Memorandum of Understanding for Sale of A320 Family Aircraft between Airbus S.A.S. and JetBlue Airways Corporation
This Memorandum of Understanding (MOU) is between Airbus S.A.S. and JetBlue Airways Corporation, outlining the main terms for JetBlue to potentially purchase various Airbus A320 family aircraft. The agreement covers aircraft specifications, pricing, delivery schedules, and customization options. It is not a binding purchase contract; final obligations depend on board approvals and execution of a definitive purchase agreement. Confidentiality and certain conditions apply until a formal contract is signed.

Contents | ||||
DEFINITIONS | 2 | |||
1. SCOPE | 7 | |||
2. STANDARD SPECIFICATION AND CUSTOMIZATION | 7 | |||
3. NEO OPTION AND RELATED MATTERS | 8 | |||
4. DELIVERY SCHEDULE, [***] AND RELATED MATTERS | 9 | |||
5. AIRCRAFT PRICING CONDITIONS | 11 | |||
6. [***] | 12 | |||
7. PAYMENTS | 12 | |||
8. OTHER PROVISIONS | 13 | |||
9. TIMELINE, CONDITIONS PRECEDENT AND SIGNATURES | 13 | |||
10 CONFIDENTIALITY | 14 | |||
11 LAW AND JURISDICTION | 14 | |||
12. ASSIGNMENT | 14 | |||
13. ENTIRE AGREEMENT | 14 | |||
14. MODIFICATIONS AND DISCLAIMERS OF RELIANCE | 15 | |||
15. COUNTERPARTS | 15 | |||
APPENDIX 1 AIRCRAFT PRICE SUMMARY | 17 | |||
APPENDIX 2 PRICE REVISION FORMULAE | 17 | |||
APPENDIX 3 CUSTOMIZATION | 17 | |||
APPENDIX 4 PERFORMANCE GUARANTEES | 17 |
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1.1 | The purpose of this memorandum of understanding (MOU) is to set out the basic new terms and conditions offered by AIRBUS to JETBLUE for (i) the purchase of the A320 Backlog Aircraft and the A321 Backlog Aircraft [***], currently contracted for under certain terms and conditions as fifty-two (52) A320 aircraft under the Existing PA and (ii) a new order requested by JETBLUE for forty (40) A320 NEO Aircraft [***]. The Aircraft are subject to the conditions set out in Paragraph 9. | ||
1.2 | JETBLUE and AIRBUS intend to enter into one or more new purchase agreements that will include the principles set out in this MOU and also amend and supersede the Existing PA with respect to the Backlog Aircraft in order to, among other things, cancel the Backlog Aircraft therein and set forth all new terms and conditions applicable to the Aircraft in one or more new purchase agreements (the Purchase Agreement), subject to Paragraph 9 below. |
A319 | A320 | A321 | ||||
Standard Specification | J.000.01000 Issue 6. March 1, 2007 | D.000.02000 Issue 7, March 1, 2007 | E.000.02000 Issue 4, March 1, 2007 | |||
Design Weights for Backlog Aircraft (MTOW/MLW/MZFW) | [***] | [***] | [***] | |||
Design Weights for A320 NEO and A321 Neo Aircraft (MTOW/MLW/MZFW) | See Paragraph 3.4 below | See Paragraph 3.4 below | See Paragraph 3.4 below |
2.1 | JETBLUE has selected the International Aero Engines for all the Backlog Aircraft. Paragraph 3.5 below describes the engine choices available for the NEO Aircraft. | ||
2.2 | Appendix 3 hereto further details the customized specification for the Aircraft. The Standard Specification, for the Aircraft as amended by Appendix 3 or otherwise amended after the date hereof by written agreement between AIRBUS and JETBLUE in the form of a specification change notice (SCN), shall be referred to as the Specification for the Aircraft. | ||
2.3 | The availability of Sharklets for A320 Backlog Aircraft and A321 Backlog Aircraft delivering in 2013 remains subject to industrial and certification constraints, provided however that each such Backlog Aircraft scheduled to deliver in 2013, shall be delivered with Sharklets in accordance with the schedule set forth herein or shall be delivered, at a minimum, with respect to A320 Backlog Aircraft, with full Sharklets provisions. | ||
2.4 | AIRBUS is considering turning certain items (including but not limited to galleys and galleys stowages), which are currently JETBLUE furnished equipment (BFE) in the Specification, into AIRBUS furnished equipment (SFE) and the parties agree that such BFE items, should they |
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become SFE, shall be [***]. The parties agree that should such BFE items become SFE items, the resulting new budget of the SCN and BFE for such items shall be [***]. |
3. | NEO OPTION AND RELATED MATTERS | ||
3.1 | AIRBUS also offers and Buyer shall purchase certain A320 family aircraft with a new engine option (the New Engine Option or NEO) applicable to the A319, A320, and A321 aircraft. The A320 family aircraft incorporating such NEO shall be referred to as the NEO Aircraft and the forty (40) incremental firm A320, A321 or A319 Aircraft ordered by JETBLUE pursuant to Paragraph 1 above shall be deemed NEO Aircraft. | ||
3.2 | The respective A319/A320/A321 NEO specifications shall be derived from the current A320 family specification, and are based on the new engines quoted below together with the required airframe structural adaptations as well as Aircraft systems and software adaptations required to operate such new engines | ||
3.3 | The NEO Aircraft specification shall incorporate the new large wingtip device (the Sharklets) currently designed by AIRBUS to enhance, among other things, the eco-efficiency and payload range performance of the A320 family aircraft. | ||
3.4 | The MLW and MZFW design weights shall be revised [***] to reflect the NEO as follows: |
A320-200 : MTOW: [***] | MLW: [***] (*) | MZFW : [***] (*) | ||
A321-200 : MTOW [***] | MLW: [***] (*) | MZFW : [***] (*) | ||
A319-100 : MTOW: [***] | MLW: [***] (*) | MZFW : [***] (*) |
