Aircraft Configuration file Flight 1 DC-9 "Iron Knuckles" Copyright © 2002 by Flight 1 Software Modified by Manny Osias All rights reserved. [FLTSIM.0] title=Cebu Pacific sim=F1_DC9-30 model= panel= sound= texture= kb_checklists=F1_DC9-30_check kb_reference=F1_DC9-30_ref Editable=0 atc_id=RP-C1505 atc_airline=Cebu Pacific atc_flight_number=1505 ui_manufacturer=Cebu Pacific ui_type=Douglas DC-9-32 ui_variation=Cebu Pacific description=DC9-32 Cebu Pacific. 3D Model & Texture files © 2002 Flight One Software & Aeromesh. Improved Flight Dynamics by Manny Osias. atc_heavy=0 [GENERAL] atc_type=MCDONNELDOUGLAS atc_model=DC9 Editable=0 performance=For Performance and Specifications, please refer to the documentation provided. [WEIGHT_AND_BALANCE] reference_datum_position= 0.0, 0.0, 0.0 empty_weight_CG_position= 0.0, 0.0, 0.0 max_number_of_stations=50 empty_weight= 52935.0 empty_weight_pitch_MOI= 1150000.0 empty_weight_roll_MOI= 525000.0 empty_weight_yaw_MOI= 910000.0 empty_weight_coupled_MOI= 0.0 max_gross_weight= 109000.0 CG_forward_limit= 0.0 CG_aft_limit= 0.0 max_number_of_stations=5 station_load.0= 5723.333496 15.5, 0.0, 0.0 station_load.1= 5723.333496 0.00, 0.0, 0.0 station_load.2= 5723.333496 -12.1, 0.0, 0.0 station_load.3= 1842.500000 10.5, 0.0, -3.5 station_load.4= 1842.500000 -10.50, 0.0, -3.5 [FORCEFEEDBACK] gear_bump_nose_magnitude=3000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=2700 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=2700 gear_bump_right_direction=500 gear_bump_right_duration=250000 ground_bumps_magnitude1=1300 ground_bumps_angle1=8900 ground_bumps_intercept1=3.0 ground_bumps_slope1=0.2 ground_bumps_magnitude2=200 ground_bumps_angle2=9100 ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 crash_direction1=1000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [AIRPLANE_GEOMETRY] wing_area= 1000.7 wing_span= 105.0 wing_root_chord= 23.0 wing_dihedral= 3.0 wing_incidence=-2.3 wing_twist= 1.0 oswald_efficiency_factor= 0.35 wing_winglets_flag= 0 wing_sweep= 24.5 wing_pos_apex_lon=0.0 wing_pos_apex_vert=0.0 htail_area= 275.5 htail_span= 36.8 htail_pos_lon= -58.3 htail_pos_vert= 16.95 htail_incidence= 0.75 htail_sweep= 30.0 vtail_area= 190.0 vtail_span= 17.15 vtail_sweep= 26.0 vtail_pos_lon= -55.8 vtail_pos_vert= 6.0 elevator_area= 78.4 aileron_area= 44.0 rudder_area= 48.4 elevator_up_limit= 26.5 elevator_down_limit= 27.0 aileron_up_limit= 15.0 aileron_down_limit= 15.0 rudder_limit= 25 elevator_trim_limit= 20.0 spoiler_limit= 59.0 spoilerons_available= 1 aileron_to_spoileron_gain= 3.0 min_ailerons_for_spoilerons= 10.0 min_flaps_for_spoilerons= 0.0 [PITOT STATIC] vertical_speed_time_constant=100 [FUEL] Fwd/Aft, Lateral, Vertical, Usable, Unusable Center1= 0.0, 0.0, -6.0, 896.0, 25.0 LeftMain= -5.0, -20.0, 0.0, 1389.0, 18.7 RightMain= -5.0, 20.0, 0.0, 1389.0, 18.7 fuel_type=2.00 number_of_tank_selectors=1 [CONTACT_POINTS] //0 Class //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 // Gear 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0= 1.0, 41.5, 0.00, -8.65, 2500.0, 0.0, 1.08, 25.0, 0.25, 2.4, 0.84, 4.0, 5.0, 0.0, 0.0, 0.0 point.1= 1.0, -6.93, -7.39, -8.70, 2500.0, 1.0, 1.67, 0.0, 0.50, 2.4, 0.65, 5.1, 6.1, 2.0, 0.0, 0.0 point.2= 1.0, -6.93, 7.39, -8.70, 2500.0, 2.0, 1.67, 0.0, 0.50, 2.4, 0.65, 5.2, 6.2, 3.0, 0.0, 0.0 // Scrapes 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.3= 2.0,-16.96, -46.50, -1.28, 750.0, 0.0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 5.0, 0.0, 0.0 point.4= 2.0,-16.96, 46.50, -1.28, 750.0, 0.0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 6.0, 0.0, 0.0 point.5= 2.0,-34.91, 0.00, -3.45, 750.0, 0.0, 0.0, 0.0, 0.00. 