US Airways 2007 Annual Report Download - page 545

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 destination airport conditions are such as to allow the required landing weight to be used without restriction. Pressure altitude is **.
2.13.2 An allowance of ** of fuel is included for taxi at the departure airport.
2.13.3 An allowance of ** of fuel is included for take-off and climb to ** above the departure airport at ** with acceleration to climb speed.
2.13.4 Climb from ** above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of ** at pressure
altitudes of ** above the destination airport are conducted in **. Climb and descent speeds below ** will be **.
2.13.5 An allowance of ** of fuel is included for approach and land at the destination airport.
2.13.6 An allowance of ** of fuel is included for taxi at the destination airport.
2.13.7 Stage distance is defined as the distance covered during climb, cruise and descent as described in paragraph 2.13.4 above.
**
2.13.8 At the end of approach and land ** of fuel will remain in the tanks. This represents the estimated fuel required for:
1) **
2) **
** Confidential Treatment Requested.
USA — Amended and Restated Airbus A320 Family Purchase Agreement LA 8F-1 — 11 of 22
EXECUTION PRIVILEGED AND CONFIDENTIAL