(*): MLW and MZFW are indicative design weights representative of the NEO Aircraft. NEO design weights shall be updated with the final specification. |
3.5 | The NEO Aircraft will be equipped with a set of either of the engine models listed below. The engine type shall be selected by JETBLUE at its sole discretion and advised to AIRBUS by the time of signature of the Purchase Agreement [***]. Upon selection, each shall be referred to as Propulsion Systems. |
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Aircraft Type | CFMI Leap-X | PW 1100 G | ||
A319-100 NEO Aircraft | LEAP-X1A24 AET (23,500 lbf) | PW1124G AET (23,500 lbf) | ||
A320-200 NEO Aircraft | LEAP-X1A26 AET (26,300 lbf) | PW1127G AET (26,300 lbf) | ||
A321-200 NEO Aircraft | LEAP-X1A32 AET (32,100 lbf) | PW1133G AET (32,100 lbf) |
AET means Airbus Equivalent Thrust |
3.6 | Each of the three (3) A320 family NEO airframe types (A319, A320, A321) are planned to be manufactured and certified by AIRBUS with each engine manufacturer (CFM and Pratt & Whitney) and each engine type and with revised design weight variants. | |
The first airframe / engine brand combination to be certified no later than shall be a NEO Aircraft of the A320 type. Further airframe/engine brand combinations will be determined by Airbus in light of commercial and industrial requirements. | ||
Other airframe / engine combinations certification shall follow in sequence, with the objective to complete all firmly ordered airframe / engine combinations certification no later than [***]. | ||
3.7 | Appendix 3 hereto further details the customized specification for the A320, A321 and A319 NEO Aircraft. |
(i) | The Aircraft shall be ready for delivery to JETBLUE at the respective Aircrafts final assembly line according to the following scheduled delivery periods (the Scheduled Delivery Periods), provided that the first row setting forth the Existing PA schedule is provided purely for reference purposes. |
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2011 | 2012 | 2013 | 2014 | 2015 | 2016 | 2017 | 2018 | 2019 | 2020 | 2021 | Total | |||||||||||||||||||||||||||||||||||||
Existing PA order A320 | 1 [***] | 7 ([***] | ) | 7 | 12 | 15 | 10 | | | | | 52 | ||||||||||||||||||||||||||||||||||||
New firm delivery schedule Backlog Aircraft | 1 A320 | 7 A320 | 4 A320 3A321 ** | 9 A321 ** | 10 A321 ** | 2 A320 8 A321 ** | 8 A320 | 22 30 | ||||||||||||||||||||||||||||||||||||||||
40 A320neo Aircraft | | | | | | | [***]* | [***]* | [***] | [***] | [***] | 40 | ||||||||||||||||||||||||||||||||||||
Total New JBU | 1 | 7 | 7 | 9 | 10 | 10 | [***] | [***] | [***] | [***] | [***] | 92 |
* | Subject to NEO engine/airframe sequence of certification-schedule subject to change as per Paragraph 4.1 (iii) below | |
** | Subject to signature of SCNs, the [***] shall be delivered with [***] while the [***] shall be delivered with [***]. |
(ii) | The above delivery positions remain subject to prior sale or other disposition until fulfillment of the conditions set out in Paragraph 9 hereunder. | ||
(iii) | The delivery schedule indicated above in Paragraph 4.1(i) may be [***]. Provided that the conditions set forth in Paragraph 9 below are fulfilled, and subject to the provisions of this Paragraph 4.1 (iii), AIRBUS shall reserve [***] or JETBLUE the deliveries stated in Paragraph 4.1(i). |
(iv) | The Scheduled Delivery Periods are for Aircraft complying with the relevant Standard Specification and may be subject to review when the final Specification has been defined. Such Scheduled Delivery Periods will only be guaranteed if the Specification is finalized and BFE is received at dates consistent with the proposed Scheduled Delivery Periods. | |
(v) | AIRBUS and JETBLUE will, no later than [***]. | |
4.2 | [***] |
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5. | AIRCRAFT PRICING CONDITIONS | |
5.1 The detailed pricing for the Backlog Aircraft and the NEO Aircraft is attached as Appendix 1 hereto. All prices in Appendix 1 are (i) expressed in US dollars (ii) expressed in [***] delivery conditions, and (iii) subject to revision until delivery of the respective Aircraft in accordance with the Airbus Price Revision Formula, subject to Paragraph 6 below, the CFMI Price Revision Formula, the IAE Price Revision Formula or the PW Price Revision Formula, detailed in Appendix 2 attached hereto, as applicable. | ||
5.2 | The Base Price of Propulsion Systems pricing set forth in Appendix 1 for the Backlog Aircraft are computed from the IAE Reference Price as set forth in the IAE Price Revision Formula, attached hereto as Appendix 2, and will adjust up to the delivery of each respective Aircraft in accordance with such IAE Price Revision Formula. | |
5.3 | The Reference Price of Propulsion Systems for the NEO Aircraft as set forth in Appendix 1 will (i) adjust up to the delivery of each respective Aircraft in accordance with either the CFMI Price Revision Formula or the PW Price Revision Formula, as applicable and (ii) correspond to the thrust rating defined for the respective Propulsion Systems in Paragraph 3.5 and may be revised to reflect thrust rating adjustments upon final NEO specification freeze. | |
5.4 | All Purchase Incentives as set forth in Appendix 1 hereto (excluding [***]), shall be made available to JETBLUE [***] and will be [***]. Unless JETBLUE gives AIRBUS notice to the contrary at least ten (10) days before delivery of the relevant Aircraft, the applicable Purchase Incentives will [***]. | |
