One of the links you provide has this:
You see this is extensive changes to the engine.
Now try thinking what would happen to LCA Mk-1 if the same approach is taken with the LCA Mk-1A.
1) Reduce Landing gear weight
2) Reduce corresponding ballast
3) Now the structure does not need to support say 400 kg weight. Ergo demands will be raised for changing structures.
4) Now F-404 engine do not need to push as hard to maintain lift to drag ratio. Ergo changing the wing size.
5) Weight saved too much. Ergo demands will be raised to tweek the FBW.
6) Now that the weight decrease has been achieved, the FBW is fixed and the wing reduced. There is space now for making the whole thing more F-16sqe. So now lets increase fuel capacity by again changing the internal layout and may be inventing a conformal tank for it.
7) But weight fuel is lesser weight-to-volume and also sloshes around and the confromals change the aerodynamics, so now again tweek the FBW and put some ballast, back into new places.
8) But weight new fuel lines and new ballast. So now this would begin to require changing the arrangement of LRUs.
Ok I will stop at this most holiest of numbers. Number 8. Jai Shani Maharaj.
You see this thing if not properly controlled will lead India (as a country) to another dead end.
Then there would be emergency purchases required. Mmmm.... Sounds familiar
.
Now set up internet forums where people will tell us how the IAF leadership has just saved the nation from dire consequences of having just 15 squadrons in flying condition.
Then off course we will be told how some other country has offered security assistance and how our ass is being saved while we remain ever-ungrateful bunch of morons.
Come on, you have heard this often enough by now.
See till ~200 kg reduction that you needed for the AESA+EW it made sense. Then somebody got excited at the prospects and mentioned 400 kg. Then somebody else got even more excited and offered earth shaking ideas for 700 kg. Then the big daddy nobel-worthy idea is given to take it all to 1000 kg reduction. And some of us Indians are now not being patriotic enough to have this bestest of product flying.
Why not just have all this done on LCA Mk-2? Why scrap the LCA Mk-2? How is all this not achievable in LCA Mk-2?
Or
Is somebody who has just learnt flying by associating with the LCA Mk-2 just feeding crap into the LCA Mk-1 capability sets by using LCA Mk-1A as a deflection point.
I just hope this LCA Mk-1A is either produced fast or dropped fast.