United Airlines 2012 Annual Report Download - page 388

Attachment A1
No. 6-1162-RCN-1937
GEnx-1B*** Engines
Page 9
2.3.3 Mission Payload
The payload for a stage length of *** nautical miles in still air (equivalent to a distance of *** nautical miles with a *** knot headwind,
representative of a *** to *** route in ***) using the conditions and operating rules defined below, shall not be less than the following guarantee
value:
NOMINAL:
*** Pounds
TOLERANCE:
*** Pounds
GUARANTEE:
*** Pounds
Conditions and operating rules:
Stage Length: The stage length is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent.
Takeoff: The airport altitude is *** feet.
The airport temperature is ***°F.
The takeoff runway available (TORA) is ***feet.
The takeoff distance available (TODA) is ***feet.
The accelerate-stop distance available (ASDA) is *** feet.
The lineup allowance adjustment to TORA and TODA is *** feet.
The lineup allowance adjustment to ASDA is *** feet.
The runway slope is *** percent downhill.
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
P.A. No. 2484
AERO-B-BBA4-M12-0853 SS12-0424