;********************************************************** ;Flight Dynamics for Douglas DC-6B with R-2800-CB16 engines ;********************************************************** ;This is the transcontinental version of the DC-6B for the intercontinental version use the -CB17 engines file [fltsim.0] title=DC-6B Transocean Air Lines 1953 sim=dc6b model= panel= sound= texture= kb_checklists=DC6B_check kb_reference=dc6b_ref atc_id=N90806 atc_id_enable=1 ui_manufacturer=Douglas ui_type=DC-6B ui_variation=Transocean Airlines 1953 description=The DC-6B was generally considered to possess the best operating economics of any piston airliner built. Transocean bought this plane from Slick airways in 1952, renamed it the "Royal Hawaiian". It crashed east of Wake Island December 7, 1953. atc_airline=Transocean atc_flight_number=21 atc_heavy=0 visual_damage=1 prop_anim_ratio=0.9 [General] performance=Four P&W R-2800-CB16\neach 2400hp for take off\n1800hp METO to 8500feet\n1700hp to 14,500 feet atc_type=DOUGLAS atc_model=DC6 [WEIGHT_AND_BALANCE] ;load assumed symetrical versus CoG reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 max_number_of_stations=2 empty_weight=63200 ;including oil, catering etc. station_load.0=1000,0,0,0 ;5 crew and bags station_load.1=10000,0,0,0 ;50 pax and bags (maximum payload with full fuel) max_gross_weight=103800 ;with -CB16 engines or 107,000 with -CB17 ;103800 - 29600 fuel=74200 and 74200 - 63200 = 11000 / 200 = 55 crew plus pax plus bags ;default ramp weight is 103,800lbs with max fuel and weight limited payload ;MLW=88,200 with -CB16 engines and MTOW originally only 100,000lbs ;Moments of Inertia ; empty_weight_roll_MOI=1920000 empty_weight_pitch_MOI=805000 empty_weight_yaw_MOI=2640000 empty_weight_coupled_MOI=0.0 [fuel] ;max fuel 4934 USG=29600lbs with -CB16 engines ; LeftMain=0,-15,0,1414,0 RightMain=0,15 ,0,1414,0 Leftaux=0,-15,0,1053,0 Rightaux=0,15 ,0,1053,0 fuel_type=1.000000 number_of_tank_selectors=1 [GeneralEngineData] engine_type=0 Engine.0=0.633, -28.500, 1.583 Engine.1=1.117, -15.933, 0.467 Engine.2=1.117, 15.933, 0.467 Engine.3=0.633, 28.500, 1.583 fuel_flow_scalar=0.97 [piston_engine] ; ;P&W R-2800-CB16=2400bhp for take off & 1800bhp at 8500 feet (low blower = METO) and 1700bhp at 14500 feet (high blower) ; cylinder_displacement=155.78 compression_ratio=6.7 number_of_cylinders=18 max_rated_rpm=2800.000000 ;for take off only max_rated_hp=2400.000000 ;for take off only fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.035000 turbocharged=1 max_design_mp=59.5 min_design_mp=5.0 critical_altitude=5000 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=1.000000 idle_rpm_friction_scalar=1.000000 [propeller] propeller_type=0 propeller_blades=3 gear_reduction_ratio=1.0 propeller_diameter=8.8 propeller_moi=26.8 beta_max=65.0 beta_min=15.0 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_reverse_available=0 min_rpm_for_feather=700.0 beta_feather=96.0 power_absorbed_cf=0.9 minimum_on_ground_beta=15.0 minimum_reverse_beta=0 defeathering_accumulators_available=0 prop_auto_feathering_available=1 min_gov_rpm=650.000000 prop_tc=0.010000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 [airplane_geometry] oswald_efficiency_factor=0.8 wing_area=1463 wing_span=117.5 wing_root_chord=12.45 wing_dihedral=7.0 wing_incidence=4.0 