Document:

EX-10.51

 Exhibit 10.51 

AMENDMENT NO. 7 
 to the

 A320 Family Aircraft Purchase Agreement 

made July 20, 2011 

between 
 AIRBUS S.A.S.

 and 
 AMERICAN
AIRLINES, INC. 
 This Amendment No. 7 to the A320 Family Purchase Agreement made July 20, 2011 (as amended, supplemented or
otherwise modified, hereinafter referred to as the “Amendment”), entered into as of November 25, 2014, by and between AIRBUS S.A.S., a société par actions simplifiée, created and existing
under French law having its registered office at 1 Rond-Point Maurice Bellonte, 31707 Blagnac-Cedex, France and registered with the Toulouse Registre du Commerce under number RCS Toulouse 383 474 814 (the “Seller”), and
AMERICAN AIRLINES, INC., a Delaware corporation having its principal office at 4333 Amon Carter Boulevard, Fort Worth, Texas 76155, United States of America (the “Buyer”). 

WITNESSETH: 
 WHEREAS, the Buyer
and the Seller entered into an Airbus A320 Family Aircraft Purchase Agreement, made July 20, 2011, which, together with all Exhibits, Appendices and Letter Agreements attached thereto and as amended, modified or supplemented from time to time
is hereinafter called the “Agreement”. 
 WHEREAS, the Buyer and the Seller have agreed to modify certain terms relating to
amended performance guarantees and new engine models; 
 NOW, THEREFORE, IT IS AGREED AS FOLLOWS: 

The capitalized terms used herein and not otherwise defined in this Amendment will have the meanings assigned to them in the Agreement. The
terms “herein,” “hereof,” and “hereunder” and words of similar import refer to this Amendment. 

  

			
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	2.	 PERFORMANCE GUARANTEES 

  

	2.1	 Letter Agreement No. 11A is deleted in its entirety and replaced with the Amended and Restated Letter Agreement No. 11A attached hereto.

  

	2.2	 Letter Agreement No. 11C is deleted in its entirety and replaced with the Amended and Restated Letter Agreement No. 11C attached hereto.

  

	2.3	 The attached Letter Agreement No. 11C-1 is hereby added to and made a part of the Agreement. 

 

	2.4	 Letter Agreement No. 11D is deleted in its entirety and replaced with the Amended and Restated Letter Agreement No. 11D attached hereto.

  

	2.5	 Letter Agreement No. 11J is deleted in its entirety and replaced with the Amended and Restated Letter Agreement No. 11J attached hereto.

  

	2.6	 Letter Agreement No. 11K is deleted in its entirety and replaced with the Amended and Restated Letter Agreement No. 11K attached hereto.

  

	2.7	 The attached Letter Agreement No. 11K-1 is hereby added to and made a part of the Agreement. 

 

	2.8	 Letter Agreement No. 11L is deleted in its entirety and replaced with the Amended and Restated Letter Agreement No. 11L attached hereto.

  

	2.9	 Upon the [*CTR], [*CTR] Performance Guarantees for the following aircraft as soon as reasonably practicable (but in no event [*CTR]): (i) A319
NEO Aircraft Performance Guarantees – [*CTR]; (ii) A319 NEO Aircraft Performance Guarantees – [*CTR]; (iii) A321 NEO Aircraft Performance Guarantees – [*CTR]; (iv) A321 NEO Aircraft Performance Guarantees – [*CTR];
(iv) A321 NEO Aircraft Performance Guarantees – [*CTR]. [*CTR] the Performance Guarantees at the [*CTR] the Performance Guarantees [*CTR]. Notwithstanding the foregoing, [*CTR] any such Performance Guarantees [*CTR]. 

 

	3.	 ASSIGNMENT 

This Amendment and the rights and obligations of the parties will be subject to the provisions of Clause 21 of the Agreement.

  

	4.	 CONFIDENTIALITY 

Each of the Seller and the Buyer agree not to disclose the terms and conditions of this Amendment to any person without the
prior written consent of the other party. Notwithstanding the foregoing, each of the Seller and the Buyer agrees that such terms and conditions may be disclosed without such prior written consent to (i) as required by law or as necessary in
connection with the enforcement of such party’s rights hereunder, and (ii) to the board of directors, managers, employees, auditors, and legal, financial and technical advisors of each party. 

