Propulsion Systems Basic Price Sample Clauses

Propulsion Systems Basic Price. The basic price of a set of two (2) Propulsion Systems is respectively: • For A319: CFM INTERNATIONAL 56-5B6/P Propulsion Systems: [***] INTERNATIONAL AERO ENGINE V2524-A5 Propulsion Systems, specifically excluding, for the avoidance of doubt, nacelles and thrust reversers): [***] • For A320: CFM INTERNATIONAL 56-5B4/P Propulsion Systems: [***] INTERNATIONAL AERO ENGINE V2527-A5 Propulsion Systems specifically excluding, for the avoidance of doubt, nacelles and thrust reversers: [***] • For A321: CFM56-5B3/P Propulsion Systems: [***] IAE V2533-A5 Propulsion Systems, specifically excluding, for the avoidance of doubt, nacelles and thrust reversers: [***] • For A330-200: GENERAL ELECTRIC CF6-80E1A3 Propulsion Systems : [***] XXXXX & XXXXXXX PW4168A Propulsion Systems: [***] The respective Propulsion Systems Basic Prices have been established in accordance with the delivery conditions prevailing in January 2006 and have been calculated from the respective Propulsion Systems Reference Prices. A320 / A330 PA – TAM – 11/2006 “[* * *]” This information is subject to confidential treatment and has been omitted and filed separately with the commission.
Sample 1
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Propulsion Systems Basic Price. The basic price of the Propulsion Systems (the “Propulsion Systems Basic Price”) shall, depending on the Propulsion Systems selected by the Buyer, be as applicable pursuant to Clauses 3.1.2.1 or 3.
Sample 1
Propulsion Systems Basic Price. The basic price of a set of two (2) Propulsion Systems including standard equipment is: - With INTERNATIONAL AERO ENGINES IAE V2524-A5: [***] A320F - LAN - AMDT 2 - Second A320 Family PA - 10/2005 - With CFM INTERNATIONAL Engines CFMI 56-5B6 /P [***] With INTERNATIONAL AERO ENGINES IAE V2527E-A5: [***] With CFM INTERNATIONAL Engines CFMI 5 B4 /P [***] The above Propulsion Systems Basic Prices have been established in accordance with the delivery conditions prevailing in [***] and have been calculated from the Propulsion Systems Reference Prices referred to in sub-Clause 4.2. The above Propulsion Systems Reference Prices are subject to adjustment in accordance with the relevant Propulsion Systems Manufacturer’s Price Revision Formula referred to in sub-Clause 4.2.
Sample 1
Propulsion Systems Basic Price. 3.3.1 The A319 IAE Propulsion Systems The Basic Price of the IAE V2524-A5 Propulsion System (excluding specifically nacelles and thrust reversers) for the A319 Aircraft, at delivery conditions prevailing in January 2005, is: US $ [***] (US dollars [***]). 3.3.2 The A319 CFMI Propulsion Systems The Basic Price of the CFMI CFM56-5B6/P Propulsion System for the A319 Aircraft, at delivery conditions prevailing in January 2005 is: US $ [***] (US dollars [***]). 3.3.3 The A320 IAE Propulsion Systems The Basic Price of a IAE V2527-A5 Propulsion System (excluding specifically nacelles and thrust reversers) for the A320 Aircraft, at delivery conditions prevailing in January 2005, is: US $ [***] (US dollars [***]). 3.3.4 The A320 CFMI Propulsion Systems The Basic Price of a CFMI CFM56-5B4/P Propulsion System for the A320 Aircraft, at delivery conditions prevailing in January 2005, is: US $ [***] (US dollars [***]).
Sample 1
Propulsion Systems Basic Price 
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Related to Propulsion Systems Basic Price

  • 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 CONFIGURATION The guarantees defined below (the “Guarantees”) are applicable to the A319-100 Aircraft as described in the Standard Specification Ref. J 000 01000 Issue 6 dated 1st March 2007 equipped with:

  • Engine A. Any internal repairs or replacement of internal components, or replacement of engine assembly.

  • 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

  • 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.

  • Primary Frequency Response Developer shall ensure the primary frequency response capability of its Large Generating Facility by installing, maintaining, and operating a functioning governor or equivalent controls. The term “functioning governor or equivalent controls” as used herein shall mean the required hardware and/or software that provides frequency responsive real power control with the ability to sense changes in system frequency and autonomously adjust the Large Generating Facility’s real power output in accordance with the droop and deadband parameters and in the direction needed to correct frequency deviations. Developer is required to install a governor or equivalent controls with the capability of operating: (1) with a maximum 5 percent droop ± 0.036 Hz deadband; or (2) in accordance with the relevant droop, deadband, and timely and sustained response settings from an approved Applicable Reliability Standard providing for equivalent or more stringent parameters. The droop characteristic shall be: (1) based on the nameplate capacity of the Large Generating Facility, and shall be linear in the range of frequencies between 59 and 61 Hz that are outside of the deadband parameter; or (2) based on an approved Applicable Reliability Standard providing for an equivalent or more stringent parameter. The deadband parameter shall be: the range of frequencies above and below nominal (60 Hz) in which the governor or equivalent controls is not expected to adjust the Large Generating Facility’s real power output in response to frequency deviations. The deadband shall be implemented: (1) without a step to the droop curve, that is, once the frequency deviation exceeds the deadband parameter, the expected change in the Large Generating Facility’s real power output in response to frequency deviations shall start from zero and then increase (for under-frequency deviations) or decrease (for over-frequency deviations) linearly in proportion to the magnitude of the frequency deviation; or (2) in accordance with an approved Applicable Reliability Standard providing for an equivalent or more stringent parameter. Developer shall notify NYISO that the primary frequency response capability of the Large Generating Facility has been tested and confirmed during commissioning. Once Developer has synchronized the Large Generating Facility with the New York State Transmission System, Developer shall operate the Large Generating Facility consistent with the provisions specified in Articles 9.5.5.1 and 9.5.5.2 of this Agreement. The primary frequency response requirements contained herein shall apply to both synchronous and non-synchronous Large Generating Facilities.

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

  • Aircraft This peril includes self-propelled missiles and spacecraft.

  • Maintenance Manual No later than 60 (sixty) days prior to the Project Completion Date, the Contractor shall, in consultation with the Authority’s Engineer, evolve a maintenance manual (the “Maintenance Manual”) for the regular and preventive maintenance of the Project Highway in conformity with the Specifications and Standards, safety requirements and Good Industry Practice, and shall provide 5 (five) copies thereof to the Authority’s Engineer. The Authority’s Engineer shall review the Maintenance Manual within 15 (fifteen) days of its receipt and communicate its comments to the Contractor for necessary modifications, if any.

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