Approach climb and landing climb config

[Driver170 42]

This is incorrect. Per CS-25.123, there is an enroute EO climb requirement. CS-25.123 says

 

I wouldn't say my paragraph is incorrect.

 

For EASA only requirement for landing is -

 

The limits are:

 

Max structural landing weight

Landing distance limit weight

Approach/climb limit weight. (Approach weight is most limiting on twin engine and the weight you will see in the table is approach weight.)

In EASA,all required at dispatch phase.

 

 

AMC2 CAT.POL.A.225 Landing – destination and alternate aerodromes

MISSED APPROACH

 

(a) For instrument approaches with a missed approach climb gradient greater than 2.5 %, the operator should verify that the expected landing mass of the aeroplane allows for a missed approach with a climb gradient equal to or greater than the applicable missed approach gradient in the OEI missed approach con guration and at the associated speed.

 

(b) For instrument approaches with DH below 200 ft, the operator should verify that the expected landing mass of the aeroplane allows a missed approach gradient of climb, with the critical engine failed and with the speed and con guration used for a missed approach of at least 2.5 %, or the published gradient, whichever is greater.