[fltsim.0]
title=Vista Liners B-737-200 Canadian north 737-200
sim=7372
model=
panel=
sound=
texture=canadian north
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_type=Boeing
atc_id_enable=1
atc_id=G-GCKP
atc_id_color=0xffffffff
editable=0
visual_damage=1
ui_manufacturer=Boeing
ui_type=737-200
ui_variation=Canadian North
description=Vista Liners 737-200, Repaint by Tatit Kisyaprakasa
atc_airline=Canadian North
[General]
atc_type=Boeing
atc_model=B732
editable=0
performance=FDE by Mike Baumann (2004) with Philip Foglar's modified landing gear contact points\n\nEngine's type: P & W JT8D-15\nStatic T/O Thrust (per engine) 15500 lb.\nMax. range 2600 nm LRC\nMax. T/O weight 128100 lbs\nCruising altitude 31 - 35000 ft Mach 0.73-0.78\nFuel weight set at 5160 US Gal 34572 lbs (no aux tanks applied)\nCruising speed 483 knots TAS\nMax. structural payload 29700 lbs\nMax landing weight 107000 lbs\nPassenger config set at 130 Pax single class, 6 crew (2 flight 4 cabin) baggage for 136
[forcefeedback]
gear_bump_nose_magnitude= 5000
gear_bump_nose_direction= 18000
gear_bump_nose_duration= 250000
gear_bump_left_magnitude= 4000
gear_bump_left_direction= 35500
gear_bump_left_duration= 250000
gear_bump_right_magnitude= 4000
gear_bump_right_direction= 00500
gear_bump_right_duration= 250000
ground_bumps_magnitude1= 2000
ground_bumps_angle1= 09000
ground_bumps_intercept1= 3.0
ground_bumps_slope1= 0.20
ground_bumps_magnitude2= 500
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
[flight_tuning]
elevator_effectiveness= 1.00
aileron_effectiveness= 1.00
rudder_effectiveness= 1.00
elevator_trim_effectiveness= 1.00
aileron_trim_effectiveness= 1.00
rudder_trim_effectiveness= 1.00
pitch_stability= 1.20
roll_stability= 1.20
yaw_stability= 1.20
cruise_lift_scalar= 1.00
parasite_drag_scalar= 1.80
induced_drag_scalar= 1.05
[WEIGHT_AND_BALANCE]
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= "450, 43.50, 0.00, 4.50,FlghtCrew x2"
station_load.1= "500, 38.00, 2.00, 5.00,Fwd Galley"
station_load.2= "250, 37.00,-2.00, 4.50,FCbnCrew x 2"
station_load.3= "6000, 25.00, 0.00, 4.50,FrwdPas x 41"
station_load.4= "2000, 22.00, 0.00,-1.00,FCrgBge x 46"
station_load.5= "7000, 2.00, 0.00, 4.50,MidPass x 42"
station_load.6= "4000,-18.00, 0.00,-1.00,ACrgBge x 90"
station_load.7= "7500,-20.00, 0.00, 4.50,AftPass x 47"
station_load.8= "250, -30.50,-2.00, 4.50,ACbnCrew x 2"
station_load.9= "700, -34.00, 2.00, 5.00,Aft Galley"
empty_weight= 65300
empty_weight_roll_MOI= 1401400
empty_weight_pitch_MOI= 1580000
empty_weight_yaw_MOI= 1500000
empty_weight_coupled_MOI= 0
max_gross_weight= 128600
[GeneralEngineData]
engine_type=1
Engine.0=-3.00,-17.00,-2.50
Engine.1=-3.00, 17.00,-2.50
fuel_flow_scalar=1.00
min_throttle_limit=-0.399902
[TurbineEngineData]
fuel_flow_gain= 0.003
inlet_area= 8.9462
rated_N2_rpm= 12250
static_thrust= 15500
afterburner_available= 0
reverser_available= 1
[jet_engine]
