[fltsim.0]
title=FB-Armee de l'Air
sim=morane
model=
panel=
sound=
texture=
checklists=
kb_checklists=test
kb_reference=test
atc_id=
atc_id_color=0x00333333
ui_manufacturer=Morane
ui_type=MS 317
ui_variation=Armee de l'Air
description=The MS.315 was developed from the earlier MS.300 primary trainer and related variants and first flew in October 1932. The MS.315 is a parasol-wing monoplane with a tailwheel landing gear with divided main gear and powered by a 135hp (101kW) Salmson 9Nc radial engine. A production run of 346 aircraft followed the four prototypes including 33 of them built after the second world war. Five high-powered MS.317/2 variants were also produced for the civil marker and a single MS.316 powered by a Regnier inverted Vee engine.  In the 1960s 40 MS.315 used as civil glider tugs were modified with a 220hp (164kW) Continental W-670K radial engine and re-designated the MS.317.
atc_heavy=0
atc_id_font=Arial Rounded MT Bold,37,1,600,0
visual_damage=0
atc_id_enable=1
atc_id_font=Arial Rounded MT Bold,37,1,600,0
atc_id_color=0x00333333
atc_id=
atc_airline=
atc_flight_number=
atc_parking_codes=DLH
atc_parking_types=RAMP
atc_heavy=0

[fltsim.1]
title=FB-Aeronavale
sim=morane
model=
panel=
sound=
texture=1
checklists=
kb_checklists=test
kb_reference=test
atc_id=
atc_id_color=0x00333333
ui_manufacturer=Morane
ui_type=MS 317
ui_variation=Aéronavale
description=The MS.315 was developed from the earlier MS.300 primary trainer and related variants and first flew in October 1932. The MS.315 is a parasol-wing monoplane with a tailwheel landing gear with divided main gear and powered by a 135hp (101kW) Salmson 9Nc radial engine. A production run of 346 aircraft followed the four prototypes including 33 of them built after the second world war. Five high-powered MS.317/2 variants were also produced for the civil marker and a single MS.316 powered by a Regnier inverted Vee engine.  In the 1960s 40 MS.315 used as civil glider tugs were modified with a 220hp (164kW) Continental W-670K radial engine and re-designated the MS.317.
atc_heavy=0
atc_id_font=Arial Rounded MT Bold,37,1,600,0
visual_damage=0
atc_id_enable=1
atc_id_font=Arial Rounded MT Bold,37,1,600,0
atc_id_color=0x00333333
atc_id=
atc_airline=
atc_flight_number=
atc_parking_codes=DLH
atc_parking_types=RAMP
atc_heavy=0

prop_anim_ratio=-1.25

[General]
performance=General characteristics\n\nCrew: 2\nLength: 7.60 m (24 ft 11¼ in)\nWingspan: 12.00 m (39 ft 4½ in)\nHeight: 2.80 m (9 ft 2¼ in)\nWing area: 21.60 m² (232.51 ft²)\nEmpty weight: 548 kg (1208 lb)\nGross weight: 860 kg (1896 lb)\nPowerplant: 1 × Salmson 9Nc radial engine\n101 kW (135 hp)\n\nPerformance\n\nMaximum speed: 170 km/h (106 mph)\nService ceiling: 5500 m (18,045 ft)
atc_type=
atc_model=
editable=1
Category=airplane

[weight_and_balance]
// ACM V2.3
max_gross_weight = 5864.3
empty_weight = 3086
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -0.3, 0, 0
empty_weight_pitch_MOI = 8533
empty_weight_roll_MOI = 5249
empty_weight_yaw_MOI = 10972
empty_weight_coupled_MOI = 0
max_number_of_stations = 3
station_load.0 = 180, 0.0,-1.2, 1.3, Pilot
station_load.1 = 180, 0.0, 1.2, 1.3, Kopilot
station_load.2 = 100,-4.0, 0.0,-1.0, Fracht

[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4, -2.85, 0, 1.71, fx_vclight

[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 0
fuel_flow_scalar = 0.866
engine.0 = 6, 0, 0,

[smokesystem]
smoke.0 = 0.31, 6.36, 0, fx_W33a_smoke.fx

[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1

[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1
number_of_tank_selectors = 1
Center1 = 0, 0, 0, 63, 0
electric_pump=0

[contact_points]
static_pitch = 12.94
static_cg_height = 5.2
tailwheel_lock = 0
max_number_of_points = 7
point.0 = 1, -15.0409, 0, -2.0375, 6000, 0, 0.3, 0, 0.1, 2.5, 1, 0, 0, 0, 0, 0
point.1 = 1, 1.8, -4.6999, -5.9, 4000, 0, 1.2, 0, 0.3, 2.5, 0.6, 0, 0, 2, 0, 0
point.2 = 1, 1.8, 4.7, -5.9, 4000, 0, 1.2, 0, 0.3, 2.5, 0.6, 0, 0, 3, 0, 0
point.3 = 2, 0.2726, -19.5, 3.0079, 6000, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, 0.2877, 19.5, 3.0148, 6000, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -16.8986, 0, 5.3367, 2000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 6.2786, 0, -1.9584, 500, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0

