[fltsim.0] title= Bf110E II/ZG 76 sim=Bf110E model= panel= sound= texture= panel_alias= sound_alias= kb_checklists= CheckList_3GR_Bf-110G-4/R3 Nachtjaeger kb_reference= atc_id=M8+CN atc_id_color=0xffffffff atc_airline= atc_flight_number=1959 prop_anim_ratio=1.36 visual_damage=1 ui_manufacturer=Messerschmitt ui_type=Bf110E ui_variation=II/ZG 76 ui_createdby=Ground Crew Design ui_typerole=WW2 Fighter Bomber description=Bf110E of II/ZG 76, the famous Sharkmouth Gruppe, during their operations on the Balkans, Creete and Greece in 1941. [fltsim.1] title=Bf110E 7./ZG 26 sim=Bf110E model= panel= sound= texture=1 panel_alias= sound_alias= kb_checklists= CheckList_3GR_Bf-110G-4/R3 Nachtjaeger kb_reference= atc_id=3U+FR atc_id_color=0xffffffff atc_airline= atc_flight_number=1959 prop_anim_ratio=1.36 visual_damage=1 ui_manufacturer=Messerschmitt ui_type=Bf110E ui_variation=7./ZG 26 ui_createdby=Ground Crew Design ui_typerole=WW2 Fighter Bomber description=Bf110E of III. Gruppe, 7. Staffel Zerstörergeschwader 26 'Horst Wessel', Sicily 1941. [fltsim.2] title=Bf110E 8./ZG 26 sim=Bf110E model= panel= sound= texture=2 panel_alias= sound_alias= kb_checklists= CheckList_3GR_Bf-110G-4/R3 Nachtjaeger kb_reference= atc_id=3U+HS atc_id_color=0xffffffff atc_airline= atc_flight_number=1959 prop_anim_ratio=1.36 visual_damage=1 ui_manufacturer=Messerschmitt ui_type=Bf110E ui_variation=8./ZG 26 ui_createdby=Ground Crew Design ui_typerole=WW2 Fighter Bomber description=Bf110E of III. Gruppe, 8. Staffel Zerstörergeschwader 26 'Horst Wessel', Africa 1941. [fltsim.3] title=Bf110E 9./ZG 26 sim=Bf110E model= panel= sound= texture=3 panel_alias= sound_alias= kb_checklists= CheckList_3GR_Bf-110G-4/R3 Nachtjaeger kb_reference= atc_id=3U+LT atc_id_color=0xffffffff atc_airline= atc_flight_number=1959 prop_anim_ratio=1.36 visual_damage=1 ui_manufacturer=Messerschmitt ui_type=Bf110E ui_variation=9./ZG 26 ui_createdby=Ground Crew Design ui_typerole=WW2 Fighter Bomber description=Bf110E of III. Gruppe, 9. Staffel Zerstörergeschwader 26 'Horst Wessel', Creete 1941. [General] atc_type=Messerschmitt atc_model=Bf110E editable=1 performance=* Weight: 12131 lbs Max 20700 lbs * Power: 1291 hp MIL 1460 hp WEP * 5.0g Corner speed: 225 mph * Max speed @ SL: 318 mph * Max speed: 368 mph @ 19000 ft * Climb rate: 2466 ft/min @ 131 mph Flight Model By: gregoryp AvHistory.org 6/6/04 03:46 PM Flight Model Workbook V2.85.12 Category=airplane [pitot_static] vertical_speed_time_constant=2 pitot_heat=1.000000 [WEIGHT_AND_BALANCE] max_gross_weight=17747 empty_weight=10295 reference_datum_position=0, 0, 0 empty_weight_CG_position=0, 0, 0 CG_forward_limit=0 CG_aft_limit=1 max_number_of_stations = 11 station_load.0 = 200, 4.837, 0.00, 1.00, PILOT // Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = 200, -2.518, 0.00, 1.00, GUNNER // Gunner Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = 0, 0.00, 0.00, 0.00 station_load.3 = 0, 0.00, 0.00, 0.00 station_load.4 = 0, 0.00, 0.00, 0.00 station_load.5 = 0, 0.00, 0.00, 0.00 station_load.6 = 0, 0.00, 0.00, 0.00 station_load.7 = 0, 0.00, 0.00, 0.00 station_load.8 = 0, 0.00, 0.00, 0.00 