Couple of questions regarding UAL SOP (standard operating procedures)
Accel. Height in the USA (unless special engine out requirement): 800'AGL thrust reduction flaps 5
What accel. Height is used in the USA at lets say KSFO RWYs 28L/R? (not sure if this has a special engine out accel height?)
ORD: 4000' and 5000' MNM alt. Requirements at 5Nm and 8nm DME. So accel. Height is increased to 5000' but then thrust reduction can no longer be at flaps 5 or can it? (5 minute takeof power limit) so what is it 1500'?
Intenational stations accel. 3000' thrust red. 1500' on ICAO noise abatement departures. What is used however when there is no noise abatement procedure in place? 800' accel. Flaps 5 thrust reduction? (like in the U.S.)
What is the cost index range used at the moment?
Would be much appreciated!