//ch47- COPYRIGHT BY V.ZHYHULSKIY - 2004
//===========================================
//===========================================
//===========================================


[fltsim.0]
title=CH-47 "Chinook" RAF
sim=CH47zh
model=
panel=
sound=
texture=
checklists=
kb_checklists=
kb_reference=
atc_id=Ch47
atc_airline=RAF
atc_flight_number=ZA705
ui_manufacturer=Boeing
prop_anim_ratio=-1.12
ui_type=CH47
ui_variation=RAF
visual_damage=1 
description=CH-47 Boeing RAF
atc_heavy=0

[fltsim.1]
title=CH-47 "Chinook" UN
sim=CH47zh
model=
panel=
sound=
texture=UN
checklists=
kb_checklists=
kb_reference=
atc_id=Ch47
atc_airline=UN
atc_flight_number=ZA705
ui_manufacturer=Boeing
prop_anim_ratio=-1.12
ui_type=CH47
ui_variation=UN
visual_damage=1 
description=CH-47 Boeing UN 
atc_heavy=0

[General]
atc_type=CH47 cHINOOK Boeing Powerplant: Two Textron Lycoming T55-L712 engines Rotor System: Three blades per hub (two hubs) Speed: 225 r/min 
performance=CH-47 Boeing
atc_type=CH47

//=================================================:

[WEIGHT_AND_BALANCE]
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=0.000000,0.000000,0.000000,0.000000
empty_weight= 1500.000

===================================
empty_weight_roll_MOI= 9000.000
empty_weight_pitch_MOI= 13000.000
empty_weight_yaw_MOI= 11500.000
empty_weight_coupled_MOI= 1000.000
max_gross_weight= 1900.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000

=======================================

[Helicopter]
low_realism_stability_scale = 2.5, 1.0, 3.0   


========================================
[fuel]
Center1= 0.000, 0.000, 0.000, 110.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0

=======================================

[contact_points]
point.0= 1.000, 7.333, -10.000, -9.50, 3003.699, 0.000, 0.520, 54.000, 1.121, 2.500, 1.261, 5.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, 7.333, 10.000, -9.50, 3003.699, 0.000, 0.520, 54.000, 1.121, 2.500, 1.261, 5.000, 5.000, 0.000, 0.000, 0.000
point.2= 1.000, -21.333, -9.333, -8.70, 3003.699, 1.000, 0.520, 0.000, 1.003, 2.500, 1.416, 8.000, 8.000, 2.000, 0.000, 0.000
point.3= 1.000, -21.333, 9.333, -8.70, 3003.699, 2.000, 0.520, 0.000, 1.003, 2.500, 1.416, 9.000, 9.000, 3.000, 0.000, 0.000
point.4= 2.000, 0.000, -125.000, 50.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
\\point.5= 2.000, 0.000, 125.000, 50.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
\\point.6= 2.000, -50.000, 0.000, -1.667, 1802.219, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
\\point.7= 2.000, 12.500, 0.000, -2.083, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
\\point.8= 4.000, -7.000, -4.250, -5.000, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000
\\point.9= 4.000, -7.000, 4.250, -5.000, 1068.000, 0.000, 0.512, 20.000, 0.800, 2.500, 0.700, 0.000, 0.000, 1.000, 0.000, 0.000
\\point.10= 4.000, 5.350, -4.250, -5.300, 1068.000, 1.000, 0.512, 0.000, 0.800, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000
\\point.11= 4.000, 5.350, 4.250, -5.300, 1068.000, 2.000, 0.512, 0.000, 0.800, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000
static_pitch= 1.40
static_cg_height= 8.1
gear_system_type=0

================================

[GeneralEngineData]
engine_type= 3
Engine.0= 10.833, 0.000, 0
Engine.1=-10.833, 0.000, 0
fuel_flow_scalar=1.00000
min_throttle_limit=0.000000

================================

[fuselage_aerodynamics]
drag_force_cf      = 0.00
side_drag_force_cf = 1.00
pitch_damp_cf      = -1.0
roll_damp_cf       = -1.0
yaw_damp_cf        = -0.0
yaw_stability_cf   = 0.57

===================================
[Reference Speeds]
flaps_up_stall_speed=54.000000
full_flaps_stall_speed=43.200000
cruise_speed=0.000000
max_indicated_speed=1000.000000

=====================================
[keyboard_response]
elevator=100.000000,180.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000

=================================
[Views]
eyepoint=2.609621,-1.755762,-0.0

==========================================

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=1, -17.95, 0.00, -5.14,  fx_beacon ,
//light.1=4,   8.00,  0.00, 0.90,  fx_vclight ,
//light.2=4,   -5.50,  0.00, 0.00,  fx_vclight ,

=================================================

[brakes]
toe_brakes_scale=1.300031
parking_brake=1

=====================================

[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000

=====================================

[hydraulic_system]
normal_pressure=0.000000

======================================

[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0

=============================================
[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second

=====================================================================
[TailHook]
tailhook_length=4                               ;(feet)
tailhook_position=-15.0, 0.0, -1.0            ;(feet) longitudinal, lateral, vertical positions from datum
cable_force_adjust=1.0

=====================================================================
[folding_wings]
wing_fold_system_type=4                    
fold_rates=0.11,0.13   
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
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
[direction_indicators]
direction_indicator.0=3,0