station_load.9 = 0, 0.00, 0.00, 0.00 station_load.10 = 0, 0.00, 0.00, 0.00 empty_weight_pitch_MOI = 15742 empty_weight_roll_MOI = 21866 empty_weight_yaw_MOI = 35535 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1 parasite_drag_scalar = 1 induced_drag_scalar = 1 elevator_effectiveness = 1 aileron_effectiveness = 1 rudder_effectiveness = 1 pitch_stability = 1 roll_stability = 1 yaw_stability = 1 elevator_trim_effectiveness = 1 //0.1 aileron_trim_effectiveness = 1 rudder_trim_effectiveness = 1 [GeneralEngineData] //======================================LONG=====Lat====Vert======= engine_type = 0 Engine.0 = 7.272, 7.582, 0.080 Engine.1 = 7.272, -7.582, 0.080 fuel_flow_scalar = 1 min_throttle_limit = 0.000000 max_contrail_temperature =-25 //Temperature (deg C) below which contrails may appear [piston_engine] power_scalar = 1 cylinder_displacement = 172.5 compression_ratio = 6.8 number_of_cylinders = 12 max_rated_rpm = 2600 max_rated_hp = 1200 fuel_metering_type = 0 cooling_type = 1 normalized_starter_torque = 0.07 //0.034 turbocharged = 1 max_design_mp = 38.9 min_design_mp = 9 critical_altitude = 22966 emergency_boost_type = 0 emergency_boost_mp_offset = 0 emergency_boost_gain_offset = 0 fuel_air_auto_mixture = 0 auto_ignition = 0 max_rpm_mechanical_efficiency_scalar = 1 idle_rpm_mechanical_efficiency_scalar = 1 max_rpm_friction_scalar = 1 idle_rpm_friction_scalar = 1 fuel_flow_scalar = 1 emergency_boost_duration = 360 [propeller] thrust_scalar = 1 propeller_type = 0 propeller_diameter = 9.833 propeller_blades = 3 propeller_moi = 28.9 beta_max = 65 beta_min = 15 min_gov_rpm = 390 prop_tc = 0.01 gear_reduction_ratio = 1.875 fixed_pitch_beta = 25 low_speed_theory_limit = 80 prop_sync_available = 1 prop_deice_available = 1 prop_feathering_available = 1 prop_auto_feathering_available = 1 min_rpm_for_feather = 700 beta_feather = 88.5 power_absorbed_cf = 0.9 defeathering_accumulators_available = 0 prop_reverse_available = 0 minimum_on_ground_beta = 1 minimum_reverse_beta = -14 rotation = 1, 1 [contact_points] max_number_of_points = 18 //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 point.0 = 1, -24.355, 0, -1.767, 2300, 0, 0.772, 45, 0.165, 1.8, 0.67, 0, 0, 0, point.1 = 1, 2.297, -7.630, -6.93, 2500, 1, 1.534, 0, 0.45, 2, 0.83, 17.0, 17.0, 2, 172, 215 point.2 = 1, 2.297, 7.630, -6.93, 2500, 2, 1.534, 0, 0.45, 2, 0.83, 21.0, 21.0, 3, 172, 215 point.3 = 2, 12.246, 0, 0.615, 2100, 0, 0, 0, 0, 0, 0, 0, 0, 4 point.4 = 2, 2.196, -7.580, -2.392, 3000, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.5 = 2, 2.196, 7.580, -2.392, 3000, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.6 = 2, -2.217, -7.580, -2.198, 3000, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.7 = 2, -2.217, 7.580, -2.198, 3000, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.8 = 2, 8.583, -7.582, -4.36, 3000, 0, 0, 0, 0, 0, 0, 0, 0, 4 point.9 = 2, 0.0, 26.645, 1.585, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.10 = 2, -24.769, 0, 4.902, 700, 0, 0, 0, 0, 0, 0, 0, 0, 9 point.11 = 2, 8.583, -7.582, -1.037, 3750, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.12 = 2, 8.583, 