A320-200 Propulsion Systems Sample Clauses

A320-200 Propulsion Systems. The Airframe shall be equipped with a set of two (2) (a) CFM International CFM56- 5B4/3 engines (or other CFM56 Series engines as may be agreed upon) or (b) International Aero Engines V2527-A5 (or other V2500 Series engines as may be agreed upon) (the “Propulsion Systems”).
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Related to A320-200 Propulsion Systems

  • Engines POSITION SERIAL NO. TOTAL HOURS TOTAL CYCLES HRS/CYCLES SINCE LAST SHOP VISIT Time Remaining to Next LIFE LIMITED PART REMOVAL PART NAME HOURS CYCLES MSN MSN

  • AIRCRAFT CONFIGURATION The guarantees defined in Paragraphs 2 and 3 below (the “Guarantees”) are applicable to the A321 Aircraft as described in the A321 Standard Specification ***** as amended by the following SCNs:

  • Aircraft Basic Price The Aircraft Basic Price is listed in Table 1 and is subject to escalation in accordance with the terms of this Purchase Agreement.

  • Aircraft The Airframe to be sold by AVSA to the Owner Trustee as provided in the Participation Agreement and to be leased under the Lease (or any permitted substitute airframe thereunder) together with two Engines (whether either is an initial Engine or a Replacement Engine) whether or not any of such initial or Replacement Engines may from time to time be installed on such Airframe or may be installed on any other airframe or on any other aircraft, including any aircraft substituted pursuant to Section 11.03

  • Airframe The Airbus A300F4-605R aircraft (excluding the Engines or engines from time to time installed thereon) to be leased by the Lessor to the Lessee pursuant to the Lease and the initial Lease Supplement and having the United States FAA Registration Number initially and manufacturer's serial number specified in the initial Lease Supplement, including (i) all Parts in respect thereof and (ii) any Replacement Airframe which may be substituted pursuant to Section 11.03

  • Technical Specifications Each Bloom System is an integrated system comprised of a fuel cell stack assembly and associated balance of plant components that converts a fuel into electricity using electrochemical means that (i) has a Nameplate Capacity of at least 0.5 kilowatts of electricity using an electrochemical process and (ii) has an electricity-only generation efficiency greater than thirty percent (30%).

  • Configuration The configuration for the Purchase Right Aircraft will be the Detail Specification for Model 767-3S2F aircraft at the revision level in effect at the time of the Supplemental Agreement. Such Detail Specification will be revised to include (i) changes required to obtain required regulatory certificates and (ii) other changes as mutually agreed upon by Boeing and Customer.

  • Spare Parts Contractor shall be responsible for obtaining vendor recommendations for spare parts and delivering such recommendations and spare parts to Owner in accordance with Section 3.4 of the Agreement.

  • Buyer Furnished Equipment 14.3.2.1 The Seller shall introduce data related to Buyer Furnished Equipment, for equipment that is installed on the Aircraft by the Seller (hereinafter “BFE Data”) into the customized Technical Data, at no additional charge to the Buyer for the initial issue of the Technical Data provided at first Aircraft Delivery, provided such BFE Data is provided in accordance with the conditions set forth in Clauses 14.3.2.2 through 14.3.2.6.

  • Spares Boeing will revise, as applicable, the customized Recommended Spares Parts List (RSPL) and Illustrated Parts Catalog (IPC).

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