US Airways 2007 Annual Report Download - page 593

A340-300 Aircraft—any or all of the Airbus A340-300 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 A340-300 Propulsion Systems installed thereon.
A340-300 Propulsion System—the four (4) CFM International CFM 56-5C4/P powerplants installed on an A340-300 Aircraft or to be installed on an
A340-300 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).
A340-300 Specification—the A340-300 Standard Specification, as amended from time to time in accordance with this Agreement.
A340-300 Standard Specification—the A340-300 standard specification document No. F.000.03000, Issue 7.3, dated July 13, 2006, to be published by
the Seller, which includes a maximum take-off weight of 276.5 metric tons, maximum landing weight of 192 metric tons and maximum zero-fuel
weight of 181 metric tons, a copy of which is annexed as Exhibit A-3.
A340-500 Aircraft—any or all of the Airbus A340-500 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 A340-500 Propulsion Systems installed thereon.
A340-500 Propulsion System—the four (4) Rolls-Royce Trent 553A2.61 powerplants installed on an A340-500 Aircraft or to be installed on an
A340-500 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) .
A340-500 Specification—the A340-500 Standard Specification, as amended from time to time in accordance with this Agreement.
A340-500 Standard Specification—the A340-500 standard specification document No. F.000.05000, Issue 2.1, dated July 13, 2006, to be published by
the Seller, which includes a maximum take-off weight of 372 metric tons, maximum landing weight of 243 metric tons and maximum zero-fuel weight
of 230 metric tons, a copy of which is annexed as Exhibit A-4.
Affiliate—with respect to any person or entity, any other person or entity directly or indirectly controlling, controlled by or under common control with
such person or entity.
USA — Airbus A330 Purchase Agreement
EXECUTION
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