thrust_scalar = 0.95
[airplane_geometry]
wing_area= 980.00
wing_span= 93.00
wing_root_chord= 19.80
wing_dihedral= 6.00
wing_incidence= 1.00
wing_twist= 0.80
oswald_efficiency_factor= 0.88
wing_winglets_flag= 0
wing_sweep= 25.00
wing_pos_apex_lon= 14.50
wing_pos_apex_vert= 0.00
htail_area= 408.00
htail_span= 36.00
htail_pos_lon= -39.50
htail_pos_vert= 7.25
htail_dihedral= 7.00
htail_incidence= 1.00
htail_sweep= 30.00
vtail_area= 405.00
vtail_span= 19.91
vtail_sweep= 35.00
vtail_pos_lon= -30.55
vtail_pos_vert= 10.30
elevator_area= 70.50
aileron_area= 26.80
rudder_area= 56.20
elevator_up_limit= 26.10
elevator_down_limit= 26.10
aileron_up_limit= 19.00
aileron_down_limit= 19.00
rudder_limit= 23.50
elevator_trim_limit= 19.00
spoiler_limit= 60.00
spoilerons_available= 1
aileron_to_spoileron_gain=1.00
min_ailerons_for_spoilerons=1.00
min_flaps_for_spoilerons=0.00
[Reference Speeds]
flaps_up_stall_speed= 145
full_flaps_stall_speed= 115
cruise_speed= 483
max_indicated_speed= 350
max_mach= 0.81
[contact_points]
//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)
// My six point landing gear contact points (one contact point per landing gear wheel) //
point.0= 1, 38.00, -0.75, -7.145, 1574.80, 0, 2.216, 70.0, 0.218, 4.10, 0.639, 6.1, 6.3, 0, 180, 250 // left nose gear wheel //
point.1= 1, 38.00, 0.75, -7.145, 1574.80, 0, 2.216, 70.0, 0.218, 4.10, 0.639, 6.1, 6.3, 0, 180, 250 // right nose gear wheel //
point.2= 1, -2.15, -11.50, -8.510, 1574.80, 1, 3.371, 0.0, 1.220 , 1.20, 0.439, 6.3, 6.7, 2, 180, 250 // left outer main wheel //
point.3= 1, -2.15, -8.75, -8.510, 1574.80, 1, 3.371, 0.0, 1.220 , 1.20, 0.439, 6.3, 6.7, 2, 180, 250 // left inner main wheel //
point.4= 1, -2.15, 11.50, -8.510, 1574.80, 2, 3.371, 0.0, 1.220 , 1.20, 0.439, 6.2, 6.6, 3, 180, 250 // right outer main wheel //
point.5= 1, -2.15, 8.75, -8.510, 1574.80, 2, 3.371, 0.0, 1.220 , 1.20, 0.439, 6.2, 6.6, 3, 180, 250 // right inner main wheel //
// Scrape points //
point.6= 2, -12.60, -48.45, 3.000, 787.80, 0. 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5, 0, 0 // left wingtip //
point.7= 2, -12.60, 48.45, 3.000, 787.80, 0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6, 0, 0 // right wingtip //
point.8= 2, -51.60, 0.00, 7.600, 787.80, 0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9, 0, 0 // tail //
point.9= 2, 52.00, 0.00, 1.750, 787.80, 0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 // nose //
point.10=2, -22.70, 0.00, -2.300, 787.80, 0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 // lower aft fuselage scrape point //
// My three point landing gear contact points (normal three points centred between the landing gear wheel pairs) //
//point.0= 1, 38.00, 0.000, -7.145, 1574.80, 0, 2.216, 70.0, 0.218, 4.10, 0.839, 6.1, 6.3, 0, 180, 250 // nose gear //
//point.1= 1, -2.15, -10.125, -8.510, 1574.80, 1, 3.371, 0.0, 1.220, 1.20, 0.639, 6.3, 6.7, 2, 180, 250 // left main //
