Originally Posted by ice2x01
3- Maximum landing climb limited weight is based on: -
A- L/G down, landing flaps and One engine inoperative.
B- L/G down, landing flaps and all engines operating.
C- L/G up, landing flaps and all engines operating.
--Can someone provide a reference for this?
The reference is FAR 25.119. The 'trap' built into this question is that there is also a "Maximum Approach Climb limited Weight" (ref. FAR 25.121(d)), which is one-engine-inoperative. Most AFM's show only a "Maximum Landing Weight limited by Climb Requirements", which is the more limiting of the two.
FlightPathOBN;
I don't agree with this statement in your reference:
Transport Category aircraft have two sets of weight limitations. "Certificate Limitations" such as Maximum Takeoff or Landing weight, and "Performance Limitations" such as Maximum Takeoff Weight permitted by climb requirements, or Runway Limited Takeoff Weight.
These performance limitations are part of the "Certificate Limitations". These apply irrespective of the type of operation, on the basis of the Certificate of Airworthiness (ref. FAR 25.1501 and 25.1533). There are additional performance limitations due to Operating Regulations such as FAR Part 121.
Regards,
HN39