ENGINE FAILURE AT or ABOVE [V.sub.1]--ACTIONS and CALLOUTS Callouts: in "BOLD TEXT"--Actions: with bullets (*) in plain text Engine Failure PF PM ** Pilot first noting Engine Failure "ENGINE FAILURE' "SET MAX POWER" * Advance thrust levers to maximum takeoff thrust
"POWER SET" [V.sub.R] "ROTATE" * Rotate towards 10[degrees] pitch attitude Positive rate "POSITIVE RATE" of climb * Verify positive rate of climb "GEAR UP" * Position gear lever UP After lift-off * Maintain F/D * Monitor speed and commanded attitude attitude "ADVISE ATC," when appropriate * Advise ATC ** Comply with airport specific "Engine Failure After Takeoff' procedure (if published); otherwise, fly runway heading "HEADING SELECT" * Select HDG SEL * Verify HDG SEL annunciates * Position A/T arm switch OFF
The aircraft with higher bypass ratio engine needs more engine takeoff thrust
to meet the takeoff filed length and engine-out climb gradient requirements, which leads to increment in the aircraft weight and a higher DOC.
Through technology enhancements that provide greater performance, efficiency and lower environmental impact, the PW307D delivers increased takeoff thrust
and improved fuel consumption compared to the PW307A engine.
In addition to fuel savings, the airline sees benefits from reduced engine takeoff thrust
, reduced emissions, greater payload and range capability, and greater operational flexibility.
The PW4000 Series is a family of large-scale commercial aircraft engines with a takeoff thrust
ranging from 52,000 to 98,000 pounds (lbs).
I then called for takeoff thrust
, and away we went.
The engine was designed to deliver 115,000 lb of takeoff thrust
to power Boeing's longer-range 777-330ER and--200LR aircraft.
In 1995, UT's aerospace and aviation research efforts paid off in the delivery of the Boeing 777, which uses P&W's 4084 jet engine - at 84,600 pounds of takeoff thrust
, the most powerful ever in commercial aviation.
The two engines produce 172,000 pounds of takeoff thrust
, equivalent to what the four engines of a 747 produced when it began service in 1970.
GE90 will be rated from 75,000 to 95,000 pounds takeoff thrust
. It is scheduled for certification at 87,400 pounds thrust in 1994 and entry into service at between 70,000 and 75,000 pounds on the new Boeing 777 in mid-1995.
Finally, the optimized value of the engine takeoff thrust
has also resulted in reduced fuel consumption.