5.5 | The availability of the engines for all Aircraft is subject to the agreement of the engine manufacturer. It is understood that the engine base and reference prices set forth in Appendix 1 and the engine price revision formulae set forth in Appendix 2 are based upon information received from the engine manufacturer and remain subject to modifications as may be issued from time to time by the engine manufacturer or any changes to the engine for these Aircraft. All engine concessions are for illustration purposes only, and subject to direct negotiation between JETBLUE and the engine manufacturers. | |
5.6 | The Final price of each Aircraft at delivery (the Final Aircraft Price) will be the sum of: |
(i) | the respective Airframe Base Price, adjusted to the date of delivery in accordance with the Airbus Price Revision Formula, | ||
(ii) | the base price of (a) the Irrevocable SCNs (New Engine Option and installation of Sharklets) and (b) the Master Charge Engine, applicable only to the CFMI Leap-X Propulsion Systems, included in this MOU or in the Purchase Agreement, and both |
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adjusted to the date of each Aircraft delivery in accordance with the Airbus Price Revision Formula, | |||
(iii) | the base price of all additional SCNs mutually agreed upon at or after signature of the MOU or Purchase Agreement and adjusted to the date of each Aircraft delivery in accordance with the Airbus Price Revision Formula, | ||
(iv) | the reference price of the applicable Propulsion Systems, as quoted by the relevant Propulsion Systems manufacturer to AIRBUS and adjusted to the date of Aircraft delivery in accordance with the relevant Propulsion Systems manufacturers price revision formula, and | ||
(v) | as the case may be, any amount from any other provisions of the Purchase Agreement and/or any other written between JETBLUE and AIRBUS. |
6. | [***] | |
7. | PAYMENTS | |
7.1 | [***] | |
In consideration of AIRBUS reserving for JETBLUE the terms and conditions, including the price conditions and deliveries, stated in this MOU, JETBLUE will pay to AIRBUS [***] per Aircraft (the [***]) (for an aggregate total of [***]. | ||
7.2 | Predelivery Payments | |
7.2.1 | AIRBUS and JETBLUE agree that, [***], the PDPs currently held by AIRBUS for the Backlog Aircraft under the Existing PA will be [***]. | |
7.2.2 | The Predelivery Payments for each Aircraft will amount to [***]. Such Predelivery Payments shall be paid to AIRBUS according to the following schedule: |
Payment Date | Amount | |
[***] | [***] * | |
On the first day of the month that is: | ||
[***] | [***] | |
[***] | [***] | |
[***] | [***] | |
TOTAL | [***] |
* | Total amount of [***] for A320 NEO Aircraft, pursuant to Paragraph 7.1 above. |
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8. | OTHER PROVISIONS |
8.1 | [***] | |
8.2 | WINGLET RETROFIT ON EXISTING FLEET OF A320-200 AIRCRAFT | |
AIRBUS will offer [***] to JETBLUE a certified winglet retrofit modification for its fleet of IAE powered in-service eligible A320-200 aircraft, [***], and for in-service availability no later than [***] (the Winglet Retrofit). If AIRBUS [***], then JETBLUE shall be entitled to terminate this MOU [***] by written notice to Airbus. | ||
8.3 | PRODUCT SUPPORT PACKAGE | |
AIRBUS will provide JETBLUE with a complete product support package for the Aircraft, including warranties, spares support, training (including the provision of A320/A321 aircraft differential data package), technical field support and A320 Backlog Aircraft, A321 Backlog Aircraft, and A320 NEO Aircraft performance guarantees. This product support package will be included in the Purchase Agreement. | ||
The performance guarantees for the A320 Backlog Aircraft and the A321 Backlog Aircraft will be substantially similar in scope and content as set forth in the performance guarantee for A320 Aircraft in the Existing PA also adjusted to reflect the A320 Backlog Aircraft Specification. | ||
The performance guarantees for the A320 NEO Aircraft will be substantially similar in scope and content as set forth in Appendixes 4A and 4B to this MOU. |
9. | TIMELINE, CONDITIONS PRECEDENT AND SIGNATURES | |
9.1 | Unless this MOU has been executed and delivered by both parties together with receipt by AIRBUS of [***] as set forth in Paragraph 7 above [***]) by June 21, 2011 (the Expiration Date), this MOU shall be deemed withdrawn and invalid. |
9.2 | (i) | This MOU, other than the confidentiality obligations and the terms of this Paragraph 9, will remain subject to (i) AIRBUS and JETBLUE s corporate and board approvals and (ii) execution of an Amendment to the Existing PA rescheduling certain Backlog Aircraft, both by no later than June 21, 2011 (the Amendment). Upon fulfillment of both (i) and (ii), this MOU shall become binding between JETBLUE and AIRBUS and |
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not subject to any other condition precedent except as set forth in Paragraph 9.2 (iii) below. Thereupon, [***], subject to Paragraph 9.2(iii), below. |
(ii) | After execution of this MOU, the parties will also work in good faith to execute the Purchase Agreement by [***]. Notwithstanding the foregoing, the Parties acknowledge that failure to agree upon certain customary and material provisions in the Purchase Agreement after good faith negotiations, including but not limited to (i) liquidated damages (ii) performance guarantees, and (iii) warranties, shall give either Party the right to terminate by [***], this MOU without penalty or further obligation to the other Party, provided that [***]. | ||
(iii) | Notwithstanding anything to the contrary in this MOU, in the event AIRBUS [***] within the timeline described in Paragraph 8.2 above , then JETBLUE shall be entitled to terminate this MOU as set forth therein above. | ||
