// Title: An-26 dynamics
// Author: Aless (thanks for the help to Curl, ALZP, UNKL, Agat, Vinni-Puh, Jurik, mikedet ...)
// Version: 26.v5.25
// Date: june/2012
//full fuel, full equip., pass empty, Baggage 3 = 400kg (100%)
//TOW 21550 kg, MAC=25.6% (with fuel)
[fltsim.0]
title=Samdim Design Antonov An-26 VVS RED 29
sim=Antonov An-26
visual_damage=1
model=
panel=noVC
sound=
texture=26_VVS_RED_29
kb_reference=
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-26
ui_variation=VVS Red 29
description=The Legendary Russian Turboprop\nAn-26 is a twin-engined turboprop transport aircraft, designed and produced in the USSR from 12 March 1968. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, [email protected]) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - [email protected]
[fltsim.1]
title=Samdim Design Antonov An-26 Avialesoochrana
sim=Antonov An-26
visual_damage=1
model=
panel=noVC
sound=
texture=26_Avialesoohrana
kb_reference=
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-26
ui_variation=AviaLesoOhrana RA-26011
description=The Legendary Russian Turboprop\nAn-26 is a twin-engined turboprop transport aircraft, designed and produced in the USSR from 12 March 1968. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, [email protected]) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - [email protected]
[fltsim.2]
title=Samdim Design Antonov An-26 CityLine HA-TCN
sim=Antonov An-26
visual_damage=1
model=nb
panel=noVC
sound=
texture=26nb_CityLine
kb_reference=
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-26
ui_variation=CityLine HA-TCN
description=The Legendary Russian Turboprop\nAn-26 is a twin-engined turboprop transport aircraft, designed and produced in the USSR from 12 March 1968. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, [email protected]) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - [email protected]
[fltsim.3]
title=Samdim Design Antonov An-26 Pskovavia RA-26134
sim=Antonov An-26
visual_damage=1
model=nb
panel=noVC
sound=
texture=26nb_Pskov_RA-26134
kb_reference=
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-26
ui_variation=Pskovavia RA-26134
description=The Legendary Russian Turboprop\nAn-26 is a twin-engined turboprop transport aircraft, designed and produced in the USSR from 12 March 1968. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, [email protected]) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - [email protected]
[fltsim.4]
title=Samdim Design Antonov An-26 DHL SP-FDP
sim=Antonov An-26
visual_damage=1
model=nb
panel=noVC
sound=
texture=26nb_DHL_SP-FDP
kb_reference=
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-26
ui_variation=DHL SP-FDP
description=The Legendary Russian Turboprop\nAn-26 is a twin-engined turboprop transport aircraft, designed and produced in the USSR from 12 March 1968. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, [email protected]) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - [email protected]
[fltsim.5]
title=Samdim Design Antonov An-26 CCCP-26211
sim=Antonov An-26
visual_damage=1
model=
panel=noVC
sound=
texture=26_CCCP-26211
kb_reference=
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-26
ui_variation=Aeroflot CCCP-26211
description=The Legendary Russian Turboprop\nAn-26 is a twin-engined turboprop transport aircraft, designed and produced in the USSR from 12 March 1968. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, [email protected]) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - [email protected]
[fltsim.6]
title=Samdim Design Antonov An-26 VVS Yellow 02 47404
sim=Antonov An-26
model=
panel=noVC
sound=
texture=26_VVS_YELLOW_02
kb_reference=
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-26
ui_variation=VVS Yellow 02 47404
