// DHC8-Q202_ver4.6 - MAY 6, 2005, Revised "DHC8-Q200 9_7" for FS9, 2 July 2010
// Design: Jean-Pierre Brisard
// Panel & Sound, Chk/Ref HTML, Docs by Barry Blaisdell
// Master Textures & Livery by Bob May
// Copyright 2010 - Premier Aircraft Design
[fltsim.0]
title=DHC8-Q202_Continental Connection (9)
sim=PAD_Dhc8
model=
panel=DHC8-9
sound=0
texture=continental
kb_checklists=Dash8_check
kb_reference=Dash8_ref
atc_id=N367PH
atc_heavy=0
atc_airline=Continental
atc_flight_number=320
atc_parking_types=gate, ramp
atc_parking_codes=
ui_manufacturer=DeHavilland
prop_anim_ratio=1.015
ui_type=Dash8-Q202
ui_variation=Continental Connection (9)
description=FS2004 DeHavilland DHC8-Q202\nTwin Turboprop Regional Airliner\nVisit the Premier Aircraft Design Web Site\nwww.premaircraft.com\nAll Files Copyright 2010.\nThe Q200 is designed for airlines and other operators who require an aircraft the same size as the Q100, but with more power and greater payload. Bombardier engineers met the challenge by mating the Q100 airframe with the more powerful Pratt & Whitney PW123 engines found on the larger Q300 aircraft.
editable=1
[General]
performance=37 Pax Regional Airliner\nLength: 73 ft\nWing Span: 85 ft\nHt: 24 ft-7 in\nWeight:22,100 lb Empty\nMax T\/O Weight:34,500 lb\nPower: 2 x 2,150 SHP P&W 123C/D Turboshafts\nMax Cruise: 277 Kts TAS\nStall Speed full flap 72 Kts\nCeiling: 25,000 ft\nRange: 970 Naut Miles
atc_type=DEHAVILLAND
atc_model=DH8B
category=airplane
editable=1
[Views]
eyepoint= -9.780, -2.150, 1.90 //(feet) longitudinal, lateral, vertical distance from reference datum
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=Landing
light.0 =1, -64.580000, 0.000000, 18.000000, (¥M
light.1 =2, -68.900000, 0.000000, 1.500000, fx_strobeh
light.2 =2, -28.900000, 42.600000, 5.600000, dhc8fx_strobe
light.3 =2, -28.900000, -42.600000, 5.600000, dhc8fx_strobe
light.4 =3, -29.300000, -42.650000, 5.600000, dhc8fx_navred
light.5 =3, -29.300000, 42.650000, 5.600000, dhc8fx_navgre
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000
autothrottle_available=0
pitch_takeoff_ga=8
use_no_default_bank=1
use_no_default_pitch=1
default_pitch_mode=0
default_bank_mode=0
max_pitch=10
max_pitch_acceleration=1
max_pitch_velocity_lo_alt=2
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000
max_pitch_velocity_hi_alt_breakpoint=28000
max_bank=25
max_bank_acceleration=1.8
max_bank_velocity=3
max_throttle_rate=0.1
nav_proportional_control=9
nav_integrator_control=0.25
nav_derivative_control=0
nav_integrator_boundary=2.5
nav_derivative_boundary=0
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0
gs_integrator_boundary=0.7
gs_derivative_boundary=0
yaw_damper_gain=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90
[WEIGHT_AND_BALANCE]
max_gross_weight =36300.0
empty_weight =23004.00000
reference_datum_position= 31.0, 0, 0 // (feet) distance from FlightSim Ref position: (1/4 chord,c/l, waterline)
empty_weight_CG_position= -31.000, -0.000, -0.000
max_number_of_stations =3
;Moments of Inertia
empty_weight_pitch_MOI =131321.60000
empty_weight_roll_MOI =88879.09000
empty_weight_yaw_MOI =174837.87000
empty_weight_coupled_MOI =0.00000
station_load.0= 170, -31.000, -1.750, 0.000, Pilot