(iv) | In the event of a termination in accordance with Paragraph 8.2 above, this MOU will then automatically and concurrently be null and void, except that (a) AIRBUS will [***], and (b) the parties agree that the Amendment will remain valid and in full force and effect, and all other terms and conditions applicable to the Backlog Aircraft shall, passim, be deemed to have remained in effect as set forth in the Existing PA prior to signature of this MOU and the parties shall undertake any such steps necessary to give effect to such reinstatement. |
10 | CONFIDENTIALITY | |
This MOU is subject to the terms contained in Clause 22.5 of the Existing PA. | ||
11 | LAW AND JURISDICTION | |
This MOU and the rights and obligations of the Parties will be governed by and construed in accordance with the laws of the State of New York. Any dispute arising hereunder will be referred to the Federal or State courts located in the Borough of Manhattan, New York City, New York, and each of the Parties irrevocably submits to and accepts such jurisdiction. | ||
It is agreed that the United Nations Convention on Contracts for the International Sale of Goods will not apply to this MOU or to the agreements contemplated herein. | ||
12. | ASSIGNMENT | |
The terms and conditions of this MOU may not be assigned by either Party to any third party without prior written consent of the other Party. | ||
13. | ENTIRE AGREEMENT |
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This MOU constitutes the complete proposal by AIRBUS to JETBLUE with respect to the potential sale of the Aircraft that are the subject hereof. This MOU supersedes any previous issues, understandings, commitments or representations whatsoever, whether oral or written, in respect thereto with respect to the subject matter contained herein. This MOU when executed will become fully binding to the extent provided in Section 9 hereof and constitute the entire agreement between the Parties (other than as provided in the immediately preceding Paragraph) and shall not be amended except by an instrument in writing of even date herewith or subsequent hereof executed by both Parties. | ||
14. | MODIFICATIONS AND DISCLAIMERS OF RELIANCE | |
This MOU may not be amended or modified except in a writing signed by both Parties. The Parties disclaim, to the maximum extent permitted by law, any reliance upon any oral statements, acts, or omissions. | ||
15. | COUNTERPARTS | |
This MOU may be executed by the Parties hereto in separate counterparts, each of which when so executed and delivered will be an original, but all such counterparts will together constitute one and the same instrument. Such counterparts may be delivered via facsimile and/or electronic mail (provided that an original is subsequently delivered). |
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AGREED AND ACCEPTED | ||||||||||
JETBLUE AIRWAYS CORPORATION | AIRBUS S.A.S. | |||||||||
By: | /s/ Dave Barger | By: | /s/ John J. Leahy | |||||||
Its: | Chief Executive Officer | Its: | Chief Operating Officer, Customers |
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A319 | Backlog Aircraft | |
A319 | NEO Aircraft | |
A320 | Backlog Aircraft | |
A320 | NEO Aircraft | |
A321 | Backlog Aircraft | |
A321 | NEO Aircraft |
PART 1 | AIRBUS PRICE REVISION FORMULA | |
PART 2 | CFMI PRICE REVISION FORMULA | |
PART 3 | IAE PRICE REVISION FORMULA | |
PART 4 | PW PRICE REVISION FORMULA |
A320 | BACKLOG AIRCRAFT | |
A320 | NEO AIRCRAFT | |
A321 | BACKLOG AIRCRAFT | |
A321 | NEO AIRCRAFT |
APPENDIX 4B A320 NEO PERFORMANCE GUARANTEE/PW
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1.1 | Base Prices | |
The base prices (Airframe Base Price, SCN Budget, New Engine Option NEO, Sharklets, and Master Charge Engine) and the airframe purchase incentives ([***]) defined in Paragraph 5 and Appendix 1 to this MOU are subject to adjustment for changes in economic conditions as measured by data obtained from the US Department of Labor, Bureau of Labor Statistics and in accordance with the provisions hereof. | ||
1.2 | Base Period | |
The base prices have been established in accordance with the average economic conditions prevailing in December 2008, January 2009, February 2009 and corresponding to a theoretical delivery in January 2010 as defined by ECIb and ICb index values indicated hereafter. | ||
1.3 | Indexes | |
Labor Index: Employment Cost Index for Workers in Aerospace manufacturing hereinafter referred to as ECI336411W, quarterly published by the US Department of Labor, Bureau of Labor Statistics, in NEWS, and found in: Table 9, WAGES and SALARIES (not seasonally adjusted): Employment Cost Indexes for Wages and Salaries for private industry workers by industry and occupational group, or such other name that may be from time to time used for the publication title and/or table, (Aircraft manufacturing, NAICS Code 336411, base month and year December 2005 = 100). | ||
The quarterly value released for a certain month (March, June, September and December) shall be the one deemed to apply for the two (2) preceding months. | ||
Index code for access on the Web site of the US Bureau of Labor Statistics: CIU2023211000000I. | ||
Material Index: Industrial Commodities (hereinafter referred to as IC) as published in PPI Detailed report (found in Table 6. Producer price indexes and percent changes for commodity groupings and individual items not seasonally adjusted or such other names that may be from time to time used for the publication title and/or table). (Base Year 1982 = 100). | ||