description=The Legendary Russian Turboprop\nAn-26 is a twin-engined turboprop transport aircraft, designed and produced in the USSR from 12 March 1968. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, [email protected]) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - [email protected]
atc_id_color=000000
[fltsim.7]
title=Samdim Design Antonov An-26 Aeroflot Red RA-26022
sim=Antonov An-26
model=nb
panel=noVC
sound=
texture=26nb_Aeroflot_RED_RA-26022
kb_reference=
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-26
ui_variation=Aeroflot Red RA-26022
description=The Legendary Russian Turboprop\nAn-26 is a twin-engined turboprop transport aircraft, designed and produced in the USSR from 12 March 1968. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, [email protected]) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - [email protected]
[fltsim.8]
title=Samdim Design Antonov An-26 Belorussian airforce
sim=Antonov An-26
model=nb
panel=noVC
sound=
texture=VVS_YELLOW_26
kb_reference=
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-26
ui_variation=VVS_YELLOW_26
description=The Legendary Russian Turboprop\nAn-26 is a twin-engined turboprop transport aircraft, designed and produced in the USSR from 12 March 1968. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, [email protected]) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - [email protected]
[fltsim.9]
title=Samdim Design Antonov An-26-100 RA-26247
sim=Antonov An-26
model=26-100
panel=noVC
sound=
texture=26-100_RA-26247
kb_reference=
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-26-100
ui_variation=Aeroflot'90 RA-26247
description=The Legendary Russian Turboprop\nAn-26 is a twin-engined turboprop transport aircraft, designed and produced in the USSR from 12 March 1968. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, [email protected]) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - [email protected]
[fltsim.10]
title=Samdim Design Antonov An-26 VVS BLUE 47
sim=Antonov An-26
model=
panel=noVC
sound=
texture=26_VVS_BLUE_47
kb_reference=
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-26
ui_variation=VVS Blue 47
description=The Legendary Russian Turboprop\nAn-26 is a twin-engined turboprop transport aircraft, designed and produced in the USSR from 12 March 1968. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, [email protected]) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - [email protected]
[fltsim.11]
title=Samdim Design Antonov An-26 VVS RED 86 50'OSAP
sim=Antonov An-26
model=
panel=noVC
sound=
texture=26_VVS_50_OSAP
kb_reference=
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-26
ui_variation=VVS RED 86 50'OSAP
description=The Legendary Russian Turboprop\nAn-26 is a twin-engined turboprop transport aircraft, designed and produced in the USSR from 12 March 1968. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, [email protected]) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - [email protected]
[fltsim.12]
title=Samdim Design Antonov An-26 VVS BLUE 01 4TsBP-PLS
sim=Antonov An-26
model=
panel=noVC
sound=
texture=26_VVS_BLUE_01_4_TsBP_i_PLS
kb_reference=
kb_checklists=Antonov An24RV_check
ui_manufacturer=Antonov
ui_type=An-26
ui_variation=VVS BLUE 01 4TsBP-PLS
description=The Legendary Russian Turboprop\nAn-26 is a twin-engined turboprop transport aircraft, designed and produced in the USSR from 12 March 1968. \n\nVisual model by D. Samborski (samdim) (c) 2012\nPainting and paintkit by Nikolai Samsonov (INS) 2012\nPanel by Mihail Karnizov (mikedet, [email protected]) (c) 2012\nGauges main contribution by S. Gritsevsky (c) 2003\nDynamics by A.Terentjevs (Aless) (c) 2012\nSounds from Mike Maarse with corrections of S. Teifel (c) 2006\n - http:\/\/samdimdesign.free.fr - [email protected]
// --- do not modify after this line ---
[General]
