One of the more important warplanes of our time, and perhaps the most important of the "Eastern bloc"; Indian Su-30MKIs reputedly kicked USAF F-15s all over the sky (tho the fairness of the exercise is disputed). Definitly something that should be quickly moved up to GA status methinx... - Aerobird Target locked - Fox One! 00:47, 22 January 2007 (UTC)[reply]

There's still a lot of work to be done here, obviously. In no particular order:

  • The lack of references and citations is a major problem.
  • Bulleted lists are overused, and should be converted into prose.
  • The issue with the subsidiary variant articles needs to be resolved. I wouldn't necessarily advocate merging them in, but they'll need a longer summary section here, at the least.
  • Is the "Su-30MK multi-role twin-seater" section supposed to be a sub-section of "Development"?
  • There doesn't seem to be any coverage of it's operational use (or, indeed, anything after the development phase).

Once the big problems get fixed, you can turn to copyediting and fiddling with the structure and coverage; but, at the moment, it's a bit premature to consider those. Kirill Lokshin 01:21, 22 January 2007 (UTC)[reply]

A very good start, but I agree with Kirill Lokshin that there remains further development to be done. Not to duplicate his comments, I would add the following observations:

Automated

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PocklingtonDan

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  • "The aircraft is comparable with USA's F/A-18E/F Super Hornet and F-15E Strike Eagle." I'm not happy with this sentence. Why is this necessary? Why contrast to a US fighter as opposed to a British, French, Israeli, Chinese or whatever one? You assume US readership. I would remove this sentence. You have already described its role, a US-specific comparison is unnccessary
  • As above, sorely lacking cites at present
  • As above, more info needed on training, operational use, etc
  • The "specifications" section should go in some kind of sidebar rather than being a section of the main article, in my opinion
  • "Differential ±15-degree deflection of the engines' axisymmetric nozzles (with turn axes positioned at 32-deg angle to each other) enables pitch/yaw thrust vectoring control" This is all Greek to me. If using concepts like this, you should link to wiki articles on them, introduce a diagram or explain them in-line, in my opinion

I think ideally you need to find smeone with understanding of and access to Russian sources, where you will hopefully find a wealth of information that you can use to expand the article - PocklingtonDan 09:15, 1 February 2007 (UTC)[reply]