Index code for access on the Web site of the US Bureau of Labor Statistics: WPU03THRU15. |
24
1.4 | Revision Formula | |
[***] |
1.5.1 | Rounding | |
The Labor Index average and the Material Index average shall be computed to the first decimal. If the next succeeding place is five (5) or more, the preceding decimal place shall be raised to the next higher figure. | ||
Each quotient shall be rounded to the nearest then thousandth (4 decimals). If the next succeeding place is five (5) or more, the preceding decimal place shall be raised to the next higher figure. | ||
The final factor shall be rounded to the nearest ten thousandth (4 decimals). | ||
The final price shall be rounded to the nearest whole number (0.5 or more rounded to 1). | ||
1.5.2 | Substitution of Indexes for Airbus Price Revision Formula | |
If; |
(i) | the United States Department of Labor substantially revises the methodology of calculation of the Labor Index or the Material Index as used in the Airbus Price Revision Formula, or | ||
(ii) | the United States Department of Labor discontinues, either temporarily or permanently, such Labor Index or such Material Index, or | ||
(iii) | the data samples used to calculate such Labor Index or such Material Index are substantially changed; | ||
AIRBUS shall select a substitute index for inclusion in the Airbus Price Revision Formula (the Substitute Index). | |||
The Substitute Index shall reflect as closely as possible the actual variance of the Labor Costs or of the material costs used in the calculation of the original Labor Index or Material Index as the case may be. | |||
As a result of the selection of the Substitute Index, AIRBUS shall make an appropriate adjustment to the Airbus Price Revision Formula to combine the successive utilization of the original Labor Index or Material Index (as the case may be) and of the Substitute Index. |
1.5.3 | Final Index Values |
25
The index values as defined in Clause 1.4. hereof shall be considered final and no further adjustment to the basic prices as revised at delivery of the Aircraft shall be made after Aircraft delivery for any subsequent changes in the published index values. | ||
1.5.4 | Limitation | |
Should the sum [***]. |
26
PART 2 CFM INTERNATIONAL PRICE REVISION FORMULA (APPLICABLE TO ENGINES ON A320 NEO AND A321 NEO AIRCRAFT) |
2.1 | Reference Price of the Propulsion Systems | |
The Reference Price for a set of two (2) CFM INTERNATIONAL LEAP-X series engines is as follows: |
US$[***] (US dollars [***] for LEAP X1A24 | |||
US$[***] (US dollars [***]) for LEAP-X1A26 | |||
US$[***] (US dollars [***]) for LEAP-X1A32 |
This Reference Price applies to the Engine type as specified in the MOU. | ||
This Reference Price is subject to adjustment for changes in economic conditions as measured by data obtained from the US Department of Labor, Bureau of Labor Statistics and in accordance with the provisions of Clauses 2.4 and 2.5 hereof. | ||
2.2 | Reference Period | |
The Reference Price for a set of two (2) CFM INTERNATIONAL LEAP-X series engines has been established in accordance with the economic conditions prevailing for a theoretical delivery in [***] as defined by CFM INTERNATIONAL by the Reference Composite Price Index (CPI) [***]. | ||
2.3 | Indexes | |
Labor Index: Employment Cost Index for Workers in Aerospace manufacturing hereinafter referred to as ECI336411W, quarterly published by the US Department of Labor, Bureau of Labor Statistics, in NEWS, and found in: Table 9, WAGES and SALARIES (not seasonally adjusted): Employment Cost Indexes for Wages and Salaries for private industry workers by industry and occupational group, or such other name that may be from time to time used for the publication title and/or table, (Aircraft manufacturing, NAICS Code 336411, base month and year December 2005 = 100 , hereinafter multiplied by [***] and rounded to the first decimal place). | ||
The quarterly value released for a certain month (March, June, September and December) shall be the one deemed to apply for the two preceding months. | ||
Index code for access on the Web site of the US Bureau of Labor Statistics: CIU2023211000000I |
27
Material Index: Industrial Commodities (hereinafter referred to as IC) as published in PPI detailed report (found in Table 6. Producer price indexes and percent changes for commodity groupings and individual items not seasonally adjusted or such other names that may be from time to time used for the publication title and/or table). (Base Year 1982 = 100). Index code for access on the Web site of the US Bureau of Labor Statistics: WPU03THRU15. |
2.4 | Revision Formula | |
[***] | ||
2.5 | General Provisions | |
2.5.1 | Roundings |
(i) | The Material index average ([***]) shall be rounded to the nearest second decimal place and the labor index average ([***]) shall be rounded to the nearest first decimal place. | ||
(ii) | [***] shall be rounded to the nearest second decimal place. | ||
(iii) | The final factor ([***]) shall be rounded to the nearest third decimal place. |
If the next succeeding place is five (5) or more, the preceding decimal place shall be raised to the next higher figure. After final computation [***] shall be rounded to the nearest whole number (0.5 rounds to 1). |
2.5.2 | Final Index Values | |
The revised Reference Price at the date of Aircraft Delivery shall not be subject to any further adjustments in the indexes. | ||
2.5.3 | Interruption of Index Publication | |
