[fltsim.0] title=Chinook ROFL sim=CH-47 model= panel= sound= texture=1 kb_checklists=ch47 kb_reference=ch47 prop_anim_ratio=-1.76 atc_id=ROFL ui_manufacturer=Boeing ui_type=Chinook ui_variation=CH47 ROFL description=THE ROFL COPTER The Chinook by Tom Woods and Mark Adams. [General] performance=Main Rotor Dia. 60 ft 0 in\nRear Rotor Dia. 60 ft 0 in\nFuselage length 50 ft 7.5 in\nWheel Base 22 ft 6.0 in\nOverall Length 99 ft 0.5 in\nRotor Mast Ht. 12 ft 4 in\nHeight to TR 18 ft .5 in\nFuselage Width 12 ft 5 in\nGround Clearance 1 ft 6 in \nWeight Empty 23,400 lbs.\nMission Gross Wt 50,000 lbs \n atc_type=HELICOPTER atc_model=H47 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=50 station_load.0="0.000000,0.000000,0.000000,0.000000,see read me" station_load.1="0.000000,10.00000,0.000000,0.000000,up to 1164lbs" station_load.2="0.000000,-10.0000,0.000000,0.000000,total allowed" empty_weight=1460.000000 empty_weight_roll_MOI=4000.000 empty_weight_pitch_MOI=6000.000 empty_weight_yaw_MOI=40000.000 empty_weight_coupled_MOI=0.000000 max_gross_weight=3200.0 [turboprop_engine] power_scalar=1.0 [propeller] thrust_scalar=1.0 propeller_type=1 propeller_diameter=6.883000 propeller_blades=2 propeller_moi=5.706520 beta_max=0.000000 beta_min=15.000000 min_gov_rpm=0.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000000 beta_feather=0.000000 power_absorbed_cf=0.000000 defeathering_accumulators_available=0 prop_reverse_available=0.000000 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [Helicopter] low_realism_stability_scale=1.0, 1.0, 1.0 //Pitch , Bank, Yaw Scalars on Stability in Low Realism Settings [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 //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, -9.650, -5.250, -7.100, 3000, 1.0, 1.13, 0.001, 0.40, 2.50, 0.60, 0.0, 0.0, 2.0, 0.0, 0.0 point.1=1, -9.650, 5.250, -7.100, 3000, 2.0, 1.13, 0.001, 0.40, 2.50, 0.60, 0.0, 0.0, 3.0, 0.0, 0.0 point.2=1, 12.650, 5.250, -6.200, 3000, 0.0, 1.13, 30.00, 0.40, 2.50, 0.80, 0.0, 0.0, 0.0, 0.0, 0.0 point.3=1, 12.650, -5.250, -6.200, 3000, 0.0, 1.13, 30.00, 0.40, 2.50, 0.80, 0.0, 0.0, 1.0, 0.0, 0.0 point.4=2, 0.000, -30.000, 7.000, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 5.0, 0.0, 0.0 point.5=2, 0.000, 30.000, 7.000, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 6.0, 0.0, 0.0 point.6=2, -42.000, 0.000, 6.000, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 9.0, 0.0, 0.0 point.7=2, 56.000, 0.000, 14.000, 0.0, 0.0, 0.00, 0.0, 0.00, 0.00, 0.00, 0.0, 0.0, 4.0, 0.0, 0.0 point.8=4, 19.600, -6.000, -2.500, 3000, 0.0, 0.00, 0.0, 0.85, 2.50, 0.60, 0.0, 0.0, 0.0, 0.0, 0.0 point.9=4, 19.600, 6.000, -2.500, 3000, 0.0, 0.00, 0.0, 0.85, 2.50, 0.60, 0.0, 0.0, 1.0, 0.0, 0.0 point.10=4, -11.333, -6.000, -4.800, 3000, 0.0, 0.00, 0.0, 0.85, 2.50, 0.60, 0.0, 0.0, 2.0, 0.0, 0.0 point.11=4, -11.333, 6.000, -4.800, 3000, 0.0, 0.00, 0.0, 0.85, 2.50, 0.60, 0.0, 0.0, 3.0, 0.0, 0.0 point.12=4, 27.000, -2.500, -2.300, 3000, 0.0, 0.00, 0.0, 0.85, 2.50, 0.60, 0.0, 0.0, 2.0, 0.0, 0.0 point.13=4, 27.000, 2.500, -2.300, 3000, 0.0, 0.00, 0.0, 0.85, 2.50, 0.60, 0.0, 0.0, 3.0, 0.0, 0.0 static_pitch=-2.0 gear_system_type=1 static_cg_height=6.7 [Views] eyepoint=26.4,1.9,3.7 [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 [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. //NOTE: These map to cyclic (fore/aft), cyclic (left/right), and anti-torque elevator=100, 180 aileron=200, 1000 rudder=200, 1000 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type=4 direction_indicator.0=3,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, 12.847, -6.158, -1.777, fx_navred light.1=3, 12.847, 6.000, -1.777, fx_navgre light.2=3, -18.841, 0.077, 4.499, fx_navwhi light.3=1, 8.6, 0.0, -3.8, fx_beacon light.4=1, -17.2, 0.0, 9.5, fx_beacon light.5=4, 27.5, -1.7, 2.5, fx_vclight light.6=4, 27.5, 1.7, 2.5, fx_vclight light.7=2, 8.6, 0.0, -3.8, fx_strobe , light.8=2, -17.2, 0.0, 9.5, fx_strobe , [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 //[SMOKESYSTEM] //smoke.0=0.00,-10.00,0.00, [fuel] LeftMain=0.0, 0.0, 0.0,21.5, 0.0 RightMain=0.0, 0.0, 0.0,21.5,0.0 LeftAux=0.0, 0.0, 0.0,21.5, 0.0 RightAux=0.0, 0.0, 0.0,21.5,0.0 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=1 [GeneralEngineData] engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=8.3,-3.0, 0.4 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=8.3, 3.0, 0.4 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [Reference Speeds] flaps_up_stall_speed=0.0 //Knots True (KTAS) full_flaps_stall_speed=0.0 //Knots True (KTAS) cruise_speed=135.0 //Knots True (KTAS) max_indicated_speed=180.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=500.0 autothrottle_available=1 pitch_takeoff_ga=0.000000 autothrottle_arming_required=1 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 [brakes] toe_brakes_scale=1.000031 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
