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Yeap, as i remembered.
Now according to time table.
Engine will be 1000SHP...but since this table has been posted in the past 4 Ton Helicopter apparently revised to be 5 Tons.
And according to the PDF you supplied.
"1000-1500hp sınıfı turboşaft motorlarda düşük yakıt tüketimi için yüksek basınç oranı ve yüksek verimli kompresörler gereklidir"
And also according to Ismail Demir Head of SSM there is a national engine development project for T-129. (as you posted.)
So, i'm taking it as it would be more than 1000 SHP... and it can probably power T-129
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