[fltsim.0]
title=AI HP67 C2 TG528
sim=Boeing737-400
model=c2
panel=
sound=
texture=tg528-01
checklists=
description=The HP.67 Hastings was a British long-range military transport of the 1940s. \n \nby Georg Hauzenberger & Hans Hermann. \nD-GHHH simulationware Germany\n1. Edition, March 2003
atc_airline=Royal
atc_flight_number=233
ui_manufacturer=Handley Page
ui_type=HP.67 Hastings
ui_variation=C.Mk1 RAF TG528
atc_heavy=0
atc_id=TG529
description=Fs Kallax Hasting only for AI use
// INSERT NEW SECTIONS ABOVE THIS LINE
// DO NOT ALTER ANYTHING BELOW THIS LINE
[WEIGHT_AND_BALANCE]
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=42971.000000
empty_weight_roll_MOI=982732.000000
empty_weight_pitch_MOI=1341571.000000
empty_weight_yaw_MOI=1319749.000000
empty_weight_coupled_MOI=0.000000
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0 = "170.0, -5.4, -2.0, 0.0, Pilot" //Weight, Lat, Lon, Vert Position
station_load.1 = "170.0, -5.4, 2.0, 0.0, Co-Pilot" //Weight, Lat, Lon, Vert Position
station_load.2 = "680.0, -14.2, 0.0, 0.0, Passenger Row 1" //Weight, Lat, Lon, Vert Position
station_load.3 = "680.0, -17.4, 0.0, 0.0, Passenger Row 2" //Weight, Lat, Lon, Vert Position
station_load.4 = "680.0, -20.7, 0.0, 0.0, Passenger Row 3" //Weight, Lat, Lon, Vert Position
station_load.5 = "680.0, -23.9, 0.0, 0.0, Passenger Row 4" //Weight, Lat, Lon, Vert Position
station_load.6 = "510.0, -27.2, 0.0, 0.0, Passenger Row 5" //Weight, Lat, Lon, Vert Position
station_load.7 = "510.0, -30.4, 0.0, 0.0, Passenger Row 6" //Weight, Lat, Lon, Vert Position
station_load.8 = "340.0, -33.7, 0.0, 0.0, Passenger Row 7" //Weight, Lat, Lon, Vert Position
station_load.9 = "340.0, -36.9, 0.0, 0.0, Passenger Row 8" //Weight, Lat, Lon, Vert Position
station_load.10 = "500.0, -23.8, 0.0, 0.0, Forward Baggage" //Weight, Lat, Lon, Vert Position
station_load.11 = "100.0, -45.5, 0.0, 0.0, Rear Cargo" //Weight, Lat, Lon, Vert Position
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0 //original = 1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[flaps.0] //Trailing Edge Flaps
type = 1 // 1 - tail, 2 - lead
span-outboard = 0.5 // 0.0 .. 1.0
extending-time = 7 // seconds
flaps-position.0 = 0 // degrees
flaps-position.1 = 11 // degrees
flaps-position.2 = 23 // degrees
flaps-position.3 = 34 // degrees
flaps-position.4 = 45.0 // degrees
damaging-speed = 140 // KIAS
blowout-speed = 175 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None
[GeneralEngineData]
engine_type=0
Engine.0=7.083333,-24.500000,0.000000
Engine.1=8.333333,-11.583333,0.000000
Engine.2=8.333333,11.583333,0.000000
Engine.3=7.083333,24.500000,0.000000
fuel_flow_scalar=1.000000
[piston_engine]
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000
cylinder_displacement=156.500000
compression_ratio=8.000000
number_of_cylinders=13
max_rated_rpm=2816.750000
max_rated_hp=1700.000000
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.300000
turbocharged=0
max_design_mp=0.000000
min_design_mp=0.000000
critical_altitude=0.000000
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0
[propeller]
propeller_type=0
propeller_diameter=12.916667
propeller_blades=3
propeller_moi=56.569282
beta_max=53.000000
beta_min=15.000000
min_gov_rpm=1400.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=20.000000
low_speed_theory_limit=80.000000
prop_sync_available=0
prop_deice_available=0
prop_feathering_available=0
prop_auto_feathering_available=0
min_rpm_for_feather=0.000000
beta_feather=0.000000
power_absorbed_cf=0.000000
defeathering_accumulators_available=0
prop_reverse_available=0
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000
[Reference Speeds] ;all KIAS - Pitot error not known so IAS set=CAS
flaps_up_stall_speed=135 //orig=115
full_flaps_stall_speed=81
cruise_speed=230
//0 Class
