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”).
Propulsion System. 2.4.1 Each A319 Airframe will be equipped with a set of two CFM International CFM56-5B6/3 engines or International Aero Engines V2524-A5 engines (such set, upon selection, an “A319 Propulsion System”).
2.4.2 Each A320 Airframe will be equipped with a set of two CFM International CFM56-5B4/3 engines or International Aero Engines V2527-A5 engines (such set, upon selection, an “A320 Propulsion System”).
2.4.3 Each A321 Airframe will be equipped with a set of two CFM International CFM56-5B3/3 engines or International Aero Engines V2533-A5 engines (such set, upon selection, an “A321 Propulsion System”).
2.4.4 Each A319 NEO Airframe will be equipped with a set of two CFM International LEAP-X1A24 engines or Xxxxx & Xxxxxxx PW1124G engines (such set, upon selection, an “A319 NEO Propulsion System”).
2.4.5 Each A320 NEO Airframe will be equipped with a set of two CFM International LEAP-X1A26 engines or Xxxxx & Whitney PW1127G engines (such set, upon selection, an “A320 NEO Propulsion System”).
2.4.6 Each A321 NEO Airframe will be equipped with a set of two CFM International LEAP-X1A32 engines or Xxxxx & Xxxxxxx PW1133G engines (such set, upon selection, an “A321 NEO Propulsion System”).
2.4.7 [CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT]
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. Each Airframe shall be equipped with a set of two (2) CFM International CFM56B3/3 engines propulsion systems (the “Propulsion Systems”).
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.
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. Eight (8) Kamewa controllable pitch, fully azithmuthing thrusters, with thrust of 48.6 mt each. Self Propelled Speed 3 - 5 knots The minimum tow requirement for the Ocean Confidence at transit draft is a tug with a minimum bollard pull of 132 short tons. If two or more tugs are used, the bollard pull shall be shared by the weaker boats as follows: Two tugs, at least 40% from the weaker boat Three tugs, at least 25% from the weakest boat Four tugs, at least 20% from the weakest boat All requirements are for towage classified as field moves in moderate environments. For towage in more significant environmental conditions and ocean tows, each move shall be evaluated by the Marine Department and insurance underwriters for selection of towing equipment. After March 1 2004, all towing vessels shall provide a bollard pull certificate acceptable to Diamond Offshore Drilling and to their Warranty Surveyor of Record. Mooring lines Number 8 (system capable of 12 lines) Chain size 3 inch Chain length 3500 feet each (1,066 meters) Chain grade NVR4S RIG type Chain breaking strength (new) 7,350 kN. Chain proof load (new) 5,733 kN. Length 2,000 ft. Chain grade NV K4 RIG type Chain breaking strength (new) 612.9 mt Chain proof load (new) 482.4 mt Length 1,500 ft. Four (4) each 10 metric ton Stevpris HP anchors w/permanent chain chaser system (no surface buoys) Windlass: Four (4) ea Pusnes 3 line electric windlasses, driven by 2 Toshiba MSC-RBKMW 900HP DC motors. Each line is equipped with a 1,000 hp water-cooled hydraulic disc brake and hydraulic band brake. Each unit is fitted with 2 — 5,000 hp hydrodynamic brakes. Each control unit is housed in a weather-protected enclosure. Each unit features continuous readout for line tension, speed, and amount of chain out. Similar Information is provided in the Pilothouse, with emergency release capability.
Propulsion System. 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.
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 the CFM LEAP 1A24 Propulsion System, the CFM LEAP 1A26 Propulsion System, the CFM LEAP 1A32 Propulsion System, the CFM LEAP 1A33 Propulsion System, the IAE V2527-A5 Propulsion Systems, the IAE V2533-A5 Propulsion Systems, the CFM 56-5B3/3 Propulsion System, the PW1124G-JM Propulsion System, the PW1127G-JM Propulsion System and the PW1133G-JM Propulsion System, as applicable. Scheduled Delivery Period – for each Aircraft, the Scheduled Delivery Year, Scheduled Delivery Quarter or Scheduled Delivery Month of such Aircraft, as applicable. UNQUOTE