[keyboard_response]
elevator = 100.0000, 180.0000
aileron = 200.0000, 1000.0000
rudder = 200.0000, 1000.0000

[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 = 00500
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 3250
ground_bumps_angle1 = 8900
ground_bumps_intercept1 = 5.0
ground_bumps_slope1 = 0.48
ground_bumps_magnitude2 = 750
ground_bumps_angle2 = 9100
ground_bumps_intercept2 = 0.075
ground_bumps_slope2 = 1.0
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000

[airplane_geometry]
//ACM_AREAW1// 0,0,0,2.4079,0.9861,0.9861,0.0516,2.3392,1.9723,1.9723
//ACM_AREAW2// 0.1032,2.2704,2.9591,2.9591,0.1550,2.2018,3.9453,3.9453,0.2064,2.1331
//ACM_AREAW3// 4.9317,4.9317,0.2583,2.0643,5.9182,5.9182,0.3100,1.9957,6.9045,6.9045
//ACM_AREAW4// 0.3616,1.9270,7.8909,7.8909,0.4135,1.8581,8.8773,8.8773,0.4652,1.7891
//ACM_AREAH1// 0,0,0,1.5341,0.2556,0.2556,0,1.4572,0.5113,0.5113
//ACM_AREAH2// 0,1.3803,0.7670,0.7670,0,1.3040,1.0226,1.0226,0,1.2273
//ACM_AREAH3// 1.2783,1.2783,0,1.1505,1.5341,1.5341,0,1.0736,1.7898,1.7898
//ACM_AREAH4// 0,0.9972,2.0455,2.0455,0,0.9204,2.3011,2.3011,0,0.8435
//ACM_AREAV1// 0,0,0,1.7983,0.1993,0.1993,0.0571,1.7115,0.3995,0.3995
//ACM_AREAV2// 0.1145,1.6251,0.5993,0.5993,0.1718,1.5384,0.7990,0.7990,0.2291,1.4520
//ACM_AREAV3// 0.9990,0.9990,0.2863,1.3653,1.1986,1.1986,0.3436,1.2788,1.3983,1.3983
//ACM_AREAV4// 0.4009,1.1921,1.5985,1.5985,0.4582,1.1057,1.7983,1.7983,0.5156,1.0190
//ACM_CAREAW1// 4.4386,4.4386,1.4364,1.9177,4.9317,4.9317,1.4622,1.9198,5.4250,5.4250
//ACM_CAREAW2// 1.4881,1.9213,5.9182,5.9182,1.5140,1.9234,6.4113,6.4113,1.5398,1.9249
//ACM_CAREAW3// 6.9045,6.9045,1.5657,1.9270,7.3976,7.3976,1.5915,1.9285,7.8909,7.8909
//ACM_CAREAW4// 1.6174,1.9305,8.3837,8.3837,1.6433,1.9321,8.8773,8.8773,1.6691,1.9340
//ACM_CAREAH1// 0,0,0.7670,1.5341,0.2556,0.2556,0.7670,1.4958,0.5113,0.5113
//ACM_CAREAH2// 0.7670,1.4572,0.7670,0.7670,0.7670,1.4190,1.0226,1.0226,0.7670,1.3803
//ACM_CAREAH3// 1.2783,1.2783,0.7670,1.3423,1.5341,1.5341,0.7670,1.3040,1.7898,1.7898
//ACM_CAREAH4// 0.7670,1.2654,2.0455,2.0455,0.7670,1.2273,2.3011,2.3011,0.7670,1.1885
//ACM_CAREAV1// 0,0,0.4494,1.3487,0.1993,0.1993,0.5066,1.3341,0.3995,0.3995
//ACM_CAREAV2// 0.5641,1.3193,0.5993,0.5993,0.6212,1.3048,0.7990,0.7990,0.6786,1.2898
//ACM_CAREAV3// 0.9990,0.9990,0.7360,1.2755,1.1986,1.1986,0.7932,1.2609,1.3983,1.3983
//ACM_CAREAV4// 0.8506,1.2460,1.5985,1.5985,0.9078,1.2316,1.7983,1.7983,0.9652,1.2170
wing_area = 463.0
wing_span = 58.250
wing_root_chord = 7.900
wing_dihedral = 6.0
wing_incidence = 3.200
wing_twist = 0.0
oswald_efficiency_factor = 0.680
wing_winglets_flag = 0
wing_sweep = 3.0
wing_pos_apex_lon = 2.500
wing_pos_apex_vert = 1.300
htail_area = 64.0
htail_span = 15.100
htail_pos_lon = -21.300
htail_pos_vert = 1.800
htail_incidence = 1.0
htail_sweep = 0.0
vtail_area = 29.0
vtail_span = 5.900
vtail_sweep = 16.0
vtail_pos_lon = -21.700
vtail_pos_vert = 3.100
elevator_area = 31.0
aileron_area = 59.0
rudder_area = 18.0
elevator_up_limit = 31.0
elevator_down_limit = 22.0
aileron_up_limit = 20.0
aileron_down_limit = 15.0
rudder_limit = 21.0
elevator_trim_limit = 5.0
spoiler_limit = 90.0
aileron_to_spoileron_gain = 0.0
min_ailerons_for_spoilerons = 0.0
min_flaps_for_spoilerons = 0.0
spoilerons_available = 0
auto_spoiler_available=0
spoiler_extension_time=0.000000
positive_g_limit_flaps_up=3.000000
positive_g_limit_flaps_down=2.000000
negative_g_limit_flaps_up=-2.000000
negative_g_limit_flaps_down=-2.000000

