PPRuNe Forums - View Single Post - Flap retraction after Single eng go around

25th Feb 2009, 06:29

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parkfell

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So we are dealing with a single engine go-around, as oppose to a loss of power etc on take-off where the emergency turn procedure is used

Mr Boeing says retract the flap normally 1000ft above airfield elevation for a B.737

Additional information : FCOM PD 32.6 for % climb gradient SE

Last edited by parkfell; 25th Feb 2009 at 11:08. Reason: Additional info:

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