0.0, 0.00, 0.0, 0.0, 9.0, 0.0, 0.0 point.6= 2.0, 52.71, 0.00, -3.25, 750.0, 0.0, 0.0, 0.0, 0.00, 0.0, 0.00, 0.0, 0.0, 4.0, 0.0, 0.0 static_pitch= 0.28 static_cg_height= 8.28 [GENERALENGINEDATA] engine_type= 1 Engine.0= -39.0, -8.7, 1.332 Engine.1= -39.0, 8.7, 1.332 fuel_flow_scalar= 0.95 [TURBINEENGINEDATA] fuel_flow_gain= 0.0033 inlet_area= 10.0 rated_N2_rpm= 29920.0 static_thrust= 14500.0 afterburner_available=0 reverser_available= 1 [JET_ENGINE] thrust_scalar=1.000 [Reference Speeds] flaps_up_stall_speed = 130.0 //Knots True (KTAS) full_flaps_stall_speed = 115.0 //Knots True (KTAS) cruise_speed = 450.0 [VIEWS] eyepoint=43.75,-1.50,3.45 [AUTOPILOT] autopilot_available=1 flight_director_available=1 default_vertical_speed=2500.0 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=100 pitch_takeoff_ga=15.0 autoland_available=0 use_no_default_pitch=1 use_no_default_bank=1 [DIRECTION_INDICATORS] direction_indicator.0=3,0 [RADIOS] // Radio Type=avail?,sby freq?,glide slope? Audio.1= 1 Com.1 = 1, 0 Com.2 = 1, 0 Nav.1 = 1, 0, 1 Nav.2 = 1, 0, 0 Adf.1 = 1 Transponder.1= 1 Marker.1= 1 [FLIGHT_TUNING] cruise_lift_scalar=1.0 pitch_stability=1.3 roll_stability=1.0 yaw_stability=1.0 parasite_drag_scalar=1.2 induced_drag_scalar=1.12 elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [LIGHTS] // Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing // Y/X/Z light.0=3, -15.7920, -46.4685, -1.0708, fx_navredm , ; navlight port light.1=3, -15.7920, 46.4685, -1.0708, fx_navgrem , ; navlight stbd light.2=2, -16.1670, -46.6027, -1.0829, fx_strobeh , ; wingtip strobe port light.4=2, -16.1670, 46.6027, -1.0829, fx_strobeh , ; wingtip strobe stbd light.6=1, -7.9310, 0.0000, -5.1524, fx_beaconb , ; red beacon lower light.8=1, 1.1968, 0.3110, 6.9080, fx_beaconh , ; red beacon upper light.10=3,-19.4954, -46.6687, -1.1305, fx_navwhih , ; poslight left light.11=3,-19.4954, 46.6687, -1.1305, fx_navwhih , ; poslight right light.12=5, 11.9234, -4.7000, -1.9035, fx_navwhih , ; wing insp light left light.13=5, 11.9234, 4.7000, -1.9035, fx_navwhih , ; wing insp light right light.14=4, 44.1000, -1.5000, 4.3000, fx_vclight , ; VC light left light.15=4, 44.1000, 1.5000, 4.3000, fx_vclight , ; VC light right [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn,1 contrail=fx_contrail_l [SMOKESYSTEM] // Z Y X smoke.0=100.0,-42.0,-8.93, fx_smoke_rx smoke.1=100.0,-42.0, 8.93, fx_smoke_rx [EXITS] number_of_exits=2 exit_rate.0=0.1 ;Percent per second exit_rate.1=0.1 ;Percent per second [KEYBOARD_RESPONSE] elevator=150.0,250.0 aileron=150.0,250.0 rudder=150.0,250.0 [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 15 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 0 // degrees flaps-position.2 = 5 // degrees flaps-position.3 = 15 // degrees flaps-position.4 = 25 // degrees flaps-position.5 = 40 // degrees flaps-position.6 = 50 // degrees damaging-speed = 280 // KIAS blowout-speed = 300 // KIAS damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.0 drag_scalar = 1.3 pitch_scalar= 1.0 system_type = 1 //Hydraulic [FLAPS.1] type = 2 // 1 - tail, 2 - lead span-outboard = 0.95 // RATIO:1 extending-time = 3 // SECONDS flaps-position.0 = 0 // SLATS STOWED flaps-position.1 = 1 // SLATS DEPLOYED damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.0 drag_scalar = 1.0 pitch_scalar=-1.0 system_type = 1 //Hydraulic