United Airlines 2012 Annual Report Download - page 412
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Attachment A2
6-1162-RCN-1937
GEnx-1B*** Engines
Page 10
The following obstacle definition is based on a straight out departure where obstacle height and distance are
specified with reference to the liftoff end of the runway:
Distance Height
1.
*** feet
*** feet
2.
*** feet
*** feet
3.
*** feet
*** feet
4.
*** feet
*** feet
5.
*** feet
*** feet
6.
*** feet
*** feet
7.
*** feet
*** feet
8.
*** feet
*** feet
9.
*** feet
*** feet
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.
P.A. No. 2484
AERO-B-BBA4-M12-0854 SS12-0424