Hi,
This work perfect for me (using the airfile (renamed) of the old hangar DH86)
I don't use VC (it's my religion dictat .. lol ) so I have no further problems
[piston_engine]
power_scalar = 1.0 //Piston power scalar
cylinder_displacement= 93.4 //Cubic inches per cylinder
compression_ratio= 6.5 //Compression ratio
number_of_cylinders=6 //Number of cylinders
max_rated_rpm= 2400 //Max rated RPM
max_rated_hp= 224 //Max rated HP
fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor
cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid
normalized_starter_torque= 0.3 //Starter torque factor
turbocharged= 0 //Is it turbocharged? 0=FALSE, 1=TRUE
max_design_mp= 0 //Max design manifold pressure, (inHg)
min_design_mp= 0 //Min design manifold pressure, (inHg)
critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet)
emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power
emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost
emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost
fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE
auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE
max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency
idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency
max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction
idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction
[propeller]
rotation= -1,-1,-1,-1 //both CCW
thrust_scalar = 1.0 //Propeller thrust scalar
propeller_type= 1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.56 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 4.94 //Propeller moment of inertia
beta_max= 0 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 0 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 0 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //Propeller gear reduction ratio
fixed_pitch_beta= 25 //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
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)
[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=0.9
aileron_effectiveness=1.000
rudder_effectiveness=1.000
[weight_and_balance]
station_load.0=3500,0,0,0
reference_datum_position = 0.0000, 0.0000, 0.0000 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-6.000000,0.000000,0.000000
empty_weight=5000.000000
empty_weight_roll_MOI=174852.000000
empty_weight_pitch_MOI=160676.000000
empty_weight_yaw_MOI=227355.000000
empty_weight_coupled_MOI=0.000000
max_gross_weight=10000.000000
[contact_points]
point.0=1,-20.784000,0.000000,-1.381000,6153.305130,0,0.625997,48.540000,0.305390,2.500000,0.726310,0,0,0,0,0
point.1=1,10.873000,-9.680000,-7.959000,6153.305130,1,0.625997,0.000000,0.407181,2.500000,0.726510,0,0,2,0,0
point.2=1,10.873000,9.680000,-7.959000,6153.305130,2,0.625997,0.000000,0.407181,2.500000,0.726510,0,0,3,0,0
point.3=2,2.083333,-27.083333,2.083333,2475.912819,0,0.000000,0.000000,0.000000,0.000000,0.000000,0,0,5,0,0
point.4=2,2.083333,27.083333,2.083333,2475.912819,0,0.000000,0.000000,0.000000,0.000000,0.000000,0,0,6,0,0
point.5=2,-25.750000,0.000000,-1.333333,2475.912819,0,0.000000,0.000000,0.000000,0.000000,0.000000,0,0,9,0,0
point.6=2,11.250000,0.000000,0.000000,2475.912819,0,0.000000,0.000000,0.000000,0.000000,0.000000,0,0,4,0,0
static_pitch=11.752000
static_cg_height=4.60000
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//6=taxi light, 7=recognition light, 8=wing light, 9=logo light
// Z, X, Y
light.0=3, 6.10, 32.91, 4.99, fx_navgre ,
light.1=3, 6.10, -32.91, 4.99, fx_navred ,
light.2=3, -21.10, 0.00, 0.36, fx_navwhi ,
[Views]
eyepoint= 3.0, -0.99, 1.70 //(feet) longitudinal, lateral, vertical distance from reference datum
[General]
performance=Wing Span: 29.4 m (96.46 ft.)\nWing Area: 99 m sq (1066 ft. sq)\nLength: 22.1 m (72.5 ft.)\nHeight: 5.574 m (18 ft. 3 in.)\nWeight Empty: 6754 kg (14859 lbs.)\nWeight Loaded: 11100 kg (24420 lbs.)\nEngines: 3 645 hp Hispano Suiza 9v\nMax Speed: 315 km\/h (195.6 mph)\nCruise Speed: 280 km\/h (173.8 mph)\nCeiling: 5000 m (16404 ft.)\nCrew: 4\nPassengers: 22-24\nRange w\/max fuel: 2000 km (1243 mi)\nRange w\/max Payload: 850 km (528 Mi)\n
[fuel]
LeftMain=0.000000,0.000000,0.000000,100.000000,0.000000
RightMain=0.000000,0.000000,0.000000,100.000000,0.000000
fuel_type=1.000000
number_of_tank_selectors=1
electric_pump=0
[airplane_geometry]
wing_area=600.000000
wing_span=64.6
wing_root_chord=12
wing_dihedral=2.999268
wing_incidence=0.000000
wing_twist=-0.999756
oswald_efficiency_factor=0.65
wing_winglets_flag=0
wing_sweep=5.000000
wing_pos_apex_lon=-1.000000
wing_pos_apex_vert=0.000000
htail_area=100.000000
htail_span=16.000000
htail_pos_lon=-27
htail_pos_vert=0.000000
htail_incidence=0.000000
htail_sweep=3.000000
vtail_area=50.000000
vtail_span=8
vtail_sweep=20.000000
vtail_pos_lon=-27.416667
vtail_pos_vert=0
elevator_area=100
aileron_area=100
rudder_area=70.000000
elevator_up_limit=27.501974
elevator_down_limit=20.626481
aileron_up_limit=19.480565
aileron_down_limit=15.000035
rudder_limit=23.995472
elevator_trim_limit=17.761692
spoiler_limit=0.000000
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000
[brakes]
toe_brakes_scale=0.4
parking_brake=1
[gear_warning_system]
gear_warning_available=0
pct_throttle_limit=0.000000
flap_limit_power=0.000000
flap_limit_idle=0.000000
[Flaps.0]
type=1
span-outboard=0.500000
extending-time=5.000000
system_type=0
flaps-position.0=0.000000,0.000000
flaps-position.1=11.250026,0.000000
flaps-position.2=22.500053,0.000000
flaps-position.3=33.750079,0.000000
flaps-position.4=45.000105,0.000000
[GeneralEngineData]
engine_type=0
Engine.0=1.000000,-13.500000,-1.500000
Engine.1=2.000000,-6.500000,-2.500000
Engine.2=2.000000,6.500000,-2.500000
Engine.3=1.000000,13.500000,-1.500000
fuel_flow_scalar=1.000000
min_throttle_limit=0.000000
[Reference Speeds]
flaps_up_stall_speed=70.000000
full_flaps_stall_speed=56.000000
cruise_speed=133.035714
max_indicated_speed=180.000000
[keyboard_response]
elevator=200.000000,1000.000000
aileron=200.000000,1000.000000
rudder=200.000000,1000.000000
[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=0
autothrottle_available=1
autothrottle_arming_required=0
autothrottle_takeoff_ga=0
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.000000
[hydraulic_system]
normal_pressure=0.000000
[stall_warning]
type=-0
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[direction_indicators]
direction_indicator.0=1,0
Note that you can also add effect as you like .......