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§23.2125 Climb information

CS-23 · Subpart B — Flight · at CS23-6 (current)

Text in force at CS23-6: from CS23-5, effective 15 Aug 2017.

(a) The applicant must determine, as applicable, climb and/or descent performance: (1) for all engines operating; (2) following a critical loss of thrust on take-off; and (3) after a critical loss of thrust, during the en route phase of flight.

ED Decision 2017/013/R · Source

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