//point.2= 1, -2.15, 10.125, -8.510, 1574.80, 2, 3.371, 0.0, 1.220, 1.20, 0.639, 6.2, 6.6, 3, 180, 250 // right main //
// Scrape points //
//point.3= 2, -12.60, -48.450, 3.000, 787.80, 0. 0.0, 0.0, 0.000, 0.00, 0.0, 0.0, 0.0, 5, 0, 0 // left wingtip //
//point.4= 2, -12.60, 48.450, 3.000, 787.80, 0, 0.0, 0.0, 0.000, 0.00, 0.0, 0.0, 0.0, 6, 0, 0 // right wingtip //
//point.5= 2, -51.60, 0.000, 7.600, 787.80, 0, 0.0, 0.0, 0.000, 0.00, 0.0, 0.0, 0.0, 9, 0, 0 // tail //
//point.6= 2, 52.00, 0.000, 1.750, 787.80, 0, 0.0, 0.0, 0.000, 0.00, 0.0, 0.0, 0.0, 4, 0, 0 // nose //
//point.7= 2, -22.70, 0.000, -2.300, 787.80, 0, 0.0, 0.0, 0.000, 0.00, 0.0, 0.0, 0.0, 4, 0, 0 // lower aft fuselage scrape point //
static_pitch= -0.25
static_cg_height= 8.40
gear_system_type= 0
[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 20
system_type= 1
damaging-speed= 250
blowout-speed= 280
lift_scalar= 0.90
drag_scalar= 0.90
pitch_scalar= 0.50
flaps-position.0= 0
flaps-position.1= 1
flaps-position.2= 2
flaps-position.3= 5
flaps-position.4= 10
flaps-position.5= 15
flaps-position.6= 25
flaps-position.7= 30
flaps-position.8= 40
[flaps.1]
type=2
span-outboard= 0.500
extending-time= 6
system_type= 1
damaging-speed= 250
blowout-speed= 280
lift_scalar= 0.80
drag_scalar= 0.80
pitch_scalar= 0.50
flaps-position.0= 0
flaps-position.1= 0.5
flaps-position.2= 0.5
flaps-position.3= 0.5
flaps-position.4= 1.0
flaps-position.5= 1.0
flaps-position.6= 1.0
flaps-position.7= 1.0
flaps-position.8= 1.0
[electrical]
autopilot= 0, 5 , 17.0
avionics_bus= 0, 10, 17.0
avionics= 1, 5 , 17.0
gear_warning= 0, 2 , 17.0
fuel_pump1= 0, 5 , 17.0
fuel_pump2= 0, 5 , 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
pitot_heat= 0, 15, 17.0
additional_system= 0, 20, 17.0
marker_beacon= 1, 2, 17.0
starter1= 0, 20, 17.0
starter2= 0, 20, 17.0
auto_brakes= 0, 15, 17.0
hydraulic_pump1= 0, 2, 17.0
hydraulic_pump2= 0, 2, 17.0
fuel_transfer_pump= 0, 5, 17.0
max_battery_voltage= 28.0
generator_alternator_voltage= 28.0
max_generator_alternator_amps= 60.0
electric_always_available= 1
engine_generator_map= 1, 1, 0, 0
[pitot_static]
vertical_speed_time_constant=999
[exits]
number_of_exits= 2
exit_rate.0 = 0.28
exit_rate.1 = 0.28
[TailHook]
tailhook_length= 4
tailhook_position= 0.0, 0.0, 0.0
cable_force_adjust= 0.5
[folding_wings]
wing_fold_system_type=4
fold_rates= 0.11,0.11
[Views]
eyepoint= 42.30, -2.10, 5.75 //43.50,-2.10,5.65
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 =3, -11.70, -48.30, 3.10, fx_navred ,
light.1 =3, -11.70, 48.30, 3.10, fx_navgre ,
light.2 =4, -15.60, -47.70, 3.00, fx_navwhi ,
light.3 =4, -15.60, 47.70, 3.00, fx_navwhi ,
light.4 =2, -12.80, -48.40, 3.10, fx_strobe ,
light.5 =2, -12.80, 48.40, 3.10, fx_strobe ,
light.6 =4, -51.55, 0.00, 7.70, fx_navwhi ,
light.7 =3, -51.55, 0.00, 7.70, fx_strobe ,
light.8 =1, 7.80, 0.00, 10.50, fx_beacon ,
light.9 =1, 6.80, 0.00, -3.20, fx_beaconb ,
