PPRuNe Forums - View Single Post - If dual eng. failure ditching had been a B737NG..what procedures would you consider?
Old 21st Jan 2009, 02:10
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Intruder
 
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Until Boeing changes their manual a clean wing is your best L/D for gliding.

Leading edge devices have a huge reduction in stall speed. The first notch of flaps is typically about 50% of the total stall reduction you get from flap extension.
On what airplane?

On the 747 there is a 20 KT reduction in stall speed (or maneuvering speed, however that may technically be defined) for each of the first 3 "notches" of flap -- 1, 5, and 10. There is another 20 KT for the last 2 increments (through 25 to 30). While the 747 Classic and 747-400 have completely different wings and LE/TE flap extension profiles (e.g., the Classic has some TE extension at Flaps 1; the 744 does not), the speed reduction increments are retained.
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