Here are the data sections, first is mine, second is the Extra;
Tango;
[propeller]
thrust_scalar = 0.6 //Propeller thrust scalar
propeller_type= 1 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 5.0 //Propeller Diameter, (feet)
propeller_blades= 2 //Number of propeller blades
propeller_moi= 3.78 //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= 30.75 //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)
Extra 300;
[propeller]
thrust_scalar = 1.0 //Propeller thrust scalar
propeller_type= 0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter= 6.2 //Propeller Diameter, (feet)
propeller_blades= 3 //Number of propeller blades
propeller_moi= 5.9 //Propeller moment of inertia
beta_max= 34 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min= 17 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm= 1400 //Miminum governed RPM
prop_tc= 0.1 //Prop time-constant
gear_reduction_ratio= 1.0 //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
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)
Tango Contact Points;
[contact_points]
static_pitch = 0.0
static_cg_height = 3.8
tailwheel_lock = 0
gear_system_type = 0
max_number_of_points = 9
point.0 = 1, 3.34, 0, -3.78, 2500, 0, 0.45, 36, 0.26, 1.500, 0.500, 0, 0, 0, 0, 0
point.1 = 1, -2.7, -3.27, -3.76, 3500, 1, 0.55, 0, 0.2, 2.5, 1.0, 0, 0, 2, 0, 0
point.2 = 1, -2.7, 3.27, -3.76, 3500, 2, 0.55, 0, 0.2, 2.5, 1.0, 0, 0, 2, 0, 0
point.3 = 2, -1.0461, -12.0937, 1.46, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0
point.4 = 2, -1.0901, 12.0822, 1.4314, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0
point.5 = 2, -15.4812, 0, -0.5438, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0
point.6 = 2, 3.2515, 0, -2.8, 2574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0
point.7 = 2, -14.6123, 0, 2.7439, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 7, 0, 0
point.8 = 2, -1.531, 0, -2.1838, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 8, 0, 0
Extra Contact Points;
[contact_points]
point.0=1, -16.50, 0.00, -1.5, 1377.95, 0, 0.4100, 180.0, 0.4, 2.5, 0.6, 0.0, 0.0, 0.0, 0.0, 0.0
point.1=1, -0.05, -2.92, -4.4, 1968.50, 1, 1.1660, 0.0, 0.6, 2.5, 0.6, 0.0, 0.0, 2.0, 0.0, 0.0
point.2=1, -0.05, 2.92, -4.4, 1968.50, 2, 1.1660, 0.0, 0.6, 2.5, 0.6, 0.0, 0.0, 3.0, 0.0, 0.0
point.3=2, -1.40, -12.45, 0.0, 787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2, -1.40, 12.45, 0.0, 787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2, -16.10, 0.00, 5.2, 787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2, 4.8, 0.00, 0.6, 787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0
static_pitch = 10.54
static_cg_height = 3.45
// Note above, the static pitch and cg height are in the 'after' section of the contact points on the Extra, and on the top in the Tango. I wonder if that might be it?
Engine location on the Tango;
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 3.5, 0.0, 0.5 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 0.29 //Fuel flow scalar
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser
Engine location on the Extra 300;
[GeneralEngineData]
engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 3.5, 0.0, 0.60 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar= 1.0 //Fuel flow scalar
min_throttle_limit = 0.0 //Minimum percent throttle. Generally negative for turbine reverser