//********************************************************
//
//                       Nord 262E
//                    version fs9-06
//                     2004 juin 21
//
//********************************************************

[fltsim.0]
title=Nord262A-21 Cimber Air
sim=Nord262EC-6
model=
panel=
sound=
texture=
kb_checklists=N262_check
kb_reference=N262_ref
kb_kneeboard_keys=N262_keys
atc_id=OY-BCO
atc_flight_number=231
atc_airline=Rousseau Aviation
atc_id_color=
ui_manufacturer= ACCIDENTES
ui_type=262A-21
ui_variation=F-BNGB
description=Model by Barneybigard 01/2004\nSound by Benoit Dubé and Jean-Pierre Bourgeois\n2D Panel and gauges by Jean-Pierre Langer\nTexture by Claus Vendelboe Holmberg 05/2006\nThe elegant Nord 262 is a high-performance, pressurized-cabin, twin-engine turboprop airplane. Piloting the beautiful Nord 262 is a logical transition into the more complex world of turbine engines and larger aircraft. See the Aircraft Information section of Help for tips on flying this aircraft.

[fltsim.1]
title=Nord262A-21 Cimber Air ( New livery )
sim=Nord262EC-6
model=
panel=
sound=
texture=Cimber OY-BCO New
kb_checklists=N262_check
kb_reference=N262_ref
kb_kneeboard_keys=N262_keys
atc_id=OY-BCO
atc_flight_number=231
atc_airline=danair
atc_id_color=
ui_manufacturer=Nord Aviation
ui_type=262A-21
ui_variation=Cimber Air OY-BCO 1986
description=Model by Barneybigard 01/2004\nSound by Benoit Dubé and Jean-Pierre Bourgeois\n2D Panel and gauges by Jean-Pierre Langer\nTexture by Claus Vendelboe Holmberg 05/2006\nThe elegant Nord 262 is a high-performance, pressurized-cabin, twin-engine turboprop airplane. Piloting the beautiful Nord 262 is a logical transition into the more complex world of turbine engines and larger aircraft. See the Aircraft Information section of Help for tips on flying this aircraft.

[fltsim.2]
title=Nord262A-21 Cimber Air (Blue livery)
sim=Nord262EC-6
model=
panel=
sound=
texture=Cimber OY-BDM
kb_checklists=N262_check
kb_reference=N262_ref
kb_kneeboard_keys=N262_keys
atc_id=OY-BDM
atc_flight_number=
atc_airline=cimberair
atc_id_color=
ui_manufacturer=Nord Aviation
ui_type=262A-21 
ui_variation=Cimber Air OY-BDM 1982
description=Model by Barneybigard 01/2004\nSound by Benoit Dubé and Jean-Pierre Bourgeois\n2D Panel and gauges by Jean-Pierre Langer\nTexture by Claus Vendelboe Holmberg 05/2006\nThe elegant Nord 262 is a high-performance, pressurized-cabin, twin-engine turboprop airplane. Piloting the beautiful Nord 262 is a logical transition into the more complex world of turbine engines and larger aircraft. See the Aircraft Information section of Help for tips on flying this aircraft.



[General]
performance=Wingspan : 21,90 m \nLength : 19,20 m \nHeight : 6,20 m \nWing area : 55,79 m2 \nMax. nr of passengers: 29 \nPower, Two Bastan VI turboprop. of 1,080 hp (1,685 kW) each. \nMax speed : 418 km.h \nCeiling : 12 000 m \nMax range : 1 490 km \nWeight (Min.) : 10 600 kg \nWeight (Max.) : 13 613 kg
atc_model=262E_C
editable=0
atc_type=Nord 
Category=airplane


[WEIGHT_AND_BALANCE]
max_gross_weight=   23368     // 10600 kg          21715.000
empty_weight=     15560         // 7060 kg            12300.000


//------------------------------------------------------------------------------------------------------------------------
reference_datum_position=     7.300, 0.000, 0.000        // ramené au bord d'attaque de la voilure
empty_weight_CG_position=    -3.500, 0.000, -3.000
//------------------------------------------------------------------------------------------------------------------------

max_number_of_stations=50

station_load.0=510,23.0,0.00,0.00,Equipage  3                                                               // 3300,-2.60,0.00,-4.50
station_load.1=87,16.8,  0.0, 0.0,Soute AV
station_load.2=420, 11.0, 0.0, 0.0,Station 2
station_load.3=600,4.40,  0.0, 0.0,Station 3
station_load.4=1000,-2.50, 0.0, 0.0,Station 4
station_load.5=770, -9.5,  0.0, 0.0,Station 5
station_load.5=0, -12.5,  0.0, 0.0,Station 6

;Moments of Inertia
empty_weight_pitch_MOI=            60749.000
empty_weight_roll_MOI=             33937.000
empty_weight_yaw_MOI=              291472.000
empty_weight_coupled_MOI=          0.000
CG_forward_limit=6.75
CG_aft_limit=3.000


