

[FLIGHT_TUNING]
cruise_lift_scalar 	= 1.35		//DHC6 data
parasite_drag_scalar	= 1.117		//DHC6 data
induced_drag_scalar	= 1.297		//DHC6 data
elevator_effectiveness	= 1.0		//may be incorrect (RK)
aileron_effectiveness   = 1.0		//may be incorrect (RK)
rudder_effectiveness    = 1.4		//may be incorrect (RK), improved due to dual tail
pitch_stability         = 1.4		//may be incorrect (RK)
roll_stability          = 1.0		//may be incorrect (RK)
yaw_stability           = 1.0		//may be incorrect (RK)
elevator_trim_effectiveness = 1.0	//may be incorrect (RK)
aileron_trim_effectiveness  = 1.0	//may be incorrect (RK)
rudder_trim_effectiveness   = 1.4	//may be incorrect (RK)

[PROPELLER]
thrust_scalar           = 1.0     	//may be incorrect (RK)      
propeller_type          = 0             
propeller_diameter      = 8.46          
propeller_blades        = 3             
propeller_moi           = 27.10       	//DHC6 data     
beta_max                = 45    	//DHC6 data        
beta_min                = 15.2          //DHC6 data  
min_gov_rpm             = 24700		//DHC6 data         
prop_tc                 = 0.001		//DHC6 data         
gear_reduction_ratio    = 14.96		//DHC6 data            
fixed_pitch_beta        = 0          	//may be incorrect (RK)  
low_speed_theory_limit  = 80      	//may be incorrect (RK)      
prop_sync_available     = 1             
prop_deice_available    = 1             
prop_feathering_available= 1            
prop_auto_feathering_available= 1    	   
min_rpm_for_feather     = 700         	//may be incorrect (RK)  
beta_feather            = 79.0     	//from documents       
power_absorbed_cf       = 0.93		//may be incorrect (RK)           
defeathering_accumulators_available= 0  
prop_reverse_available  = 1             
minimum_on_ground_beta  = 1.0            
minimum_reverse_beta    = -14.0         

[TURBINEENGINEDATA]
fuel_flow_gain          = 0.080   //DHC6 data 
inlet_area              = 0.6111   
rated_N2_rpm            = 32934  //26000 
static_thrust           = 123.0 //LBs, may be incorrect (RK)        
afterburner-available   = 0

[TURBOPROP_ENGINE]
power_scalar            = 1.00   
maximum_torque          = 1317		//DHC6 data 

[ELECTRICAL]
//BusType, MaxAmpLoad, MinVoltage      //BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)

flap_motor	= 0, 5, 35.0
gear_motor 	=
autopilot 	= 1, 2, 35.0
avionics_bus 	= 0, 7, 17.0
avionics 	= 1, 10, 17.0
pitot_heat 	= 0, 2, 25.0 
additional_system = 0, 8, 21.0
marker_beacon 	= 0, 1, 25.0
gear_warning 	= 2, 2, 24.0
fuel_pump 	= 0, 5, 20.0
starter1 	= 0, 10, 19.0 
starter2 	= 0, 10, 19.0 
light_nav 	= 0, 5, 21.0
light_beacon 	= 0, 5, 22.0
light_landing 	= 4, 8, 85.0
light_taxi 	= 4, 5, 80.0
light_strobe 	= 4, 5, 95.0
light_panel 	= 0, 2, 21.0
light_cabin 	= 0, 2, 22.0
prop_sync 	= 2, 5, 24.0
auto_feather 	= 4, 5, 100.0
auto_brakes=
standby_vacuum=
hydraulic_pump 	= 4, 5, 90.0
fuel_transfer_pump = 4, 5, 100.0
propeller_deice = 4, 10, 85.0
light_recognition=
light_wing=
light_logo=
directional_gyro = 4, 2, 100.0
directional_gyro_slaving 	= 4, 3, 95.0
max_battery_voltage = 27.0
generator_alternator_voltage = 115.0
max_generator_alternator_amps = 450.0
engine_generator_map= 1,1
electric_always_available = 0