light.10 =4, 43.10, -1.50, 6.00, fx_vclight ,
// Wing and Flap Tip Vortices - delete the "//" before light.14 - light.17 to activate //
//light.14=6, -21.00, -48.25, 3.00, fx_contrail_s_short_wide // Left wing tip vortex //
//light.15=6, -21.00, 48.25, 3.00, fx_contrail_s_short_wide // Right wing tip vortex //
//light.16=8, -19.00, -35.5, 0.85, fx_contrail_s_short_thin // Left flap tip vortex //
//light.17=8, -19.00, 35.5, 0.85, fx_contrail_s_short_thin // Right flap tip vortex //
[keyboard_response]
elevator= 150,250
aileron= 150,250
rudder= 150,250
[direction_indicators]
direction_indicator.0=3,0
[fuel]
Center1= 3.00, 0.00, -2.00, 2302.00, 0.00
LeftMain= -1.00, -19.00, 0.00, 1429.00, 0.00
RightMain=-1.00, 19.00, 0.00, 1429.00, 0.00
fuel_type= 2
number_of_tank_selectors=1
electric_pump=0
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 500
autothrottle_available= 1
use_no_default_pitch= 1
use_no_default_bank= 1
pitch_takeoff_ga= 8
autothrottle_arming_required= 1
autothrottle_takeoff_ga= 1
autothrottle_max_rpm= 102
default_pitch_mode=0
default_bank_mode=0
max_pitch= 12.00
max_pitch_acceleration= 1.00
max_pitch_velocity_lo_alt= 2.00
max_pitch_velocity_hi_alt= 1.50
max_pitch_velocity_lo_alt_breakpoint= 20000
max_pitch_velocity_hi_alt_breakpoint= 28000
max_bank= 30.00
max_bank_acceleration= 1.80
max_bank_velocity= 3.00
max_throttle_rate= 0.10
nav_proportional_control= 9.00
nav_integrator_control= 0.25
nav_derivative_control= 0.00
nav_integrator_boundary= 2.50
nav_derivative_boundary= 0.00
gs_proportional_control= 9.52
gs_integrator_control= 0.26
gs_derivative_control= 0.00
gs_integrator_boundary= 0.70
gs_derivative_boundary= 0.00
yaw_damper_gain= 1.00
[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
Adf.2= 1
Transponder.1= 1
Marker.1= 1
[SMOKESYSTEM]
// With permission - David Maltby's BAC 1-11 engine smoke effect vertically adjusted and renamed for the 737-200 //
Smoke.0= 0.0, -13.00, -17.00, JT8D-15_SMOKE_R
Smoke.1= 0.0, -13.00, -17.00, JT8D-15_SMOKE_L
Smoke.2= 0.0, -13.00, 17.00, JT8D-15_SMOKE_R
Smoke.3= 0.0, -13.00, 17.00, JT8D-15_SMOKE_L
// Old engine smoke effect
//smoke.0= -2.50, -13.00, -17.00, fx_hjg_707
//smoke.1= -2.50, -13.00, 17.00, fx_hjg_707
[EFFECTS]
wake= fx_wake
water= fx_spray
dirt= fx_tchdrt
concrete= fx_sparks
touchdown= fx_tchdwn_m, 1 // Modified touch down effect for six gear contact points
//touchdown= fx_tchdwn, 1 // Default touch down effect for normal three gear contact points
Contrail=
startup=
windshield_rain_effect_available= 1
[brakes]
toe_brakes_scale= 0.800
parking_brake= 1
[gear_warning_system]
gear_warning_available= 1
pct_throttle_limit= 0.099976
flap_limit_power= 24.637185
flap_limit_idle= 0.974028
[hydraulic_system]
electric_pumps= 0
engine_map= 1,1,0,0
normal_pressure= 3000
[stall_warning]
type= 1
[attitude_indicators]
attitude_indicator.0= 1
[turn_indicators]
turn_indicator.0= 1,0
