[fltsim.0]
title=BRF738W
sim=737800
model=
panel=
sound=
texture=
kb_checklists=Boeing737-400_check
kb_reference=Boeing737-400_ref
atc_id=A9C-AWL
atc_airline=Bahrain Royal Flight
atc_flight_number=1
ui_manufacturer=Boeing
ui_type=BBJ2
ui_variation=Bahrain Royal Flight
description=On October 11, 1999 Boeing launched the BBJ2, based on the stretched 737-800 airframe, which is 5.84m (19ft 2in) longer than the BBJ, and is offering 25% greater cabin space (and 100% more baggage space), but has slightly reduced range. It is fitted with between three and seven auxiliary belly fuel tanks. The winglets are standard on this version. The first delivery was made on February 28, 2001.
atc_heavy=0
visual_damage=1
[General]
atc_type=BOEING AIRCRAFT
atc_model=B738
performance=Power: 2x CFM56-7B26 @ 26438 lbs\/thrust\nMTOW: 172,475 lbs\nMLW: 144,009 lbs (70% fuel)\nZFW: 126,200 lbs\nV1\/VR\/V2: 135\/145\/165 kts (MTOW)\nVref: 135-140 kts (MLW)\nNormal Cruise: M.78-M.80\nRange: 3383nm\nLength: 129 ft 6 in (33.6 m)\nHeight: 41 ft 2 in (12.5 m)\nWingspan: 112 ft 7 in (34.4 m). 737-700 FDE by Shawn Anderson - Project Kittyhawk.
[forcefeedback]
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=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 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
[flight_tuning]
cruise_lift_scalar= 0.83
pitch_stability= 1.20
roll_stability= 1.10
yaw_stability= 1.10
parasite_drag_scalar= 1.20
induced_drag_scalar= 1.20
elevator_effectiveness= 1.00
aileron_effectiveness= 0.90
rudder_effectiveness= 0.90
elevator_trim_effectiveness= 0.32
aileron_trim_effectiveness= 1.00
rudder_trim_effectiveness= 1.00
[WEIGHT_AND_BALANCE]
reference_datum_position=0.00,0.00,0.00
empty_weight_CG_position=0.00,0.00,0.00
max_number_of_stations=60
station_load.0=200,60.00,-1.90,4.00
station_load.1=190,60.00, 1.90,4.00
station_load.2=6216,14.50,-17.30,-4.10
station_load.3=6216,14.50, 17.30,-4.10
station_load.4=800,55.50,-2.50,3.80
station_load.5=800,55.50, 2.50,3.80
station_load.6=800,52.16,-2.50,3.80
station_load.7=340,48.82,-2.50,4.00
station_load.8=170,48.82,2.50,4.00
station_load.9=413,45.48,-2.50,4.00
station_load.10=270,45.48,2.50,4.00
station_load.11=190,42.14,-2.50,4.00
station_load.12=380,42.14,2.50,4.00
station_load.13=340,38.80,-2.50,4.00
station_load.14=510,38.80,2.50,4.00
station_load.15=250,35.46,-2.50,4.00
station_load.16=170,35.46,2.50,4.00
station_load.17=340,32.12,-2.50,4.00
station_load.18=510,28.78,-2.50,4.00
station_load.19=170,28.78,2.50,4.00
station_load.20=340,25.44,2.50,4.00
station_load.21=510,22.10,-2.50,4.00
station_load.22=340,22.10,2.50,4.00
station_load.23=170,18.76,-2.50,4.00
station_load.24=370,18.76,2.50,4.00
station_load.25=340,15.42,2.50,4.00
station_load.26=510,12.08,-2.50,4.00
station_load.27=170,12.08,2.50,4.00
station_load.28=260,8.74,-2.50,4.00
station_load.29=170,8.74,2.50,4.00
station_load.30=340,5.40,-2.50,4.00
station_load.31=510,5.40,2.50,4.00
station_load.32=510,2.06,-2.50,4.00
station_load.33=170,2.06,2.50,4.00
station_load.34=170,-1.28,-2.50,4.00
station_load.35=340,-1.28,2.50,4.00
station_load.36=170,-4.62,2.50,4.00
station_load.37=510,-7.96,-2.50,4.00
station_load.38=510,-7.96,2.50,4.00
station_load.39=290,-11.30,-2.50,4.00
station_load.40=170,-11.30,2.50,4.00
station_load.41=840,-14.64,-2.50,4.00
station_load.42=170,-17.98,2.50,4.00