atc_type=An26
atc_model=An26
editable=0
performance="Cruise Speed\n237 kts 440 km\/hr\n\nEngine\n2 x Ivchenko AI-20VT 2820 hp each\n\nPropeller\n4-Bladed Constant Speed (diam. 3.9 m)\n\nMaximum Range\n1376 nm 1548 mi 2,500 km\n\nService Ceiling\n20,000 ft\t 6000 m\n\nEmpty Weight\n34282 lb\t 15550 kg\n\nMaximum Gross Weight\n52,911 lb\t 24,000 kg\n\nLength\n78 ft, 1 in 23.80 m\n\nWingspan\n 95 ft, 9.5 in\t 29.2 m\n\nHeight\n28 ft, 1.5 in\t 8.58 m\n\nCrew 5\nSeating 40\n\nPayload\n12,1225 lb 5500 kg"
[Propeller]
thrust_scalar=1.0
propeller_type=0
propeller_diameter=12.795
propeller_blades=4
propeller_moi=300
beta_max=49.99
beta_min=8.0
min_gov_rpm=13900.00
prop_tc=0.006
gear_reduction_ratio=12.1285
fixed_pitch_beta=15
low_speed_theory_limit=60.0
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=500.000
beta_feather=93.320
power_absorbed_cf=1.000
defeathering_accumulators_available=0
prop_reverse_available=1.000000
minimum_on_ground_beta=0.000000
rotation=-1 -1
minimum_reverse_beta=-14.000000
[Turboprop_engine]
power_scalar=1.05
maximum_torque=11349.83 //10614.3602 lbs*ft
max_rpm_mechanical_efficiency_scalar=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.00
idle_rpm_friction_scalar=1.0
[TurbineEngineData]
fuel_flow_gain=0.0045 //0.003
inlet_area=1.000
rated_N2_rpm=15100
static_thrust=470
afterburner_available=0
[flight_tuning]
cruise_lift_scalar=1.0
pitch_stability=2.0
roll_stability=2.000
yaw_stability=2.000
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.300
aileron_effectiveness=1.300
rudder_effectiveness=1.00
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000
hi_alpha_on_roll=1 //multiplier on the effects on roll at high angles of attack
hi_alpha_on_yaw=1 //multiplier on the effects on yaw at high angles of attack
p_factor_on_yaw=1 //multipliers on the effects induced by rotating propellers
torque_on_roll=1
prop_effect_on_pitch=1
prop_effect_on_yaw=1
gyro_precession_on_yaw=1
gyro_precession_on_pitch=1
gyro_precession_on_roll=1
[weight_and_balance]
// ACM V2.3
max_gross_weight = 52910.95
empty_weight = 34281.89
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0.46, 0, 0
empty_weight_pitch_MOI = 259455
empty_weight_roll_MOI = 167514
empty_weight_yaw_MOI = 336548
empty_weight_coupled_MOI = 0
max_number_of_stations = 1
station_load.0 = 2289,-6.4194,0,0,Weight
[lights]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -3, -47.8, 3.24, fx_navredm
light.1 = 3, -3, 47.8, 3.24, fx_navgrem
light.2 = 2, -34.59, 0, 8.89, fx_beaconh_an24
light.3 = 2, -6.2, 0, -4.44, fx_beacon_an24
light.4 = 3, -47.3, 0, 4.29, fx_navwhi
light.5 = 4, 23, 2, 2, fx_vclight
light.6 = 4, 23, -2, 2, fx_vclight
light.7 = 5, 14.21, 26.42, -5.3, fx_land_an24_light,
light.8 = 5, 14.21, -26.42, -5.3, fx_land_an24_light,
light.9 = 5, 0.95, -26.37, 3.38, fx_land_an24,
light.10 = 5, 0.95, 26.37, 3.38, fx_land_an24,
light.11 = 6, 11.21, 17.1, 0.3, fx_taxi_an24,
light.12 = 6, 11.21, -17.1, 0.3, fx_taxi_an24,
light.13 = 6, 0.95, -26.37, 3.38, fx_land_an24,
light.14 = 6, 0.95, 26.37, 3.38, fx_land_an24,
[GeneralEngineData]
//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
engine_type = 5
fuel_flow_scalar = 1.01
engine.0 = 11.90, -12.95, 3,
engine.1 = 11.9, 12.956, 3,
min_throttle_limit=0.000000
[smokesystem]
smoke.0 = 0,-30.86,-5.28, fx_fallsw5.fx
[effects]
wake = fx_wake
water = fx_spray
dirt = fx_tchdrt
concrete = fx_sparks
touchdown = fx_tchdwn_s, 1
[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type = 2
number_of_tank_selectors = 2
LeftMain = 0.485, -10, 4.3, 435.9, 0
LeftAux = 0.485, -17.4, 4.3, 499.3, 0
RightMain = 0.485, 10, 4.3, 435.9, 0
RightAux = 0.485, 17.4, 4.3, 499.3, 0
electric_pump=0
[contact_points]
static_pitch = -0.3
static_cg_height = 7
tailwheel_lock = 0
max_number_of_points = 16
