Originally Posted by
suninmyeyes
Calapine
On a modern Boeing pressing the TOGA switch will result in a pitch up to approximately 15 degrees and thrust being applied which will give a climb rate of 2000 feet per minute. A second press of the TOGA switches will give a full power climb.
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Can you give me a formal reference for that statement? I have always believed your statement to be exactly correct, but I cannot find any reference to the dual TOGA go around double push difference. I fly the 752, 753, 764, 763, and I cannot find any reference to the first push, second push difference. Thanks!