// 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 [fltsim.0] title=CasaC295M Czech AF sim=PAD_casa295 model=M panel=casa295m_x sound=heavyturbo texture=czechcamo kb_checklists=CASA295_check kb_reference=CASA295_ref atc_id=0455 atc_airline=Air Force atc_flight_number=CZ0455 atc_parking_types=gate,ramp atc_parking_codes=ramp ui_manufacturer=CASA ui_type=C-295M ui_variation=Czech AF Camo 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=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