[fltsim.0] title=Bristol 130 Bombay sim=Bombay model= panel= sound= texture= description=The Bristol Bombay was designed as a dual role Transport-bomber for service in Africa and the middle east. A 1931 design, it was dated when it entered service in 1939. Even so, the Bombay did stellar work in the Mediteranean and Africa, even operating as bombers on occasion. [WEIGHT_AND_BALANCE] empty_weight =13800.00000 reference_datum_position = 0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = 0.000, 0.000, 0.000 max_number_of_stations =16 ;Moments of Inertia empty_weight_pitch_MOI =148843.00000 empty_weight_roll_MOI =89229.00000 empty_weight_yaw_MOI =185419.00000 station_load.0= 170, 14.600, -4.000, 2.000, //Pilot station_load.1= 170, 14.600, 4.000, 2.000, //Co-Pilot station_load.2= 0, 0.000, 0.000, 0.000 station_load.3= 0, 0.000, 0.000, 0.000 station_load.4= 0, 0.000, 0.000, 0.000 station_load.5= 0, 0.000, 0.000, 0.000 station_load.6= 0, 0.000, 0.000, 0.000 station_load.7= 0, 0.000, 0.000, 0.000 station_load.8= 0, 0.000, 0.000, 0.000 station_load.9= 0, 0.000, 0.000, 0.000 station_load.10= 0, 0.000, 0.000, 0.000 station_load.11= 0, 0.000, 0.000, 0.000 station_load.12= 0, 0.000, 0.000, 0.000 station_load.13= 0, 0.000, 0.000, 0.000 station_load.14= 0, 0.000, 0.000, 0.000 station_load.15= 0, 0.000, 0.000, 0.000 empty_weight_coupled_MOI=0.00000 [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 =1.00000 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 [piston_engine] power_scalar =1.00000 cylinder_displacement=194.77778 compression_ratio=6.50000 number_of_cylinders=9 max_rated_rpm=2750.00000 max_rated_hp=1030.00000 fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.03470 turbocharged=1 max_design_mp=54.00000 min_design_mp=1.00000 critical_altitude=21000.00000 emergency_boost_type=0 emergency_boost_mp_offset=0.00000 emergency_boost_gain_offset=0.00000 auto_ignition=0 fuel_air_auto_mixture=0 emergency_boost_duration=0.00000 max_rpm_mechanical_efficiency_scalar=1.00000 idle_rpm_mechanical_efficiency_scalar=1.00000 max_rpm_friction_scalar=1.00000 idle_rpm_friction_scalar=1.00000 [propeller] thrust_scalar =1.00000 propeller_type=0 propeller_diameter=15.00000 propeller_blades=2 propeller_moi=78.61025 beta_min=15.00000 beta_max=65.00000 min_gov_rpm=1200.00000 prop_tc=0.01000 gear_reduction_ratio=1.50000 fixed_pitch_beta=0.00000 low_speed_theory_limit=75.22788 prop_sync_available=1 prop_deice_available=0 prop_feathering_available=1 prop_auto_feathering_available=1 min_rpm_for_feather=700.00000 beta_feather=88.50000 power_absorbed_cf=0.90000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=1.00000 minimum_reverse_beta=-14.00000 [exits] number_of_exits = 1 exit_rate.0 = 0.4 ;Percent per second [electrical] max_battery_voltage = 24.0 generator_alternator_voltage = 28.0 max_generator_alternator_amps = 60.0 [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 static_pitch = 9.520 static_cg_height = 7.500 max_number_of_points=0 gear_system_type=1 tailwheel_lock=0 point.0=1.000000,-35.750000,0.000000,-2.666667,1399.900827,0.000000,0.618821,55.740000,0.374504,2.500000,0.661983,5.000000,5.000000,0.000000,0.000000,0.000000 point.1=1.000000,2.583333,-9.416667,-8.666667,1999.862615,1.000000,0.618821,0.000000,0.930345,2.500000,0.425010,0.000000,0.000000,2.000000,0.000000,0.000000 point.2=1.000000,2.583333,9.416667,-8.666667,1999.862615,2.000000,0.618821,0.000000,0.930345,2.500000,0.425010,0.000000,0.000000,3.000000,0.000000,0.000000 point.3=2.000000,0.000000,-39.000000,1.000000,799.945046,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,0.000000,39.000000,1.000000,799.945046,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-39.000000,0.000000,-1.750000,799.945046,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,19.000000,0.000000,-4.416667,799.945046,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 [Views] eyepoint= 23.04, -1.22, 2.34 //(feet) longitudinal, lateral, vertical distance from reference datum [LIGHTS] panel=0, 0, 7.0, fx_vclight [GeneralEngineData] Engine.0=8.000, -12.000, 0.000 Engine.1=8.000, 12.000, 0.000 engine_type=0 