[fltsim.0]
title= Pander S.4 Panderjager
sim= A26_invader
model=
panel= vc
sound=
texture=
kb_checklists=
kb_reference=
atc_id= PH-OST
ui_manufacturer= Pander & Zoonen
ui_type= S.4
ui_variation= Dutch Syndicate
atc_heavy=0
atc_airline=
atc_flight_number=
description=A-26C - Two Pratt\/Whitney R-2800-27 air-cooled radials
[General]
atc_type= Pander
atc_model= S4
performance=A-26C - Two Pratt\/Whitney R-2800-27 air-cooled radials\n+ Empty Weight: 28480 lbs\n+ Max Power: 2000 Hp\n+ Maneuver speed: 319 mph @ 5.0 g\n+ Max speed: 353 mph @ 15600 ft\n+ Max speed at sea-level: 313 mph\n+ Climb rate: 1650 ft\/min @ 136 mph\nFlight Dynamics By: Jerry Beckwith\nMudpond Virtual Aircraft\nFD Build 35 - 3\/25\/07 12:20 PM\nFlight Dynamics Workbook V2006.A26
[Views]
eyepoint = 2.31, -0.85, 3.504
[fuel]
LeftMain = 0, 5.0, 0, 287, 0
RightMain = 0, -5.0, 0, 287, 0
Center1 = 7.0, 0, 0, 287, 0
fuel_type = 1
number_of_tank_selectors = 2
electric_pump=1
[WEIGHT_AND_BALANCE]
empty_weight = 7 056
max_gross_weight = 12568
reference_datum_position = 0, 0, 0
empty_weight_CG_position = 0, 0, 0
station_load.0 = 170, 2.3, -1.0, 0
station_load.1 = 170, 2.3, 1.0, 0
station_load.2 = 170, -4.3, 1.0, 0
empty_weight_pitch_MOI = 103047
empty_weight_roll_MOI = 73697
empty_weight_yaw_MOI = 164187
empty_weight_coupled_MOI = 0
empty_weight_coupled_MOI = 0.000
[GeneralEngineData]
engine_type = 0
Engine.0 = 6.9, -8.6, 0
Engine.1 = 12.2, 0, 0.9
Engine.2 = 6.9, 8.6, 0
min_throttle_limit = 0.1
master_ignition_switch = 0
fuel_flow_scalar = 1
[piston_engine]
critical_altitude= 19800
cylinder_displacement= 108.33 //Cubic inches per cylinder
compression_ratio= 5.1 //Compression ratio
number_of_cylinders= 9
max_rated_rpm= 2415
max_rated_hp= 420
fuel_metering_type= 1
cooling_type= 0
normalized_starter_torque= 3
turbocharged= 1
max_design_mp= 42.7 //TOGA
min_design_mp= 0
emergency_boost_type=0
emergency_boost_mp_offset=0.000000
emergency_boost_gain_offset=0.000000
fuel_air_auto_mixture=0
auto_ignition=0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000
[propeller]
thrust_scalar = 1.22 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 9.0 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 12.76 //Propeller moment of inertia
beta_max= 65.0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 15.0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1000 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.613 //Propeller gear reduction ratio
fixed_pitch_beta= 0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit= 80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available= 0 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available= 0 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available= 0 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available= 0 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather= 0 //Minimum RPM for prop feathering
beta_feather= 0 //Feathering pitch angle (degrees)
power_absorbed_cf= 0 //Coefficient of friction for power absorbed by propeller in feather
defeathering_accumulators_available= 0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available= 0 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta= 0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta= 0 //Minimum pitch angle in reverse, (degrees)
[airplane_geometry]
oswald_efficiency_factor=0.888253
wing_area = 454.000000
wing_span = 54.7
wing_root_chord = 13.5
wing_pos_apex_lon = 3.25
wing_pos_apex_vert = 0.0
wing_dihedral = 0
wing_incidence = 1.499634
wing_twist = 0
wing_winglets_flag = 0
wing_sweep = 0
htail_area =34.000000
htail_span =10.500000
htail_pos_lon = -23.300
htail_pos_vert = 0.000
htail_incidence =-0.999756
htail_sweep = 40.000
vtail_area =15.000000
vtail_span =4.815880
vtail_sweep =0.000000
vtail_pos_lon = -26.000
vtail_pos_vert = 3.400
elevator_area =13.260000
aileron_area =18.900000
rudder_area =8.230000
elevator_up_limit = 18.000
elevator_down_limit = 15.000
aileron_up_limit = 18.000
aileron_down_limit = 18.000
rudder_limit = 25.000
elevator_trim_limit = 15.000
spoiler_limit = 0
spoilerons_available = 0
aileron_to_spoileron_gain = 0
min_ailerons_for_spoilerons = 0
min_flaps_for_spoilerons = 0
[Reference Speeds]
flaps_up_stall_speed = 57
full_flaps_stall_speed = 49
cruise_speed = 180
max_indicated_speed = 268 ;this may be a generous estimate and needs to warn Vno not Vne due to the unpatched weather module bugs within FS9 which are only corrected by a registered copy of FSUIPC.
