US Airways 2007 Annual Report Download - page 592

0 DEFINITIONS
For all purposes of this Agreement, except as otherwise expressly provided or unless the context otherwise requires, the following terms will have the
following meanings:
A330-200 Aircraft—any or all of the Airbus A330-200 model aircraft to be sold to the Buyer by the Seller pursuant to this Agreement, together with all
components, equipment, parts and accessories installed in or on such aircraft and the A330-200 Propulsion Systems installed thereon.
A330-200 Propulsion System—the two (2) Pratt & Whitney PW 4168A, two (2) Pratt & Whitney PW 4170, two (2) General Electric CF6 80E1A4 or
two (2) Rolls-Royce Trent 772B powerplants installed on an A330-200 Aircraft or to be installed on an A330-200 Aircraft at Delivery, each composed
of the powerplant (as such term is defined in Chapters 70-80 of the applicable ATA Specification, but limited to the equipment, components, parts and
accessories included in the powerplant, as so defined).
A330-200 Specification—the A330-200 Standard Specification, as amended from time to time in accordance with this Agreement.
A330-200 Standard Specification—the A330-200 standard specification document No. G.000.02000, Issue 4.3, dated July 13, 2006, to be published by
the Seller, which includes a maximum take-off weight of 233 metric tons, maximum landing weight of 182 metric tons and maximum zero-fuel weight
of 170 metric tons, a copy of which is annexed as Exhibit A-1.
A330-300 Aircraft—any or all of the Airbus A330-300 model aircraft to be sold to the Buyer by the Seller pursuant to this Agreement, together with all
components, equipment, parts and accessories installed in or on such aircraft and the A330-300 Propulsion Systems installed thereon.
A330-300 Propulsion System—the two (2) Pratt & Whitney PW 4170, two (2) General Electric CF6 80E1A4 or two (2) Rolls-Royce Trent 772B
powerplants installed on an A330-300 Aircraft or to be installed on an A330-300 Aircraft at Delivery, each composed of the powerplant (as such term is
defined in Chapters 70-80 of the applicable ATA Specification, but limited to the equipment, components, parts and accessories included in the
powerplant, as so defined).
A330-300 Specification—the A330-300 Standard Specification, as amended from time to time in accordance with this Agreement.
A330-300 Standard Specification—the A330-300 standard specification document No. G.000.03000, Issue 7.3, dated July 13, 2006, to be published by
the Seller, which includes a maximum take-off weight of 233 metric tons, maximum landing weight of 187 metric tons and maximum zero-fuel weight
of 185 metric tons, a copy of which is annexed as Exhibit A-2.
USA — Airbus A330 Purchase Agreement
EXECUTION
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