point.0 = 1, 22.4, 0, -7.2, 800, 0, 1.147, 35, 0.26, 2.9, 0.5, 3.5, 4, 0, 0, 0
point.1 = 1, -1.932, -13.1, -8.1, 1400, 1, 1.6, 0, 0.79, 2.5, 0.59, 4.0, 4.5, 2, 0, 0
point.2 = 1, -1.932, 13.1, -8.1, 1400, 2, 1.6, 0, 0.79, 2.5, 0.59, 4.0, 4.5, 2, 0, 0
point.3 = 2, 28.029, 0, -3.953, 9000, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.4 = 2, -2.41, 0, -5.0895, 6000, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.5 = 2, -36.506, 0, -0.4302, 6000, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2.00, -5.22, -47.50, 3.42, 3000, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 5, 0, 0
point.7 = 2.00, -5.22, 47.50, 3.43, 3000, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 6, 0, 0
point.8 = 2.00, -1.22, -47.50, 3.42, 3000, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 5, 0, 0
point.9 = 2.00, -1.22, 47.50, 3.42, 3000, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 6, 0, 0
point.10 = 2.00, 2.70, -12.50, -1.30, 6000, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 5, 0, 0
point.11 = 2.00, 2.70, 12.50, -1.30, 6000, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 6, 0, 0
point.12 = 2, -39.1238, 0, 19.9963, 3000, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0
point.13 = 2, -33.6847, 0, 8.9965, 3000, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0
point.14 = 2.00, 4.45, 0.00, 5.50, 3000, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.00, 0.00, 7, 0, 0
point.15 = 2, 23.8057, 0, 3.2579, 3000, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0
gear_system_type=0
[keyboard_response]
elevator = 150.000000, 250.000000
aileron = 150.000000, 250.000000
rudder = 150.000000, 250.000000
[forcefeedback]
gear_bump_nose_magnitude = 3000
gear_bump_nose_direction = 18000
gear_bump_nose_duration = 250000
gear_bump_left_magnitude = 2700
gear_bump_left_direction = 9000
gear_bump_left_duration = 250000
gear_bump_right_magnitude = 2700
gear_bump_right_direction = 27000
gear_bump_right_duration = 250000
ground_bumps_magnitude1 = 1300
ground_bumps_angle1 = 08900
ground_bumps_intercept1 = 3.0
ground_bumps_slope1 = 0.20
ground_bumps_magnitude2 = 200
ground_bumps_angle2 = 09100
ground_bumps_intercept2 = 1.075
ground_bumps_slope2 = 0.035
crash_magnitude1 = 10000
crash_direction1 = 01000
crash_magnitude2 = 10000
crash_direction2 = 9000
crash_period2 = 75000
crash_duration2 = 2500000
stick_shaker_magnitude = 2000
stick_shaker_direction = 0
stick_shaker_period = 111111
[airplane_geometry]
//ACM_AREAW1// 0,0,0,2.8011,1.6222,1.6222,0,2.6610,3.2444,3.2444
//ACM_AREAW2// 0,2.5210,4.8666,4.8666,0,2.3809,6.4888,6.4888,0,2.2408
//ACM_AREAW3// 8.1110,8.1110,0,2.1008,9.7332,9.7332,0,1.9607,11.3554,11.3554
//ACM_AREAW4// 0,1.8207,12.9777,12.9777,0,1.6806,14.5999,14.5999,0,1.5406
//ACM_AREAH1// 0,0,0,3.3223,0.5537,0.5537,0.1692,3.3254,1.1074,1.1074
//ACM_AREAH2// 0.3385,3.3286,1.6611,1.6611,0.5078,3.3318,2.2148,2.2148,0.6771,3.3350
//ACM_AREAH3// 2.7685,2.7685,0.8464,3.3381,3.3223,3.3223,1.0157,3.3413,3.8760,3.8760
//ACM_AREAH4// 1.1850,3.3445,4.4297,4.4297,1.3543,3.3477,4.9834,4.9834,1.5236,3.3508
//ACM_AREAV1// 0,0,0,4.8920,0.5435,0.5435,0.2534,4.7541,1.0871,1.0871
//ACM_AREAV2// 0.5069,4.6162,1.6306,1.6306,0.7603,4.4783,2.1742,2.1742,1.0138,4.3404
//ACM_AREAV3// 2.7177,2.7177,1.2673,4.2025,3.2613,3.2613,1.5207,4.0646,3.8049,3.8049
//ACM_AREAV4// 1.7742,3.9267,4.3484,4.3484,2.0277,3.7888,4.8920,4.8920,2.2811,3.6509
//ACM_CAREAW1// 7.2999,7.2999,1.4005,1.9607,8.1110,8.1110,1.4005,1.9327,8.9221,8.9221
//ACM_CAREAW2// 1.4005,1.9047,9.7332,9.7332,1.4005,1.8767,10.5443,10.5443,1.4005,1.8487
//ACM_CAREAW3// 11.3554,11.3554,1.4005,1.8207,12.1666,12.1666,1.4005,1.7927,12.9777,12.9777
//ACM_CAREAW4// 1.4005,1.7647,13.7888,13.7888,1.4005,1.7366,14.5999,14.5999,1.4005,1.7086
//ACM_CAREAH1// 0,0,1.6611,3.3223,0.5537,0.5537,1.8304,3.4085,1.1074,1.1074