  

			
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	11.	 COUNTERPARTS 

This Amendment 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 but one and the same instrument. 

  

			
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 If the foregoing correctly sets forth your understanding, please execute the original and one
(1) copy hereof in the space provided below and return a copy to the Seller. 
  

			
	 Very truly yours,

	
	AIRBUS S.A.S.
		
	 By:
		 /s/ Airbus S.A.S

			Name: Airbus S.A.S
			Title: Senior Vice President Contracts

 Accepted and Agreed: 
  

			
	 AMERICAN AIRLINES, INC.

		
	 By:
		 /s/ American Airlines, Inc.

			 Name: American Airlines, Inc.

			 Title: Vice President, Fleet Planning

  

			
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 AMENDED AND RESTATED 

LETTER AGREEMENT NO. 11A 
 TO A320
FAMILY AIRCRAFT PURCHASE AGREEMENT 
 Dated as of July 20, 2011 

November 25, 2014 
 American
Airlines, Inc. 
 4333 Amon Carter Boulevard 

Fort Worth, Texas 76155 
 Re:
A319 AIRCRAFT PERFORMANCE GUARANTEE – CFM CFM56-5B6/3 ENGINES 
 Dear Ladies and Gentlemen, 

American Airlines, Inc. (the “Buyer”) and Airbus S.A.S. (the “Seller”) have entered into an A320 Family
Aircraft Purchase Agreement dated as of July 20, 2011 (as supplemented and amended by the other letter agreements, and as otherwise supplemented, amended or modified from time to time, the “Agreement”) which covers, among other
matters, the sale by the Seller and the purchase or lease by the Buyer of certain Aircraft, under the terms and conditions set forth in said Agreement. The Buyer and the Seller have agreed to set forth in this Amended and Restated Letter Agreement
No. 11A (this “Letter Agreement”) certain additional terms and conditions regarding the sale and lease of the Aircraft. Letter Agreement No. 11A dated as of July 20, 2011 to the Agreement is hereby amended and
restated to read in its entirety as set forth herein. 
 Capitalized terms used herein and not otherwise defined in this Letter Agreement
have the meanings assigned thereto in the Agreement. The terms “herein,” “hereof” and “hereunder” and words of similar import refer to this Letter Agreement. 

Both parties agree that this Letter Agreement will constitute an integral, nonseverable part of said Agreement, that the provisions of said
Agreement are hereby incorporated herein by reference, and that this Letter Agreement will be governed by the provisions of said Agreement, except that if the Agreement and this Letter Agreement have specific provisions which are inconsistent, the
specific provisions contained in this Letter Agreement will govern. 

  

			
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	1	 AIRCRAFT CONFIGURATION 

The guarantees defined in Paragraphs 2, 3, 4 and 5 below (the “Guarantees”) are applicable to the A319
Aircraft as described in the A319 Standard Specification [*CTR] for: 
  

	1.1	 Basic Configuration (not applicable to Paragraph 3.2) 

  

	 	i)	 [*CTR] 

  

	 	ii)	 [*CTR] 

  

	 	iii)	 the following design weights: 

  

			
	 Maximum Take-Off Weight (MTOW)
	  	 [*CTR]

	 Maximum Landing Weight (MLW)
	  	 [*CTR]

	 Maximum Zero Fuel Weight (MZFW)
	  	 [*CTR]

  

	1.2	 Optional Configuration 

  

	 	i)	 [*CTR] 

  

	 	ii)	 [*CTR] 

  

	 	iii)	 the following design weights: 

  

			
	 Maximum Take-Off Weight (MTOW)
	  	 [*CTR]

	 Maximum Landing Weight (MLW)
	  	 [*CTR]

	 Maximum Zero Fuel Weight (MZFW)
	  	 [*CTR]

 hereinafter referred to as the “Specification” without taking into account any
further changes thereto as provided in the Agreement. 
  

