Common use of AIRCRAFT CONFIGURATION Clause in Contracts

AIRCRAFT CONFIGURATION. 5.1 The guarantees contained in this Attachment are based on the Aircraft configuration as defined in the original release of Detail Specification TBD (hereinafter referred to as the Detail Specification). Appropriate adjustment shall be made for changes in such Detail Specification approved by the Customer and Boeing or otherwise allowed by the Purchase Agreement which cause changes to the flight performance, sound levels, and/or weight and balance of the Aircraft. Such adjustment shall be accounted for by Boeing in its evidence of compliance with the guarantees. 5.2 The guarantee payloads of Paragraph 2.3.1 and 2.3.2 will be adjusted by Boeing for the effect of the following on OEW and the Manufacturer’s Empty Weight guarantee of Section 3 will be adjusted by Boeing for the following in its evidence of compliance with the guarantees: (1) Changes to the Detail Specification or any other changes mutually agreed upon between the Customer and Boeing or otherwise allowed by the Purchase Agreement. (2) The difference between the component weight allowances given in Appendix IV of the Detail Specification and the actual weights.

AIRCRAFT CONFIGURATION. 5.1 4.1 The guarantees contained in this Attachment are based on the Aircraft configuration as defined in the original release of Detail Specification TBD D019A001X1A38P-1 Revision C (hereinafter referred to as the Detail Specification). Appropriate adjustment shall be made for changes in such Detail Specification approved by the Customer and Boeing or otherwise allowed by the Purchase Agreement which cause changes to the flight performance, sound levels, performance and/or weight and balance of the Aircraft. Such adjustment shall be accounted for by Boeing in its evidence of compliance with the guarantees. 5.2 4.2 The guarantee payloads payload of Paragraph 2.3.1 and 2.3.2 2.5.1 will be adjusted by Boeing for the effect of the following on OEW MEW and the Manufacturer’s Empty Weight guarantee of Section 3 will be adjusted by Boeing for the following in its evidence of compliance with the guarantees: (1) Changes to the Detail Specification or any other changes mutually agreed upon between the Customer and Boeing or otherwise allowed by the Purchase Agreement. (2) The difference between the component weight allowances given in Appendix IV of the Detail Specification and the actual weights.

AIRCRAFT CONFIGURATION. 5.1 4.1 The guarantees contained in this Attachment are based on the Aircraft configuration as defined in Boeing Document ****, Revison N, **** dated April 15, 2014, plus any changes mutually agreed to or otherwise allowed by the Purchase Agreement to be incorporated into the original release of the Customer’s Detail Specification TBD (hereinafter referred to as the Detail Specification). Appropriate adjustment shall be made for changes in such Detail Specification approved by the Customer and Boeing or otherwise allowed by the Purchase Agreement which cause changes to the flight performance, sound levels, performance and/or weight and balance of the Aircraft. Such adjustment shall be accounted for by Boeing in its evidence of compliance with the guarantees. 5.2 4.2 The guarantee payloads of Paragraph 2.3.1 and 2.3.2 will be adjusted by Boeing for the effect of the following on OEW and the Manufacturer’s Empty Weight guarantee of Section 3 will be adjusted by Boeing for the following in its evidence of compliance with the guarantees: (1) Changes to the Detail Specification or any other changes mutually agreed upon between the Customer and Boeing or otherwise allowed by the Purchase Agreement. (2) The difference between the component weight allowances given in Appendix IV E of the Detail Specification and the actual weights. 4.3 GEnx series engines include any offerable thrust rating with a common xxxx of materials. Compliance with the guarantees is not dependent on the thrust rating chosen.

AIRCRAFT CONFIGURATION. 5.1 4.1 The guarantees contained in this Attachment are based on the Aircraft configuration as defined in the original release of Detail Specification TBD D019A001XIA38P-3 (hereinafter referred to as the Detail Specification). Appropriate adjustment shall be made for changes in such Detail Specification approved by the Customer and Boeing or otherwise allowed by the Purchase Agreement which cause changes to the flight performance, sound levels, performance and/or weight and balance of the Aircraft. Such adjustment shall be accounted for by Boeing in its evidence of compliance with the guarantees. 5.2 4.2 The guarantee payloads payload of Paragraph 2.3.1 and 2.3.2 2.5.1 will be adjusted by Boeing for the effect of the following on OEW MEW and the Manufacturer’s 's Empty Weight guarantee of Section 3 will be adjusted by Boeing for the following in its evidence of compliance with the guarantees: (1) Changes to the Detail Specification or any other changes mutually agreed upon between the Customer and Boeing or otherwise allowed by the Purchase Agreement. (2) The difference between the component weight allowances given in Appendix IV of the Detail Specification and the actual weights.

