Discontinued Approach case
...continued
Accompanying conditions being:
1) Critical engine out, remainder at Max Contingency Power,
2) Either the final approach configuration for all engines operating or in the configuration that can be achieved within 1200m HORIZONTALLY from the start of the procedure for a Discontinued Approach,with engine failure late in the aproach;
3)A speed not less than 1.2Vms, or for four-engined aircraft where the application of power results in a significant reduction in Vs,1.15Vms,where this latter value is appropriate to the configuration as specified for the aircraft type for a one engine out Discontinued Approach procedure.The speed must also be NOT LESS than Vmcl for the configuration.The speed should also be NOT GREATER than the recommended Decision Height Speed.
Last edited by Trackdiamond; 25th Dec 2013 at 05:08.