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US Airways 2007 Annual Report Download - page 507

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Pressure altitude : **

Ambient temperature : **

Take-off run available (TORA) : **

Take-off distance available : **

Accelerate-stop distance available : **

Slope : **

Wind : **

Line-up allowance TOD : **

Line-up allowance ASD : **

Obstacles (height and distance : **

from end of TORA) : **

: **

the maximum permissible weight at the start of TORA shall **

1.2 Second Segment

The New A320 (IAE Powered) Aircraft shall **

1.3 Landing Field Length

FAR certified dry landing field length at an New A320 (IAE Powered) Aircraft gross weight of **at sea level pressure altitude shall be not more than

**.

1.4 Specific Range

1.4.1 The nautical miles per pound of fuel at an New A320 (IAE Powered) Aircraft gross weight of ** at a pressure altitude of ** conditions at a true Mach

number of ** shall be not less than a guaranteed value of **.

1.4.2 The nautical miles per pound of fuel at an New A320 (IAE Powered) Aircraft gross weight of ** at a pressure altitude of ** conditions at a true Mach

number of ** shall be not less than a guaranteed value of **.

2 MISSION GUARANTEES

** Confidential Treatment Requested.

USA — Amended & Restated Airbus A320 Family Purchase Agreement LA 8E-1 — 3 of 14

EXECUTION PRIVILEGED AND CONFIDENTIAL