[CONTACT_POINTS]
//        1     2      3      4      5   6   7     8   9     10   11   12   13   14   15  16
point.0 = 1,  12.7,   0.0 , -7.40, 1000, 0, 1.2,   45, 0.50, 2.0, 0.6, 0, 0, 0,  0,  250
point.1 = 1,  -2.5,  -6.7,  -8.28, 2000, 1, 2.25,  0,  1.0, 1.0, 0.6, 0, 0, 2,  0,  250
point.2 = 1,  -2.5,   6.7,  -8.28, 2000, 2, 2.25,  0,  1.0, 1.0, 0.6, 0, 0, 3,  0,  250
point.3 = 2, 0.11, -36.0, 2.1, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0		//left wing
point.4 = 2, 0.11, 36.0, 2.1, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0		//right wing
point.5 = 2,  18.5,   0.00, -3.5,  1000, 0, 0,     0,  0,     0,   0,   0,   0,   4,  0,  0 
point.6 = 2, -20.23, -8.60, -2.1, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0		//left tail
point.7 = 2, -20.23, 8.60, -2.1, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0		//right tail

max_number_of_points = 8
static_pitch = -1        
static_cg_height = 7.35     
gear_system_type=0        

[GEAR_WARNING_SYSTEM]
gear_warning_available = 0 

[BRAKES]
parking_brake = 1        
toe_brakes_scale = 0.8  
auto_brakes = 0
differential_braking_scale = 1
hydraulic_system_scalar = 1  //On brakes dependant on the hydraulic system, ratio hyd system to max brake hyd pressure

[HYDRAULIC_SYSTEM]
normal_pressure = 1000.0       //DHC6 data    
electric_pumps  = 0      
engine_map      = 1,1,0,0  

[VIEWS]

[VIEWS]
eyepoint= 8.5, -1.45, -1.3

[EXITS]
number_of_exits = 2
exit.0 = 0.3, -6.05,-3.01,-1.2, 0 	//1.open rate % per sec; 2.position; 3. 0-main, 1-cargo, 2-emerg
exit.0 = 0.2, -15.00,-2.28,-1.78, 1 	//1.open rate % per sec; 2.position; 3. 0-main, 1-cargo, 2-emerg

[FLAPS.0] 				//trailing edge flaps
system_type      = 1			//Hydraulic     
span-outboard    = 0.4
extending-time   = 12   
damaging-speed   = 170   
blowout-speed    = 190   
lift_scalar	 = 0
drag_scalar      = 0
pitch_scalar     = 0
flaps-position.0 = 0
flaps-position.1 = 15
flaps-position.2 = 25
flaps-position.3 = 40
type = 1                                         


[FLAPS.1] 				//leading edge flaps

system_type      = 1     		//Hydraulic
span-outboard    = 0.2
extending-time   = 12   
damaging-speed   = 185   
blowout-speed    = 200   
lift_scalar	 = 1.3
drag_scalar      = 0
pitch_scalar     = 1.0
flaps-position.0 = 0
flaps-position.1 = 7
flaps-position.2 = 16
type=2

[ATTITUDE_INDICATORS]
attitude_indicator.0 = 1

[DIRECTION_INDICATORS]
direction_indicator.0 = 1

[TURN_INDICATORS]
turn_indicator.0 = 1,0

[VACUUM_SYSTEM]
max_pressure=5.15 
vacuum_type=1 

[PNEUMATIC_SYSTEM]
max_pressure=18         //
bleed_air_scalar=1      

[PITOT_STATIC]
vertical_speed_time_constant = 1 
pitot_heat = 1.0

[EFFECTS]
water=fx_spray
wake = fx_wake
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
startup=Aerosoft_Twotter_Start
contrail=Aerosoft_Twotter_Smoke
SnowTrack=fx_snowtrack
WheelSnowSpray=fx_WheelSnowSpray
WheelWetSpray=fx_WheelWetSpray

