US Airways 2007 Annual Report Download - page 450

Pressure altitude: **
Ambient temperature: **
Take-off run available ("TOR"): **
Take-off distance available: **
Accelerate-stop distance available: **
Slope: **
Wind: **
Obstacle (height and distance **
from end of runway): **
**
the maximum permissible weight at the start of ground run will **
1.4 Second Segment Climb
The Original A319 Aircraft will **
1.5 Altitude Capability
At an Original A319 Aircraft gross weight of ** the Original A319 Aircraft will be capable of maintaining:
- a rate of climb of **,
- **
- a maneuver of **
at a guaranteed pressure altitude of not less than **
1.6 En-route One Engine Inoperative
The Original A319 Aircraft will **.
1.7 Approach Climb
The Original A319 Aircraft will **.
1.8 Landing Climb
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
** CONFIDENTIAL TREATMENT REQUESTED.
USA — Amended and Restated Airbus A320 Family Purchase Agreement LA 8B-2 — 3 of 10
EXECUTION PRIVILEGED AND CONFIDENTIAL