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Emirates 521

Printed page 84. PDF page 98.

height of 35 ft in two seconds at a vertical speed of 512 ft per minute, even though the engine thrust levers and EPR remained at idle. The Operator's Go-around and Missed Approach Procedure required both pilots to verify rotation
Open official document at PDF page 98Runway Impact during Attempted Go-Around: Emirates Boeing 777-31H A6-EMW

Emirates 521

Printed page 88. PDF page 102.

when the landing gear was selected to `up' had the TO/GA switch been pushed and/or the engine thrust levers been manually advanced to achieve go-around thrust. Analysis of the EEC data by the engine manufacturer indicated that the EEC was
Open official document at PDF page 102Runway Impact during Attempted Go-Around: Emirates Boeing 777-31H A6-EMW

Emirates 521

Printed page 99. PDF page 113.

the go-around procedural steps thoroughly as the Aircraft was gaining height while the engine thrust levers remained at idle. Their actions could have been conditioned by the training sessions where they had executed the normal go-around procedures when the A/T
Open official document at PDF page 113Runway Impact during Attempted Go-Around: Emirates Boeing 777-31H A6-EMW

Emirates 521

Printed page 123. PDF page 137.

alerting system was not designed to give a configuration warning for a go-around with the engine thrust levers not advancing towards the TO/GA thrust position. (p) The B777 provides an alert to the flight crew and a EICAS amber caution
Open official document at PDF page 137Runway Impact during Attempted Go-Around: Emirates Boeing 777-31H A6-EMW

Emirates 521

Printed page 134. PDF page 148.

During the attempted go-around, except for the last three seconds prior to impact, both engine thrust levers, and therefore engine thrust, remained at idle. Consequently, the Aircraft's energy state was insufficient to sustain flight. (b) The flight crew did not
Open official document at PDF page 148Runway Impact during Attempted Go-Around: Emirates Boeing 777-31H A6-EMW

Emirates 521

Printed page ix. PDF page 9.

did not observe that both thrust levers had remained at the idle position and that the engine thrust remained at idle. The Aircraft quickly sank towards the runway as the airspeed was insufficient to support the climb. As the Aircraft
Open official document at PDF page 9Runway Impact during Attempted Go-Around: Emirates Boeing 777-31H A6-EMW