	2	 GUARANTEED PERFORMANCE 

  

	2.1	 Take-Off 

  

	2.1.1	 Take-Off Field Length 

The FAR approved Take-Off Field Length at an A319 Aircraft gross weight of [*CTR] at the start of ground run at sea level
pressure altitude in [*CTR] be not more than: 
  

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	2.1.2	 Take-Off Weight 

When the A319 Aircraft is operated in departure airport conditions [(*CTR)] as follows: 

 

					
	 Pressure altitude
	  	 	: [*CTR]	  
	 Temperature
	  	 	: [*CTR]	  
	 Take-Off Run Available (TORA)
	  	 	: [*CTR]	  
	 Take-Off Distance Available (TODA)
	  	 	: [*CTR]	  

  

			
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	 Accelerate Stop Distance Available (ASDA)
	  	 	: [*CTR]	  
	 Slope
	  	 	: [*CTR]	  
	 Wind
	  	 	: [*CTR]	  
	 Obstacles
	  	 	: [*CTR]	  
	 (height and distance from beginning of TORA)
	  	 	: [*CTR]	  

 the FAR approved Take-Off Weight of the A319 Aircraft at the start of ground run shall be not
less than: 
  

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	2.2	 Landing Field Length 

The FAR approved dry Landing Field Length at an A319 Aircraft gross weight of [*CTR] at sea level pressure altitude shall benot
more than: 
  

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	3	 MISSION GUARANTEES 

  

	3.1	 Mission Payload [*CTR] 

The A319 Aircraft will be capable of carrying a Payload of not less than 

 

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 [(*CTR)] 
  

	3.1.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.1.2	 An allowance of [*CTR] 

  

	3.1.3	 An allowance of [*CTR] 

  

	3.1.4	 [*CTR] 

  

	3.1.5	 An allowance of [*CTR] 

  

	3.1.6	 An allowance of [*CTR] 

  

	3.1.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.1.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

			
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	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.2	 Mission Payload [*CTR] 

The A319 Aircraft will be capable of carrying a Payload of not less than 

 

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 [*CTR] 
  

	3.2.1	 The departure airport conditions [(*CTR)] are as follows: 

 

					
	 Pressure altitude
	  	 	: [*CTR]	  
	 Temperature
	  	 	: [*CTR]	  
	 Take-Off Run Available (TORA)
	  	 	: [*CTR]	  
	 Take-Off Distance Available (TODA)
	  	 	: [*CTR]	  
	 Accelerate-Stop Distance Available (ASDA)
	  	 	: [*CTR]	  
	 Slope
	  	 	: [*CTR]	  
	 Wind
	  	 	: [*CTR]	  
	 Obstacle
	  	 	: [*CTR]	  
	 (height and distance from beginning of TORA)
	  			

 The destination airport conditions are such as to allow the required Landing Weight to be used
without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.2.2	 An allowance of [*CTR] 

  

	3.2.3	 An allowance of [*CTR] 

  

	3.2.4	 [*CTR] 

  

	3.2.5	 An allowance of [*CTR] 

  

	3.2.6	 An allowance of [*CTR] 

  

	3.2.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.2.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

			
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	3.3	 Mission Block Fuel 

In carrying a fixed payload of [*CTR] of the A319 Aircraft will be not more than 

 

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 when the A319 Aircraft is operated as defined here below. 

 

	3.3.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.3.2	 An allowance of [*CTR] 

  

	3.3.3	 An allowance of [*CTR] 

  

	3.3.4	 [*CTR] 

  

	3.3.5	 An allowance of [*CTR] 

  

	3.3.6	 An allowance of [*CTR] 

  

	3.3.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.3.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.4	 The Mission Payload and Block Fuel guarantees are based on an estimated fixed Operating Weight Empty of [*CTR] (see Appendix A).

  

	4	 MANUFACTURER’S WEIGHT EMPTY GUARANTEE 

The Seller guarantees a Manufacturer’s Weight Empty of the A319 Aircraft as defined in Paragraph 1 above of not more than

  

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 This is the Manufacturer’s Weight Empty of the A319 Aircraft as defined in
Section 13-10 of the A319 Standard Specification as amended by the SCN’s defined in Paragraph 1 above and which will be derived from the weighing of the A319 Aircraft and subject to adjustment as defined in the Paragraph 8 below. 