If the US Department of Labor substantially revises the methodology of calculation or discontinues any of these indexes referred to hereabove, AIRBUS shall reflect the substitute for the revised or discontinued index selected by CFM INTERNATIONAL, such substitute index to lead in application to the same adjustment result, insofar as possible, as would have been achieved by continuing the use of the original index as it may have fluctuated had it not been revised or discontinued. | ||
Appropriate revision of the formula shall be made to accomplish this result. | ||
2.5.4 | Annulment of the Formula |
28
Should the above escalation provisions become null and void by action of the US Government, the Reference Price shall be adjusted due to increases in the costs of labor and materiel which have occurred from the period represented by the applicable Reference Composite Price Index to the twelfth (12th) month prior to the scheduled month of Aircraft Delivery. | ||
2.5.5 | Limitation | |
Should the ratio [***]. |
29
PART 3 | INTERNATIONAL AERO ENGINES PRICE REVISION FORMULA (APPLICABLE TO ENGINES ON ALL BACKLOG AIRCRAFT) |
3.1 | Reference Price of Propulsion Systems | |
The Reference Price for a set of two (2) INTERNATIONAL AERO ENGINES is as follows: |
US$[***] (US dollars [***]) for V2524-A5 series Engines, | |||
US$[***] (US dollars [***]) for V2527-A5 series Engines and | |||
USD [***] (US dollars [***]) for V2533-A5 series Engines. |
This Reference Price applies to the Engine type as specified in the MOU. | ||
This Reference Price is subject to adjustment for changes in economic conditions as measured by data obtained from the US Department of Labor, Bureau of Labor Statistics, and in accordance with the provisions hereof. | ||
3.2 | Reference Period | |
The above Reference Price has been established in accordance with the averaged economic conditions prevailing in June 2005, July 2005 and August 2005 (delivery conditions January 2006), as defined, according to INTERNATIONAL AERO ENGINES by the ECIb and ICb, index values indicated in Clause 3.4. hereof. | ||
3.3 | Indexes | |
Labor Index: Employment Cost Index for Workers in Aerospace manufacturing hereinafter referred to as ECI336411W, quarterly published by the US Department of Labor, Bureau of Labor Statistics, in NEWS, and found in: Table 9, WAGES and SALARIES (not seasonally adjusted): Employment Cost Indexes for Wages and Salaries for private industry workers by industry and occupational group, or such other name that may be from time to time used for the publication title and/or table, (Aircraft manufacturing, NAICS Code 336411, base month and year December 2005 = 100). | ||
The quarterly value released for a certain month (March, June, September and December) shall be the one deemed to apply for the two preceding months. | ||
Index code for access on the Web site of the US Bureau of Labor Statistics: CIU2023211000000I | ||
Material Index: Industrial Commodities (hereinafter referred to as IC) as published in PPI detailed report (found in Table 6. Producer price indexes and percent changes for |
30
commodity groupings and individual items not seasonally adjusted or such other names that may be from time to time used for the publication title and/or table). (Base Year 1982 = 100). | ||
Index code for access on the Web site of the US Bureau of Labor Statistics: WPU03THRU15. | ||
3.4 | Revision Formula | |
[***] |
31
3.5 | General Provisions | |
3.5.1 | Roundings |
(i) | [***] and [***] shall be calculated to the nearest tenth (1 decimal). | ||
(ii) | Each quotient ([***]) shall be calculated to the nearest ten-thousandth (4 decimals). | ||
(iii) | The final factor shall be rounded to the nearest ten-thousandth (4 decimals). |
If the next succeeding place is five (5) or more the preceding decimal place shall be raised to the nearest higher figure. | ||
After final computation [***] shall be rounded to the nearest whole number (0.5 rounds to 1). | ||
3.5.2 | Final Index Values | |
The revised Reference Price at the date of Aircraft delivery shall be the final price and shall not be subject to any further adjustments in the indexes. | ||
If no final index values are available for any of the applicable month, the then published preliminary figures shall be the basis on which the Revised Reference Price shall be computed. | ||
3.5.3 | Interruption of Index Publication | |
If the US Department of Labor substantially revises the methodology of calculation or discontinues any of these indexes referred to hereabove, AIRBUS shall reflect the substitute for the revised or discontinued index selected by INTERNATIONAL AERO ENGINES, such substitute index to lead in application to the same adjustment result, insofar as possible, as would have been achieved by continuing the use of the original index as it may have fluctuated had it not been revised or discontinued. | ||
Appropriate revision of the formula shall be made to accomplish this result. | ||
3.5.4 | Annulment of Formula | |
Should the above escalation provisions become null and void by action of the US Government, the Reference Price shall be adjusted due to increases in the costs of labor and materiel which have occurred from the period represented by the applicable Reference Price Indexes to the fifth (5th), sixth (6th) and seventh (7th) month prior to the scheduled Aircraft delivery. |
32
3.5.5 | Limitation | |
Should the revised Reference Price [***], the final price shall be [***]. |
33
PART 4 | PRATT AND WHITNEY PRICE REVISION FORMULA (APPLICABLE TO ENGINES ON A320 NEO AND A321 NEO AIRCRAFT) |
4.1 | Reference Price of the Propulsion Systems |
US$[***] (US dollars [***]) for PW1124G, | |||
US$[***] (US dollars [***]) for PW1127G, and | |||
