US Airways 2007 Annual Report Download - page 506

PREAMBLE
The guarantees defined below ("the Guarantees") are applicable to the New A320 (IAE Powered) Aircraft as described in the Technical Specification
** for:
a) **
b) The fitting of International Aero Engines V2527-A5 propulsion system
and without taking into account any further changes thereto as provided in the Agreement.
All Guarantees specified in this document are **
1 GUARANTEED PERFORMANCE
1.1 Take-off
1.1.1 FAR take-off field length at an New A320 (IAE Powered) Aircraft gross weight of **at the start of TORA at sea level pressure altitude in ** conditions
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) : **
: **
: **
: **
: **
: **
the maximum permissible weight at the start of TORA shall **
1.1.3 When operated under the following conditions **:
** Confidential Treatment Requested.
USA — Amended & Restated Airbus A320 Family Purchase Agreement LA 8E-1 — 2 of 14
EXECUTION PRIVILEGED AND CONFIDENTIAL