US Airways 2007 Annual Report Download - page 428

The A318 Aircraft will **.
1.7 Approach Climb
The A318 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
1.9.1 FAR certified dry landing field length at an A318 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 A318 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 defined in Paragraph 1.3.3.
**
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 **.
2.1.3 Climb from ** above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of ** at a pressure
altitude of ** above the destination airport are conducted in **conditions. Climb and descent profiles are respectively ** Mach number and **.
** Confidential Treatment Requested.
USA—Amended and Restated Airbus A320 Family Purchase Agreement LA 8A-2 — 4 of 12
EXECUTION PRIVILEGED AND CONFIDENTIAL