Engine Stability Sample Clauses

Engine Stability. Technical support is provided to ensure that engine stability and starting reliability are maintained. Service evaluation programs for proposed improvements are initiated and monitored to determine their effectiveness. In addition, problems relating to engine control systems which impact engine stability and performance are analyzed.
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Related to Engine Stability

  • Compatibility 1. Any unresolved issue arising from a mutual agreement procedure case otherwise within the scope of the arbitration process provided for in this Article and Articles 25A to 25G shall not be submitted to arbitration if the issue falls within the scope of a case with respect to which an arbitration panel or similar body has previously been set up in accordance with a bilateral or multilateral convention that provides for mandatory binding arbitration of unresolved issues arising from a mutual agreement procedure case.

  • 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.

  • Technical Specifications The Technical Specifications furnished on the CD are intended to establish the standards for quality, performance and technical requirements for all labor, workmanship, material, methods and equipment necessary to complete the Work. When specifications and drawings are provided or referenced by the County, these are to be considered part of the Scope of Work, and to be specifically documented in the Detailed Scope of Work. For convenience, the County supplied specifications, if any, and the Technical Specifications furnished on the CD.

  • 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:

  • Traceability 11.1 Under the terms of this Agreement, Supplier shall have and operate a process to ensure that all Products, sub-assemblies and the components contained therein supplied to the Buyer are completely Traceable back to manufacturer by batch or lot or date code.

  • Validation To validate the notice requirements outlined in Section 5.3, the Assuming Institution shall provide the Receiver (i) an Affidavit of Publication to meet the publication requirements outlined in Section 5.3(a) and (ii) the Assuming Institution will prepare an Affidavit of Mailing in a form substantially similar to Exhibit 2.3B after mailing the seven (7) day Notice to Depositors as required under Section 5.3(b).

  • Stability Testing Patheon may be requested to conduct stability testing on the Products in accordance with the protocols set out in the Specifications for the separate fees and during the time periods set out in Schedule C to a Product Agreement. Patheon will not make any changes to these testing protocols without prior written approval from Client. If a confirmed stability test failure occurs, Patheon will notify Client within one Business Day, after which Patheon and Client will jointly determine the proceedings and methods to be undertaken to investigate the cause of the failure, including which party will bear the cost of the investigation. Patheon will not be liable for these costs unless it has failed to perform the Manufacturing Services in accordance with the Specifications, cGMPs, and Applicable Laws. Patheon will give Client ail stability test data and results at Client’s request.

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