station_load.1= 170, -31.000, 1.750, 0.000, Front
station_load.2= 5000, -31.000, 0.000, 0.000, Payload
[flight_tuning]
cruise_lift_scalar=1.00000
parasite_drag_scalar=1.00000
induced_drag_scalar=1.00000
elevator_effectiveness=1.00000
aileron_effectiveness=1.00000
rudder_effectiveness=1.00000
pitch_stability=1.00000
roll_stability=1.00000
yaw_stability=1.00000
elevator_trim_effectiveness=1.00000
aileron_trim_effectiveness=1.00000
rudder_trim_effectiveness=1.00000
hi_alpha_on_roll=1.00000
hi_alpha_on_yaw=1.00000
p_factor_on_yaw=1.00000
torque_on_roll=1.00000
gyro_precession_on_roll=1.00000
gyro_precession_on_yaw=1.00000
[GeneralEngineData]
engine_type =5
Engine.0 =-28.400, -13.300, -0.000
Engine.1 =-28.400, 13.300, -0.000
fuel_flow_scalar =0.50000
min_throttle_limit =-0.50000
[propeller]
thrust_scalar =1.10000
propeller_type =0
propeller_diameter =13.00000
propeller_blades =4
propeller_moi =249.51300
beta_max =45.00000
beta_min =12.00000
min_gov_rpm =25520.00000
prop_tc =0.00400
gear_reduction_ratio =17.00000
fixed_pitch_beta =0.00000
low_speed_theory_limit =80.00000
prop_sync_available =1
prop_deice_available =1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather =700.00000
beta_feather =79.30000
power_absorbed_cf =0.90000
defeathering_accumulators_available=0
prop_reverse_available =1
minimum_on_ground_beta =1.00000
minimum_reverse_beta =-14.00000
[TurbineEngineData]
fuel_flow_gain =0.01100
inlet_area =0.02500
rated_N2_rpm =29920.00000
static_thrust =200.00000
reverser_available=0
afterburner_available=0
afterburner_throttle_threshold=0.01100
ThrustSpecificFuelConsumption=0.01100
AfterBurnThrustSpecificFuelConsumption=0.01100
[turboprop_engine]
power_scalar =1.10000
maximum_torque =9668.45455
[electrical]
//BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
//BusType, MaxAmpLoad, MinVoltage
autopilot = 0, 5 , 1.0
avionics_bus = 0, 10, 10.0
avionics = 1, 5 , 10.0
gear_warning = 0, 2 , 1.0
fuel_pump = 0, 5 , 1.0
light_nav = 0, 5 , 1.0
light_beacon = 0, 5 , 1.0
light_landing = 0, 5 , 7.0
light_taxi = 0, 5 , 7.0
light_strobe = 0, 5 , 7.0
light_panel = 0, 5 , 1.0
pitot_heat = 0, 15, 1.0
additional_system = 0, 20, 1.0
marker_beacon = 1, 2, 1.0
starter1 = 0, 20, 1.0
starter2 = 0, 20, 1.0
starter3 = 0, 20, 1.0
starter4 = 0, 20, 1.0
auto_brakes = 0, 15, 1.0
hydraulic_pump = 0, 2, 1.0
fuel_transfer_pump = 0, 5, 1.0
max_battery_voltage=28.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=160.0
electric_always_available=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]
max_number_of_points =8
static_pitch = -0.500
static_cg_height = 6.100
gear_system_type=0
tailwheel_lock=0
//point.0 = 1, -5.0, 0.00, -6.245, 2500, 0, 0.800, 70.0, 0.296, 2.5, 0.9516, 5.0, 6.0, 0, 0.0 , 0.0
point.0= 1, -10.400, 0.000, -6.300, 2500, 0, 0.800, 76.000, 0.296, 2.500, 0.952, 5.000, 6.000, 0
point.1= 1, -34.400, -12.990, -6.500, 3000, 1, 1.250, 0.000, 0.675, 2.501, 0.800, 6.000, 7.000, 0
point.2= 1, -34.400, 12.990, -6.500, 3000, 2, 1.250, 0.000, 0.675, 2.501, 0.800, 6.000, 7.000, 0
point.3= 2, -31.600, -42.500, 5.390, 1200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5
point.4= 2, -31.600, 42.500, 5.390, 1200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6
point.5= 2, -68.600, 0.000, 1.220, 1200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9
