United Airlines 2012 Annual Report Download - page 413
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Attachment A2
6-1162-RCN-1937
GEnx-1B*** Engines
Page 11
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.
Descent:
The Aircraft descends from the final cruise altitude at *** KCAS to an altitude of *** feet above the destination
airport altitude.
Throughout the descent, the cabin pressure will be controlled to a maximum rate of descent equivalent to *** feet
per minute ***.
The temperature is standard day during descent.
Approach and
Landing Maneuver:
The Aircraft decelerates to the final approach speed while extending landing gear and flaps, then descends and
lands.
The destination airport altitude is *** feet.
Fixed Allowances:
For the purpose of this guarantee and for the purpose of establishing compliance with this guarantee, the following
shall be used as fixed quantities and allowances:
Taxi-Out:
Fuel
*** Pounds
Takeoff and Climbout Maneuver:
Fuel
*** Pounds
Distance
*** Nautical Miles
Approach and Landing Maneuver:
Fuel
*** Pounds
P.A. No. 2484
AERO-B-BBA4-M12-0854 SS12-0424