Every engine having a different value is perfect, I want something that we can put in on an per engine basis.
So if you fly an early version of the f16, you have to be aware of the engine limitation, but if you fly a later version you don't
So to speak yes, The F-16A/B model had PW-100 engines in them. While the F-16C/D block 25 had improved PW-100 enigines
While the F1-6C/D block 32 converted over to the GE F110 engine and redesigned larger inlet.
A few quick specs
PW F100Compressor: Dual Spool Axial compressor with 3 fan and 10 compressor stages
Bypass ratio: 0.36:1
Combustors: annular
Turbine: 2 low-pressure and 2 high-pressure stages
PerformanceMaximum thrust: 79 kilonewtons (17,800 lbf) military thrust, 129.7 kilonewtons (29,160 lbf) with afterburner
Overall pressure ratio: 32:1
Turbine inlet temperature: 1,350 °C (2,460 °F)[6]
Specific fuel consumption: Military thrust: 77.5 kg/(kN·h) (0.76 lb/(lbf·h)) Full afterburner: 197.8 kg/(kN·h) (1.94 lb/(lbf·h))
Thrust-to-weight ratio: 7.8:1
GE F110Compressor: 2 spool: 3 fan and 9 high pressure compressor stages
Combustors: annular
Turbine: 2 low-pressure and 1 high-pressure stages
PerformanceMaximum thrust: F110-GE-129: 29,500 pounds; F110-GE-132: 32,000 pounds
Overall pressure ratio: 29.9:1 - 30.4:1
Turbine inlet temperature: 2750F (1510C)[4]
Thrust-to-weight ratio: F110-GE-129: 7.29; F110-GE-132: 7.90