[fltsim.0] title=CL215 "Canada Manitoba" sim=CL215_CAN model= panel= sound= texture=manitoba checklists= description=CL215 file air Land version.\nThe Bombardier-Canadair CL215 is a boat-type amphybian with two piston radial engine. \nIts main use is in the firefighting role, with a secondary transport role.Two main water tank with a capacity of about 2,673 Lit.\nFirst flew on October 1967.\nOriginal Model , copyright © 2001 by Massimo Taccoli\nwww.maxtac.it\nAir file by Andrea CINI ui_manufacturer=Bombardier/Canadair ui_type=CL215 ui_variation=Canada Manitoba atc_heavy=0 atc_id= atc_airline= atc_flight_number= [fltsim.1] title=CL215 "Canada Ontario" sim=CL215_CAN model= panel= sound= texture=Ontario checklists= description=The Bombardier-Canadair CL215 is a boat-type amphybian with two piston radial engine. \nIts main use is in the firefighting role, with a secondary transport role.Two main water tank with a capacity of about 2,673 Lit.\nFirst flew on October 1967.\nOriginal Model , copyright © 2001 by Massimo Taccoli\nwww.maxtac.it\nAir file by Andrea CINI ui_manufacturer=Bombardier/Canadair ui_type=CL215 ui_variation=Canada Ontario atc_heavy=0 atc_id= atc_airline= atc_flight_number= [fltsim.2] title=CL215 "Canada Quebec" sim=CL215_CAN model= panel= sound= texture=Quebec checklists= description=CL215 file air Land version.\nThe Bombardier-Canadair CL215 is a boat-type amphybian with two piston radial engine. \nIts main use is in the firefighting role, with a secondary transport role.Two main water tank with a capacity of about 2,673 Lit.\nFirst flew on October 1967.\nOriginal Model , copyright © 2001 by Massimo Taccoli\nwww.maxtac.it\nAir file by Andrea CINI ui_manufacturer=Bombardier/Canadair ui_type=CL215 ui_variation=Canada Quebec atc_heavy=0 atc_id= atc_airline= atc_flight_number= [fltsim.3] title=CL215 "Canada Conifair" sim=CL215_CAN model= panel= sound= texture=Conifair checklists= description=CL215 file air Land version.\nThe Bombardier-Canadair CL215 is a boat-type amphybian with two piston radial engine. \nIts main use is in the firefighting role, with a secondary transport role.Two main water tank with a capacity of about 2,673 Lit.\nFirst flew on October 1967.\nOriginal Model , copyright © 2001 by Massimo Taccoli\nwww.maxtac.it\nAir file by Andrea CINI ui_manufacturer=Bombardier/Canadair ui_type=CL215 ui_variation=Canada Conifair atc_heavy=0 atc_id= atc_airline= atc_flight_number= [General] performance=Max Cruise Speed\t181 kts\nMaximum Range\t1,405 mls\nInitial rate of climb 1,000 ft\/min\nMTOW as land based Water bomber 43,500 lbs\nMTOW as water based 37,700 lbs\nPower plant : two P&W R-2800 each rated at 2100 bhp for ttake off and 1,800 bhp continuous.\nFuel max capacity 1266 imp-gal in 16 identical bladder type fuel cells. atc_type=BOMBARDIER/Canadair atc_model=CL215 [WEIGHT_AND_BALANCE] empty_weight=26810.000 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=170.000, 12.000, -4.000, 2.000 //Pilot Weight (lbs), station_load.1=170.000, 12.000, -4.000, 2.000 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=180000.000 empty_weight_roll_MOI=220000.000 empty_weight_yaw_MOI=272331.000 empty_weight_coupled_MOI=0.000 max_gross_weight=37700.