AIRCRAFT CONFIGURATION. 5.1 The guarantees contained in this Attachment are based on the Aircraft configuration as defined in the original release of Detail Specification TBD (hereinafter referred to as the Detail Specification). Appropriate adjustment shall be made for changes in such Detail Specification approved by the Customer and Boeing or otherwise allowed by the Purchase Agreement which cause changes to the flight performance, sound levels, and/or weight and balance of the Aircraft. Such adjustment shall be accounted for by Boeing in its evidence of compliance with the guarantees. 5.2 The guarantee payloads payload of Paragraph 2.3.1 and 2.3.2 will be adjusted by Boeing for the effect of the following on OEW and the Manufacturer’s Empty Weight guarantee of Section 3 will be adjusted by Boeing for the following in its evidence of compliance with the guarantees: (1) Changes to the Detail Specification or any other changes mutually agreed upon between the Customer and Boeing or otherwise allowed by the Purchase Agreement. (2) The difference between the component weight allowances given in Appendix IV of the Detail Specification and the actual weights.

AIRCRAFT CONFIGURATION. 5.1 4.1 The guarantees contained in this Attachment are based on the Aircraft configuration as defined in the original release of Detail Specification TBD D019A001XIA38P-2 (hereinafter referred to as the Detail Specification). Appropriate adjustment shall be made for changes in such Detail Specification approved by the Customer and Boeing or otherwise allowed by the Purchase Agreement which cause changes to the flight performance, sound levels, performance and/or weight and balance of the Aircraft. Such adjustment shall be accounted for by Boeing in its evidence of compliance with the guarantees. 5.2 4.2 The guarantee payloads payload of Paragraph 2.3.1 and 2.3.2 2.5.1 will be adjusted by Boeing for the effect of the following on OEW MEW and the Manufacturer’s 's Empty Weight guarantee of Section 3 will be adjusted by Boeing for the following in its evidence of compliance with the guarantees: (1) Changes to the Detail Specification or any other changes mutually agreed upon between the Customer and Boeing or otherwise allowed by the Purchase Agreement. (2) The difference between the component weight allowances given in Appendix IV of the Detail Specification and the actual weights.

AIRCRAFT CONFIGURATION. 5.1 4.1 The guarantees contained in this Attachment are based on the Aircraft configuration as defined in the original release of Detail Specification TBD (hereinafter referred to as the Detail Specification). Appropriate adjustment shall be made for changes in such Detail Specification approved by the Customer and Boeing or otherwise allowed by the Purchase Agreement which cause changes to the flight performance, sound levels, performance and/or weight and balance of the Aircraft. Such adjustment shall be accounted for by Boeing in its evidence of compliance with the guarantees. 5.2 4.2 The guarantee payloads of Paragraph 2.3.1 and 2.3.3 and the specified payloads of Paragraph 2.3.2 and 2.3.4 block fuel guarantees will be adjusted by Boeing for the effect of the following on OEW and the Manufacturer’s Empty Weight guarantee of Section 3 will be adjusted by Boeing for the following in its evidence of compliance with the guarantees: (1) Changes to the Detail Specification or any other changes mutually agreed upon between the Customer and Boeing or otherwise allowed by the Purchase Agreement. (2) The difference between the component weight allowances given in Appendix IV of the Detail Specification and the actual weights.

