// PREMIER AIRCRAFT DESIGN
// FSX, Casa C295M 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
// SAR Air Show livery by Bob May
[fltsim.0]
title=CasaC295 Brazil Pelicano
sim=PAD_casa295
model=M
panel=casa295m_x
sound=heavyturbo
texture=brazilian_pelicano
atc_id=2811
atc_flight_number=2811
atc_airline=air force
atc_parking_types=RAMP
atc_parking_codes=
ui_manufacturer=CASA
ui_type=C-295M
ui_variation=Brazilian AF Pelicano Squadron
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.
visual_damage=1
atc_heavy=0
editable=1
[General]
atc_type=CASA
atc_model=295
editable=1
Category=airplane
performance=Military transport\nCrew 3 (2 pilots + loadmaster)\nLoad 71 fully equiped troops\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: 2,600 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= 2500, 10.000, 0.000, -5.000, Payload
station_load.3= 5000, -0.000, 0.000, -5.000, payload
station_load.4= 2500, -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=1800
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, -60.265000, 0.000000, 16.500000, 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
[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 =5.400, -14.200, -0.000
Engine.1 =5.400, 14.200, -0.000
fuel_flow_scalar =0.45000
min_throttle_limit =-0.50000
[propeller]
thrust_scalar =1.00000
propeller_type =0
propeller_diameter =12.00000
propeller_blades =6
propeller_moi =154.08716
beta_max =45.00000
beta_min =12.00000
min_gov_rpm =25520.00000
prop_tc =0.00400
gear_reduction_ratio =17.00000
fixed_pitch_beta =0.00000
low_speed_theory_limit =80.00000
prop_sync_available =1
prop_deice_available =1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather =700.00000
beta_feather =79.30000
power_absorbed_cf =0.90000
defeathering_accumulators_available=0
prop_reverse_available =1
minimum_on_ground_beta =1.00000
minimum_reverse_beta =-14.00000
[TurbineEngineData]
fuel_flow_gain =0.01100
inlet_area =0.02500
rated_N2_rpm =29920.00000
static_thrust =300.00000
reverser_available=0
afterburner_available=0
afterburner_throttle_threshold=0.01100
ThrustSpecificFuelConsumption=0.01100
AfterBurnThrustSpecificFuelConsumption=0.01100
[turboprop_engine]
power_scalar =1.25000
maximum_torque =7892.92045
[electrical]
//BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
//BusType, MaxAmpLoad, MinVoltage
autopilot = 0, 5 , 1.0
avionics_bus = 0, 10, 10.0
avionics = 1, 5 , 10.0
gear_warning = 0, 2 , 1.0
fuel_pump = 0, 5 , 1.0
light_nav = 0, 5 , 1.0
light_beacon = 0, 5 , 1.0
light_landing = 0, 5 , 7.0
light_taxi = 0, 5 , 7.0
light_strobe = 0, 5 , 7.0
light_panel = 0, 5 , 1.0
pitot_heat = 0, 15, 1.0
additional_system = 0, 20, 1.0
marker_beacon = 1, 2, 1.0
starter1 = 0, 20, 1.0
starter2 = 0, 20, 1.0
starter3 = 0, 20, 1.0
starter4 = 0, 20, 1.0
auto_brakes = 0, 15, 1.0
hydraulic_pump = 0, 2, 1.0
fuel_transfer_pump = 0, 5, 1.0
max_battery_voltage=28.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=160.0
electric_always_available=0
//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, 420.000, 0.000
RightMain = -0.000, 9.100, 3.900, 420.000, 0.000
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