US$[***] (US dollars [***]) for PW1133G. |
The Reference Price is subject to adjustment for changes in economic conditions as measured by data obtained from the US Department of Labor, Bureau of Labor Statistics, and in accordance with the provisions hereof. |
4.2 | Base Period |
The Reference Price has been established in accordance with the average economic conditions prevailing in December 2008, January 2009, February 2009 and corresponding to a theoretical delivery in January 2010 as defined by ECIb, ICb and C10b index values indicated hereafter. |
4.3 | Indexes |
Labor Index: Employment Cost Index for Workers in Aerospace manufacturing hereinafter referred to as ECI336411W, quarterly published by the US Department of Labor, Bureau of Labor Statistics, in NEWS, and found in Table 9, WAGES and SALARIES (not seasonally adjusted): Employment Cost Indexes for Wages and Salaries for private industry workers by industry and occupational group, or such other name that may be from time to time used for the publication title and/or table, (Aircraft manufacturing, NAICS Code 336411, base month and year December 2005 = 100). | |||
The quarterly value released for a certain month (March, June, September and December) shall be the one deemed to apply for the two preceding months. | |||
Index code for access on the Web site of the US Bureau of Labor Statistics: CIU2023211000000I. | |||
Material Index: Industrial Commodities (hereinafter referred to as IC) as published in PPI Detailed Report (found in Table 6. Producer Price indexes and percent changes for |
34
commodity and service groupings and individual items not seasonally adjusted or such other names that may be from time to time used for the publication title and/or table). (Base Year 1982 = 100). | |||
Index code for access on the Web site of the US Bureau of Labor Statistics: WPU03THRU15 | |||
Metal Index: Metals and metal products Code 10 (hereafter referred to as C10) as published in PPI Detailed Report (found in Table 6. Producer Price indexes and percent changes for commodity and service groupings and individual items not seasonally adjusted or such other names that may be from time to time used for the publications title and/or table). (Base 1982 = 100). | |||
Index code for access on the Web site of the US Bureau of Labor Statistics: WPU10. |
4.4 | Revision formula |
[***] |
4.5 | General Provisions |
4.5.1 | Roundings | |
The Labor Index average, the Material Index average, and the Metal Index average shall be computed to the first decimal. If the next succeeding place is five (5) or more, the preceding decimal place shall be raised to the next higher figure. | ||
Each quotient ([***]), ([***]) and ([***]) shall be rounded to the nearest ten-thousandth (4 decimals). If the next succeeding place is five (5) or more, the preceding decimal place shall be raised to the next higher figure. | ||
The final factor shall be rounded to the nearest ten-thousandth (4 decimals). | ||
The final price shall be rounded to the nearest whole number (0.5 or more rounded to 1). |
4.5.2 | Substitution of Indexes for Price Revision Formula |
If: |
(i) | the United States Department of Labor substantially revises the methodology of calculation of the Labor Index , the Material Index, or the Metal Index as used in the Price Revision Formula, or |
35
(ii) | the United States Department of Labor discontinues, either temporarily or permanently, such Labor Index , such Material Index, or such Metal Index, or | ||
(iii) | the data samples used to calculate such Labor Index , such Material Index, or such Metal Index are substantially changed; |
Pratt and Whitney shall select a substitute index for inclusion in the Price Revision Formula (the Substitute Index) and AIRBUS shall reflect such Substitute Index. | |||
The Substitute Index shall reflect as closely as possible the actual variance of the labor costs, of the material costs, or of the metal costs used in the calculation of the original Labor Index, Material Index, or Metal Index as the case may be. | |||
As a result of the selection of the Substitute Index, an appropriate adjustment to the Price Revision Formula shall be performed, to combine the successive utilization of the original Labor Index, Material Index or Metal Index (as the case may be) and of the Substitute Index. |
36
4.5.3 | Final Index Values |
The Index values as defined in Clause 4 above shall be considered final and no further adjustment to the adjusted Reference Price as revised at Aircraft Delivery (or payment of such revised amounts, as the case may be) shall be respectively made after Aircraft Delivery (or payment of such adjusted amounts, as the case may be) for any subsequent changes in the published Index values. |
4.5.4 | Limitation |
Should the sum of [***]. |
APPENDIX 3 |
issue 7.0 dated 1st March 2007
A320-200 SCNs | Estimated BFE Budget | |||||||
[***] | [***] | |||||||
ATA | TITLE | per aircraft | per aircraft | Comments | ||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] |
37
A320-200 SCNs | Estimated BFE Budget | |||||||
[***] | [***] | |||||||
ATA | TITLE | per aircraft | per aircraft | Comments | ||||
[***] | [***] | [***] | [***] | [***] | ||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
57-00 | Installation of sharklets | [***] | Subject to industrial and certification constraints | |||||
72-00 | A320-200 engine selection V2527-A5 at 25,400 lbf | (**) | [***] | |||||
TOTAL OF SCNS AND ESTIMATED BFE BUDGET $US DC01/2010 PER AIRCRAFT | [***] | [***] |
38
It may differ from the nominal thrust that will be eventually indicated by the engine manufacturer.
