US Airways 2007 Annual Report Download - page 520

PREAMBLE
The guarantees defined below ("the Guarantees") are applicable to the New A320 (CFM Powered) as described in the Technical Specification ** for:
a) Increased Design Weights to:
Maximum Take-Off Weight **
Maximum Landing Weight **
Maximum Zero Fuel Weight **
b) The fitting of CFM International CFM56-5B4/P propulsion system
and without taking into account any further changes thereto as provided in the Agreement.
All Guarantees specified in this document are applicable to aircraft to be delivered from 2009 onwards.
1 GUARANTEED PERFORMANCE
1.1 Take-off
1.1.1 FAR take-off field length at an New A320 (CFM Powered) Aircraft gross weight of **at the start of TORA at sea level pressure altitude in ** shall be
not more than a guaranteed value of **.
1.1.2 When operated under the following conditions (representative of PHX 25R):
Pressure altitude : **
Ambient temperature : **
Take-off run available (TORA) : **
Take-off distance available : **
Accelerate-stop distance available : **
Slope : **
Wind : **
Line-up allowance TOD : **
Line-up allowance ASD : **
Obstacles (height and distance : **
from end of TORA) : **
: **
: **
: **
: **
: **
** Confidential Treatment Requested.
USA — Amended and Restated Airbus A320 Family Purchase Agreement
EXECUTION
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PRIVILEGED AND CONFIDENTIAL