T_TO [kN]	Max. Rated Takeoff Thrust
P [kW]	Equivalent Power (of a turboprop engine)
l_CABIN [m]	Cabin Length
h_CABIN [m]	Cabin Height
d_F,I [m]	Cabin Width
V_CABIN [m³]	Passenger Compartment Volume
h_F [m]	Fuselage Height
w_F [m]	Fuselage Width
l_A/C [m]	Aircraft Length
b_W [m]	Wingspan
h_A/C [m]	Aircraft Height
l_T [m]	Track (distance between the centerline of the wheels)
l_WB [m]	Wheelbase (horizontal distance between the centers of the front and rear wheels)
S_W [m²]	Wing Area
λ_W	Wing Taper Ratio
φ_25,W [°]	¼ Chord Sweep Wing
S_V [m²]	Vertical Tail Reference Area
b_V [m]	Vertical Tail Height
λ_V	Vertical Tail Taper Ratio
φ_25,V [°]	¼ Chord Sweep Vertical Tail
S_H [m²]	Horizontal Tail Reference Area
b_H [m]	Horizontal Tailspan
λ_H	Vertical Tail Taper Ratio
φ_25,H [°]	¼ Chord Sweep Horizontal Tail
V_MO [kt]	Maximum Cruise Speed
M_MO [Mach]	Maximum Cruise Mach
M_CR [Mach]	Cruise Speed
h_MCR [FL]	Maximum Certified Flight Level
h_CR [FL]	Cruise Altitude
R_MPL [nm]	Range Maximum Payload
R_M,pax [nm]	Range with Maximum Passengers
R_PLMR [nm]	Maximum Range
m_MR [kg]	Maximum Ramp Mass
m_MTO [kg]	Maximum Take-Off Mass
m_ML [kg]	Maximum Landing Mass
m_MZF [kg]	Maximum Zero Fuel Mass
m_OE [kg]	Operating Empty Mass
m_MPL [kg]	Maximum Payload
m_PLMR [kg]	Payload at Maximum Range
V_CARGO [m³]	Cargo Compartment Volume
n_M,SEAT	Maximum Certified Seats
n_SEAT	Number of Seats in Standard Configuration