 

	5	 NOISE GUARANTEE 

  

	5.1	 Noise Certification 

The A319 Aircraft [*CTR] 

[*CTR] 

  

			
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	5.2	 [*CTR] Noise 

The A319 Aircraft [*CTR] 

This guarantee applies for the following conditions: 
  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

							
	 Station
	  	 Distance from

[*CTR] threshold

(m)
	  	 Sideline Distance to

runway extended

centerline

(m)
	  	 Height above

ground

(m)

	 [*CTR]
	  	[*CTR]	  	[*CTR]	  	[*CTR]
	 [*CTR]
	  	[*CTR]	  	[*CTR]	  	[*CTR]

 This guarantee does not apply to the [*CTR]. 

This guarantee is based on [*CTR]. 
  

	5.3	 Interior Noise in Flight 

  

	5.3.1	 Cockpit 

At a pressure altitude of [*CTR] the guaranteed A-weighted Sound Pressure Level (SPL) and the Speech Interference Level (SIL)
shall be as follows: 
  

			
	 	  	Guarantee
	 SPL [dB(A)]
	  	[*CTR]
	 SIL [dB]
	  	[*CTR]

 Noise levels shall be measured at the Captain’s and First Officer’s seat position at
head level with normal cockpit air conditioning and ventilation in operation. 
  

	5.3.2	 Cabin 

At a pressure altitude of [*CTR] the guaranteed A-weighted Sound Pressure Level (SPL) and the Speech Interference Level (SIL)
shall be as follows: 
  

					
	 	  	 	  	Guarantee
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
		  	SIL [dB]	  	[*CTR]
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
	  	SIL [dB]	  	[*CTR]

 Noise levels shall be measured at a height of [*CTR] above the passenger compartment floor on
the aisle center lines in the passenger seated area. 

  

			
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	5.4	 Ramp Noise 

The APU noise during ground operation of the A319 Aircraft [*CTR] 

[*CTR] 
  

	6	 GUARANTEE CONDITIONS 

  

	6.1	 The certification requirements for the A319 Aircraft, except where otherwise noted, will be as stated in Section 02 of the Specification.

  

	6.2	 For the determination of FAR take-off and landing performance [*CTR] 

When establishing take-off performance [*CTR] 
  

	6.3	 Climb, cruise and descent performance associated with the Guarantees will include [*CTR] 

Cruise performance at [*CTR] 
  

	6.4	 Where applicable the Guarantees assume the use of an approved fuel having a density of [*CTR] 

 

	6.5	 Sound levels are to be specified in decibels (dB), at a reference pressure of [*CTR] 

The definition of dB(A) shall be that specified as the “A-scale” weighting given in [*CTR] 

The Speech Interference Level (SIL) is defined as the [*CTR] 

 

	7	 GUARANTEE COMPLIANCE 

  

	7.1	 Compliance with the Guarantees will be demonstrated [*CTR] 

 

	7.2	 Compliance with the take-off and landing elements of the Guarantees will be demonstrated [*CTR] 

 

	7.3	 Compliance [*CTR] will be demonstrated [*CTR] 

  

	7.4	 Compliance with the Manufacturer’s Weight Empty guarantee will be demonstrated [*CTR] 

 

	7.5	 The [*CTR] will be used to demonstrate compliance with the guarantees of certification noise levels. 

The A319 Aircraft will have a [*CTR] 

  

			
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 Compliance with the interior noise and APU noise guarantees will be demonstrated
[*CTR] 
 [*CTR] 

The [*CTR] will be used to demonstrate compliance with the guarantee in Paragraph 5.2. 

 

	7.6	 Data [*CTR] will be adjusted as required [*CTR] accordance with established aeronautical practices to show compliance with the Guarantees.

  

	7.7	 The Seller undertakes to furnish the Buyer with [*CTR] demonstrating compliance with the Guarantees [*CTR] 

 

	8	 ADJUSTMENT OF GUARANTEES 

  

	8.1	 In the event of any change to any law, governmental regulation or requirement or interpretation thereof (“Rule Change”) by any
governmental agency made subsequent to the date of the Agreement and such Rule Change affects the A319 Aircraft configuration or performance or both required to obtain certification the Guarantees will be appropriately modified to reflect the effect
of any such change. 

  

	8.2	 The Guarantees apply to the A319 Aircraft as described in Paragraph 1 above and may be adjusted in the event of: 

 

	 	a)	 Any further configuration change which is the subject of an SCN 

 

	 	b)	 Changes required to obtain certification which cause changes to the performance or weight of the A319 Aircraft. 

