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:
AIRCRAFT CONFIGURATION. 4.1. The guarantees contained in this Attachment are based on the Aircraft configuration as defined in the original release of Detail Specification D019U002 (hereinafter referred to as the Detail Specification). Appropriate adjustment shall be made for changes in such Detail Specification approved by the Buyer and Boeing or otherwise allowed by the Purchase Agreement which cause changes to the flight 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. 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 including Change Requests, Master Changes, Change Orders or any other changes mutually agreed upon between the Buyer 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. The guarantees defined below ("the Guarantees") are applicable to the A319-100 Aircraft as described in the Technical Specification ***, as amended by a Specification Change Notices ("SCN's") for i) implementation of CFM International CFM56-5B7/P engines
AIRCRAFT CONFIGURATION. The guarantees defined in Paragraphs 2 and 3 below (the “Guarantees”) are applicable to the A319 Aircraft as described in the A319 Standard Specification ***** as amended by the ***** SCNs including:
(iii) hereinafter referred to as the “Specification” without taking into account any further changes thereto as provided in the Agreement except as provided in Paragraph 6 below (for purposes of this Letter Agreement No. 6C the “A319 Aircraft”).
AIRCRAFT CONFIGURATION. The guarantees defined below (the "Guarantees") are applicable to the A330-300 aircraft (the “Aircraft” for the purpose of this Appendix 1) as described in the Technical Specification ***, as amended by the Specification Change Notices for:
(i) installation of GENERAL ELECTRIC CF6-80E1A4 engines; and
(ii) without taking into account any further changes thereto as provided in the Purchase Agreement (the “Specification” for the purpose of this Appendix 1).
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. 2.1 The initial configuration of Customer's Model Aircraft has been defined by Boeing 737-7, 737-8, 737-8200, 737-9, 737-10 Airplane Description Document No. *** dated *** as described in Article 1 and Exhibit A of the Purchase Agreement (Initial Configuration). Final configuration of the 737-10 Aircraft (Final Configuration) will be completed using the then-current Boeing configuration documentation in accordance with the following schedule:
2.1.1 No later than *** prior to the first 737-10 Aircraft's scheduled delivery, Boeing and Customer will discuss potential *** features.
2.1.2 Within *** after that meeting, Boeing will provide Customer with a proposal for those *** features that can be incorporated into the 737-10 Aircraft during production.
2.1.3 Customer will then have *** to accept or reject the *** features.
2.1.4 Within *** following Final Configuration, Boeing and Customer will execute a written amendment to the Purchase Agreement which will reflect the following:
2.1.4.1 Changes applicable to the basic Model 737-10 aircraft which are developed by Boeing between the date of signing of the Purchase Agreement and date of Final Configuration.
2.1.4.2 Incorporation into Exhibit A of the Purchase Agreement, by written amendment, those *** features which have been agreed to by Customer and Boeing (Customer Configuration Changes);
2.1.4.3 Revisions to the Supplemental Exhibit BFE1 to reflect the selection dates and on-dock dates of BFE;
2.1.4.4 Changes to the *** Features Prices, and *** to adjust for the difference, if any, between the prices estimated in Table 1 of the Purchase Agreement for *** features reflected in the *** and the actual prices of the *** features reflected in the Customer Configuration Changes. Such changes will not result in a *** to the *** provided in Table 1.
AIRCRAFT CONFIGURATION. 3.1 The guarantees contained in this Attachment are based on the Aircraft configuration as defined in Boeing Document ***, ***, 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 (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 and/or weight and balance of the Aircraft. Such adjustment shall be accounted for by Boeing in its evidence of compliance with the guarantees.
3.2 The guarantee payloads of Paragraph 2.4.1, 2.4.2, 2.4.4, and 2.4.5 and the specified payloads of Paragraph 2.4.3 and 2.4.6 block fuel guarantees will be adjusted by Boeing for the effect of the following on OEW 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 seat weight allowances to be incorporated into the Detail Specification and the actual weights.
AIRCRAFT CONFIGURATION. 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 and/or weight and balance of the Aircraft. Such adjustment shall be accounted for by Boeing in its evidence of compliance with the guarantees.
AIRCRAFT CONFIGURATION. The guarantees listed below are based on the CRJ-900 Aircraft configuration as defined in Bombardier Aerospace Type Specification RAD-690-100 issue NC, and equipped with GE CF34-8C5 engines as defined in GE Engines Performance Model L0073X. The weight data corresponds to the [***] lb ([***] ) MTOW design weight option. Appropriate adjustments shall be made for any changes in configuration of the Aircraft which have been approved by the Buyer and Bombardier Aerospace, Regional Aircraft ("Bombardier") or otherwise allowed by the Purchase Agreement and which cause changes to the performance of the Aircraft.
