ADDITIONAL AIRCRAFT SPECIFICATION Sample Clauses

ADDITIONAL AIRCRAFT SPECIFICATION. The Additional Aircraft shall be manufactured under the Specification.
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ADDITIONAL AIRCRAFT SPECIFICATION 

Related to ADDITIONAL AIRCRAFT SPECIFICATION

  • 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%).

  • 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:

  • 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.

  • Product Specifications The Company agrees that all Products sold to Xxxx hereunder shall conform to the respective specifications set forth on Schedule A or to such other specifications as are from time to time agreed upon by the Parties.

  • Quality Specifications SANMINA-SCI shall comply with the quality specifications set forth in its Quality Manual, incorporated by reference herein, a copy of which is available from SANMINA-SCI upon request.

  • Changes to Specifications All Specifications and any changes thereto agreed to by the parties from time to time shall be in writing, dated and signed by the parties. Any change to the Process shall be deemed a Specification change. No change in the Specifications shall be implemented by Catalent, whether requested by Client or requested or required by any Regulatory Authority, until the parties have agreed in writing to such change, the implementation date of such change, and any increase or decrease in costs, expenses or fees associated with such change (including any change to Unit Pricing). Catalent shall respond promptly to any request made by Client for a change in the Specifications, and both parties shall use commercially reasonable, good faith efforts to agree to the terms of such change in a timely manner. As soon as possible after a request is made for any change in Specifications, Catalent shall notify Client of the costs associated with such change and shall provide such supporting documentation as Client may reasonably require. Client shall pay all costs associated with such agreed upon changes. If there is a conflict between the terms of this Agreement and the terms of the Specifications, this Agreement shall control. Catalent reserves the right to postpone effecting changes to the Specifications until such time as the parties agree to and execute the required written amendment.

  • 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.

  • Delivery Schedule The scheduled months of delivery of the Aircraft are listed in the attached Table 1. Exhibit B describes certain responsibilities for both Customer and Boeing in order to accomplish the delivery of the Aircraft.

  • Aircraft Description The Option Aircraft are described by Boeing Detail Specification D6-38808, Revision E, dated September 15, 1995, as amended and revised pursuant to the 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

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