Navigate / EASA
AMC1 29.1310 Power source capacity and distribution

ED Decision 2023/001/R

In determining compliance with sub-paragraphs (b) and (c) of CS 29.1310, the power loads may be assumed to be reduced under a monitoring procedure consistent with safety in the kinds of operations authorised. Loads not required for controlled flight need not be considered for the two-engine inoperative condition on rotorcraft with three or more engines.

[Amdt No: 29/11]