 

	9	 EXCLUSIVE GUARANTEES 

The Guarantees are exclusive and are provided in lieu of any and all other performance and weight guarantees of any nature
which may be stated, referenced or incorporated in the Specification or any other document. 
  

	10	 UNDERTAKING REMEDIES 

  

	10.1	 Should the A319 Aircraft fail to meet any of the Guarantees specified in this Letter Agreement the Seller will [*CTR] 

[*CTR] 
  

	 	(i)	 [*CTR] 

  

	 	(ii)	 [*CTR] 

  

	 	(iii)	 [*CTR] 

  

	 	(iv)	 [*CTR] 

  

	10.2	 [*CTR] 

  

			
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	10.3	 The Seller’s maximum liability in respect of deficiency in performance of any A319 Aircraft will be [*CTR] 

 

	11	 DUPLICATE REMEDIES 

Except as provided in Paragraph 10, the remedies provided to the Buyer under this Guarantee are not cumulative of any other
remedies provided to the Buyer under any other warranty or guarantee contained in the Agreement and the Buyer will not be entitled to duplicate remedies with respect to any single defect or costs incurred for any single defect. 

 

	12	 ASSIGNMENT 

This Letter Agreement and the rights and obligations of the parties will be subject to the provisions of Clause 21 of the
Agreement; provided, however, this Letter Agreement may not be assigned by the Buyer under either Clause 21.5 or 21.6 without the express written consent of the Seller, which the Seller may withhold in its sole discretion. 

 

	13	 CONFIDENTIALITY 

This Letter Agreement is subject to the terms and conditions of Clause 22.11 of the Agreement. 

 

	14	 COUNTERPARTS 

This Letter Agreement 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. 

  

			
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 If the foregoing correctly sets forth your understanding, please execute the original and one
(1) copy hereof in the space provided below and return a copy to the Seller. 
  

			
	 Very truly yours,

	
	 AIRBUS S.A.S.

		
	 By:
	 	 /s/ Airbus S.A.S.

		 	 Name: Airbus S.A.S

		 	 Title: Senior Vice President Contracts

 Accepted and Agreed 
  

			
	 AMERICAN AIRLINES, INC.

		
	 By:
	 	 /s/ American Airlines, Inc.

		 	 Name: American Airlines, Inc.

		 	 Title: Vice President, Fleet Planning

  

			
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 APPENDIX A TO AMENDED AND RESTATED LETTER AGREEMENT NO. 11A 

 

			
	 Layout Number: [*CTR]
	  	 MTOW (lb): [*CTR]

	 Seating: [*CTR]
	  	 MLW (lb): [*CTR]

	 Total: [*CTR]
	  	 MZFW (lb): [*CTR]

  

					
	 	  	Weight (lb)	 
	 	  	 	 
	 Manufacturer’s Weight Empty Standard Specification [*CTR]
	  	 	[*CTR]	  
	 [*CTR]
	  	 	[*CTR]	  
	 Manufacturer’s Weight Empty (MWE) for the purpose of Paragraph 4
	  	 	[*CTR]	  
		
	 Cabin changes
	  	 	[*CTR]	  
	 [*CTR]
	  	 	[*CTR]	  
	 Manufacturer’s [*CTR] equipment [*CTR] and cargo hold fire extinguishers)
	  	 	[*CTR]	  
		  	  
	  
	 
	 Customized MWE
		 	[*CTR]	  
		
	 Operator’s Items
				
	 Unusable fuel
		 	[*CTR]	  
	 Oil for engines, IDG and APU
		 	[*CTR]	  
	 Water
		 	[*CTR]	  
	 Water tank precharge
		 	[*CTR]	  
	 Aircraft documents and tool kit
		 	[*CTR]	  
	 Passenger seats and lifejackets
		 	[*CTR]	  
	 Galley structure
		 	[*CTR]	  
	 Fixed equipment
		 	[*CTR]	  
	 Catering and removable equipment
		 	[*CTR]	  
	 Emergency equipment
		 	[*CTR]	  
	 Crew and crew baggage
		 	[*CTR]	  
		  	  
	  
	 
	 Total Operator’s Items
		 	[*CTR]	  
		
	 Operating Weight Empty (OWE) for the purpose of Paragraph 3
		 	[*CTR]	  

  