wing_twist=0.0 htail_area=180.0 htail_span=37 htail_pos_lon=-38 htail_pos_vert=0.0 htail_incidence=0.0 htail_sweep=0.0 htail_area=210.9 vtail_area=93.4 vtail_span=19 vtail_sweep=0.0 vtail_pos_lon=-36 vtail_pos_vert=3 wing_winglets_flag=0 wing_sweep=0.0 wing_pos_apex_lon=0.0 wing_pos_apex_vert=0.0 elevator_area=108.9 aileron_area=43.82 rudder_area=49 elevator_up_limit=27.5 elevator_down_limit=20.0 aileron_up_limit=19.5 aileron_down_limit=15.0 rudder_limit=23.5 elevator_trim_limit=19.5 spoiler_limit=60.0 ;for cowl flap drag spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [Flaps.0] type=1 span-outboard=0.5 extending-time=22.0 flaps-position.0=0,0 flaps-position.1=10,174 flaps-position.2=20,174 flaps-position.3=30,174 flaps-position.4=40,152 flaps-position.5=50,152 [autopilot] autopilot_available=1 use_no_default_bank=1 use_no_default_pitch=1 flight_director_available=0 default_vertical_speed=100 ;default is zero IRL - 100 is closest available value in FS2002 autothrottle_available=0 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=0.000000 pitch_takeoff_ga=8.000000 [Reference Speeds] ;all KIAS - Pitot error not known so IAS set=CAS flaps_up_stall_speed=105 full_flaps_stall_speed=81 cruise_speed=180 [exits] number_of_exits=1 exit_rate.0=0.1 [Radios] Audio.1=1 Com.1=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [contact_points] static_pitch=0.5 static_cg_height=8.3 point.0=1.000, 30.500, 0.000, -10.300, 2000.000, 0.000, 1.500, 70.000, 1.000, 1.300, 0.898, 4.000, 10.000, 1.000, 174, 185 point.1=1.000, -2.400, -12.400, -10.000, 1500.000, 1.000, 2.000, 0.000, 1.000, 1.300, 0.898, 4.000, 10.000, 2.000, 174, 185 point.2=1.000, -2.400, 12.400, -10.000, 1500.000, 2.000, 2.000, 0.000, 1.000, 1.300, 0.898, 4.000, 11.000, 3.000, 174, 185 point.3=2.000, -5.167, -57.000, 3.500, 1574.000, 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, -5.167, 57.000, 3.500, 1574.000, 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, -56.833, 0.000, -1.200, 1574.000, 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, 30.500, 0.000, -0.660, 1574.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.7= 5, -30.90, -5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 3.0, 3.2, 0, 0.0, 0.0 point.8= 5, -30.90, 5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 3.1, 3.5, 0, 0.0, 0.0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit 5= landing light.0=3, -2.2, -58.21, 3.45, fx_navred light.1=3, -2.2, 58.21, 3.45, fx_navgre light.2=3, -64.04, 0.00, 2.30, fx_navwhi light.3=1, -55.95, 0.00, 20.30, fx_beacon light.4=4, 32, -2.50, 3.0, fx_vclight , light.5=4, 32, -2.50, 4.0, fx_vclight , light.6=4, 31.5, -2.50, 2.0, fx_vclight , light.7=4, 31.5, 2.5, 2.0, fx_vclight , light.8=4, 32, 2.50, 3.0, fx_vclight , light.9=4, 31, 2.50, 4.5, fx_vclight , [SMOKESYSTEM] smoke.0=-0.417, -6.333, -28.500, fx_smoke_w smoke.1=-0.833, -4.917, -15.833, fx_smoke_w smoke.2=-0.833, -4.917, 15.833, fx_smoke_w smoke.3=-0.417, -6.333, 28.500, fx_smoke_w [direction_indicators] direction_indicator.0=1,0 [keyboard_response] elevator=450.000000,1000.000000 aileron=450.000000,1000.000000 rudder=450.000000,1000.000000 [Views] eyepoint=30.294533,-2.104209,3.606102 //normal VC //eyepoint=-21.294533,-2.104209,3.606102 //wing view //eyepoint=10.294533,-2.104209,3.606102 //engine view
