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Attachment A1
No. 6-1162-RCN-1937
GEnx-1B*** Engines
Page 17
Takeoff and Climbout Maneuver:
Fuel *** Pounds
Distance *** Nautical Miles
Approach and Landing Maneuver:
Fuel *** Pounds
Taxi-In (shall be consumed from the reserve fuel):
Fuel *** Pounds
Usable reserve fuel remaining upon completion of the approach and landing maneuver: *** Pounds
For information purposes, the reserve fuel is based on *** percent of a contingency allowance equivalent to the fuel
required for a *** minute cruise on a standard day at an *** Mach number, *** feet and a maximum landing
weight of *** Pounds
2.3.6 Operational Empty Weight Basis
The Operational Empty Weight (OEW) derived in Paragraph 2.3.7 is the basis for the mission guarantees of Paragraphs 2.3.1, 2.3.2, 2.3.3, 2.3.4,
and 2.3.5.
P.A. No. 2484
AERO-B-BBA4-M12-0853 SS12-0424