CS-25 V2min definition.
From CS-25:
(b) V2MIN, in terms of calibrated airspeed, may not be less than –
(1) 1·13 VSR for –
(i) Two-engined and three-engined turbo-propeller powered aeroplanes; and
(ii) Turbojet powered aeroplanes without provisions for obtaining a significant reduction in the one-engine inoperative power-on stall speed;
(2) 1·08 VSR for –
(i) Turbo-propeller powered aeroplanes with more than three engines; and
(ii) Turbojet powered aeroplanes with provisions for obtaining a significant reduction in the one-engine-inoperative power-on stall speed.
Does anyone have an example of a turbojet powered aeroplane with provisions for obtaining a significant reduction in the one-engine-inoperative power-on stall speed?
If so, how does it do it?