[AIRPLANE_GEOMETRY]
wing_area                   = 427.5         //@ Square feet 420
wing_span                   = 71.18            //@ Feet 
wing_root_chord             = 6.1012           //@ Feet
wing_dihedral               = 0             //@ Degrees 
wing_incidence              = 4           //@ Degrees
wing_twist                  = 0             //@ Degrees
oswald_efficiency_factor    = 0.849754564666103          //@ Measure of lift effeciency of wing
wing_winglets_flag          = 0             //@ Are winglets available?
wing_sweep                  = 4             //@ Degrees, wing leading edge
wing_pos_apex_lon           = 1.148          //@ Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert          = 2.045           //@ Feet, vertical distance from reference point, positive going up
htail_area                  = 88.87          //@ Square feet
htail_span                  = 17.407          //@ Feet
htail_pos_lon               = -19.109         //@ Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert              = 2.3157             //@ Feet, vertical distance from reference point, positive going up
htail_incidence             = 5            //@ Degrees
htail_sweep                 = 15             //@ Degrees, horizontal tail leading edge
vtail_area                  = 67.94            //@ Square feet
vtail_span                  = 5.248          //@ 0Feet, tip to body
vtail_sweep                 = 30            //@ Degrees, vertical tail leading edge
vtail_pos_lon               = -21.67         //@ Feet, longitudinal distance from reference point, 
vtail_pos_vert              = 4.488             //@ Feet, vertical distance from reference point
elevator_area               = 32.47            //@ Square feet
aileron_area                = 41.45         //@ Square feet
rudder_area                 = 18.14            //@ Square feet
elevator_up_limit           = 27            //@ Degrees
elevator_down_limit         = 19            //@ Degrees
aileron_up_limit            = 22          //@ Degrees
aileron_down_limit          = 16.20            //@ Degrees
rudder_limit                = 22            //@ Degrees, 16 inboard
, 22 outboard 

elevator_trim_limit         = 25            //@ Degrees, 15 up, 25 down
spoiler_limit               = 60            //@ Degrees, inboard 45, outboard 60 deg
spoiler_extension_time      = 2            //@ Seconds, maybe incorrect
spoilerons_available        = 0
aileron_to_spoileron_gain   = 0.000000
min_ailerons_for_spoilerons = 0.000000
min_flaps_for_spoilerons    = 0.000000
auto_spoiler_available      = 1 
flap_to_aileron_scale	    = 0.5	
positive_g_limit_flaps_up   =  3.0               //Design G load tolerance (positive, flaps up)
positive_g_limit_flaps_down =  2.0               //Design G load tolerance (positive, flaps down) 
negative_g_limit_flaps_up   = -2.0               //Design G load tolerance (negative, flaps up) 
negative_g_limit_flaps_down = -1.0               //Design G load tolerance (negative, flaps down) 
spoiler_handle_available 	= 1
fly_by_wire = 0
load_safety_factor          =  1.5               //Design G load safety factor 

[REFERENCE SPEEDS]
flaps_up_stall_speed    = 66
full_flaps_stall_speed  = 60
cruise_speed            = 147
max_mach                = 0.40
max_indicated_speed     = 205		//slightly improved (RK)

[AUTOPILOT]
autopilot_available= 1
flight_director_available= 0
default_vertical_speed= 750
autothrottle_available= 0
pitch_takeoff_ga=8
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=27000
max_bank=25
max_bank_acceleration=1.8
max_bank_velocity=3
max_throttle_rate=0.10
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

[FORCEFEEDBACK]
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111
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      
 
[LIGHTS]
light.0 = 3,  -1.4,  -35.3,  1.8,  fx_navredm ,
light.1 = 2,  -1.4,  -35.3,  1.8,  fx_strobeh ,
light.2 = 3,  -1.4,   35.3,  1.8,  fx_navgrem ,
light.3 = 2,  -1.4,   35.3,  1.8,  fx_strobeh ,
light.4 = 4,    2.50,  0.0,  -1.64, Aerosoft_Twotter_VC_Cabin,
light.5 = 4,    7.00,  0.0,  -2.0, Aerosoft_Twotter_VC_Cabin,
light.6 = 4,    8.00,  1.7,  -2.0, Aerosoft_Twotter_VC_Cabin,
light.7 = 4,   8.00,  -1.7,  -2.0, Aerosoft_Twotter_VC_Cabin,
//light.8 = 4,   -6.50,  0.0,  -1.64, fx_navredm,
//light.9 = 4,   -1.50,  0.0,  -1.64, fx_navredm,


[STALL_WARNING]
type=1
stick_shaker=1

[DEICE_SYSTEM]
structural_deice_type=2  

[RADIOS] 
Audio.1 = 1 
Com.1 = 1, 0 
Com.2 = 1, 0 
Nav.1 = 1, 0, 1 
Nav.2 = 1, 0, 1 
Adf.1 = 1 
Adf.2 = 1 
Transponder.1 = 1 
Marker.1 = 1

[keyboard_response]
elevator=170.0,220.0
aileron=170.0,220.0
rudder=170.0,220.0