United Airlines 2012 Annual Report Download - page 389
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Attachment A1
No. 6-1162-RCN-1937
GEnx-1B*** Engines
Page 10
Maximum takeoff thrust is used for the takeoff.
The takeoff gross weight shall conform to FAA Regulations.
Climbout
Maneuver:
Following the takeoff to *** feet, the Aircraft accelerates to *** KCAS while climbing to ***feet above the departure
airport altitude and retracting flaps and landing gear.
Climb: The Aircraft climbs from *** feet above the departure airport altitude to *** feet altitude at *** KCAS.
The Aircraft then accelerates at a rate of climb of *** feet per minute to the recommended climb speed for minimum
block fuel.
The climb continues at the recommended climb speed for minimum block fuel until *** Mach number is reached.
The climb continues at *** Mach number to the initial cruise altitude.
The temperature is standard day during climb.
Maximum climb thrust is used during climb.
Cruise: The Aircraft cruises at ***Mach number.
The initial cruise altitude is *** feet.
A step climb or multiple step climbs of *** feet altitude may be used when beneficial to minimize fuel burn.
The temperature is standard day during cruise.
The cruise thrust is not to exceed maximum cruise thrust except during a step climb when maximum climb thrust may
be used.
P.A. No. 2484
AERO-B-BBA4-M12-0853 SS12-0424