Questions regarding AS 365 N2

[nickel]

Hi,

I have a few questions about AS 365 N2. It seems like it is not possible to find a flight manual for this helicopter and configuration information is relatively sparse (except for basic things, they are plentiful!) in Internet.

I appreciate the help if anybody knows following:
- What is the nominal engine, main and tail rotor RPM's
- What are the main and rail rotor twist?
- In tech specs it is listed that the Vne for this helicopter is 303 km/h. What I would like to know is, what happens in AS 365 N2 after Vne? Stall? Excessive vibration? Is the helicopter able to exceed Vne in level flight?

Thanks in Advance

[Epiphany]

- What is the nominal engine, main and tail rotor RPM's?

Well....off the top of my head.....

Ng - 51800 rpm (@100%)
Nf - 41586 rpm
MR - 350 rpm
TR - 4706 rpm

- What are the main and rail rotor twist?

MR blade twist is 6 deg (0 deg at tip to 6 deg at root)
Fenestron blade twist 7.2 deg (2.2 at tip to 9.4 at root)

Main Rotor -
- In tech specs it is listed that the Vne for this helicopter is 303 km/h. What I would like to know is, what happens in AS 365 N2 after Vne? Stall? Excessive vibration? Is the helicopter able to exceed Vne in level flight?

Gawd knows - retreating blade stall I would imagine but I have never wanted to find out and I doubt if you would reach VNE in anything other than a dive.

[nickel]

Thanks for the answers!

Do you also know the collective and cylic ranges of the main rotor and collective range of the tail rotor?