US Airways 2007 Annual Report Download - page 1132

1 AIRCRAFT CONFIGURATION
1.1 The Guarantees defined below are applicable to the A350-900 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 ** at the start of Take-Off Distance Available (TODA) at Sea Level pressure altitude
in ** 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 A350 Purchase Agreement LA 8-2.B – 2 of 16
EXECUTION PRIVILEGED AND CONFIDENTIAL