Engine:

MILTHRUST   [LBS]
MAXTHRUST   [LBS]
tsfc        [-] not used
atsfc       [-] not used
idlen1      [%]
idlen2      [%] not used
maxn1       [%]
maxn2       [%] not used
betarangeend[%] 
    if ThrottleCmd < betarangeend/100.0 then engine power=idle, propeller pitch
    is controled by ThrottleCmd (between MINPITCH and  REVERSEPITCH).
    if ThrottleCmd > betarangeend/100.0 then engine power increases up to max reverse power
reversemaxpower [%]
    max engine power in reverse mode
augmented   [boolean] not used
augmethod   [boolean] not used
injected    [boolean] not used
maxpower    [HP]
idlefuelflow [pph] not used
fuelconsumption [pph/HP] for N1=100%
n1idle_max_delay [-] time constant for N1 change
maxstartenginetime [sec]
    after this time the automatic starting cycle is interrupted when the engine
    doesn't start (0=automatic starting not present)
startern1   [%]
    when starting starter spin up engine to this spin
ielumaxtorque [lb.ft]
    if torque>ielumaxtorque limiters decrease the throttle
    (ielu = Integrated Electronic Limiter Unit)
itt_delay [-] time constant for ITT change
    (ITT = Inter Turbine Temperature)

Tables:
ENG_POWER_RPM_N1
    engine power [HP] depending on prop_RPM and N1
IIT_N1
    ITT [deg C] depending on N1 and engine run (0=off / 1=running)

Thrust_Tables:
ENG_POWER_COEF_AIRPRESSURE_AIRSPEED
    engine power coeficient [-] depending on air pressure (altitude) and airspeed
other thrust tables are not used