			
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 AMENDED AND RESTATED 

LETTER AGREEMENT NO. 11C 
 TO A320
FAMILY AIRCRAFT PURCHASE AGREEMENT 
 Dated as of July 20, 2011 

As of November 25, 2014 

American Airlines, Inc. 
 4333
Amon Carter Boulevard 
 Fort Worth, Texas 76155 

Re: A319 NEO AIRCRAFT PERFORMANCE GUARANTEE – PW1124G-JM ENGINES 

Dear Ladies and Gentlemen, 

American Airlines, Inc. (the “Buyer”) and Airbus S.A.S. (the “Seller”) have entered into an A320 Family
Aircraft Purchase Agreement dated as of July 20, 2011 (as supplemented and amended by the other letter agreements, and as otherwise supplemented, amended or modified from time to time, the “Agreement”) which covers, among other
matters, the sale by the Seller and the purchase or lease by the Buyer of certain Aircraft, under the terms and conditions set forth in said Agreement. The Buyer and the Seller have agreed to set forth in this Amended and Restated Letter Agreement
No. 11C (this “Letter Agreement”) certain additional terms and conditions regarding the sale and lease of the Aircraft. Letter Agreement No. 11C dated as of July 20, 2011 to the Agreement is hereby amended and
restated to read in its entirety as set forth herein. 
 Capitalized terms used herein and not otherwise defined in this Letter Agreement
have the meanings assigned thereto in the Agreement. The terms “herein,” “hereof” and “hereunder” and words of similar import refer to this Letter Agreement. 

Both parties agree that this Letter Agreement will constitute an integral, nonseverable part of said Agreement, that the provisions of said
Agreement are hereby incorporated herein by reference, and that this Letter Agreement will be governed by the provisions of said Agreement, except that if the Agreement and this Letter Agreement have specific provisions which are inconsistent, the
specific provisions contained in this Letter Agreement will govern. 

  

			
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	1	 AIRCRAFT CONFIGURATION 

The guarantees defined in Paragraphs 2, 3, 4 and 5 below (the “Guarantees”) are applicable to the A319 NEO Aircraft
as described in the A319 Standard Specification [*CTR] for: 
  

	1.1	 Basic Configuration (not applicable to Paragraph 3.2) 

  

	 	i)	 [*CTR] 

  

	 	ii)	 [*CTR] 

  

	 	iii)	 the following design weights: 

  

					
	 Maximum Take-Off Weight (MTOW)
	  	 	[*CTR]	  
	 Maximum Landing Weight (MLW)
	  	 	[*CTR]	  
	 Maximum Zero Fuel Weight (MZFW)
	  	 	[*CTR]	  

  

	1.2	 Optional Configuration 

  

	 	i)	 [*CTR] 

  

	 	ii)	 [*CTR] 

  

	 	iii)	 the following design weights: 

  

					
	 Maximum Take-Off Weight (MTOW)
	  	 	[*CTR]	  
	 Maximum Landing Weight (MLW)
	  	 	[*CTR]	  
	 Maximum Zero Fuel Weight (MZFW)
	  	 	[*CTR]	  

 hereinafter referred to as the “Specification” without taking into account any
further changes thereto as provided in the Agreement. 
  

	2	 GUARANTEED PERFORMANCE 

  

	2.1	 Take-Off 

  

	2.1.1	 Take-Off Field Length 

The FAR approved Take-Off Field Length at an A319 NEO Aircraft gross weight of [*CTR] at the start of ground run at sea level
pressure altitude in [*CTR] be not more than: 
  

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	2.1.2	 Take-Off Weight 

When the A319 NEO Aircraft is operated in departure airport conditions [*CTR] as follows: 

 

					
	 Pressure altitude
	  	 	: [*CTR]	  
	 Temperature
	  	 	: [*CTR]	  
	 Take-Off Run Available (TORA)
	  	 	: [*CTR]	  
	 Take-Off Distance Available (TODA)
	  	 	: [*CTR]	  
	 Accelerate Stop Distance Available (ASDA)
	  	 	: [*CTR]	  
	 Slope
	  	 	: [*CTR]	  
	 Wind
	  	 	: [*CTR]	  
	 Obstacles
	  	 	: [*CTR]	  
	 (height and distance from beginning of TORA)
	  	 	: [*CTR]	  

