US Airways 2007 Annual Report Download - page 1091

1 AIRCRAFT CONFIGURATION
1.1 The Guarantees defined below are applicable to the A350-800 XWB Aircraft powered by Rolls Royce Trent XWB engines, as described in the Standard
Specification ** and in the Aircraft Description Document **, herein after referred as "the Specification" without taking into account any further changes
thereto as provided in the Agreement.
2 GUARANTEED PERFORMANCE
2.1 Take-off Field Length
FAR take-off field length ("TOFL") at an Aircraft gross weight of 540,133 lb (245,000 kg) at the start of Take-Off Distance Available (TODA) at Sea
Level pressure altitude in ISA+15°C conditions will be **.
2.2 Second Segment Climb
The Aircraft will meet FAR 25 regulations for one engine inoperative climb after take-off, undercarriage retracted, at a weight corresponding to the stated
weight at the start of ground run, at the altitude and temperature, and in the configuration of flap angle and safety speed required to comply with the
performance guaranteed in paragraph 2.1 and 2.3.
2.3 Take-off Weight
2.3.1 When operated under the following conditions **
Pressure altitude : **
Ambient temperature : **
Take-off run available : **
Take-off distance available : **
Accelerate-stop distance available : **
Slope : **
Wind : **
Line-up allowance TOD : **
Line-up allowance ASD : **
Obstacles (Height/Distance above/from start of TODA): **
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** Confidential Treatment Requested.
USA — Amended and Restated Airbus A350 XWB Purchase Agreement
EXECUTION
LA 8-1.B — 2 of 18
PRIVILEGED AND CONFIDENTIAL