MastanKhan
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Although I had no intention of bringing in LCA as a comparison platform, I will still answer your post. The basic flaw in your reasoning is the assumtion that the LCA mk2 structure has to change just becaue of a different engine. The airforce outlined the new requirement with additional external stores from 4000 to 5000, along wit additional length with a stretched nosecone. If LCA was a aluminium body fighter tooling would have been easy, but due to extensive kevlar and CFRP composite, the entire molds need to be retooled and re tested.
Apart from that this is our first self designed aircraft hence teething problems are inevitable, a far as other "joint production" lines are concerned, they have worked satisfactorily since 1978, right?
Sir,
I am hardly ever disrespectful----but please allow me to say---it is out of sheer stupidity the Lca is where it is---. Just because it is the first aircraft---does not mean that the things need to be changed every time an air marshall of the indian air force takes a sneeze.
The world's engineering technology and development for futuristic systems will be doomed if it moved with the speed at which Lca has moved---and please no fighting over these comments. Thank you.