United Airlines 2012 Annual Report Download - page 382
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Attachment A1
No. 6-1162-RCN-1937
GEnx-1B*** Engines
Page 3
2.2.2 The gross weight capability at an altitude of *** feet, on an ISA+10°C day, at *** Mach number, and satisfying the conditions defined below, shall
not be less than the following guarantee value:
NOMINAL: *** Pounds
TOLERANCE: *** Pounds
GUARANTEE: *** Pounds
Conditions:
1) The Aircraft shall be capable of maintaining level cruising flight using not more than maximum cruise thrust.
2) The Aircraft shall be capable of maintaining a rate of climb of *** feet per minute using not more than maximum climb thrust.
3) The Aircraft shall be capable of at least a ***g maneuver load factor at buffet onset.
2.3 Mission
2.3.1 Mission Range
The still air range with a *** pound payload using the conditions and operating rules defined below, shall not be less than the following guarantee
value:
NOMINAL: *** Nautical Miles
TOLERANCE: *** Nautical Miles
GUARANTEE: *** Nautical Miles
Conditions and operating rules:
Still Air Range: The still air range is defined as the sum of the distances for the climbout maneuver, climb, cruise, and descent.
Takeoff: The airport altitude is ***.
The takeoff gross weight is ***the airport conditions.
The takeoff gross weight shall conform to FAA Regulations.
P.A. No. 2484
AERO-B-BBA4-M12-0853 SS12-0424