US Airways 2007 Annual Report Download - page 816

the maximum permissible take-off weight at the start of Take-off Distance Available shall be not less than a guaranteed value of ** (Max Structural)
2.3.2 When operated under the following conditions **
Pressure altitude : **
Ambient temperature : **
Take-off run available : **
Take-off distance available : **
Accelerate-stop distance available : **
Slope : **
Wind : **
Line-up allowance TODA/TORA : **
Line-up allowance ASDA : **
Obstacles (Height/Distance above/from end of TODA): **
**
**
**
**
**
the maximum permissible take-off weight at the start of Take-off Distance Available shall be not less than a guaranteed value of ** (Max Structural).
2.3.3 When operated under the following conditions **
Pressure altitude : **
Ambient temperature : **
Take-off run available : **
Take-off distance available : **
Accelerate-stop distance available : **
Slope : **
Wind : **
Line-up allowance TODA/TORA : **
Line-up allowance ASDA : **
Obstacles : **
the maximum permissible take-off weight at the start of Take-off Distance Available shall be not less than a guaranteed value of ** (Max Structural).
2.3.4 When operated under the following conditions **
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USA — Airbus A330 Purchase Agreement
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