Everything is possible...but:
Originally Posted by FCTM AO20 says
This section provides recommendations on thrust levers management in case of inoperative reverser(s). These recommendations are applicable in case of in-flight failure (including engine failure) and/or in case of MEL dispatch with reverser(s) deactivated.
So I copy-pasted the MEL extract because it was easier for me AND because in that particular case the in-flight failure procedure described in the FCTM was identical to the MEL operational proc (as mentioned above).