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

cruise_lift_scalar=1.0

hi_alpha_on_roll=1.0
hi_alpha_on_yaw=1.0

p_factor_on_yaw=1.0
torque_on_roll=1.0
gyro_precession_on_roll=1.0
gyro_precession_on_yaw=1.0



[GeneralEngineData]
engine_type=5
//------------------------------------------------------------------------------------------------------------------------
Engine.0=                7.00,   -9.51,  -0.96                       //5.06
Engine.1=                7.00,    9.51,  -0.96                        // 5.06
//------------------------------------------------------------------------------------------------------------------------

min_throttle_limit=-0.450000
fuel_flow_scalar=0.765

[exits]
number_of_exits=2	
exit_rate.0=0.3
exit_rate.1=0.3

[propeller]
propeller_type=0
propeller_diameter= 10.49
propeller_blades=       3
propeller_moi=19.000
beta_max=62.000
beta_min=0.000
min_gov_rpm=30450.000
prop_tc=0.004
gear_reduction_ratio=21.0957     //17.600
fixed_pitch_beta=0
low_speed_theory_limit=80.000
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=700.000
beta_feather=90.00
power_absorbed_cf=0.900
defeathering_accumulators_available=0
prop_reverse_available=1
minimum_on_ground_beta=0.000
minimum_reverse_beta=-20.000
thrust_scalar=1.000

[TurbineEngineData]
fuel_flow_scalar=1.000000
fuel_flow_gain=0.01                     //0.025
inlet_area=0.300
rated_N2_rpm=33500   // 29920.000
static_thrust=400.000
afterburner_available=0
reverser_available=1

[turboprop_engine]
maximum_torque=        3265  //        3360.000
power_scalar=                          1.000
max_rpm_mechanical_efficiency_scalar=  1.000
idle_rpm_mechanical_efficiency_scalar= 1.000
max_rpm_friction_scalar=               1.000
idle_rpm_friction_scalar=              1.000

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

flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 5 , 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2 , 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
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



[contact_points]
//0  Classe                       (1=train,  2=pt.contact, 3=patins,  4=flotteurs
//1  Position longitudinale       (pieds)
//2  Position latérale            (pieds)
//3  Position verticale           (pieds)
//4  Seuil dommage impact         (pieds/minute)
//5  Freins                       (0=aucun, 1=Gauche, 2=Droit)
//6  Rayon roues                  (pieds)
//7  angle braquage               (degrés)
//8  Compression statique         (pieds) (0 si rigide)
//9  Ratio compression max/statique
//10 Ratio amortissement          (0=non amortie, 1=amortissement critique)
//11 Temps de sortie train        (secondes)
//12 Temps rentrée train          (secondes)
//13 Sound Type
//14 vitesse max rentrée train    (kias)
//15 vitesse max endomage train   (kias)
// Distances mesurées dans Gmax, 
//     0     X       Y       Z      4     5      6        7      8     9       10     11     12      13     14    15
//------------------------------------------------------------------------------------------------------------------------
//point.0=1, 18.70,  0.000, -11.050, 2600, 0.000, 0.288,  28.00, 0.215, 3.700, 0.900, 5.000, 6.000, 0.000, 0.000, 0.000
//point.1=1, -4.75, -5.020, -10.850, 2600, 1.000, 0.568,  0.000, 0.520, 0.700, 0.900, 7.000, 8.000, 2.000, 0.000, 0.000
//point.2=1, -4.75,  5.020, -10.850, 2600, 2.000, 0.568,  0.000, 0.520, 0.700, 0.900, 8.000, 9.000, 3.000, 0.000, 0.000
point.0=1, 18.70,  0.000, -10.650, 2600, 0.000, 0.288,  28.00, 0.215, 3.700, 0.900, 5.000, 6.000, 0.000, 0.000, 0.000
point.1=1, -4.75, -5.020, -10.350, 2600, 1.000, 0.568,  0.000, 0.520, 0.700, 0.900, 7.000, 8.000, 2.000, 0.000, 0.000
point.2=1, -4.75,  5.020, -10.350, 2600, 2.000, 0.568,  0.000, 0.520, 0.700, 0.900, 8.000, 9.000, 3.000, 0.000, 0.000

//------------------------------------------------------------------------------------------------------------------------
point.3=2.000,  0.000, -33.417, 5.000, 2600.00, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4=2.000,  0.000,  33.417, 5.000, 2600.00, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5=2.000, -34.750,  0.000, 1.000, 2600.00, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6=2.000,  13.000,  0.000, 1.000, 2600.00, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch=     1.0
static_cg_height= 10.6

//------------------------------------------------------------------------------------------------------------------------
gear_system_type=0

[Views]
//------------------------------------------------------------------------------------------------------------------------
//Exterior
//eyepoint=8.20,-1.25,-1.55
//Interior
//eyepoint=8.60,-1.35,-1.55
eyepoint=1.50,-1.25,-1.55

