[fltsim.0] JABIndex=7 title=DH82a Tiger Moth OO-TGM sim=dh82 model=ns panel=red sound= texture=OOTGM checklists= kb_checklists=DH82_check kb_reference=DH82_ref kb_notes=DH82_notes ui_manufacturer=De Havilland ui_type=DH82 Tiger Moth ui_variation=Civil - Belgian OO-TGM description=De Havilland's basic trainer. The Tiger Moth was a derivative of the DH60T Moth trainer adapted to the requirements of the RAF.\n OO-TGM is currently owned and operated by The Flying Legends which is based at the airfield of Kortrijk-Wevelgem in Belgium.\n atc_heavy=0 atc_id=OOTGM atc_airline= atc_flight_number= [General] performance=Span\t29ft4ins\nLength\t23ft11ins\nWeight (empty)\t1,115lb.\nPower:\tDH.Gypsy Major 4 cyl. 130 hp\nDesigner:\tJohn Woodside 2002 atc_type=DEHAVILLAND atc_model=DH82 [propeller] thrust_scalar=0.82 // evolved propeller_type=1 propeller_diameter=6.300 // checked propeller_blades=2 // checked propeller_moi=5.000 rotation=-1 beta_max=0.000 beta_min=0.000 min_gov_rpm=500.000 prop_tc=0.100 gear_reduction_ratio=1.000 fixed_pitch_beta=21.200 // evolved low_speed_theory_limit=80.000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000 beta_feather=0.000 power_absorbed_cf=0.000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000 minimum_reverse_beta=0.000 [piston_engine] power_scalar=1.0 max_rpm_mechanical_efficiency_scalar=1.0 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 cylinder_displacement=90.3 // evolved compression_ratio=5.25 // checked number_of_cylinders=4 max_rated_rpm=2350.000 // checked max_rated_hp=130.000 // checked fuel_metering_type=1 // checked cooling_type=0 // checked normalized_starter_torque=0.300 turbocharged=0 max_design_mp=0.000 min_design_mp=0.000 critical_altitude=0.000 // n/a emergency_boost_type=0 // n/a emergency_boost_mp_offset=0.000 // n/a emergency_boost_gain_offset=0.000 // n/a fuel_air_auto_mixture=0 auto_ignition=0 [flight_tuning] cruise_lift_scalar=0.503 pitch_stability=1.000 roll_stability=1.00 yaw_stability=1.101 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.900 rudder_effectiveness=1.00 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [WEIGHT_AND_BALANCE] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.200, 0.000, 0.000 max_number_of_stations=50 station_load.0=135.000, 0.500, 0.000, 0.000 empty_weight=1115.000 // checked empty_weight_roll_MOI=1500.000 empty_weight_pitch_MOI=1596.000 empty_weight_yaw_MOI=3000.000 empty_weight_coupled_MOI=0.000 max_gross_weight=1825.000 // checked CG_forward_limit=0.000 CG_aft_limit=1.000 [fuel] Center1=0.500, 0.000, 3.000, 22.800, 1.000 fuel_type=1.000 number_of_tank_selectors=1 [airplane_geometry] wing_area=239.000 // checked wing_span=41.00 // should be 29.33 but adjusted for biplane wing_root_chord=4.383 // checked wing_dihedral=2.750 // checked wing_incidence=2.000 // checked but reduced from 4 to 2 wing_twist=0.000 // checked oswald_efficiency_factor=0.800 // no idea wing_winglets_flag=0 wing_sweep=5.8156 // checked - top wing wing_pos_apex_lon=2.000 wing_pos_apex_vert=3.000 htail_area=27.200 // checked htail_span=9.8300 // checked htail_pos_lon=-12.500 htail_pos_vert=2.600 htail_incidence=0.000 // checked htail_sweep=0.000 // checked vtail_area=12.200 // checked vtail_span=3.950 // checked vtail_sweep=0.000 // checked vtail_pos_lon=-12.500 vtail_pos_vert=2.600 elevator_area=13.800 // checked aileron_area=22.400 // checked rudder_area=9.400 // checked elevator_up_limit=27.500 // checked elevator_down_limit=20.000 // checked aileron_up_limit=19.481 aileron_down_limit=10.00 rudder_limit=31.5 // checked elevator_trim_limit=19.481 spoiler_limit=0.000 spoilerons_available=0 aileron_to_spoileron_gain=0.000 min_ailerons_for_spoilerons=0.000 min_flaps_for_spoilerons=0.000 [contact_points] // FORE LEFT UP ROD BRAKE WH RA STANG SCOM C/R DR EXT RET ST AL D/AS point.0=3, -16.0, 0.0, -1.7, 1180.0, 0, 0.115, 31.0, 0.388, 2.5, 0.835, 0.0, 0.0, 0.0, 0.0, 0.0 //TAIL point.1=1, 1.5, -2.5, -5.2, 1574.0, 0, 0.765, 0.0, 0.428, 2.5, 0.750, 0.0, 0.0, 2.0, 0.0, 0.0 //LEFT point.2=1, 1.5, 2.5, -5.2, 1574.0, 0, 0.765, 0.0, 0.428, 2.5, 0.750, 0.0, 0.0, 3.0, 0.0, 0.0 //RIGHT point.3=2, -1.5, -14.6, -1.0, 787.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0 //LWS point.4=2, -1.5, 14.6, -1.0, 787.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0 //RWS point.5=2, 6.0, 0.0, -2.5, 787.0, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 9.0, 0.0, 0.0 //TS static_pitch=11.5000 static_cg_height=4.4827 [GeneralEngineData] engine_type=0 Engine.0=7.180, 0.000, 1.100 fuel_flow_scalar=1.000 [Reference Speeds] flaps_up_stall_speed=39.000 // checked full_flaps_stall_speed=37.000 // checked - all values not run through FSEdit cruise_speed=74 [keyboard_response] elevator=150.000, 250.000 aileron=150.000, 250.000 rudder=150.000, 250.000 [Views] eyepoint=-2.958, 0.000, 1.5416 [electrical] max_battery_voltage=0 generator_alternator_voltage=0 [autopilot] autopilot_available=0 flight_director_available=0 [direction_indicators] direction_indicator.0=1,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [LIGHTS] light.0=4,-4.60,0.0,0.0,fx_vclight_red [SMOKESYSTEM] smoke.0=0.00, -5.70, 0.00, fx_smoke_w //Note: settings below are for wingtip smoke if desired. Remove the forward slashes //smoke.1=0.00, -0.20, 15.00, fx_redssmoke_red //smoke.2=0.00, -0.20, -15.00, fx_redssmoke_blue [forcefeedback] gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds