US Airways 2007 Annual Report Download - page 818

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).
2.4 Landing Field Length
FAR certified dry landing field length ("LFL") at an Aircraft gross weight of ** at Sea Level pressure altitude shall not be more than a guaranteed value
of
**.
2.5 Speed
Level flight speed at an Aircraft gross weight of ** at a pressure altitude of ** in ISA+10C conditions using a thrust not exceeding maximum cruise thrust
will be not less than a guaranteed true Mach number of **.
3 MISSION GUARANTEES
3.1 Mission Payload: **
The A340-300 Aircraft shall 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:
3.1.1 The departure airport conditions ** are as defined in paragraph 2.3.3 above.
The destination airport conditions are such to allow the required Landing Weight to be used without any restriction. Pressure altitude is **.
3.1.2 An allowance of ** of fuel and ** is considered for engine start-up and taxi-out.
3.1.3 An allowance of ** of fuel and ** is included for take-off and climb to ** pressure altitude with acceleration to climb speed at a temperature of **. No
credit is taken for the distance covered in these segments.
3.1.4 Climb from ** pressure altitude up to cruise altitude using maximum climb thrust, cruise at
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USA — Airbus A330 Purchase Agreement
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