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.441 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=60.0 [contact_points] //Gear point.0=1, 20.863, 0.000, -14.720, 3333, 0.000, 0.935, 80.000, 0.300, 2.500, 0.800, 10, 14.000, 0.000, 0.000, 0.000 point.1=1, -3.159, -8.671, -14.220, 3333, 1.000, 1.693, 0.000, 0.200, 2.500, 0.800, 10, 14.000, 2.000, 0.000, 0.000 point.2=1, -3.159, 8.671, -14.220, 3333, 2.000, 1.693, 0.000, 0.200, 2.500, 0.800, 10, 14.000, 3.000, 0.000, 0.000 //Float point.3=4.000, 25.000, -2.000, -11.000, 3333.000, 0.000, 0.000, 30.000, 1.000, 2.500, 0.650, 0.000, 0.000, 0.000, 0.000, 0.000 point.4=4.000, 25.000, 2.000, -11.000, 3333.000, 0.000, 0.000, 30.000, 1.000, 2.500, 0.650, 0.000, 0.000, 1.000, 0.000, 0.000 point.5=4.000, -8.000, -7.000, -11.000, 3333.000, 0.000, 0.000, 0.000, 1.000, 2.500, 0.650, 0.000, 0.000, 2.000, 0.000, 0.000 point.6=4.000, -8.000, 7.000, -11.000, 3333.000, 0.000, 0.000, 0.000, 1.000, 2.500, 0.650, 0.000, 0.000, 3.000, 0.000, 0.000 //Scrape point.7=2.000, -7.000, -43.000, -8.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.8=2.000, -7.000, 43.000, -8.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.9=2.000, -36.000, 0.000, -8.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.10=2.000, 22.000, 0.000, -8.000, 1800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch=1.2127 static_cg_height=14.28 [Views] eyepoint=16.84, -1.91, -3.5 //(feet) longitudinal, lateral, vertical distance from reference datum [fuel] Center1=0.000, 0.000, 0.000, 1516.000, 1516.000 \\load of water LeftMain=0.000, 0.000, 0.000, 633.000, 0.000 RightMain=0.000, 0.000, 0.000, 633.000, 0.000 fuel_type=1.000 number_of_tank_selectors=1 [airplane_geometry] wing_area=1280.000 wing_span=94.000 wing_root_chord=4.917 wing_dihedral=1.000 wing_incidence=1.000 wing_twist=-3.999 oswald_efficiency_factor=0.944 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=3.280 wing_pos_apex_vert=0.000 htail_area=331.000 htail_span=36.083 htail_pos_lon=-32.000 htail_pos_vert=0.000 htail_incidence=3.246 htail_sweep=0.000 vtail_area=90.000 vtail_span=10.817 vtail_sweep=0.000 vtail_pos_lon=-30.000 vtail_pos_vert=6.000 elevator_area=36.000 aileron_area=19.000 rudder_area=18.000 elevator_up_limit=14.324 elevator_down_limit=14.324 aileron_up_limit=19.481 aileron_down_limit=19.481 rudder_limit=27.502 elevator_trim_limit=13.751 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 [GeneralEngineData] engine_type=0 Engine.0=7.917, -12.083, 2.083 Engine.1=7.917, 12.083, 2.083 fuel_flow_scalar=0.125 <<<<<<<<<<<<<<< [piston_engine] cylinder_displacement=155.770 compression_ratio=6.750 number_of_cylinders=18 max_rated_rpm=2700.000 max_rated_hp=2100.00 fuel_metering_type=0 cooling_type=0 normalized_starter_torque=0.035 turbocharged=1 <<<<<<<<<<<<<<< max_design_mp=52.999999 min_design_mp=1.000000 critical_altitude=21500.000000 emergency_boost_type=0 emergency_boost_mp_offset=10.000000 emergency_boost_gain_offset=0.660000 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 power_scalar=1.000 [propeller] propeller_type=0 propeller_diameter=13.33 propeller_blades=3 propeller_moi=62.17 beta_max=65.00 beta_min=30.00 <<<<<<<<<<<<<<<< min_gov_rpm=1800.000 prop_tc=0.01 gear_reduction_ratio=2 fixed_pitch_beta=0.000 low_speed_theory_limit=80.000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=1 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 thrust_scalar=1.901 [Reference Speeds] flaps_up_stall_speed=65.000 full_flaps_stall_speed=52.000 cruise_speed=177.333 [keyboard_response] elevator=100.000, 180.000 aileron=200.000, 1000.000 rudder=200.000, 1000.000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000 autothrottle_available=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=1 autothrottle_max_rpm=100.000 <<<<<<<<<<<<<< evtl. Schub bei Start zu gering pitch_takeoff_ga=8.000 use_no_default_bank=1 <<<<<<<<<<<<<