//ACM_CAREAH2// 1.9997,3.4947,1.6611,1.6611,2.1690,3.5810,2.2148,2.2148,2.3383,3.6672
//ACM_CAREAH3// 2.7685,2.7685,2.5076,3.7534,3.3223,3.3223,2.6768,3.8397,3.8760,3.8760
//ACM_CAREAH4// 2.8461,3.9259,4.4297,4.4297,3.0154,4.0121,4.9834,4.9834,3.1847,4.0984
//ACM_CAREAV1// 0,0,1.2230,3.6690,0.5435,0.5435,1.4764,3.7268,1.0871,1.0871
//ACM_CAREAV2// 1.7299,3.7845,1.6306,1.6306,1.9834,3.8423,2.1742,2.1742,2.2368,3.9001
//ACM_CAREAV3// 2.7177,2.7177,2.4903,3.9579,3.2613,3.2613,2.7438,4.0157,3.8049,3.8049
//ACM_CAREAV4// 2.9972,4.0735,4.3484,4.3484,3.2507,4.1313,4.8920,4.8920,3.5042,4.1890
wing_area = 807.1
wing_span = 95.80
wing_root_chord = 9.19
wing_dihedral = 0
wing_incidence = 0.0
wing_twist = 0.00
oswald_efficiency_factor = 0.65
wing_winglets_flag = 0
wing_sweep = 0
wing_pos_apex_lon = 2.3
wing_pos_apex_vert = 4.3
htail_area = 213.4
htail_span = 32.70
htail_pos_lon = -36.50
htail_pos_vert = 4.3
htail_incidence = -3.00
htail_sweep = 17
vtail_area = 192.4
vtail_span = 16.05
vtail_sweep = 25
vtail_pos_lon = -34
vtail_pos_vert = 4.3
elevator_area = 55.54
aileron_area = 65.87
rudder_area = 53.819
elevator_up_limit = 30.0
elevator_down_limit = 15.0
aileron_up_limit = 24.0
aileron_down_limit = 16.0
rudder_limit = 25.000
elevator_trim_limit = 80
spoiler_limit = 0.000
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000
spoilerons_available = 0
[electrical]
max_battery_voltage = 27
generator_alternator_voltage = 28
max_generator_alternator_amps = 600
electric_always_available = 0
flap_motor = 0, 5, 17
gear_motor = 0, 5, 17
autopilot = 0, 5, 17
avionics_bus = 0, 10, 17
avionics = 1, 5, 17
pitot_heat = 0, 15, 17
additional_system = 0, 2, 17
marker_beacon = 1, 2, 17
gear_warning = 0, 2, 17
fuel_pump = 0, 5, 17
starter1 = 0, 20, 17
starter2 = 0, 20, 17
light_nav = 0, 5, 10
light_beacon = 0, 5, 10
light_landing = 0, 5, 17
light_taxi = 0, 5, 17
light_strobe = 0, 5, 10
light_panel = 0, 5, 10
[Flaps.0]
type=1
span-outboard=0.600
extending-time=16.000
system_type=1
damaging-speed=0.0 //162.000
blowout-speed=0.0 //170.000
lift_scalar=1.0
drag_scalar=1.0
pitch_scalar=1.0
flaps-position.0= 0.000, 0.0
flaps-position.1= 5.000, 0.0
flaps-position.2=10.000, 0.0
flaps-position.3=15.000, 0.0
flaps-position.4=20.000, 0.0
flaps-position.5=25.000, 0.0
flaps-position.6=30.000, 0.0
flaps-position.7=38.000, 0.0
[Flaps.1]
type=1
span-outboard=0.600
extending-time=6.300
system_type=1
damaging-speed=0.0 //162.000
blowout-speed=0.0 //170.000
lift_scalar=0.2
drag_scalar=0.1
pitch_scalar=0.05
flaps-position.0= 0.000, 0.0
flaps-position.1= 5.000, 0.0
flaps-position.2=10.000, 0.0
flaps-position.3=15.000, 0.0
///===================================================
[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=0.075,0.075
[exits]
number_of_exits = 3
exit_rate.0 = 0.2 ;Percent per second
exit_rate.1 = 0.2 ;Percent per second
exit_rate.2 = 0.2 ;Percent per second
[Reference Speeds]
flaps_up_stall_speed=102.000
full_flaps_stall_speed=82.800
cruise_speed=215.000
max_indicated_speed=292.000000
max_mach=0.650000
[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, 1
Adf.1=1
Transponder.1=1
Marker.1=1
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=1000.000000
autothrottle_available=0
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
use_no_default_bank=0 //For no wing leveler when AP On
use_no_default_pitch=0 //For no pitch holding when AP On
autoland_available=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
[brakes]
toe_brakes_scale=0.518815
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=55.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[pitot_static]
vertical_speed_time_constant=1.0 //0.7
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[Views]
eyepoint=22.2, -1.70, 2.1
[direction_indicators]
direction_indicator.0=3,0