737 – S/E, when is additional go-around thrust required ?
In the 737 QRH, One Engine Inop Landing, Descent Checklist the following statement appears:
“If additional go-around thrust is desired, below 10,000 feet configure the pressurisation system for a no engine bleed landing:” It then goes on to configure the pneumatics panel accordingly.
My question is, how are we supposed to know when this is required? In the all engines case we have go-around climb gradient/weight tables, are these also valid for engine out?
S & L