[fltsim.0]
title= B727-294 Avensa (1969)
sim=b727
visual_damage=1
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=YV-74C
atc_airline= Avensa
atc_flight_number=74C
ui_manufacturer=Boeing
ui_type=727-294
ui_variation= Avensa (1969)
description=Model:Mike Stone\nRepaint :Claudio Sanchez\n Introduced into service in February 1964, the 727 trijet became an immediate hit with flight crews and passengers alike. With a fuselage width the same as the 707 (and the later 737 and 757), it provided jet luxury on shorter routes. With sophisticated, triple-slotted trailing edge flaps and new leading-edge slats, the 727 had unprecedented low-speed landing and takeoff performance for a commercial jet and could be accommodated by smaller airports than the 707 required.(www.boeing.com)\nThis is an almost close possible model of a 727-294 seen on a picture of 1969 with its respective big outlined logo includes panel,lights,smoke, and some reflective parts,visual damage
atc_heavy=0
[General]
atc_type=Boeing
atc_model=B727
editable=0
performance=Max speed: 598 mph\nRange: 2,728 mi\nCeiling: 33,000 ft.\nEmpty weight: 99,370\nLoaded: 190,090\nPassengers: 145 typical
[pitot_static]
vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI
[WEIGHT_AND_BALANCE]
max_gross_weight = 209000.000
empty_weight = 100000.000
reference_datum_position = 0.000, 0.000, 0.000
empty_weight_CG_position = 0.000, 0.000, 0.000
max_number_of_stations = 50
station_load.0 = 20000.000, 0.000, 0.000, 0.000
;Moments of Inertia
empty_weight_pitch_MOI = 5600000.000
empty_weight_roll_MOI = 1400000.000
empty_weight_yaw_MOI = 4000000.000
empty_weight_coupled_MOI = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.000
induced_drag_scalar =1.000
elevator_effectiveness =1.000
aileron_effectiveness =1.000
rudder_effectiveness =1.000
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness =1.000
rudder_trim_effectiveness =1.000
[GeneralEngineData]
engine_type = 1
Engine.0 = -45.000, -9.000, 4.000
Engine.1 = -45.000, 9.000, 4.000
fuel_flow_scalar = 1.000
Engine.2= -60.000, 0.000, 3.000
[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 18.000
rated_N2_rpm = 29920.000
static_thrust = 16000.000
afterburner_available = 0
reverser_available = 1
[SMOKESYSTEM]
smoke.0=-5.00, -75.00, 10.00, fx_smoke_rx
smoke.1=-5.00, -75.00, 0.00, fx_smoke_rx
smoke.2=-5.00, -75.00, -10.00, fx_smoke_rx
[jet_engine]
thrust_scalar =1.000
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor = 0, 5 , 17.0
gear_motor = 0, 5 , 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 20, 17.0
marker_beacon = 1, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 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
//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)
//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= 1.000, 40.000, 0.000, -8.200, 1181.100, 0.000, 1.442, 55.920, 0.800, 2.500, 0.900, 4.000, 4.000, 0.000, 0.000, 0.000
point.1= 1.000, -7.750, -8.580, -9.000, 1574.800, 1.000, 1.442, 0.000, 1.000, 2.500, 0.900, 6.900, 6.900, 2.000, 0.000, 0.000
point.2= 1.000, -7.750, 8.580, -9.000, 1574.800, 2.000, 1.442, 0.000, 1.000, 2.500, 0.900, 7.100, 7.100, 3.000, 0.000, 0.000
point.3= 2.000, -14.170, -47.330, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -14.170, 47.330, 0.000, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -54.000, 0.000, 2.830, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 42.670, 0.000, -3.750, 787.400, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
max_number_of_points = 21
static_pitch= -1.000
static_cg_height= 8.000
[Views]
eyepoint=43.7, -1.31, 3.55 //(feet) longitudinal, lateral, vertical distance from reference datum
[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
Transponder.1 = 1
Marker.1 = 1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -22.89, -53.20, 0.85, fx_navredm ,
light.1 = 3, -22.89, 53.20, 0.85, fx_navgrem ,
light.2 = 3, -80.73, 0.00, 23.16, fx_navwhih ,
light.3 = 2, -24.00, -53.53, 0.85, fx_strobeh ,
light.4 = 2, -24.00, 53.53, 0.85, fx_strobeh ,
light.5 = 2, 3.36, 0.00, -4.21, fx_beaconb ,
light.6 = 1, 29.96, 0.00, 9.15, fx_beaconh ,
light.7 = 4, 60.87, 0.00, 6.39, fx_vclight ,
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[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=3,0
[exits]
number_of_exits = 2
exit_rate.0 = 0.4 ;Percent per second
exit_rate.1 = 0.4 ;Percent per second
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8;
[fuel]
Center1 =0.000000,0.000000,0.000000,2313.000000,0.000000
LeftMain =-3.000000,-19.000000,0.000000,1499.000000,0.000000
RightMain =-3.000000,19.000000,0.000000,1499.000000,0.000000
fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1
[airplane_geometry]
wing_area = 1400.000
wing_span = 108.000
wing_root_chord = 25.000
wing_dihedral = 2.000
wing_incidence = 1.000
wing_twist = -0.500
oswald_efficiency_factor= 0.750
wing_winglets_flag = 0
wing_sweep = 35.000
wing_pos_apex_lon = 12.000
wing_pos_apex_vert = 0.000
htail_area = 350.000
htail_span = 35.000
htail_pos_lon = -60.000
htail_pos_vert = 24.000
htail_incidence = 0.000
htail_sweep = 30.000
vtail_area = 440.000
vtail_span = 20.000
vtail_sweep = 35.000
vtail_pos_lon = -45.000
vtail_pos_vert = 8.000
elevator_area = 45.000
aileron_area = 25.000
rudder_area = 59.000
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 = 10.000
min_flaps_for_spoilerons = 0.000
[Reference Speeds]
flaps_up_stall_speed = 140.000
full_flaps_stall_speed = 110.000
cruise_speed = 515.000
[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
[Flaps.0]
type= 1
span-outboard= 0.400
extending-time= 8.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.500
drag_scalar= 0.500
pitch_scalar= 0.250
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 2.000, 0.000
flaps-position.3= 5.000, 0.000
flaps-position.4= 10.000, 0.000
flaps-position.5= 15.000, 0.000
flaps-position.6= 25.000, 0.000
flaps-position.7= 30.000, 0.000
flaps-position.8= 40.000, 0.000
[Flaps.1]
type= 1
span-outboard= 0.400
extending-time= 8.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.500
drag_scalar= 0.500
pitch_scalar= 0.250
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
flaps-position.2= 2.000, 0.000
flaps-position.3= 5.000, 0.000
flaps-position.4= 10.000, 0.000
flaps-position.5= 15.000, 0.000
flaps-position.6= 25.000, 0.000
flaps-position.7= 30.000, 0.000
flaps-position.8= 40.000, 0.000
[Flaps.2]
type= 2
span-outboard= 0.800
extending-time= 4.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 4.000
drag_scalar= 0.400
pitch_scalar= 0.200
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 0.000, 0.000
flaps-position.3= 1.000, 0.000
[Flaps.3]
type= 2
span-outboard= 0.800
extending-time= 4.000
system_type= 1
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 0.500
drag_scalar= 0.500
pitch_scalar= 0.250
flaps-position.0= 0.000, 0.000
flaps-position.1= 0.000, 0.000
flaps-position.2= 0.000, 0.000
flaps-position.3= 1.000, 0.000
