G limits without Anti G system active
Does anyone know of any guidance material for what are the max and min G limits that can be performed by a pilot with an aircrafts anti G system disabled.
The aircraft is limited to +7 and -3.5 G, but the anti G system will not be operational, however testing of the G indicator is required for verification.
I realise this is quite a subjective question but Im interested if there are any recommendations available for this.