US Airways 2007 Annual Report Download - page 558

PREAMBLE
The guarantees defined below ("the Guarantees") are applicable to the New A321 (IAE Powered) Aircraft 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 provisions for two Additional Centre Tanks ("ACT")
c) **
d) **
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 A321 (IAE 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 **:
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 LA 8F-2 — 2 of 20
EXECUTION PRIVILEGED AND CONFIDENTIAL