// PREMIER AIRCRAFT DESIGN
// Casa C295AEW for FS2004, 12 June 2011
// FSDS model, panel design, XML gauge design by Jean-Pierre Brisard
// FD and Master Textures by Bob May
// Copyright 2011 - Premier Aircraft Design


[fltsim.0]
title=CASA C-295 Radar, 0
sim=PW-127
model=AEW
panel=MIO
sound=
texture=EADS AEW
kb_checklists=CASA295_check
kb_reference=CASA295_ref
atc_id=C295
atc_airline=EADS
atc_flight_number=C295
atc_parking_types=RAMP_CARGO
atc_parking_codes=C295
ui_manufacturer=CASA
ui_type=C-295AEW
ui_variation=EADS AEW
ui_typerole="Military Transport"
ui_createdby="Premier Aircraft Design"
prop_anim_ratio=1.015
description=The C-295 is a further development of the commercially successful Spanish–Indonesian transport aircraft CASA CN-235 with a stretched fuselage, 50% more payload capability and new PW127G turboprop engines. The C-295 made its maiden flight in 1998. The first order came from the Spanish Air Force.
They are manufactured and assembled in the Airbus Military facilities in the San Pablo Airport, in Seville, Spain.
The C-295 is in service with the Armed Forces of more than 10 countries. More than 80 C295s have been contracted.
atc_heavy=0
editable=1



[General]
atc_type=CASA
atc_model=295
editable=1
Category=airplane



performance=maritime patrol\nCrew varies (2 pilots + electronic equipment operators\nLength: 80.3 ft\nWing Span: 84.8 ft\nWeight:30,700 lb Empty\nMax T\/O Weight:51,146 lb\nPower: 2 x 2,645 SHP P&W 127G Turboshafts\nMax Cruise: 300 Kts TAS\nStall Speed (with flaps) 90 Kts\nCeiling: 28,000 ft\nRange: 4,600 Naut Miles with std fuel load.
category=airplane
editable=1

[WEIGHT_AND_BALANCE]
max_gross_weight =51000.0
empty_weight =30700.30000

reference_datum_position= 0.0, 0, 0 // (feet) distance from FlightSim Ref position: (1/4 chord,c/l, waterline)
empty_weight_CG_position= -0.000, -0.000, -0.000

max_number_of_stations =5



;Moments of Inertia
empty_weight_pitch_MOI   =196481.92000
empty_weight_roll_MOI    =132979.91000
empty_weight_yaw_MOI     =300000.00000
empty_weight_coupled_MOI =0.00000
station_load.0=  170,  -0.000, -1.750, 0.000, Pilot
station_load.1=  170,  -0.000,  1.750, 0.000, First Officer
station_load.2= 500,  10.000,  0.000, -5.000, Payload
station_load.3= 2000,  -0.000,  0.000, -5.000, payload
station_load.4= 500, -10.000,  0.000, -5.000, payload


[Views]
eyepoint= 26.293,-1.847,-2.809 // 39.108,-0.97,-1.674 (feet) longitudinal, lateral, vertical distance from reference datum



[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.000000
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_max_rpm=10000
pitch_takeoff_ga=10
use_no_default_bank=1
use_no_default_pitch=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=25
max_bank_acceleration=1.8
max_bank_velocity=3
max_throttle_rate=0.1
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=0
autothrottle_takeoff_ga=0


[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=Landing

light.0 =4, 27.420, -1.000000, -5.55, fx_vclightwhi
light.1 =4,27.4200, 1.000000, -5.55, fx_vclightwhi
light.2 =2, -44.83, 0.000000, -0.73, fx_strobeh
light.3 =2, -3.206, 42.217,1.208, fx_strobeh
light.4 =2, -3.206, -42.217, 1.208, fx_strobeh
light.5 =1, -8.92, 0.000000, -9.40, fx_padbeaconh
light.6 =1, -41.24, 0.000000, 15.35, fx_padbeaconh
light.7 =3, -0.059, -40.000, 1.208, fx_navredh
light.8 =3, -0.059, 40.000, 1.208, fx_navgreh
;light.9 =4,  0.000,  0.000, -5.000, fx_vclighth
light.10=4, 6.000,  0.000, -5.000, fx_vclighth
;light.11=4,-15.000,  0.000, -5.000, fx_vclighth