39
dated 1st March 2007
A320-200 NEO | ||||
SCN Budget | ||||
[***] | ||||
ATA | TITLE | per aircraft | ||
[***] | [***] | [***] | ||
57-00 | Installation of sharklets | [***] | ||
72-00 | A320-200 NEO engine selection : CFMI LEAP-X1A26 at 26,300 lbf (**) or PW PW1127G at 26,300 lbf (**) | [***] | ||
TOTAL OF IRREVOCABLE SCNS [***] PER AIRCRAFT | [***] |
40
A320-200 NEO | Estimated | |||||||
SCN Budget | BFE Budget | |||||||
[***] | [***] | |||||||
ATA | TITLE | per aircraft | per aircraft | Comments | ||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | [***] | ||||
[***] | [***] | [***] | [***] | [***] | ||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | [***] | ||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] |
41
A320-200 NEO | Estimated | |||||||
SCN Budget | BFE Budget | |||||||
[***] | [***] | |||||||
ATA | TITLE | per aircraft | per aircraft | Comments | ||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | |||||
53-40 | [***] | [***] | [***] |
42
A320-200 NEO | Estimated | |||||||
SCN Budget | BFE Budget | |||||||
[***] | [***] | |||||||
ATA | TITLE | per aircraft | per aircraft | Comments | ||||
TOTAL OF ADDITIONAL SCNS AND ESTIMATED BFE BUDGET [***] PER AIRCRAFT | [***] | [***] | ||||||
GRAND TOTAL SCN AND BFE BUDGET FOR A320-200 EQUIPPED WITH NEO [***] PER AIRCRAFT | [***] | [***] |
[***] | ||
(**) : | The indicated thrust is the Airbus Equivalent Thrust at Mach number 0.25 / ISA +15C / sea level thrust divided by 0.8 (representative of sea level aircraft performance). |
43
dated 1st March 2007
Estimated | ||||||||
BFE Budget | ||||||||
A321-200 SCNs | [***] | |||||||
[***] | per | |||||||
ATA | TITLE | per aircraft | aircraft | Comments | ||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | [***] | ||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] |
44
Estimated | ||||||||
BFE Budget | ||||||||
A321-200 SCNs | [***] | |||||||
[***] | per | |||||||
ATA | TITLE | per aircraft | aircraft | Comments | ||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
57-00 | Installation of sharklets | [***] | Subject to industrial and certification contraints | |||||
72-00 | A321-200 engine selection V2533-A5 at 31,700 lbf (**) | [***] | ||||||
TOTAL OF SCNS AND ESTIMATED BFE BUDGET [***] PER AIRCRAFT | [***] | [***] |
[***] | ||
(**) | : The indicated thrust is the Airbus Equivalent Thrust at Mach number 0.25 / ISA +15C / sea level thrust divided by 0.8 (representative of sea level aircraft performance). |
45
A321-200 SCNs | Estimated BFE Budget | |||||||
[***] | [***] | |||||||
ATA | TITLE | per aircraft | per aircraft | Comments | ||||
[***] | ETOPS 120mn requirement | [***] | [***] |
46
A321-200
issue 4.0 dated 1st
March 2007
A321-200 NEO | ||||
SCN Budget | ||||
[***] | ||||
ATA | TITLE | per aircraft | ||
[***] | [***] | [***] | ||
57-00 | Installation of sharklets | [***] | ||
72-00 | A321-200 NEO engine selection : CFMI LEAP-X1A32 at 32,100 lbf (**) or PW PW1133G at 32,100 lbf (**) | [***] | ||
TOTAL OF IRREVOCABLE SCNS [***] PER AIRCRAFT | [***] |
47
A321-200 NEO | Estimated | |||||||
BFE Budget | ||||||||
SCN Budget | [***] | |||||||
ATA | TITLE | [***] per aircraft | per aircraft | Comments | ||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | [***] | ||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] |
48
A321-200 NEO | Estimated | |||||||
BFE Budget | ||||||||
SCN Budget | [***] | |||||||
ATA | TITLE | [***] per aircraft | per aircraft | Comments | ||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | ||||||
[***] | [***] | [***] | [***] | |||||
[***] | [***] | [***] | [***] | |||||
TOTAL OF ADDITIONAL SCNS AND ESTIMATED BFE BUDGET - [***] PER AIRCRAFT | [***] | [***] | ||||||
GRAND TOTAL SCN AND BFE BUDGET FOR A321-200 EQUIPPED WITH NEO - [***] PER AIRCRAFT | [***] | [***] |
[***] | ||
(**) | : The indicated thrust is the Airbus Equivalent Thrust at Mach number 0.25 / ISA +15C / sea level thrust divided by 0.8 (representative of sea level aircraft performance). |
A321-200 NEO | Estimated | |||||||
BFE Budget | ||||||||
SCN Budget | [***] | |||||||
ATA | TITLE | [***] per aircraft | per aircraft | Comments | ||||
[***] | [***] | [***] | [***] |
49
118-29 Queens Blvd
Forest Hills, New-York 11375
1 | AIRCRAFT CONFIGURATION | |
The guarantees defined in Paragraphs 2 and 3 below (the Guarantees) are applicable to the A320 Aircraft as described in the A320 Standard Specification D 000 02000 Issue 7 dated 1st March 2007 as amended by SCNs for: | ||
i) NEO aircraft configuration | ||
ii) installation of CFM LEAP-X1A26 engines | ||
iii) the following design weights: |
Maximum Take-Off Weight (MTOW) [***] | |||
Maximum Landing Weight (MLW) [***] | |||
Maximum Zero Fuel Weight (MZFW) [***] |
hereinafter referred to as the Specification without taking into account any further changes thereto as provided in the Agreement. |
2 | [***] |
8 | UNDERTAKING REMEDIES | |
Should the A320 Aircraft fail to meet any of the Guarantees specified in this Letter Agreement the Seller [***]. |
AIRBUS S.A.S. | ||||
By: | ||||
Title: | ||||
JETBLUE AIRWAYS | ||||
By: | ||||
Title: | ||||
118-29 Queens Blvd
Forest Hills, New-York 11375
1 | AIRCRAFT CONFIGURATION | |
The guarantees defined in Paragraphs 2 and 3 below (the Guarantees) are applicable to the A320 Aircraft as described in the A320 Standard Specification D 000 02000 Issue 7 dated 1st March 2007 as amended by SCNs for: | ||
i)NEO aircraft configuration | ||
ii)installation of Pratt and Whitney PW1127G engines | ||
iii)the following design weights: | ||
Maximum Take-Off Weight (MTOW) [***] | ||
Maximum Landing Weight (MLW) [***] | ||
Maximum Zero Fuel Weight (MZFW) [***] | ||
hereinafter referred to as the Specification without taking into account any further changes thereto as provided in the Agreement. | ||
2 | [***] |
8 | UNDERTAKING REMEDIES | |
Should the A320 Aircraft fail to meet any of the Guarantees specified in this Letter Agreement [***] |
AIRBUS S.A.S. | ||||
By: | ||||
Title: | ||||
JETBLUE AIRWAYS | ||||
By: | ||||
Title: | ||||