station_load.43=510,-21.32,-2.50,4.00
station_load.44=190,-21.32,2.50,4.00
station_load.45=340,-24.66,2.50,4.00
station_load.46=340,-28.00,-2.50,4.00
station_load.47=340,-28.00,2.50,4.00
station_load.48=810,-31.34,-2.50,4.00
station_load.49=290,-31.34,2.50,4.00
station_load.50=190,-34.68,-2.50,4.00
station_load.51=340,-38.02,2.50,4.00
station_load.52=340,-41.36,-2.50,4.00
station_load.53=510,-41.36,2.50,4.00
station_load.54=170,-44.70,-2.50,4.00
station_load.55=290,-44.70,2.50,4.00
station_load.56=170,-48.04,2.50,4.00
station_load.57=2900,-51.50,0.00,3.80
station_load.58=6750,35.00,0.00,-1.00
station_load.59=8300,-25.00,0.00,-1.00
empty_weight=83790.00
empty_weight_roll_MOI=1854568.00
empty_weight_pitch_MOI=1794268.00
empty_weight_yaw_MOI=2209567.00
empty_weight_coupled_MOI=1300.00
max_gross_weight=154500.000000
[GeneralEngineData]
engine_type= 1
Engine.0= 13.50, -17.30, -4.10
Engine.1= 13.50, 17.30, -4.10
fuel_flow_scalar=0.6273
min_throttle_limit=-0.299902
[TurbineEngineData]
fuel_flow_gain= 0.0020
inlet_area= 21.9320
rated_N2_rpm= 14120.0000
static_thrust= 24438.0000
afterburner_available=0
reverser_available= 1
[jet_engine]
thrust_scaler = 0.3431
[airplane_geometry]
wing_area= 1341.000
wing_span= 112.700
wing_root_chord= 11.910
wing_dihedral= 6.200
wing_incidence= 1.000
wing_twist= -0.500
oswald_efficiency_factor= 0.882
wing_winglets_flag= 0
wing_sweep= 25.000
wing_pos_apex_lon= 11.600
wing_pos_apex_vert= 0.000
htail_area= 348.000
htail_span= 47.100
htail_pos_lon= -52.150
htail_pos_vert= 7.000
htail_incidence= 0.697
htail_sweep= 30.000
vtail_area= 308.000
vtail_span= 27.200
vtail_sweep= 35.000
vtail_pos_lon= -44.600
vtail_pos_vert= 10.300
elevator_area= 70.500
aileron_area= 26.900
rudder_area= 56.200
elevator_up_limit= 22.500
elevator_down_limit= 19.500
aileron_up_limit= 20.000
aileron_down_limit= 20.000
rudder_limit= 26.000
elevator_trim_limit= 20.000
spoiler_limit= 60.000
spoilerons_available= 1
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=6.000
min_flaps_for_spoilerons=0.000
[Reference Speeds] //ONLY FOR AI USE, HAS NO EFFECT ON ACTUAL FLYING
flaps_up_stall_speed = 140
full_flaps_stall_speed = 115
cruise_speed = 475
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//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)
max_indicated_speed=350.000000
max_mach=0.839990
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[contact_points]
point.0= 1, 51.00, 0.00, -7.75, 1574.80, 0.00, 2.20, 78.00, 0.21, 3.50, 0.87, 5.00, 5.00, 0.00, 0.00, 0.00 //nose gear
point.1= 1, -1.75, -9.50, -8.50, 1574.80, 1, 1.366, 0.0, 0.308, 3.5, 0.839, 5.30, 5.70,2, 200, 280 //left main
point.2= 1, -1.75, 9.50, -8.50, 1574.80, 2, 1.366, 0.0, 0.308, 3.5, 0.839, 5.20, 5.60,3, 200, 280 //right main
point.3= 2, -13.00, -58.85, 4.65, 787.80, 0. 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0, 0 //left wing
point.4= 2, -13.00, 58.85, 4.65, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0, 0 //right wing
point.5= 2, -69.15, 0.00, 9.50, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0, 0 //tail(set for hstab strike)
point.6= 2, 69.55, 0.00, 1.00, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0, 0 //nose
point.7= 2, -45.15, 0.00, -1.50, 787.80, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0, 0, 0 //aft fuse scrape point
static_pitch=-1.00
static_cg_height=8.70