[flight_tuning]
cruise_lift_scalar=1.00000
parasite_drag_scalar=1.00000
induced_drag_scalar=1.00000
elevator_effectiveness=1.00000
aileron_effectiveness=1.00000
rudder_effectiveness=1.00000
pitch_stability=1.00000
roll_stability=1.00000
yaw_stability=1.00000
elevator_trim_effectiveness=1.10000
aileron_trim_effectiveness=1.00000
rudder_trim_effectiveness=1.00000
hi_alpha_on_roll=1.00000
hi_alpha_on_yaw=1.00000
p_factor_on_yaw=1.00000
torque_on_roll=1.00000
gyro_precession_on_roll=1.00000
gyro_precession_on_yaw=1.00000


[GeneralEngineData]
engine_type = 5
Engine.0 = 3.392, -13.579, 3.701
Engine.1 = 3.392, 13.579, 3.701
fuel_flow_scalar=0.825
min_throttle_limit=-0.12
max_contrail_temperature=-35

[TurbineEngineData]
fuel_flow_gain=0.01 //adjusted to have only slight overshot
inlet_area=0.800 
rated_N2_rpm=20016 //spec=20016 was 23850
static_thrust=280 //was 343
afterburner_available=0 

[turboprop_engine]
power_scalar=1.0 
maximum_torque=12365 
max_rpm_mechanical_efficiency_scalar=1.0
idle_rpm_mechanical_efficiency_scalar=1.0
max_rpm_friction_scalar=1.0
idle_rpm_friction_scalar=1.0

[propeller]
thrust_scalar=1.13 
propeller_type=0 
propeller_diameter=11.4 //12.9
propeller_blades=6 
propeller_moi=90 //60 //was 90
beta_max=30 //spec=24 was 65
beta_min=5.5 // spec=14 adjusted to small NP drop when blade pitch jumps
min_gov_rpm=14171  //was 16695 //0.708 x rated RPM = min NP=70.8%
prop_tc=0.0003 //adjusted to have only slight overshot
gear_reduction_ratio=16.68  //spec=16.68 was 19.875
fixed_pitch_beta=0.0 
low_speed_theory_limit=80 
prop_sync_available=1 
prop_deice_available=1 
prop_feathering_available=1 
prop_auto_feathering_available=1 
min_rpm_for_feather=700 //was 480 //840
beta_feather=78.5  //spec=78.5
power_absorbed_cf=0.990 
defeathering_accumulators_available=0 
prop_reverse_available=1 
minimum_on_ground_beta=0.0 //spec=-1 adjusted to supress rev sound
minimum_reverse_beta=-14 //-10.5  //spec=-14 adjusted to avoid drop on NP
//rotation=-1 -1 -1 -1    //clockwise rotation               
//rotation=1 1 1 1     //anti clockwise rotation

[electrical]
//BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
//BusType, MaxAmpLoad, MinVoltage
max_battery_voltage = 28
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0
flap_motor = 0, 0, 17
gear_motor = 0, 0, 17
autopilot = 0, 0, 17
avionics_bus = 0, 0, 17
avionics = 1, 0, 17
pitot_heat = 0, 0, 17
additional_system = 0, 0, 17
marker_beacon = 1, 0, 17
gear_warning = 0, 0, 17
fuel_pump = 0, 0, 17
starter1 = 0, 0, 17
starter2 = 0, 0, 17
starter3 = 0, 0, 17
starter4 = 0, 0, 17
light_nav = 0, 0, 17
light_beacon = 0, 0, 17
light_landing = 0, 0, 17
light_taxi = 0, 0, 17
light_strobe = 0, 0, 17
light_panel = 0, 0, 17
prop_sync = 0, 0, 17
auto_feather = 0, 0, 17
auto_brakes = 0, 0, 17
standby_vacuum = 0, 0, 17
hydraulic_pump = 0, 0, 17
fuel_transfer_pump = 0, 0, 17
propeller_deice = 0, 0, 17

        //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]

max_number_of_points =4

static_pitch = 0.442
static_cg_height = 11.535
gear_system_type=0
tailwheel_lock=0
point.0= 1, 21.365, 0.000, -11.900, 1250, 0, 0.575, 45.000, 0.120, 2.500, 0.826, 5.000, 6.000, 0
point.1= 1, -4.600, -7.970, -12.160, 3000, 1, 0.675, 0.000, 0.675, 2.500, 0.800, 7.000, 7.000, 0
point.2= 1, -4.600, 7.970, -12.160, 3000, 1, 0.675, 0.000, 0.675, 2.500, 0.800, 7.000, 7.000, 0
point.3= 5, 20.900, 0.000, -7.300, 1600, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 1.000, 1.000, 0



