[fltsim.0]
title=FlightFX DC-9-51 Northwest Old
sim=dc9-51
model=
panel=
sound=
texture=nwa70
checklists=
atc_id=N787NC
atc_airline=Northwest
atc_flight_number=951
ui_manufacturer=Douglas
ui_type=DC-9-51
ui_variation=Northwest Old
description=Feel free to paint, see readme...:-)

[General]
atc_type=McDonnell Douglas
atc_model=DC9
performance=Length: 125 ft 7 in (38.30 m)\nHeight: 28 ft 0 in (8.53 m)\nWingspan: 93 ft 4 in (28.45 m)\n\nMax Takeoff Weight: 114 000 lbs (51 756 kg)\n\nEngines: 2 x JT8D-17 turbofans rated @ 16000 lbs\nNormal Cruise: .74 Mach at 30,000 - 35,000 feet\nRange: 1 685nm  (2 712km)\n\nOriginal FDE by Sam Chin with New Modifications by Mike Baumann SGA/FFX (C)(2003)

[forcefeedback]
gear_bump_nose_magnitude=3000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=2700           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=1300            ; 0 - 10000
ground_bumps_angle1=08900               ; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200             ; 0 - 10000
ground_bumps_angle2=09100               ; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000                  ; 0 - 10000
crash_direction1=01000                  ; 0 - 35999 degrees
crash_magnitude2=10000                  ; 0 - 10000
crash_direction2=9000                   ; 0 - 35999 degrees
crash_period2=75000                     ; in microseconds
crash_duration2=2500000                 ; in microseconds

[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.100
roll_stability=1.100
yaw_stability=1.100
parasite_drag_scalar=1.200
induced_drag_scalar=1.200
elevator_effectiveness=1.200
aileron_effectiveness=1.100
rudder_effectiveness=1.100
elevator_trim_effectiveness=1.200
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.100

[jet_engine]
thrust_scalar=1.200

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations=56
station_load.0=  225, 58.00, -1.70, 2.00
station_load.1=  225, 58.00,  1.70, 2.00
station_load.2= 1500, 48.55, -3.00, 2.00
station_load.3= 1500, 48.55,  3.00, 2.00
station_load.4=  240, 48.55, -1.00, 2.00
station_load.5=  340, 47.16, -2.00, 2.00
station_load.6=  170, 47.16,  2.00, 2.00
station_load.7=  170, 44.54, -2,00, 2.00
station_load.8=  340, 44.54,  2.00, 2.00
station_load.9=  170, 41.92,  2.00, 2.00
station_load.10= 340, 39.30, -2.00, 2.00
station_load.11= 340, 39.30,  2.00, 2.00
station_load.12= 170, 36.68, -2.00, 2.00
station_load.13= 510, 34.06,  2.00, 2.00
station_load.14= 340, 31.44, -2.00, 2.00
station_load.15= 340, 31.44,  2.00, 2.00
station_load.16= 6449, 30.28, 0.00, -2.00
station_load.17= 340, 28.82, -2.00, 2.00
station_load.18= 340, 28.82,  2.00, 2.00
station_load.19= 340, 26.20, -2.00, 2.00
station_load.20= 170, 26.20,  2.00, 2.00
station_load.21= 170, 23.58, -2.00, 2.00
station_load.22= 510, 23.58,  2.00, 2.00
station_load.23= 170, 20.96,  2.00, 2.00
station_load.24= 170, 18.34, -2.00, 2.00
station_load.25= 170, 18.34,  2.00, 2.00
station_load.26= 340, 15.72, -2.00, 2.00
station_load.27= 510, 15.72,  2.00, 2.00
station_load.28= 340, 13.10, -2.00, 2.00
station_load.29= 340, 13.10,  2.00, 2.00
station_load.30= 170, 10.48, -2.00, 2.00
station_load.31= 170, 10.48,  2.00, 2.00
station_load.32= 510,  7.86,  2.00, 2.00
station_load.33= 170,  5.24, -2.00, 2.00
station_load.34= 170,  5.24,  2.00, 2.00
station_load.35= 340,  2.62, -2.00, 2.00
station_load.36= 170,  2.62,  2.00, 2.00
station_load.37= 170,  0.00, -2.00, 2.00
station_load.38= 510,  0.00,  2.00, 2.00
station_load.39= 170, -2.62, -2.00, 2.00
station_load.40= 170, -2.62,  2.00, 2.00
station_load.41= 340, -5.24, -2.00, 2.00
station_load.42= 170, -5.24,  2.00, 2.00
station_load.43= 170, -7.86, -2.00, 2.00 
station_load.44= 340, -7.86,  2.00, 2.00
station_load.45= 340, -10.48, -2.00, 2.00
station_load.46= 170, -10.48, 2.00, 2.00
station_load.47= 170, -13.10, -2.00, 2.00
station_load.48= 340, -13.10, 2.00, 2.00
station_load.49= 340, -15.72, -2.00, 2.00
station_load.50= 170, -15.72, 2.00, 2.00
station_load.51= 170, -18.34, -2.00, 2.00
station_load.52= 170, -18.34, 2.00, 2.00
station_load.53= 2908, -18.58, 0.00, -2.00
station_load.54= 3205, -27.45, -8.80, 2.60
station_load.55= 3205, -27.45,  8.80, 2.60
empty_weight= 83693.000
empty_weight_roll_MOI= 1927400.000
empty_weight_pitch_MOI= 1729855.000
empty_weight_yaw_MOI= 2151112.000
empty_weight_coupled_MOI= 1300.000
max_gross_weight= 108362.399

