[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