The AL-41F1 are in the same category with the latest F110-GE-132. Those engines are NOT 5th generation material and that's the bottom line and the most important stuff to remember. We both acknowledged this much.
Thrust wise (remember thrust is just a part of an engine performance) the PAK-FA will only lag behind the F-22 with those engines because both use two. So to give you an example of thrust in military aircraft you have something like:
1. F-22 Raptor: 2 x
Pratt & Whitney F119 engines = 35,000 x 2 = 70,000lbs of thrust total
2. Pak-FA + SU-35S: 2 x
AL-41F1 engines = 33,000 x 2 = 66,000 lbs of thrust total
3. Su-27, Su-30, Su-34:
2 x AL-31F M1 engines = 60,400 lbs thrust total
4. F-15E: 2 x
F110-GE-229 = 30,000 x 2 = 60,000 lbs of thrust total
Now bellow this top four the picture changes dramatically.
You have the:
-Eurofighter typhoon with 2 x
Rolls Royce EJ200 which each provides max 20,000 lbs of thrust = 40,000lbs total
-The F-18 with 2 x
GE F404 engines which each provides max 18,000 lbs of thrust = 36,000lbs total
-The new F-16E/F which sports the new
F110-GE-132 engine which provides 32,500 lbs of thrust total
-The Swedish Gripen with 1 x
GE F414G engine which provides 22,000 lbs of thrust total
And then you have the daddy of the engines, the
F135-GE engine which power the F-35 and provides a whooping 44,000 lbs of thrust. So if the F-35 had two of those it would sport something short of 90,000lbs of thrust putting it in its own category completely.
Now, the 44,000lbs of thrust that the F135 provide are indeed not a lot for the specific airplane and thats why all the negative comments of being slow. But then, 44,000 lbs of thrust are double of what Gripen has, more than the twin engine F-18 and Typhoon and more than the new F16F/E new F110 model engine.
Now what did i achieve with all these numbers? Certainly not proving that an aircraft is better than the other. You can't really draw any conclusions by looking JUST at the thrust, not even for the aircraft's speed. Speed is a function of engine performance, weight and how air-dynamic is the shape of the aircraft (drag). You can't even draw a conclusion not even for the engine itself by just looking the thrust it generates. You need to look other stuff like reliability, fuel efficiency, hours of life etc.
The numbers are there just to understand a tiny part of the philosophy of manufacturing each engine and aircraft model.