7.582, -1.037, 3750, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.13 = 2, -24.916, 0, 0.074, 2000, 0, 0, 0, 0, 0, 0, 0, 0, 4 point.14 = 2, 0.0, -15.0, 1.345, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.15 = 2, 0.0, 15.0, 1.345, 1000, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.16 = 2, -14.0, 0, -0.594, 3000, 0, 0, 0, 0, 0, 0, 0, 0, 4 point.17 = 2, 7.917, 0, -1.211, 3000, 0, 0, 0, 0, 0, 0, 0, 0, 4 static_pitch = 10.6 static_cg_height = 6.1 gear_system_type = 1 [Views] eyepoint = 4.651, 0.00, 3.0 //orig 3.087 [flaps.0] //Trailing Edge Flaps type = 1 span-outboard = 0.5 extending-time = 5 flaps-position.0 = 0 flaps-position.1 = 16, 214 flaps-position.2 = 33, 204 flaps-position.3 = 50, 195 damaging-speed = 214 blowout-speed = 233 system_type = 1 lift_scalar = 1 //0 drag_scalar = 1 //0 pitch_scalar = 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 160 electric_always_available = 1 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 10, 17 avionics = 1, 5, 17 pitot_heat = 0, 2, 17 additional_system = 0, 20, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 starter2 = 0, 20, 17 starter3 = 0, 20, 17 starter4 = 0, 20, 17 light_nav = 0, 5, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 5, 17 prop_sync = 0, 15, 17 auto_feather = 0, 15, 17 auto_brakes = 0, 15, 17 standby_vacuum = 0, 15, 17 hydraulic_pump = 0, 2, 17 fuel_transfer_pump = 0, 5, 17 propeller_deice = 0, 5, 17 light_recognition = 0, 5, 17 light_wing = 0, 5, 17 light_logo = 0, 5, 17 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 startup = fx_engstrt.fx [SMOKESYSTEM] //===Class==============================VERT======LONG=========LAT=======Effect Name===============(NOTE : VERT NOT RECOG BY FS9)====================================================== SMOKE.0 = 0.00, -3.00, -26.600, FX_HB_BF110E_CONTRAIL_s, SMOKE.1 = 0.00, -3.00, 26.600, FX_HB_BF110E_CONTRAIL_s, [LIGHTS] // types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 6=Taxi, 7=Recognition, 8=Wing, 9=Logo, 10=Cabin //===================================Class====Long=====Lat=====Vert====Effect Name===================================================================== LIGHT.0 = 3, 1.263, -26.392, 1.570, fx_navred, LIGHT.1 = 3, 1.263, 26.392, 1.570, fx_navgre, LIGHT.2 = 3, -27.162, 0.000, 1.735, fx_navwhi, LIGHT.3 = 4, 4.951, 0.000, 3.087, fx_vclighth, LIGHT.4 = 5, 2.931, -13.333, 0.617, fx_landing, //==================================================== CANNON EFFECTS ============ RCB NEEDED ============================================================================== //====================================CLASS===LONG======LAT=====VERT=====EFFECT NAME====================================================================== light.5 = 10, 11.920, -0.410, 1.580, SpitfireCannon, // PORT INSIDE TOP COWL MG17 7.9mm light.6 = 10, 11.350, -0.870, 1.180, SpitfireCannon, // PORT OUTSIDE MIDDLE COWL MG17 7.9mm light.7 = 10, 12.350, 0.390, 1.580, SpitfireCannon, // STARB INSIDE TOP COWL MG17 7.9mm light.8 = 10, 11.380, 0.870, 1.180, SpitfireCannon, // STARB OUTSIDE MIDDLE COWL MG17 7.9mm LIGHT.9 = 10, 10.300, -0.333, -0.580, SpitfireCannon, // MG