[GeneralEngineData]
engine_type=1
Engine.0= -27.45, -8.80 , 2.60
Engine.1= -27.45,  8.80,  2.60
fuel_flow_scalar=0.900

[SMOKESYSTEM]
smoke.0= 2.60, -38.00,  -8.80, SMOKE_JT8D
smoke.1= 2.60, -38.00,   8.80, SMOKE_JT8D
smoke.2= 1.30, -17.00,  49.75, fx_contrail_320
smoke.3= 1.30, -17.00, -49.75, fx_contrail_320

[TurbineEngineData]
fuel_flow_gain= 0.019
inlet_area= 7.0833
rated_N2_rpm= 29920.000
static_thrust= 16000.000
afterburner_available= 0
reverser_available= 1

[airplane_geometry]
wing_area= 1315.000
wing_span= 99.200
wing_root_chord= 17.100
wing_dihedral= 2.999
wing_incidence= 0.000
wing_twist= -0.302
oswald_efficiency_factor= 0.887
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 10.550
wing_pos_apex_vert= -1.100
htail_area= 381.000
htail_span= 36.833
htail_pos_lon= -57.50
htail_pos_vert= 19.20
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 224.000
vtail_span= 17.065
vtail_sweep= 0.000
vtail_pos_lon= -50.00
vtail_pos_vert= 12.00
elevator_area= 95.250
aileron_area= 40.080
rudder_area= 38.080
elevator_up_limit= 27.502
elevator_down_limit= 20.626
aileron_up_limit= 19.481
aileron_down_limit= 14.897
rudder_limit= 23.491
elevator_trim_limit= 19.481
spoiler_limit= 59.989
spoilerons_available= 1
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 9.969
min_flaps_for_spoilerons= 0.000

[Reference Speeds]
flaps_up_stall_speed= 132.000
full_flaps_stall_speed= 105.600
cruise_speed= 413.099

        //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]
point.0=1.000, 59.000, 0.000, -8.200, 1574.803, 0.000, 1.504, 70.000, 0.293, 2.500, 0.655, 6.500, 6.500, 0.000, 250.0, 300.0
point.1=1.000, -1.000,-8.700, -7.850, 1574.803, 1.000, 2.504,  0.000, 0.393, 2.500, 0.700, 6.900, 6.900, 2.000, 250.0, 300.0
point.2=1.000, -1.000, 8.700, -7.850, 1574.803, 2.000, 2.504,  0.000, 0.393, 2.500, 0.700, 7.100, 7.100, 3.000, 250.0, 300.0
point.3=2.000,-12.000,-49.700, 1.300,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000,   0.0,   0.0
point.4=2.000,-12.000, 49.700, 1.300,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000,   0.0,   0.0
point.5=2.000, 67.350,  0.000,-0.550,  787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000,   0.0,   0.0
point.6=2.000,-61.450,  0.000, 19.200, 787.402, 0.000, 0.000,  0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000,   0.0,   0.0
static_pitch=0.000
static_cg_height=8.200

