[fltsim.0]
title=Raytheon B1900D - MOZAMBIQUE
sim=b19lam2k
model=
panel=
sound=
texture=
kb_checklists=Beech_B1900D_check
kb_reference=Beech_B1900D_ref
ui_manufacturer=Raytheon
ui_type=B1900D
ui_variation=Brawn cream
atc_type=Beechcraft
atc_id_enable=1
atc_id=CS-VMA
editable=0
description=Raytheon-Beechcraft B1900D\nTwin Turbo Prop Regional Airliner\nLAM - Mozambique Reg # CS-VMA\nDesign,FD,MP,Graphics\nby Barry Blaisdell\nFS2K paint & night textures\nby Mario Coelho\nPremier Aircraft Design\nhttp:\/\/www.flightsimnetwork.com\/premaircraft\/\n\n

[forcefeedback]
stick_shaker_magnitude=5000		; 0 - 10000
stick_shaker_direction=0		; 0 - 35999 degrees
stick_shaker_period=111111		; in microseconds
gear_bump_nose_magnitude=3000		; 0 - 10000
gear_bump_nose_direction=18000		; 0 - 35999 degrees
gear_bump_nose_duration=250000		; in microseconds
gear_bump_left_magnitude=2700		; 0 - 10000
gear_bump_left_direction=9000		; 0 - 35999 degrees
gear_bump_left_duration=250000		; in microseconds
gear_bump_right_magnitude=2700		; 0 - 10000
gear_bump_right_direction=27000		; 0 - 35999 degrees
gear_bump_right_duration=250000		; in microseconds
ground_bumps_magnitude1=1300		; 0 - 10000
ground_bumps_angle1=08900		; 0 - 35999 degrees
ground_bumps_intercept1=3.0
ground_bumps_slope1=0.20
ground_bumps_magnitude2=200		; 0 - 10000
ground_bumps_angle2=09100		; 0 - 35999 degrees
ground_bumps_intercept2=1.075
ground_bumps_slope2=0.035
crash_magnitude1=10000			; 0 - 10000
crash_direction1=01000			; 0 - 35999 degrees
crash_magnitude2=10000			; 0 - 10000
crash_direction2=9000			; 0 - 35999 degrees
crash_period2=75000			; in microseconds
crash_duration2=2500000			; in microseconds

[WEIGHT_AND_BALANCE]
empty_weight=9090				// (pounds)
reference_datum_position=0.0, 0, 0	// (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0.0, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
station_load.0=170,  5.0, -2.0, 0.0		//Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=170,  5.0,  2.0, 0.0		//Co-Pilot        Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=170, -2.1, -2.0, 0.0		//Passenger       Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=170, -2.1,  2.0, 0.0		//Passenger       Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=170, -5.3, -2.0, 0.0		//Passenger       Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5=170, -5.3,  2.0, 0.0		//Passenger       Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6=170, -8.9, -2.0, 0.0		//Passenger       Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
empty_weight_roll_MOI=36455.000000
empty_weight_pitch_MOI=31143.000000
empty_weight_yaw_MOI=54792.000000
empty_weight_coupled_MOI=1300.000000

[pitot_static]
vertical_speed_time_constant=1		//Increasing this value will cause a more instantaneous reaction in the VSI

[electrical]
max_battery_voltage=0

[General]
performance=19  Passenger\nTwin Turboprop\nRegional Commuter\nLength:57 ft - 10 in\nWing Span: 58ft\nHeight: 15 ft - 6 in\nZFW : 15,000 lb\n16,950# MTOW\nStall 84\/101\nMax Cruise: 288 kt\nMax ROC 2500 fpm@SL\nPower: 2 x 1279 shp\nP&WCanada PT6A-67D\nMax Fuel: 665 USG\nRange: 1500 nm\nDesigner: Barry Blaisdell\nbarrywb@snet.net\nPainted by Mario Coelho\nmcrabbit@iol.pt \nSept, 2001\n\n

[fuel]
LeftMain=0.000000,0.000000,0.000000,332.000000,0.000000
RightMain=0.000000,0.000000,0.000000,332.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area=343.000000
wing_span=57.833333
wing_root_chord=5.916667
wing_dihedral=5.998535
wing_incidence=0.000000
wing_twist=-0.999756
oswald_efficiency_factor=1.707327
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=100.000000
htail_span=20.000000
htail_pos_lon=-25.000000
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=90.000000
vtail_span=10.816654
vtail_sweep=0.000000
vtail_pos_lon=-27.000000
vtail_pos_vert=5.833333
elevator_area=25.000000
aileron_area=12.120000
rudder_area=15.300000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=14.896903
rudder_limit=23.491270
elevator_trim_limit=19.480565
spoiler_limit=59.988681
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[contact_points]
point.0=1.000000,13.166667,0.000000,-4.583333,1574.803150,0.000000,0.602106,39.480000,0.255676,2.500000,0.700990,6.000000,6.000000,0.000000,0.000000,0.000000
point.1=1.000000,-1.833333,-8.416667,-4.750000,1574.803150,1.000000,0.602106,0.000000,0.255806,2.500000,0.700900,9.000000,9.000000,2.000000,0.000000,0.000000
point.2=1.000000,-1.833333,8.416667,-4.750000,1574.803150,2.000000,0.602106,0.000000,0.255806,2.500000,0.700900,9.000000,9.000000,3.000000,0.000000,0.000000
point.3=2.000000,2.166667,-33.416667,4.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,2.166667,33.416667,4.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-26.416667,0.000000,-1.083333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,14.000000,0.000000,-1.083333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=0.000000
static_cg_height=4.917881

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=19.996227,0.000000
flaps-position.2=39.992454,0.000000

[GeneralEngineData]
engine_type=1
Engine.0=3.000000,-9.250000,-0.166667
Engine.1=3.000000,9.250000,-0.166667
fuel_flow_scalar=1.000000

[TurbineEngineData]
fuel_flow_gain=0.001172
inlet_area=3.485280
rated_N2_rpm=29920.000000
static_thrust=2904.400000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=101.000000
full_flaps_stall_speed=80.800000
cruise_speed=288.996090

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=13.661622,-1.166236,4.998155

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=3,0