Yes you are right, the only point here is maintenance ease and as you said a great turn around time. The vane system is a fixed unit easily cleaned once designed for an easy turn around compared to the tail rotor design complexity. That is the only reason the notar system is far better for the naval and airforce choppers. Design for the entire notar system is perfected already. I don't think we shouldn't make notar versions for all the HAL helicopters and make an entire range of notar helicopters.
Woah! - I never said 'great' turn around time - the F22 probably has the worst TAT of any 4+ gen aircraft in service today!
Okay, let me explain.
Airflow in tubes is very different from that in a 3 dimensional space which is open. The major challenge is 'predictability' of the flow.
Inside the tube - the fluid flow will be like a 'vortex' with a constant speed in the centre of the tube due to the continuous flow of the air. As it reaches the 'vanes' - there the flow will 'break' into turbulent flow which will be based on the flow of the air outside the tube - which will in this case be in 3 dimensions (the rotor downwash - predictable to a certain degree, the 'backward flow' - helicopter moving forward and the residual flow due to the Coanda effect on a curved surface. So, now your vanes will have to move in a direction perpendicular to the axial flow of the air to counteract the main rotor torque. This will create a turbulent layer which will induce parasitic drag - reducing efficiency.
Add to this the need for ensuring that the 'pipe' remains free from any debris inside (as it will disturb the flow adding more unpredictability).
Often you will hear the word 'trade-off' being used. The trade off for a 'slightly more' silent helicopter is higher maintenance, unpredictable or complex flow, requiring more complex surfaces.
A major part of the 'noise' of a helicopter is the blade slap when the succeeding blade enters the vortex created by the preceding blade. The tail rotor creates a higher frequency noise (at it rotates at a slightly higher RPM). One way of reducing the noise from a tail rotor is to house it in a duct (called a fenestron) with higher blade count where the tip vortexes are absorbed into the fenestron reducing the 'b;ade slap' and frequency attenuation that automatically happens due to the higher blade count. The other is using a 'non cruciform' tail blade design like that seen on the Apache.
Hope this helps.