[Radios]
Com.1 = 1, 0
Com.2 = 0, 0
Nav.1 = 1, 0, 0
Nav.2 = 0, 0, 0
Adf.1 = 1 .
Adf.2 = 0
Transponder.1 = 1
Audio.1 = 1
Marker.1 = 1
[contact_points]
//GEAR
point.0 = 1, -26.00, 0, -0.5, 1200, 0, 1.01, 40, 0.3 , 2.5, 0.9 , 0, 0, 0, 0, 0
point.1 = 1, 2.2, -8.92, -5.8, 1600, 1, 1.98, 0, 0.4 , 2.5, 0.85, 8, 10, 2, 200, 300
point.2 = 1, 2.2, 8.92, -5.8, 1600, 2, 1.98, 0, 0.4 , 2.5, 0.85, 8, 10, 3, 200, 300
//SCRAPES
static_pitch = 10
static_cg_height = 6.3
tailwheel_lock = 0
gear_system_type = 0
[brakes]
parking_brake = 1
toe_brakes_scale = 0.25
[hydraulic_system]
normal_pressure = 732.0
electric_pumps = 0
engine_map = 1,1,0,0 //pumps on Eng1,2
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing, 8=Wing, 9=logo, 10=cabin
light.0 = 4, 3.647, 1.6325, 2.3501, fx_vclight_red //Red Cockpit Light Left Side
light.1 = 9, 3.647, -1.6325 2.3501, fx_vclight_red //Red Cockpit Light Right Side
light.2 = 8, -5.05, 0, 4.12, fx_vclight_red //Red Cabin Light
light.3 = 10, -5.05, 0, 4.12, fx_vclight //White Cabin Light
eyepoint = 2.31, -0.85, 3.604
[keyboard_response]
elevator =200, 1000
aileron =200, 1000
rudder =200, 1000
[direction_indicators]
direction_indicator.0=1,0
direction_indicator.1=2,0
[attitude_indicators]
attitude_indicator.0 = 1
attitude_indicator.1 = 2
[turn_indicators]
turn_indicator.0=2,0
[autopilot]
autopilot_available = 1
flight_director_available = 0
default_vertical_speed = 500
autothrottle_available = 0
autothrottle_arming_required = 0
autothrottle_max_rpm = 90
autothrottle_takeoff_ga = 1
default_pitch_mode=0
pitch_takeoff_ga = 3
max_pitch_velocity_lo_alt_breakpoint = 10000
max_pitch_velocity_hi_alt_breakpoint = 18000
max_pitch = 10
max_pitch_acceleration = 1
max_pitch_velocity_lo_alt = 2
max_pitch_velocity_hi_alt = 1.5
max_bank= 25
max_bank_acceleration = 1.8
max_bank_velocity = 3
max_throttle_rate = 0.1
nav_proportional_control = 9
nav_integrator_control = 0.25
nav_derivative_control = 0
nav_integrator_boundary = 2.5
nav_derivative_boundary = 0
gs_proportional_control = 15
gs_integrator_control = 0.26
gs_derivative_control = 0
gs_integrator_boundary = 0.7
gs_derivative_boundary = 0
yaw_damper_gain = 0
use_no_default_bank=0
use_no_default_pitch=0
default_bank_mode=2
[forcefeedback]
ground_bumps_magnitude1=2600 ; 0 - 10000
ground_bumps_angle1=8900 ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.6
ground_bumps_magnitude2=1200 ; 0 - 10000
ground_bumps_angle2=9100 ; 0 - 35999 degrees
ground_bumps_intercept2=0.085
ground_bumps_slope2=0.65
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=3500000 ; in microseconds
[stall_warning]
type=1 ;unlikely in real life
[exits]
number_of_exits = 1
exit_rate.0 = 0.27 ;Percent per second
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
startup=fx_engstrt_jenny
touchdown=fx_tchdwn_s, 1
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 100
flap_motor = 0, 15 , 17.0
gear_motor = 0, 15 , 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 15 , 17.0
additional_system = 0, 20, 17.0
starter1 = 0, 20, 17.0
starter2 = 0, 20, 17.0
starter3 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_strobe = 0, 1 , 17.0
light_panel = 0, 1 , 17.0
light_strobe = 0, 1 , 17.0
light_cabin = 0, 2 , 17.0
light_logo = 0, 1 , 17.0
directional_gyro = 1, 5 , 17.0
[flight_tuning]
p_factor_on_yaw = 0.01
torque_on_roll = 0.01
gyro_precession_on_yaw = 0.01
gyro_precession_on_pitch = 0.01
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=1
flaps-position.0=0.000000,0.000000
flaps-position.1=15.000000,0.000000
flaps-position.2=30.000000,0.000000
flaps-position.3=45.000000,0.000000
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
