[fltsim.0] title=R.C.A.F. SA-16 sim=Albatross model= panel=1 sound= texture= kb_checklists= kb_reference= ui_manufacturer=Grumman ui_type=R.C.A.F. 9310 ui_variation=Tundra Queen SA-16 description=A total of 10 Grumman G-111 "Alberts" were acquired by the RCAF on 5 August, 1960 to replace their remaining Cansos in the Search and Rescue role. The triphibious "Alberts" proved to be just as rugged and adaptable as the venerable Cansos. In 1970 they were replaced by the Buffalo and SAR helicopters, thus causing the CF to be deprived of its last fixed wing amphibians. In their decade of operation the fleet had logged between 5,946 and 7,498 hours per airframe. atc_heavy=0 atc_id=9310 atc_airline=Airforce atc_flight_number= [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, 19.200, 0.000, -14.750, 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, -14.550, 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, -14.550, 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, -5.000, -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, 5.000, -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, 4.000, -34.800, -9.700, 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, 4.000, 34.800, -9.700, 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=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 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 <<<<<<<<<<<<<
