[fltsim.0]
title=Spifire Mk1a
sim=Spit1A
model=
panel=
sound=
texture=
KB_checklists =Spit1A_Check
atc_id=Spit Mk1
atc_airline=WARBIRD
atc_flight_number=1A
atc_heavy=0
ui_manufacturer=Supermarine
ui_type=fighter RAF
ui_variation=1A
visual_damage=1
description=Supermarine Spitfire Mk IA, JZ-E (AR213), 57 OTU, RAF, flown by F/O J.H. "Ginger" Lacey, 1942.




[General]
performance=Length:  29' 11" \nHeight:  11' 4.75" \nWingspan:  36' 10" \nEmpty Weight:  4,900 lb \nGross Weight:  5,900 lb \nMaximum Speed:  365 mph \nService Ceiling:  37,200 ft \nRange:  510 miles \nPowerplant:  One Rolls Royce V-1650-7 Merlin 1,030 hp \n12 cylinder V12 inline \nArmament:  Eight MG 0.303 in Browning\n\nGMAX model by A.F.Scrub March 2009\n
Category=airplane

[LIGHTS]
         
//#1=beacon  #2=strobe  #3=nav    #10=reheat
//#4=cockpit #5=landing #6=taxi
//#7=recog   #8=wing    #9=logo
//---------------originals----------------------------
light.0=5,    6.00,   -19.0,  -1.20,  fx_navred
light.1=5,    6.00,   19.0,   -1.40,  fx_navgre
light.2=5,   -1.66,    0.00,  -3.50,  fx_beacon
light.3=5,  -17.20,    0.00,   1.00,  fx_beacon 


/---------- ExhaustFlames--------uses wing/taxi/logo 
//index,type,  long,   lat,    vert,  fx_filename 
light.4=8,   8.0,   -1.60,   0.2,  fx_V12_IDLE_port 
light.5=8,   8.0,    1.60,   0.2,  fx_V12_IDLE_starb 
light.6=6,   8.0,   -1.60,   0.2,  fx_V12_MAX_port 
light.7=6,   8.0,    1.60,   0.2,  fx_V12_MAX_starb 
light.8=9,   8.0,   -1.60,   0.2,  fx_V12_Exhaust 
light.9=9,   8.0,    1.60,   0.2,  fx_V12_Exhaust 


//------------ Guns ----------------------uses strobe
light.10=2,   8.50,    7.10, -2.1,  Fx_Wing_guns
light.11=2,   8.50,   -7.10, -2.1,  Fx_Wing_guns
light.12=2,   8.40,    10.10, -1.9,  Fx_Wing_guns
light.13=2,   8.40,   -10.10, -1.9,  Fx_Wing_guns
light.14=2,   8.00,    13.0, -1.7,  Fx_Wing_guns
light.15=2,   8.00,   -13.0, -1.7,  Fx_Wing_guns

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
empty_weight=5088.000000
empty_weight_roll_MOI=6039.000000
empty_weight_pitch_MOI=8279.000000
empty_weight_yaw_MOI=12990.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=7632.000000
[fuel]
Center1=1.000000,0.000000,0.000000,48.000000,0.000000
Center2=-5.280000,0.000000,0.980000,37.000000,0.000000
LeftMain=0.400000,-5.100000,0.000000,14.000000,0.000000
RightMain=0.400000,5.100000,0.000000,14.000000,0.000000
External1=-0.600000,0.000000,-1.400000,50.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=235.000000
wing_span=37.000000
wing_root_chord=6.333333
wing_dihedral=4.998779
wing_incidence=0.000000
wing_twist=0.000000
oswald_efficiency_factor=0.890997
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=28.000000
htail_span=14.750000
htail_pos_lon=-16.666667
htail_pos_vert=0.000000
htail_incidence=-0.192261
htail_sweep=0.000000
vtail_area=13.000000
vtail_span=4.110961
vtail_sweep=0.000000
vtail_pos_lon=-17.250000
vtail_pos_vert=5.500000
elevator_area=13.050000
aileron_area=12.730000
rudder_area=10.410000
elevator_up_limit=30.000000
elevator_down_limit=20.000000
aileron_up_limit=15.000000
aileron_down_limit=15.000000
rudder_limit=30.000000
elevator_trim_limit=18.000000
spoiler_limit=60.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
auto_spoiler_available=0
spoiler_extension_time=10.000000
positive_g_limit_flaps_up=7.500000
positive_g_limit_flaps_down=5.000000
negative_g_limit_flaps_up=-6.000000
negative_g_limit_flaps_down=-5.000000

[contact_points]
point.0=1.000000,-18.583333,0.000000,-1.833333,1574.803150,0.000000,0.542052,43.380000,0.479464,2.500000,0.772717,5.000000,5.000000,0.000000,0.000000,0.000000
point.1=1.000000,3.333333,-4.500000,-6.166667,1574.803150,1.000000,0.542052,0.000000,0.389267,2.500000,0.516121,5.000000,5.000000,2.000000,0.000000,0.000000
point.2=1.000000,3.333333,4.500000,-6.166667,1574.803150,2.000000,0.542052,0.000000,0.389267,2.500000,0.516121,5.000000,5.000000,3.000000,0.000000,0.000000
point.3=2.000000,0.416667,-17.083333,-1.666667,2175.542876,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,0.416667,17.083333,-1.666667,2175.542876,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-19.583333,0.000000,-1.666667,2175.542876,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,7.666667,0.000000,-3.500000,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=10.953369
static_cg_height=5.420807
gear_system_type=1


[brakes]
toe_brakes_scale=1.000000
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=1
flaps-position.0=0.000000,0.000000
flaps-position.1=45.000000,0.000000
[GeneralEngineData]
engine_type=0
Engine.0=9.250000,0.000000,0.000000
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000
[piston_engine]
cylinder_displacement=137.500000
compression_ratio=6.000000
number_of_cylinders=12
max_rated_rpm=2800.000000
max_rated_hp=1030.000000
fuel_metering_type=0
cooling_type=1
normalized_starter_torque=0.035000
turbocharged=1
max_design_mp=60.999999
min_design_mp=1.000000
critical_altitude=25000.000000
emergency_boost_type=3
emergency_boost_mp_offset=6.100000
emergency_boost_gain_offset=0.540000
fuel_air_auto_mixture=1
auto_ignition=1
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_diameter=11.167000
propeller_blades=3
propeller_moi=42.506502
beta_max=65.000000
beta_min=15.000000
min_gov_rpm=1200.000000
prop_tc=0.010000
gear_reduction_ratio=2.380000
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0.000000
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000
[Reference Speeds]
flaps_up_stall_speed=80.000000
full_flaps_stall_speed=64.000000
cruise_speed=250.000000
max_indicated_speed=444.398438
[keyboard_response]
elevator=350.000000,500.000000
aileron=450.000000,1000.000000
rudder=200.000000,1000.000000

[Views]
eyepoint=0.294763,0.000000,1.666052

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
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
[hydraulic_system]
electric_pumps=0
engine_map=1,0,0,0
normal_pressure=6.930556
[stall_warning]
type=1
stick_shaker=0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=1,0
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=1,1,1,1
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=0.000000
[deice_system]
structural_deice_type=0