[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 60
electric_always_available = 0

[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;Percent per second

[Flaps.0]
type=0
span-outboard=0.000000
extending-time=0.000000
system_type=0

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=2.0
aileron_effectiveness=5.0
rudder_effectiveness=1.0
pitch_stability=2.0
roll_stability=1.4
yaw_stability=1.3
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[Reference Speeds]
flaps_up_stall_speed=54
full_flaps_stall_speed=54
cruise_speed=97
max_indicated_speed=162.0000

[piston_engine]
power_scalar=1.0                              //Piston power scalar
cylinder_displacement=232.91                   //Cubic inches per cylinder
compression_ratio=5.5                          //Compression ratio
number_of_cylinders=6                           //Number of cylinders
max_rated_rpm=2500                             //Max rated RPM
max_rated_hp=310                               //Max rated HP
fuel_metering_type=1                           //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type=1                                 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque=0.3                  //Starter torque factor
turbocharged=0                                 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp=0                                //Max design manifold pressure, (inHg)
min_design_mp=0                                //Min design manifold pressure, (inHg)
critical_altitude=0                            //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type=0                         //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset=0                    //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset=0                  //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture=0                        //Automixture available? 0=FALSE, 1=TRUE
auto_ignition=0                                //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar=0.8       //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar=1.0      //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar=1.0                    //Scalar on maximum RPM friction
idle_rpm_friction_scalar=1.8                   //Scalar on idle RPM friction

[propeller]
thrust_scalar=1.0                             //Propeller thrust scalar
propeller_type=1                               //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=9.84                        //Propeller Diameter, (feet)
propeller_blades=2                             //Number of propeller blades
propeller_moi=16                               //Propeller moment of inertia
beta_max=0                                     //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=0                                     //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=0                                  //Miminum governed RPM
prop_tc=0.1                                    //Prop time-constant
gear_reduction_ratio=1.0                       //Propeller gear reduction ratio
fixed_pitch_beta=25                            //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80                      //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=0                          //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1                         //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=0                    //Prop feathering available?  0=FALSE, 1=TRUE
prop_auto_feathering_available=0               //Prop auto-feathering available?  0=FALSE, 1=TRUE
min_rpm_for_feather=0                          //Minimum RPM for prop feathering
beta_feather=0                                 //Feathering pitch angle (degrees)
power_absorbed_cf=0                            //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0          //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=0                       //Prop reverse available?  0=FALSE, 1=TRUE
minimum_on_ground_beta=0                       //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=0                         //Minimum pitch angle in reverse, (degrees)

[Views]
eyepoint=-4.00,0.00,2.00

[anemometers]
anemometer.0 = -4,6, 0.0, 4.8     //Position from Datum

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=300.0000
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=100
pitch_takeoff_ga=8.0000
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10.0000
max_pitch_acceleration=1.0000
max_pitch_velocity_lo_alt=2.0000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.0000
max_pitch_velocity_hi_alt_breakpoint=28000.0000
max_bank=25.0000
max_bank_acceleration=1.800000
max_bank_velocity=3.0000
max_throttle_rate=0.100000
nav_proportional_control=9.0000
nav_integrator_control=0.250000
nav_derivative_control=0.0000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.0000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.0000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.0000
yaw_damper_gain=0.0000

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.0=0
Audio.1=0
Com.1=0, 0
Com.2=0, 0
Nav.1=0, 0, 0
Nav.2=0, 0, 0
Adf.1=0
Transponder.1=0
Marker.1=0

[brakes]
brakes_available=0
toe_brakes_scale=0.5
parking_brake=1
differential_braking_scale = 1.0

[hydraulic_system]
normal_pressure=0.0000

[stall_warning]
type=1
stick_shaker=0

[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=2,0

[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2

[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.000000
vacuum_type=1
electric_backup_pressure=0.000000
engine_map=0,1,0,0
[pneumatic_system]
max_pressure=0.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0
[CameraDefinition.201]
Title=EZdok Aircraft Universal camera
Guid={D8D67955-2E9B-4e75-9D8B-8EFFBBFAC65B}
Description=Universal camera for EZdok cam utility
Origin=Center
SnapPbhAdjust=Swivel
SnapPbhReturn=FALSE
PanPbhAdjust=Swivel
PanPbhReturn=FALSE
Track=None
ShowAxis=FALSE
AllowZoom=TRUE
InitialZoom=0.40
ShowWeather=Yes
InitialXyz=0,0,0
InitialPbh=10, 0, 0
XyzAdjust=TRUE
Category=Aircraft
MomentumEffect=FALSE
ClipMode=Minimum
HotKeySelect=4