point.6= 2, 0.000, 0.000, -3.920, 1200, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4
point.7= 5, -30.900, 5.250, -7.300, 1600, 0, 0.000, 50.000, 0.000, 0.000, 1.000, 1.100, 1.500, 0
[gear_warning_system]
gear_warning_available =1
pct_throttle_limit =0.09998
flap_limit_idle =15.01149
flap_limit_power =30.02299
[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1,0
Com.2=1, 0
Nav.1=1, 0, 1
Nav.2=1, 0, 0
Adf.1=1
Transponder.1=1
Marker.1=1
[brakes]
parking_brake =1
toe_brakes_scale =1.06300
auto_brakes=0
hydraulic_system_scalar=0.00000
differential_braking_scale=0.00000
[hydraulic_system]
normal_pressure =3000.00000
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[flaps.0]
type= 1
system_type=0
span-outboard= 0.500
extending-time= 6.0
damaging-speed=250.0
blowout-speed=300.0
flaps-position.0=0.00
flaps-position.1=11.67
flaps-position.2=23.33
flaps-position.3=35.00
lift_scalar=1.00
drag_scalar=1.00
pitch_scalar=1.00
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=1,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
LeftMain = -31.000, -9.100, 3.900, 420.000, 0.000
RightMain = -31.000, 9.100, 3.900, 420.000, 0.000
fuel_type =2
number_of_tank_selectors =1
electric_pump=1
fuel_dump_rate=0.02000
anemometer_pump=0
manual_pump=0
engine_driven_pump=0
[airplane_geometry]
wing_area =585.00000
wing_span =85.00000
wing_root_chord =7.23000
wing_dihedral =2.50000
wing_incidence =1.00000
wing_twist =0.20000
oswald_efficiency_factor=0.75000
wing_winglets_flag =0
wing_sweep =0.00000
wing_pos_apex_lon =-28.18303
wing_pos_apex_vert =0.00000
htail_area =73.00000
htail_span =32.37000
htail_pos_lon =-61.62000
htail_pos_vert =0.00000
htail_incidence =0.00000
htail_sweep =0.00000
vtail_area =43.27000
vtail_span =15.08000
vtail_sweep =0.00000
vtail_pos_lon =-62.54000
vtail_pos_vert =1.72000
elevator_area =40.43000
aileron_area =42.12000
rudder_area =27.54000
elevator_up_limit =25.00000
elevator_down_limit =25.00000
aileron_up_limit =20.00000
aileron_down_limit =20.00000
rudder_limit =30.00000
elevator_trim_limit =20.00000
spoiler_limit =60.00000
spoilerons_available =1
aileron_to_spoileron_gain =0.00000
min_ailerons_for_spoilerons =0.00000
min_flaps_for_spoilerons =0.00000
spoiler_extension_time=2.00000
spoiler_handle_available=1
auto_spoiler_available=1
positive_g_limit_flaps_up=2.70000
negative_g_limit_flaps_up=-2.16000
positive_g_limit_flaps_down=1.89000
negative_g_limit_flaps_down=-1.62000
load_safety_factor=1.00000
[Reference Speeds]
flaps_up_stall_speed = 102.0 //Knots True (KTAS)
full_flaps_stall_speed = 82.0 //Knots True (KTAS)
cruise_speed =280.00000
max_indicated_speed =290.00000
max_mach=0.60000
[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= 150.0, 250.0
aileron= 150.0, 250.0
rudder= 150.0, 250.0
[stall_warning]
type=1
[direction_indicators]
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
[direction_indicators]
direction_indicator.0=3,0
[brakes]
toe_brakes_scale=1.062532
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[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
[GPWS]
max_warning_height=0
sink_rate_fpm=-1500
excessive_sink_rate_fpm=-2000
climbout_sink_rate_fpm=-100
flap_and_gear_sink_rate_fpm=-100