gear_system_type=0
[Flaps.0]
type= 1
span-outboard=0.800
extending-time=25.00
system_type=1
damaging-speed= 0.000
blowout-speed= 0.000
lift_scalar= 1.200
drag_scalar= 1.000
pitch_scalar= 0.800
flaps-position.0= 0.000
flaps-position.1= 1.000
flaps-position.2= 2.000
flaps-position.3= 5.000
flaps-position.4= 10.000
flaps-position.5= 15.000
flaps-position.6= 25.000
flaps-position.7= 30.000
flaps-position.8= 40.000
[flaps.1] //Leading Edge slats
type=2
span-outboard=0.800
extending-time=6.00
system_type=1
damaging-speed=280
blowout-speed=320
lift_scalar=1.000
drag_scalar=0.800
pitch_scalar=0.500
flaps-position.0=0.000
flaps-position.1=5.000
flaps-position.2=10.000
[electrical]
//BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
autopilot = 0, 5 , 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
pitot_heat = 0, 15, 17.0
additional_system = 0, 20, 17.0
marker_beacon = 1, 2, 17.0
starter1 = 0, 20, 17.0
starter2 = 0, 20, 17.0
auto_brakes = 0, 15, 17.0
hydraulic_pump = 0, 2, 17.0
fuel_transfer_pump = 0, 5, 17.0
max_battery_voltage = 28.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps= 60.0
electric_always_available = 1
[pitot_static]
vertical_speed_time_constant = 999 //Increasing this value will cause a more instantaneous reaction in the VSI
[exits]
number_of_exits = 2
exit_rate.0 = 0.28
exit_rate.1 = 0.28
[TailHook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=0.5
[folding_wings]
wing_fold_system_type=4
fold_rates=0.15,0.15
[Views]
eyepoint=68.00,0.00,5.10
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 =1, 8.20, 0.00, 10.30, B738_BCNU , //upper beacon
light.1 =1, 4.50, 0.00, -4.60, B738_BCNL , //lower beacon
light.2 =3, -64.00, 0.00, 7.60, fx_navwhi , //aft id
light.3 =2, -64.00, 0.00, 7.60, B738_STROBE , //aft strobe
light.4=4, 60.00, 0.00, 5.50, B738_vclight , //cockpit splash
light.5=5, 28.50, -6.65, 2.50, fx_navwhi , //left inspection light
light.6=5, 28.50, 6.65, 2.50, fx_navwhi , //right inspection light
light.7=5, 26.00, -6.00, 5.00, B738wing , //-----|
light.8=5, 26.00, 6.00, 5.00, B738wing , //-----|
light.9=5, 12.40, -19.10, 16.40, B738wing , //-----|
light.10=5, 12.40, 19.10, 16.40, B738wing , //inspection light splashes on wings and engines,normally lit druing t/o+landings
[keyboard_response]
elevator=150,250
aileron= 150,250
rudder= 150,250
[direction_indicators]
direction_indicator.0=3,0
[fuel]
Center1= 11.50, 0.00,-1.50, 4302.00, 7.00
LeftMain= 4.50, -20.00, 0.00, 1288.00, 8.00
RightMain= 4.50, 20.00, 0.00, 1288.00, 8.00
fuel_type=2
number_of_tank_selectors=1
electric_pump=0
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 1800.0
autothrottle_available= 1
autothrottle_arming_required= 1
autothrottle_max_rpm= 98
autothrottle_takeoff_ga= 1
pitch_takeoff_ga= 8
use_no_default_pitch= 1
use_no_default_bank= 1
default_pitch_mode=0
default_bank_mode=0
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
[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1 = 1
Com.1 = 1, 1
Com.2 = 1, 1
Nav.1 = 1, 1, 1
Nav.2 = 1, 1, 0
Adf.1 = 1
Adf.2 = 1
Transponder.1 = 1
Marker.1 = 1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdr5
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[brakes]
toe_brakes_scale=0.887403
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=24.637185
flap_limit_idle=0.974028
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