//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
[contact_points]
//index=type, long pos, lat pos, vert pos, damage tresh ft/min, brake, whl rad ft, trn angle, stat compr, comp rat, damp rat, exttime, rettime, sound, spdlmt, spddamg
point.0=1.000000,-43.500000,0.000000,-2.000000,2574.803150,0.000000,1.212000,80.000000,0.218980,2.500000,0.572585,8.000000,8.000000,0.000000,200.000000,220.000000
point.1=1.000000,6.416667,-12.083333,-10.800000,2574.803150,1.000000,2.497000,0.000000,0.436587,2.500000,0.720916,8.000000,10.000000,2.000000,200.000000,220.000000
point.2=1.000000,6.416667,12.083333,-10.800000,2574.803150,2.000000,2.497000,0.000000,0.436587,2.500000,0.720916,8.000000,10.000000,3.000000,200.000000,220.000000
point.3=2.000000,-4.166667,-56.666667,0.500000,574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,-4.166667,56.666667,0.500000,574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-50.666667,0.000000,2.416667,574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,32.250000,0.000000,0.833333,574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=9.807070
static_cg_height=9.502963
static_pitch = 12.76
static_cg_height = 9.9
gear_system_type=1 //Hydraulic
tailwheel_lock = 1
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 0.0 //Flap angle that activates warning at idle
flap_limit_power = 16.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 0.3 //Brake scalar
differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected
[hydraulic_system]
normal_pressure = 732.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint = -6.495, -1.512, 3.217
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -27.20, -46.3, 0.65, fx_navredm ,
light.1 = 3, -27.20, 46.3, 0.65, fx_navgrem ,
light.2 = 3, -64.00, 0.00, 2.72, fx_navwhi ,
light.3 = 1, -36.80, 0.00, 6.25, fx_beaconh ,
light.4 = 4, -6.00, 0.00, 1.80, fx_vclight,
light.5 = 4, -33.00, 0.00, 4.20, fx_vclighth,
[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
Adf.2 = 1
Transponder.1 = 0
Marker.1 = 1
[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 =200, 1000
aileron =200, 1000
rudder =200, 1000
[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=1,0
direction_indicator.1=2,0
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 1
attitude_indicator.1 = 2
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2=Vacuum Gyro
turn_indicator.0=2,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_jenny
touchdown=fx_tchdwn_s, 1
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 25
max_generator_alternator_amps = 100
[fuel]
LeftMain = -22.55, -6.7, -3.0, 202.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain= -22.55, 6.7, -3.0, 202.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1 = -22.55, 0.0, -2.7, 200.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
electric_pump=1
[airplane_geometry]
wing_area=1281.000000
wing_span=102.000000
wing_root_chord=12.583333
wing_dihedral=1.999512
wing_incidence=0.000000
wing_twist=-0.999756
oswald_efficiency_factor=1.671110
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=300.000000
htail_span=33.166667
htail_pos_lon=-34.166667
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=0.000000
vtail_area=194.000000
vtail_span=15.880806
vtail_sweep=0.000000
vtail_pos_lon=-34.166667
vtail_pos_vert=1.500000
elevator_area=156.520000
aileron_area=168.200000
rudder_area=67.900000
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
[autopilot]
autopilot_available= 1
flight_director_available= 0
pitch_takeoff_ga=0.0
default_vertical_speed=700.000000
autothrottle_available=0
direction_indicator=1
attitude_indicator =1
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 = 0.0
default_bank_mode=2 //Default to Heading Hold
[General]
performance=Four P&W R-2800-CB16\neach 2400hp for take off\n1800hp METO to 8500feet\n1700hp to 14,500 feet