See if this is what you need:
;===================== FLAPS =====================
[FLAPS.0]
type = 1 ; Flap type 0 = None, 1 = trailing edge, 2 = leading edge
system_type = 0 ; Flap system type 0 = electrical, 1 = hydraulic, 2 = pneumatic, 3 = manual, 4 = none
span-outboard = 0.6 ; Outboard span area (added area) (percentage, non dimensional)
extending-time = 3 ; Flap extension time (SECONDS)
damaging-speed = 120 ; Speed above which flap is damaged (Kts)
blowout-speed = 170 ; Speed above which flap is blown out (Kts)
maneuvering_flaps = 0
lift_scalar = 1.3 ; Scalar coefficient to ponderate global flap lift coef (non dimensioned)
drag_scalar = 1.3 ; Scalar coefficient to ponderate global flap drag coef (non dimensioned)
pitch_scalar = 1 ; Scalar coefficient to ponderate global flap pitch coef (non dimensioned)
max_on_ground_position = 2 ; Dynamically set in-tool to last flap-position index by defaut when -1 is found.
flaps-position.0 = 0, -1, 0
flaps-position.1 = 20, -1, 0.25
flaps-position.2 = 42, -1, 1