INSTALL
- - take the layout.json which is next to the bagolu-kitfox-fm.README.txt file and copy it to the Official directory
- (...)\pkgs\Official\OneStore\bt-kitfox-sti
- there's allready a layout.json in this folder : you can keep a backup of this file if you want, but the provided file needs to replace it.
- - Copy the subfolder bagolu-kitfox-fm located next to the README file into the community folder.
- In community folder, you should have :
- community\bagolu-kitfox-fm\
- and inside this folder : manifest.json and other files (including another layout.json: do not modify them)
- update of plane characteristics taken from Kitfox website (they were wrong) :
max_gross_weight = 1320
empty_weight = 825
wing_area =148
wing_span =32
- Added copilot and bagages slots (there was only a pilot station) :
max_number_of_stations = 3 ; Number of payload stations (actual CG points from POH used)
station_load.0 = 170, 1.2, -0.5, -0.5, TT:MENU.PAYLOAD.PILOT, 1
station_load.1 = 170, 1.2, 0.5, -0.5, TT:MENU.PAYLOAD.COPILOT, 5
station_load.2 = 150, -1.0, 0, 0, TT:MENU.PAYLOAD.BAGGAGE, 6
- Corrected fuel tanks to Kitfox website values :
LeftMain = 0.5, -5, 2.5, 13.5, 0.5
RightMain = 0.5, 5, 2.5, 13.5, 0.5
- Modification of flaps behavior :
lift_coef_flaps = 0.03
- replaced the single stage flap to 3 position flaps :
max_on_ground_position=3
flaps-position.0 = 0, -1, 0
flaps-position.1 = 16, -1, 0.5
flaps-position.2 = 33, -1, 0.75
flaps-position.3 = 46, -1, 1
- correction of engine values to match the 915i :
max_rated_hp=141
min_cruise_rpm=1800
engine_mechanical_efficiency_table = 0:0.5, 1000:0.52, 2000:0.52, 5000:0.7, 5100:0.7, 5500:0.7, 6000:0.5
engine_friction_table = -600:-65, 600:65, 1000:17, 6000:17
egt_factor_from_pct_power = 0:0.7, 0.5:0.894, 0.64:0.956, 0.75:0.98, 1:1
egt_delta_from_mixture_ratio = 0.043:-100, 0.05:-89.7, 0.067:-50, 0.07:0, 0.075:-4.9, 0.083:-80, 0.108:-120.5
engine_friction_table = -600:-65, 600:65, 1000:17, 6000:17
turbocharged=1
critical_altitude=15000
- correction of manifold pressure at idle engine mode :
manifold_efficiency_table=0.000000:0.220000, 1.000000:0.970000
- correction of the propeller :
min_gov_rpm=300
beta_max=35
- brakes too strong
toe_brakes_scale=0.3
- CG correction to gain stability on ground
empty_weight_CG_position = -0.5, 0, -1.5
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