fuel_flow_scalar=1.00000 [fuel] LeftMain= 0.000, -5.100, 0.500, 200.000, 0.000 RightMain= 0.000, 5.100, 0.500, 200.000, 0.000 Center1= 0.000, 0.000, 0.000, 100.000, 0.000 fuel_type=1 number_of_tank_selectors=0 electric_pump=0 [General] performance=+ Empty Weight: 13800 lbs + Max Power: 1030 Hp + Maneuver speed: 136 mph @ 7.0 g + Max speed: 193 mph @ 21000 ft + Max speed at sea-level: 165 mph + Climb rate: 1200 ft/min @ 73 mph Flight Dynamics By: Peperez Bismarck and Peperez FD Build 25 - 6/18/06 06:28 AM Flight Dynamics Workbook V2.84.65 editable=1 [airplane_geometry] wing_area=1340.00000 wing_span=95.75000 wing_root_chord=14.00000 wing_dihedral=3.00000 wing_incidence=0.00000 wing_twist=0.00000 oswald_efficiency_factor=0.88000 wing_winglets_flag=0 wing_sweep=0.00000 wing_pos_apex_lon=3.49869 wing_pos_apex_vert=0.00000 htail_area=100.00000 htail_span=40.00000 htail_pos_lon=-30.00000 htail_pos_vert=0.00000 htail_incidence=0.00000 htail_sweep=0.00000 vtail_area=40.00000 vtail_span=10.33000 vtail_pos_lon=-30.00000 vtail_pos_vert=0.00000 vtail_sweep=0.00000 elevator_area=40.00000 aileron_area=30.00000 rudder_area=20.00000 elevator_up_limit=30.00000 elevator_down_limit=20.00000 aileron_up_limit=15.00000 aileron_down_limit=15.00000 rudder_limit=30.00000 elevator_trim_limit=18.00000 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 [brakes] toe_brakes_scale=0.64089 [smokesystem] smoke.0=0 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.00000 flap_limit_idle=22.50000 flap_limit_power=11.25000 [Reference Speeds] flaps_up_stall_speed=53.00755 full_flaps_stall_speed=53.00755 cruise_speed=104.27714 max_indicated_speed=300.00000 max_mach=0.42300 [autopilot] autopilot_available=1 flight_director_available=0 autothrottle_available=0 autothrottle_arming_required=0 default_pitch_mode=0 default_bank_mode=0 use_no_default_bank=1 use_no_default_pitch=1 default_vertical_speed=1000.00000 autothrottle_takeoff_ga=1.00000 autothrottle_max_rpm=90.00000 pitch_takeoff_ga=8.00000 max_pitch=10.00000 max_pitch_acceleration=1.00000 max_pitch_velocity_lo_alt=2.00000 max_pitch_velocity_hi_alt=1.50000 max_pitch_velocity_lo_alt_breakpoint=20000.00000 max_pitch_velocity_hi_alt_breakpoint=28000.00000 max_bank=25.00000 max_bank_acceleration=1.80000 max_bank_velocity=3.00000 max_throttle_rate=0.10000 nav_proportional_control=9.00000 nav_integrator_control=0.25000 nav_derivative_control=0.00000 nav_integrator_boundary=2.50000 nav_derivative_boundary=0.00000 gs_proportional_control=9.52000 gs_integrator_control=0.26000 gs_derivative_control=0.00000 gs_integrator_boundary=0.70000 gs_derivative_boundary=0.00000 yaw_damper_gain=0.00000 [hydraulic_system] normal_pressure=1000.00000 [AirWrench] Aircraft_Length=81.39000 Vmax_sl=160.00000 Vmax_ca=183.70000 V_rc=93.70000 Climb_Rate=954.70000 Climb_Weight=14140.00000 Max_gforce=7.00000 Emergency_hp=1030.00000 nose_position_lon=28.49000 ActualIncidence=0.00000 ActualTwist=0.00000 ActualTailIncidence=0.00000 Aircraft_Type=1 FlowCorrection=1.00000 Power_Correction=1.00000 JetAltitude=0.00000 turboprop_critical_altitude=0.00000 target_roll_Vopt=133.60000 target_roll_rate=7.80000 pitch_damping=1.00000 yaw_damping=1.00000 elevator_scalar=1.00000 rudder_scalar=1.00000 Elevator_FF=50.00000 Aileron_FF=-50.00000 Roll_Response=40.00000 Control_Response=100.00000 V_Max_Control=193.30000 V_Zero_Control=386.70000 Spin_Stability=100.00000 Stall_Stability=100.00000 Elevator_Propwash=1.00000 Rudder_Propwash=1.00000 spoiler_time=0.00000 afterburner_thrust=0.00000 mach_scale=1.00000 spoiler_type=1 spoiler_cd=0.00000 spoiler_cl=0.00000 spoiler_cm=0.00000 update_flaps_enabled=0 flaps_type=1 flaps_cd_scalar=0.00000 flaps_cm_scalar=0.00000 vfe_enabled=0 gear_cd_scalar=0.00000 gear_cm_scalar=0.50000 cylinder_head_temperature=501.00000 exhaust_gas_temperature=1201.00000 fuel_pressure=20.00000 oil_pressure=60.00000 oil_temperature=241.00000 radiator_temperature=211.00000 exhaust_pressure_ratio=0.00000 interstage_turbine_temperature=-459.00000 knots_flag=0 cfs1_flag=0 laminar_flow=0 fixed_wing_pos=0 AirWrenchVersion=1.01.30 [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
