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:
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Samples: Letter Agreement (China Eastern Airlines Corp LTD), Letter Agreement (China Eastern Airlines Corp LTD)
AIRCRAFT CONFIGURATION. The guarantees defined below (the “Guarantees”) are applicable to the A319A320-100 200 Aircraft as described in the Standard Specification Ref. J D 000 01000 02000 Issue 6 7 dated 1st March 2007 equipped with:
Appears in 2 contracts
Samples: Letter Agreement (China Eastern Airlines Corp LTD), Letter Agreement (China Eastern Airlines Corp LTD)
AIRCRAFT CONFIGURATION. The guarantees defined below (the “Guarantees”) are applicable to the A319A321-100 200 Aircraft as described in the Standard Specification Ref. J E 000 01000 02000 Issue 6 4 dated 1st March 2007 equipped with:
Appears in 2 contracts
Samples: Letter Agreement (China Eastern Airlines Corp LTD), Letter Agreement (China Eastern Airlines Corp LTD)
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:
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AIRCRAFT CONFIGURATION. The guarantees defined below (the “Guarantees”) are applicable to the A319A320-100 200 Aircraft as described in a) the Standard Specification Ref. J D 000 01000 02000 Issue 6 8 dated 20th June 2011 or b) the Standard Specification Ref. D 000 02000 Issue 7 dated 1st March 2007 equipped with2007, as amended by Specification Change Notices (“SCN’s”) for:
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AIRCRAFT CONFIGURATION. The guarantees defined below (the “Guarantees”) are applicable to the A319A321-100 200 Aircraft as described in the Standard Specification Ref. J reference E 000 01000 02000 Issue 6 5 dated 1st March 2007 equipped with20th June 2011 amended by Specification Change Notices (SCNs) for:
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AIRCRAFT CONFIGURATION. The guarantees defined below (the “Guarantees”) are applicable to the A319A321-100 200 Aircraft as described in a) the Standard Specification Ref. J E 000 01000 02000 Issue 6 5 dated 20th June 2011 or b) the Standard Specification Ref. E 000 02000 Issue 4 dated 1st March 2007 equipped with2007, as amended by Specification Change Notices (“SCN’s”) for:
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AIRCRAFT CONFIGURATION. The guarantees defined below (the “Guarantees”) are applicable to the A319A321-100 200 Aircraft as described in the Standard Specification Ref. J E 000 01000 02000 Issue 6 5 dated 1st March 2007 equipped with20th June 2011 as amended by Specification Change Notices (“SCN’s”) for installation of following engines:
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AIRCRAFT CONFIGURATION. The guarantees defined below (the “"Guarantees”") are applicable to the A319A321-100 200 Aircraft as described in the Standard Specification Ref. J 000 01000 Issue 6 dated 1st March 2007 ***equipped with:
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AIRCRAFT CONFIGURATION. The guarantees defined below (the “"Guarantees”") are applicable to the A319A330-100 200 Aircraft as described in the Standard Specification Ref. J G 000 01000 02000 Issue 6 4.5 dated 1st March 2007 equipped with:30th April 2008 and amended by SCN for
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AIRCRAFT CONFIGURATION. The guarantees defined below (the “"Guarantees”") are applicable to the A319A330-100 200 Aircraft equipped with General Electric CF6-80E1A4 propulsion system as described in the Standard Specification Ref. J G 000 01000 02000 Issue 6 4.5 dated 1st March 2007 equipped with:30th April 2008 without taking into account any further changes thereto as provided in the Agreement (the "Specification" for the purposes of this Letter Agreement).
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AIRCRAFT CONFIGURATION. The guarantees defined below (the “"Guarantees”") are applicable to the A319A321-100 200 Aircraft as described in the Standard Specification Ref. J E 000 01000 02000 Issue 6 4 dated 1st March 2007 equipped with:
Appears in 1 contract
AIRCRAFT CONFIGURATION. The guarantees defined below (the “"Guarantees”") are applicable to the A319A330-100 300 Aircraft equipped with General Electric CF6-80E1A4 propulsion system as described in the Standard Specification Ref. J G 000 01000 03000 Issue 6 7.5 dated 1st March 2007 equipped with:30th April 2008 without taking into account any further changes thereto as provided in the Agreement (the "Specification" for the purposes of this Letter Agreement).
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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:
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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 7 dated 1st March 2007 equipped with20th June 2011 as amended by Specification Change Notices (“SCN’s”) for installation of following engines:
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AIRCRAFT CONFIGURATION. The guarantees defined below (the “Guarantees”) are applicable to the A319-100 Aircraft as described in a) the Standard Specification Ref. J 000 01000 Issue 7 dated 20th June 2011 or b) the Standard Specification Ref. J 000 01000 Issue 6 dated 1st March 2007 equipped with2007, as amended by Specification Change Notices (“SCN’s”) for:
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AIRCRAFT CONFIGURATION. The guarantees defined below ("the “Guarantees”") are applicable to the A319A350-100 800 Aircraft as described in the Standard Specification Ref. J G 000 01000 08000 Issue 6 A dated 1st March 2007 equipped with:February 28th, 2005 and [...***...].
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AIRCRAFT CONFIGURATION. The guarantees defined below (the “"Guarantees”") are applicable to the A319A330-100 200 Aircraft equipped with Rolls-Xxxxx Xxxxx 772B "EP" propulsion system as described in the Standard Specification Ref. J G 000 01000 02000 Issue 6 4.5 dated 30th April 2008 for deliveries from 1st March 2007 equipped with:quarter 2009 onwards without taking into account any further changes thereto as provided in the Agreement (the "Specification" for the purposes of this Letter Agreement).
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AIRCRAFT CONFIGURATION. The guarantees defined below (the “Guarantees”) are applicable to the A319A320-100 200 Aircraft as described in the Standard Specification Ref. J D 000 01000 02000 Issue 6 8 dated 1st March 2007 equipped with20th June 2011 as amended by Specification Change Notices (“SCN’s”) for installation of following engines:
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AIRCRAFT CONFIGURATION. The guarantees defined below (the “"Guarantees”") are applicable to the A319A320-100 200 Aircraft as described in the Standard Specification Ref. J D 000 01000 02000 Issue 6 7 dated 1st March 2007 equipped with:
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AIRCRAFT CONFIGURATION. The guarantees defined below (the “"Guarantees”") are applicable to the A319A330-100 300 Aircraft as described in the Standard Specification Ref. J G 000 01000 03000 Issue 6 7.5 dated 1st March 2007 equipped with:30th April 2008 and amended by SCN for
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