It is intresting I was wondering why I purchased CS- 737ADV. I just checked Cfg, file and found CS over powered these engines. Now I can fly to the moon.
I wonder how CS selected static power settings as 25,000Lbs.
[TurbineEngineData]
fuel_flow_gain = 0.002 //Gain on fuel flow
inlet_area = 19.6 //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920 //RPM, second stage compressor rated value
static_thrust = 25000
afterburner_available = 0 //Afterburner available?
reverser_available = 1 //Thrust reverser available?
ThrustSpecificFuelConsumption = 0.385 //Thrust specific fuel consumption (Jets)
AfterBurnThrustSpecificFuelConsumption = 0 //TSFC with afterburn/reheat engaged
Update:
I just made a test flight with 737-200ADV at your AP. with GW 106,000lbs. Used RW close to 3000Ft.
I told you with this power I can go to the Moon.
http://img692.imageshack.us/img692/9951/khyrl.jpg