AIRCRAFT CONFIGURATION. 5.1 The guarantees contained in this Attachment are based on the Aircraft configuration as defined in the original release of Detail Specification TBD (hereinafter referred to as the Detail Specification). Appropriate adjustment shall be made for changes in such Detail Specification approved by the Customer and Boeing or otherwise allowed by the Purchase Agreement which cause changes to the flight performance, sound levels, and/or weight and balance of the Aircraft. Such adjustment shall be accounted for by Boeing in its evidence of compliance with the guarantees. 5.2 The guarantee payloads of Paragraph 2.3.1 2.3.1, 2.3.2, and 2.3.2 2.3.3 will be adjusted by Boeing for the effect of the following on OEW and the Manufacturer’s Empty Weight guarantee of Section 3 will be adjusted by Boeing for the following in its evidence of compliance with the guarantees: (1) Changes to the Detail Specification or any other changes mutually agreed upon between the Customer and Boeing or otherwise allowed by the Purchase Agreement. (2) The difference between the component weight allowances given in Appendix IV of the Detail Specification and the actual weights.

AIRCRAFT CONFIGURATION. 5.1 4.1 The guarantees contained in this Attachment are based on the Aircraft configuration as defined in the original release Revision C of Detail Specification TBD D019A001GOT38P-1 (hereinafter referred to as the Detail Specification). Appropriate adjustment shall be made for changes in such Detail Specification approved by the Customer and Boeing or otherwise allowed by the Purchase Agreement which cause changes to the flight performance, sound levels, performance and/or weight and balance of the Aircraft. Such adjustment shall be accounted for by Boeing in its evidence of compliance with the guarantees.. Attachment to Letter Agreement No. 6-1162-DME-1153 CFM56-7B27/B1 Engines Page 5 5.2 4.2 The guarantee payloads of Paragraph 2.3.1 and 2.3.2 will be adjusted by Boeing for the effect of the following on OEW and the Manufacturer’s 's Empty Weight guarantee of Section 3 will be adjusted by Boeing for the following in its evidence of compliance with the guarantees: (1) Changes to the Detail Specification or any other changes mutually agreed upon between the Customer and Boeing or otherwise allowed by the Purchase Agreement. (2) The difference between the component weight allowances given in Appendix IV of the Detail Specification and the actual weights.

AIRCRAFT CONFIGURATION. 5.1 The guarantees contained in this Attachment are based on the Aircraft configuration as defined in the original release of Detail Specification TBD D019A001ASA39E-1 (hereinafter referred to as the Detail Specification). Appropriate adjustment shall be made for changes in such Detail Specification approved by the Customer and Boeing or otherwise allowed by the Purchase Agreement which cause changes to the flight performance, sound levels, and/or weight and balance of the Aircraft. Such adjustment shall be accounted for by Boeing in its evidence of compliance with the guarantees. 5.2 The guarantee payloads of Paragraph 2.3.1 and 2.3.2 will be adjusted by Boeing for the effect of the following on OEW and the Manufacturer’s 's Empty Weight guarantee of Section 3 will be adjusted by Boeing for the following in its evidence of compliance with the guarantees: (1) Changes to the Detail Specification or any other changes mutually agreed upon Attachment to Letter Agreement 6-1162-SCR-112 CFM56-7B26E Engines Page #PageNum# between the Customer and Boeing or otherwise allowed by the Purchase Agreement. (2) The difference between the component weight allowances given in Appendix IV of the Detail Specification and the actual weights.

AIRCRAFT CONFIGURATION. 5.1 6.1 The guarantees contained in this Attachment are arc based on the Aircraft configuration as defined in the original release of Detail Specification TBD (hereinafter referred to as the Detail Specification). Appropriate adjustment shall be made for changes in such Detail Specification approved by the Customer and Boeing or otherwise allowed by the Purchase Agreement which cause changes to the flight performance, sound levels, performance and/or weight and balance of the Aircraft. Such adjustment shall be accounted for by Boeing in its evidence of compliance with the guarantees. 5.2 6.2 The guarantee payloads of Paragraph 2.3.1 2.1.1, 2.1.3, 2.1.5, and 2.3.2 2.1.7 and the specified payloads of the guarantee block fuels of Paragraphs 2.1.2, 2.1.4, 2.1.6, and 2.1.8 will be adjusted by Boeing for the effect of the following on OEW and the Manufacturer’s Empty Weight guarantee of Section 3 will be adjusted by Boeing for the following in its evidence of compliance with the guarantees: (1) Changes to the Detail Specification or any other changes mutually agreed upon between the Customer and Boeing or otherwise allowed by the Purchase Agreement. (2) The difference between the component weight allowances given in Appendix IV of the Detail Specification and the actual weights.