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CS 23.2125 Climb information

Normal-Category Aeroplanes (CS-23) · CS-23 · EAR revision 13 May 2026

IRImplementing rule

CS 23.2125Climb information

(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.

IR · CS 23.2125 — CS-23 · ED Decision 2017/013/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

AMCAcceptable means of compliance

AMC1 23.2125Climb information

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ASTM F44 F3264 Standard Specification for Normal Category Aeroplanes Certification

5.6 Climb Information F3179/F3179M-22e1 Standard Specification for Performance of Aircraft [AMC & GM to CS-23: Issue 4] [AMC & GM to CS-23: Issue 5]

AMC · AMC1 23.2125 — CS-23 · ED Decision 2026/003/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

AMCAcceptable means of compliance

AMC2 23.2125Climb information

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CS-23 Amdt 4

23.66 Takeoff climb: one engine inoperative

23.67 Climb: One engine inoperative

23.69 En route climb/descent

23.71 Glide: single engine airplanes

AMC · AMC2 23.2125 — CS-23 · ED Decision 2017/025/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

AMCAcceptable means of compliance

AMC3 23.2125Climb information

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None

AMC · AMC3 23.2125 — CS-23 · ED Decision 2017/025/R · CS-23 Easy Access Rules · EAR revision 13 May 2026

All rules in SUBPART B — FLIGHT

Consolidated from the EASA Easy Access Rules (revision 13 May 2026, extracted 17 Aug 2026) for convenience. Not the official publication — verify against the Official Journal of the European Union and the EASA publications before operational use.

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