US Airways 2007 Annual Report Download - page 427

1.3 Take-off
1.3.1 FAR take-off field length at an A318 Aircraft gross weight of ** at the start of ground run at sea level pressure altitude in ** will be not more than a
guaranteed value of **.
1.3.2 FAR take-off field length at an A318 Aircraft gross weight of ** at the start of ground run at sea level pressure altitude at an ambient temperature of **
will be not more than a guaranteed value of **.
1.3.3 When operated under the following conditions (**):
Pressure altitude: **
Ambient temperature: **
Take-off run available ("TOR"): **
Take-off distance available: **
Accelerate-stop distance available: **
Slope: **
Wind: **
Obstacles (height and distance **
from end of TOR) **
**
the maximum permissible weight at the start of ground run will **.
1.4 Second Segment Climb
The A318 Aircraft will **.
1.5 Altitude Capability
At an A318 Aircraft gross weight of ** conditions, the A318 Aircraft will be capable of maintaining:
— a rate of climb of **
— a rate of climb of **
— a maneuver of **
at a guaranteed pressure altitude of not less than **
1.6 En-route One Engine Inoperative
** Confidential Treatment Requested.
USA—Amended and Restated Airbus A320 Family Purchase Agreement LA 8A-2 — 3 of 12
EXECUTION PRIVILEGED AND CONFIDENTIAL