FF 20mm cannon LIGHT.10 = 10, 10.300, 0.333, -0.580, SpitfireCannon, // MG FF 20mm cannon //=========================================== KRAZY'S EXH ==================================================================================================== LIGHT.11 = 6, 3.533, -9.320, 0.375, FX_HB_BF110E_OUTSIDE_PORT LIGHT.12 = 6, 3.533, 9.320, 0.375, FX_HB_BF110E_OUTSIDE_STARB LIGHT.13 = 6, 3.300, -5.880, -1.000, FX_HB_BF110E_INSIDE_PORT LIGHT.14 = 6, 3.300, 5.880, -1.000, FX_HB_BF110E_INSIDE_STARB [keyboard_response] elevator = 350, 500 aileron = 450, 1000 rudder = 200, 1000 [direction_indicators] direction_indicator.0 = 1, 0 [exits] number_of_exits = 1 exit_rate.0 = 0.4 [autopilot] autopilot_available = 1 flight_director_available = 0 default_vertical_speed = 1000 autothrottle_available = 0 autothrottle_arming_required = 0 autothrottle_max_rpm = 90 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8 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 [fuel] //=Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(US gallons), Unusable (US gallons) LeftMain = 0.935, -3.658, 0.00, 96.06452, 3.0 RightMain = 0.935, 3.658, 0.00, 96.06452, 3.0 LeftAux = -1.75, -3.658, 0.00, 66.68473, 2.0 RightAux = -1.75, 3.658, 0.00, 66.68473, 2.0 fuel_type = 1 number_of_tank_selectors = 2 electric_pump = 1 [airplane_geometry] wing_area = 413.33 wing_span = 53.2708333333333 wing_root_chord = 7.75903011341416 wing_dihedral = 5.5 wing_incidence = 0 wing_twist = 0 oswald_efficiency_factor = 0.790121889842047 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 1.93975752835354 wing_pos_apex_vert = 0 htail_area = 36.78 htail_span = 15.12 htail_pos_lon =-25.58 htail_pos_vert = 0 htail_incidence = 0 htail_sweep = 0 vtail_area = 18.78 vtail_span = 5.06 vtail_sweep = 0 vtail_pos_lon =-25.58 vtail_pos_vert = 0 elevator_area = 19.288 aileron_area = 13.244 rudder_area = 14.34 elevator_up_limit = 27 elevator_down_limit = 24 aileron_up_limit = 22.4 aileron_down_limit = 11.2 rudder_limit = 32 elevator_trim_limit = 18 spoiler_limit = 1 spoilerons_available = 0 aileron_to_spoileron_gain = 0 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 auto_spoiler_available=0 spoiler_extension_time=1.000000 positive_g_limit_flaps_up=3.750000 positive_g_limit_flaps_down=3.750000 negative_g_limit_flaps_up=-2.250000 negative_g_limit_flaps_down=-2.250000 [Reference Speeds] flaps_up_stall_speed = 79.1 full_flaps_stall_speed = 66 cruise_speed = 146 max_indicated_speed = 382.796 [brakes] toe_brakes_scale = 0.641 parking_brake = 1 [gear_warning_system] gear_warning_available = 0 pct_throttle_limit = 0.0999 flap_limit_power = 37.500 flap_limit_idle = 18.750 [hydraulic_system] electric_pumps = 0 engine_map = 1, 1, 0, 0 normal_pressure = 1000.00 [stall_warning] type = 1 stick_shaker=1 [attitude_indicators] attitude_indicator.0 = 1 [turn_indicators] turn_indicator.0 = 1, 0 [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 [vacuum_system] max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=4.900000 engine_map=1,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=0.150000 [deice_system] structural_deice_type=0