[gear_warning_system]
gear_warning_available =1
pct_throttle_limit =0.09998
flap_limit_idle    =15.01149
flap_limit_power  =30.02299

[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

[brakes]
parking_brake =1
toe_brakes_scale =1.06300
auto_brakes=0
hydraulic_system_scalar=0.00000
differential_braking_scale=1.00000

[hydraulic_system]
normal_pressure =3000.00000
electric_pumps  = 0         //no electric pumps
engine_map      = 1,1,0,0   //pumps on Eng1,2

[flaps.0]
type= 1
system_type=0
span-outboard= 0.500
extending-time= 6.0
damaging-speed=250.0
blowout-speed=300.0
flaps-position.0=0.00
flaps-position.1=5.00
flaps-position.2=15.00
flaps-position.3=25.00
flaps-position.4=35.00
lift_scalar=1.00
drag_scalar=0.95
pitch_scalar=-1.00



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

[fuel]
LeftMain  = -0.000, -9.100, 3.900, 2020.000, 10.000
RightMain = -0.000,  9.100, 3.900, 2020.000, 10.000
fuel_type =2
number_of_tank_selectors =1                    
electric_pump=1
fuel_dump_rate=0.02000
anemometer_pump=0
manual_pump=0
engine_driven_pump=0

[airplane_geometry]
wing_area               =605.00000
wing_span               =90.00000
wing_root_chord         =7.06000
wing_dihedral           =2.50000
wing_incidence          =1.00000
wing_twist              =0.00000
oswald_efficiency_factor=0.75000
wing_winglets_flag      =0
wing_sweep              =0.00000
wing_pos_apex_lon       =1.68197
wing_pos_apex_vert      =0.00000
htail_area              =75.50000
htail_span              =34.27000
htail_pos_lon           =-33.01000
htail_pos_vert          =0.00000
htail_incidence         =0.00000
htail_sweep             =0.00000
vtail_area              =44.75000
vtail_span              =15.97000
vtail_sweep             =0.00000
vtail_pos_lon           =-33.98000
vtail_pos_vert          =1.68000
elevator_area           =41.81000
aileron_area            =43.56000
rudder_area             =28.49000
elevator_up_limit       =25.00000
elevator_down_limit     =25.00000
aileron_up_limit        =20.00000
aileron_down_limit      =20.00000
rudder_limit            =30.00000
elevator_trim_limit     =20.00000
spoiler_limit           =0.00000
spoilerons_available    =0
aileron_to_spoileron_gain =0.00000
min_ailerons_for_spoilerons =0.00000
min_flaps_for_spoilerons =0.00000
auto_spoiler_available=1
spoiler_extension_time=0.00000 
positive_g_limit_flaps_up=3.00000
positive_g_limit_flaps_down=2.10000
negative_g_limit_flaps_up=-2.40000
negative_g_limit_flaps_down=-1.80000
spoiler_handle_available=0
load_safety_factor=1.00000

[Reference Speeds]
flaps_up_stall_speed    = 102.0                  //Knots True (KTAS)
full_flaps_stall_speed   = 82.0                  //Knots True (KTAS)
cruise_speed                =300.00000
max_indicated_speed     =390.00000
max_mach=0.70000

[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to  1/2 and 1/8 respectively.
elevator= 150.0, 250.0
aileron= 150.0, 250.0
rudder= 150.0, 250.0

[stall_warning]
type=1
stick_shaker=1

[direction_indicators]
direction_indicator.0=3,0

[exits]
number_of_exits=2
exit_rate.0=0.3                               ;Percent per second
exit_rate.1=0.3                               ;Percent per second

[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position = -15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust = 1.0


[brakes]
toe_brakes_scale=1.062532
parking_brake=1

[gear_warning_system]
gear_warning_available=1
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=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[pitot_static]
pitot_heat=1.000000

[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

[GPWS]
max_warning_height=0
sink_rate_fpm=-1500
excessive_sink_rate_fpm=-2000
climbout_sink_rate_fpm=-100
flap_and_gear_sink_rate_fpm=-100

[folding_wings]
wing_fold_system_type=4
fold_rates=0.6,0.6


[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1
crash_magnitude1=10000
crash_direction1=1000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000
stick_shaker_magnitude=5000
stick_shaker_direction=0
stick_shaker_period=111111