//------------------------------------------------------------------------------------------------------------------------

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=4, 6.10, 0, -0.55, fx_vclighth
light.1=4, 0.10, 0, -0.55, fx_vclighth
light.2=4,-6.10, 0, -0.55, fx_vclighth

//------------------------------------------------------------------------------------------------------------------------

[pitot_static]
vertical_speed_time_constant=1.0 
pitot_heat=1.000000

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


[keyboard_response]
elevator=150,250
aileron=150,250
rudder=150,250

[direction_indicators]
direction_indicator.0=3,0

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

[fuel]
LeftMain=   -3.50, -9.70, 0.00, 330.000, 0.000
RightMain= -3.50,  9.70, 0.00, 330.000, 0.000
fuel_type=2   //  jet A  6.6 lb/gal
number_of_tank_selectors=1
electric_pump=1

[airplane_geometry]
wing_area=                    592.000
wing_span=                    71.083
wing_root_chord=              10.17
wing_dihedral=                2.500
wing_incidence=               3.000
wing_twist=                  -0.500
oswald_efficiency_factor=     0.85
wing_winglets_flag=           0
wing_sweep=                   0.000
wing_pos_apex_lon=          0.00
wing_pos_apex_vert=           0.000

htail_area=                   100.00            //  183.000
htail_span=                   29.000
htail_pos_lon=                -29.00
htail_pos_vert=               -3.50
htail_incidence=           2.000
htail_sweep=                  0.000

vtail_area=                   116.000
vtail_span=                   14.250
vtail_sweep=                  0.000
vtail_pos_lon=                -29.00
vtail_pos_vert=               1.89

elevator_area=                83.00
aileron_area=                 27.33
rudder_area=                  110.32
elevator_up_limit=20.000
elevator_down_limit=15.000

aileron_up_limit=25.000
aileron_down_limit=25.000

rudder_limit=20.000
elevator_trim_limit=50.000

spoiler_limit=0.01
spoilerons_available=1
aileron_to_spoileron_gain=0.01
min_ailerons_for_spoilerons=0.01
min_flaps_for_spoilerons=0.01
auto_spoiler_available=0
spoiler_extension_time=2.000000
positive_g_limit_flaps_up=3.846154
positive_g_limit_flaps_down=2.991453
negative_g_limit_flaps_up=-2.991453
negative_g_limit_flaps_down=-2.000000

[Reference Speeds]
flaps_up_stall_speed=87.000   //  à 10600 kg
full_flaps_stall_speed=73.000  //  à 10600 kg
cruise_speed=190.000
max_indicated_speed=214.000000
max_mach=0.50

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1200
autothrottle_available=1
pitch_takeoff_ga=8.500000
autothrottle_arming_required=1       //requis par T de B de Jean-Pierre
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000

[forcefeedback]
stick_shaker_magnitude=50           //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               

[Flaps.0]
type=1
span-outboard=0.500
extending-time=15.000
system_type=0
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=          1.000
drag_scalar=          1.000
pitch_scalar=         0.000
flaps-position.0=0.000, 0.000
flaps-position.1=5.000, 0.000
flaps-position.2=11.000, 0.000
flaps-position.3=25.000, 0.000

[Flaps.1]
type=1
span-outboard=0.500
extending-time=15.000
system_type=0
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=  1.00
drag_scalar=  1.00
pitch_scalar=0.000
flaps-position.0=0.000, 0.000
flaps-position.1=5.000, 0.000
flaps-position.2=15.000, 0.000
flaps-position.3=35.000, 0.000

[brakes]
toe_brakes_scale=        1.2
parking_brake=           1 

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494


[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000

[stall_warning]
type=2      // 1
stick_shaker=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[TailHook]
tailhook_length=1.0                           ;(feet)
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=2
[fltsim.3]
title=Nord262A-21 Rousseau Aviation
sim=Nord262EC-6
model=
panel=
sound=
texture=Rousseau Aviation F-BNGB 1970
kb_checklists=N262_check
kb_reference=N262_ref
kb_kneeboard_keys=N262_keys
atc_id=F-bngb
atc_flight_number=000
atc_airline=Rousseau Aviation
atc_id_color=
ui_manufacturer=Nord Aviation
ui_type=262A-21
ui_variation=Rousseau Aviation F-BNGB 1970
description=Model by Barneybigard 01/2004\nSound by Benoit Dubé and Jean-Pierre Bourgeois\n2D Panel and gauges by Jean-Pierre Langer\nTexture by Claus Vendelboe Holmberg 05/2006\nThe elegant Nord 262 is a high-performance, pressurized-cabin, twin-engine turboprop airplane. Piloting the beautiful Nord 262 is a logical transition into the more complex world of turbine engines and larger aircraft. See the Aircraft Information section of Help for tips on flying this aircraft.Repintado por José Pajuelo Ramos para Air Alandalus charter Disasters


