Propulsion System Sample Clauses

Propulsion System. 2.3.1 Each A320 Airframe will be equipped with a set of two (2) CFM International LEAP-X1A26 engines (such set, an “A320 Propulsion System”). Each A319 Airframe will be equipped with a set of two (2) CFM International LEAP-X1A24 engines (such set, an “A319 Propulsion System”).
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Propulsion System. The Aircraft will be shall be equipped with a propulsion system comprising a set of four (4) Engine Alliance GP7270 engines including the related standard equipment (“Propulsion System”).
Propulsion System the CFM LEAP X-1A24 Propulsion System, the CFM LEAP X-1A27 Propulsion System, the CFM LEAP X-1A32 Propulsion System, the IAE V2527-A5 Propulsion System, the IAE V2533-A5 Propulsion System, the PW1124G Propulsion System, the PW1127G Propulsion System and the PW1133G Propulsion System, as applicable. PW Propulsion System – the PW1124G Propulsion System, the PW1127G Propulsion System and the PW1133G Propulsion System, as applicable. Standard Specification – the A319 Standard Specification, the A320 Standard Specification and the A321 Standard Specification, as applicable. 2 TYPE FLEXIBILITY
Propulsion System. Each Airframe shall be equipped with a set of two (2) CFM International LEAP-1 A26 engines propulsion systems (the “Propulsion Systems”).
Propulsion System. System that provides propulsion for the vehicle proportional to operator commands. Includes, as applicable, the EDS or HDS, energy storage system and the ESC or HSC. Propulsion Power Unit (PPU). System of components that provide tractive power, such as traction motor. Real-Time Clock (RTC). Computer clock that keeps track of the current time. Regenerative Braking. Deceleration of the bus by switching motors to act as generators, which return vehicle kinetic energy to the energy storage system.
Propulsion System. Propulsion system components, specifically the engine or drive motors, and generators (for hybrid technology) and drive and non-drive axles shall be warranted to be free from Defects and Related Defects for the standard 2 years or 200,000 miles, whichever comes first. The propulsion system manufacturer’s standard warranty, delineating items excluded from the Extended Warranty, submitted in accordance with the Request for Pre- Offer Change.
Propulsion System. The Contractor shall perform a complete propulsion system vibration analysis, including torsional and lateral (whirling) vibration and solid body dynamic motion, and submit the analysis and findings to ABS, the Owner's Representative, and each drivetrain component supplier for approval prior to finalizing the system arrangement and start of component fabrication. Approval from each drivetrain component supplier shall include confirmation of the mass and elastic strain data used in the analysis, and confirmation that the findings are within acceptable limits. The propulsion train shall be free from excessive torsional, longitudinal, and flexural vibrations throughout the full range of engine operating speeds in accordance with ABS Rules. The Contractor shall modify the shafting arrangement as necessary to eliminate serious torsional, flexural, and longitudinal vibrations within the normal operating range of the propulsion system. Barred speed ranges within the normal operating speeds of the engine shall be unacceptable, as will raising the idle or lowering the maximum continuous rpm to avoid barred speeds.
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Propulsion System. ‌ Valley Metro, in collaboration with the City, shall determine the most appropriate propulsion system for the Project utilizing a Traction Electrification System, Off Wire Technology, or a combination thereof. The Parties shall take into consideration capital cost, availability per the Project Master Schedule, public safety, operational reliability, maintenance costs and aesthetics. The City has a strong preference to solutions that support off-wire systems.
Propulsion System. The last paragraph of Clause 2.3.1 of the Agreement, as amended by Paragraph 3.1 of Letter Agreement No. 9 (Specification Matters) to the Agreement, is deleted and replaced with the following quoted text: QUOTE If the Buyer has not selected the Group 1 A320 Propulsion System as of the date of this Agreement, such choice will be made no later than ***** UNQUOTE
Propulsion System. 1.3.2 The Buyer hereby selects the following Propulsion Systems with respect to the Aircraft rank 96, 112, 114 and 119 through and including rank 134: for each A321 Aircraft: CFM INTERNATIONAL 56-5B3/3. “[* * *]” This information is subject to confidential treatment and has been omitted and filed separately with the commission.
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