US Airways 2007 Annual Report Download - page 416

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 **. Climb and descent profiles are respectively **Mach number and **.
2.1.4 An allowance of ** of fuel is included for approach and land at the destination airport.
2.1.5 Stage distance is defined as the distance covered during climb, cruise and descent as described in Paragraph 2.1.3 above.
** Confidential Treatment Requested.
USA—Amended and Restated Airbus A320 Family Aircraft Purchase Agreement LA 8A-1 — 4 of 12
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