US Airways 2007 Annual Report Download - page 440

FAR minimum landing climb gradient requirements using the landing flap configuration required to show compliance with Paragraph 1.9.1 will **
1.9 Landing Field Length
1.9.1 FAR certified dry landing field length at an Original A319 Aircraft gross weight of ** at sea level pressure altitude will not be more than a guaranteed
value of **.
1.9.2 When operated according to FAR regulations and under the following conditions **:
Pressure altitude: **
Ambient temperature: **
Landing distance available: **
Wind: **
the maximum permissible landing weight will be **
2. MISSION GUARANTEES
2.1 The Original A319 Aircraft will be capable of carrying a guaranteed payload of not less than ** over a still air stage distance of ** when operated under
the conditions defined below:
2.1.1 The departure airport conditions are as follows:
Pressure altitude: **
Ambient temperature: **
Take-off run available: **
Take-off distance available: **
Accelerate-stop distance available: **
Slope: **
Wind: **
Obstacles (height and distance **
from start of roll): **
**
The destination airport conditions are such as to allow the required landing weight to be used without restriction. **
2.1.2 An allowance of ** of fuel is included for take-off and climb to ** above the departure airport with acceleration to climb speed at an ambient
temperature of **
** Confidential Treatment Requested.
USA — Amended and Restated Airbus A320 Family Aircraft Purchase Agreement LA 8B-1 — 4 of 11
EXECUTION PRIVILEGED AND CONFIDENTIAL