§27.67 Climb: one engine inoperative.

For multiengine helicopters, the steady rate of climb (or descent), at VY (or at the speed for minimum rate of descent), must be determined with-- (a) Maximum weight; (b) [The critical engine inoperative and the remaining engines at either-- (1) Maximum continuous power and, for helicopters for which certification for the use of 30-minute OEI power is requested, at 30-minute OEI power; or (2) Continuous OEI power for helicopters for which certification for the use of continuous OEI power is requested.]