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 2 , 0
gear_motor=0, 2 , 0
autopilot=0, 2 , 0
avionics_bus=0, 2 , 0
avionics=0, 2 , 0
pitot_heat=0, 2 , 0
additional_system=0, 2 , 0
marker_beacon=0, 2 , 0
gear_warning=0, 2 , 0
fuel_pump=0, 2 , 0
starter1=0, 2 , 0
starter2=0, 2 , 0
starter3=0, 2 , 0
starter4=0, 2 , 0
light_nav=0, 2 , 0
light_beacon=0, 2 , 0
light_landing=0, 2 , 0
light_taxi=0, 2 , 0
light_strobe=0, 2 , 0
light_panel=0, 2 , 0
prop_sync=0, 2 , 0
auto_feather=0, 2 , 0
auto_brakes=0, 2 , 0
standby_vacuum=0, 2 , 0
hydralic pump=0, 2 , 0
fuel_transfer_pump=0, 2 , 0
propeller_deice=0, 2 , 0
propeller_deice=0, 2 , 0	
light rocognition=0, 2 , 0
light_wing=0, 2 , 0
light_logo=0, 2 , 0

[pitot_static]
vertical_speed_time_constant=1		//Increasing this value will cause a more instantaneous reaction in the VSI

[TailHook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=0.7

[Views]
eyepoint=58.0, -1.70, 4.70

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -11.85,  49.60,  1.30, MD80_NAVG ,     //right nav light
light.1=3, -11.85, -49.60,  1.30, MD80_NAVR ,     //left nav light
light.2=2, -12.20,  49.75,  1.30, MD80_STROBE ,   //right strobe
light.3=2, -12.20, -49.75,  1.30, MD80_STROBE ,   //left strobe
light.4=3, -16.20, -49.40,  1.25, fx_navwhi ,     //left id
light.5=3, -16.20,  49.40,  1.25, fx_navwhi ,     //right id
light.6=5,  20.10,   5.65,  1.52, MD80_INSPEC ,   //right wing inspection light
light.7=5,  20.10,  -5.65,  1.52, MD80_INSPEC ,   //left wing inspection light
light.8=5, -17.85,   5.55,  1.52, MD80_INSPEC2 ,  //right engine inspection light
light.9=5, -17.85,  -5.55,  1.52, MD80_INSPEC2 ,  //left engine inspection light
light.10=5, 15.58,   5.15, -0.68, MD80_NAVW ,     //right runway turnoff
light.11=5, 15.58,  -5.15, -0.68, MD80_NAVW ,     //left runway turnoff
light.12=6, 70.00,   0.00, -8.60, MJ772TL ,       //nose gear light splash
light.13=1,  0.03,   0.00, -4.60, MD80_BCNL ,     //lower beacon strobe
light.14=1,  4.10,   0.00,  8.55, MD80_BCNU ,     //upper beacon strobe
light.15=4, 57.50,  -1.50,  5.00, fx_vclight ,    //cockpit light
light.16=4, 57.50,   1.50,  5.00, fx_vclight ,    //cockpit light
light.17=3, -57.50,  7.50,  18.35, MD80_LOGO ,    //right logo light
light.18=3, -57.50, -7.50,  18.35, MD80_LOGO ,    //left logo light

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[direction_indicators]
direction_indicator.0=3,0

[fuel]
Center1=    0.00,   0.00, 0.00,  988.00, 0.00
LeftMain=  -1.80, -20.83, 0.00, 1347.00, 0.00
RightMain= -1.80,  20.83, 0.00, 1347.00, 0.00
fuel_type=2.000000
number_of_tank_selectors=1

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=99.000000
pitch_takeoff_ga=8.000000
use_no_default_pitch=1
use_no_default_bank=1

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1, 1, 1
Nav.2=1, 1, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 10.000
system_type= 1
damaging-speed= 280.000
blowout-speed= 320.000
lift_scalar= 1.200
drag_scalar= 1.200
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 7.998, 0.000
flaps-position.2= 15.997, 0.000
flaps-position.3= 23.995, 0.000
flaps-position.4= 31.994, 0.000
flaps-position.5= 39.992, 0.000

[Flaps.1]
type= 2
span-outboard= 0.000
extending-time= 1.500
system_type= 1
damaging-speed= 280.000
blowout-speed= 320.000
lift_scalar= 1.000
drag_scalar= 1.100
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000