  

			
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 the FAR approved Take-Off Weight of the A319 NEO Aircraft at the start of ground
run shall be not less than: 
  

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	2.2	 Landing Field Length 

The FAR approved dry Landing Field Length at an A319 NEO Aircraft gross weight of [*CTR] at sea level pressure altitude shall
be not more than: 
  

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	3	 MISSION GUARANTEES 

  

	3.1	 Mission Payload [*CTR] 

The A319 NEO Aircraft will be capable of carrying a Payload of not less than 

 

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 [*CTR] 
  

	3.1.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.1.2	 An allowance of [*CTR] 

  

	3.1.3	 An allowance of [*CTR] 

  

	3.1.4	 [*CTR] 

  

	3.1.5	 An allowance of [*CTR] 

  

	3.1.6	 An allowance of [*CTR] 

  

	3.1.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.1.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

			
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	3.2	 Mission Payload [*CTR] 

The A319 NEO Aircraft will be capable of carrying a Payload of not less than 

 

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 [*CTR] 
  

	3.2.1	 The departure airport conditions [*CTR] are as follows: 

 

					
	 Pressure altitude
	  	 	: [*CTR]	  
	 Temperature
	  	 	: [*CTR]	  
	 Take-Off Run Available (TORA)
	  	 	: [*CTR]	  
	 Take-Off Distance Available (TODA)
	  	 	: [*CTR]	  
	 Accelerate-Stop Distance Available (ASDA)
	  	 	: [*CTR]	  
	 Slope
	  	 	: [*CTR]	  
	 Wind
	  	 	: [*CTR]	  
	 Obstacle
	  	 	: [*CTR]	  
	 (height and distance from beginning of TORA)
	  			

 The destination airport conditions are such as to allow the required Landing Weight to be used
without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.2.2	 An allowance of [*CTR] 

  

	3.2.3	 An allowance of [*CTR] 

  

	3.2.4	 [*CTR] 

  

	3.2.5	 An allowance of [*CTR] 

  

	3.2.6	 An allowance of [*CTR] 

  

	3.2.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.2.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.3	 Mission Block Fuel 

In carrying a fixed payload of [*CTR] of the A319 NEO Aircraft will be not more than 

 

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 when the A319 NEO Aircraft is operated as defined here below. 

 

	3.3.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.3.2	 An allowance of [*CTR] 

  

			
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	3.3.3	 An allowance of [*CTR] 

  

	3.3.4	 [*CTR] 

  

	3.3.5	 An allowance of [*CTR] 

  

	3.3.6	 An allowance of [*CTR] 

  

	3.3.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.3.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.4	 The Mission Payload and Block Fuel guarantees are based on an estimated fixed Operating Weight Empty of [*CTR] (see Appendix A).

  

	4	 MANUFACTURER’S WEIGHT EMPTY GUARANTEE 

The Seller guarantees a Manufacturer’s Weight Empty of the A319 NEO Aircraft as defined in Paragraph 1 above of not more
than 
  

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 This is the Manufacturer’s Weight Empty of the A319 NEO Aircraft as defined in
Section 13-10 of the A319 Standard Specification as amended by the SCN’s defined in Paragraph 1 above and which will be derived from the weighing of the A319 NEO Aircraft and subject to adjustment as defined in the Paragraph 8 below. 

 

	5	 NOISE GUARANTEE 

  

	5.1	 Noise Certification 

The A319 NEO Aircraft [*CTR] 

[*CTR] 
  

	5.2	 [*CTR] Noise 

The A319 NEO Aircraft [*CTR] 

This guarantee applies for the following conditions: 
  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

			
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	 Station
	  	 Distance

from [*CTR]

threshold

(m)
	  	 Sideline Distance to

runway extended

centerline

(m)
	  	 Height

above
 ground

(m)

	 [*CTR]
	  	[*CTR]	  	[*CTR]	  	[*CTR]
	 [*CTR]
	  	[*CTR]	  	[*CTR]	  	[*CTR]

 This guarantee does not apply to the [*CTR] 

This guarantee is based on [*CTR] 
  

	5.3	 Interior Noise in Flight 

  

	5.3.1	 Cockpit 

At a pressure altitude of [*CTR] the guaranteed A-weighted Sound Pressure Level (SPL) and the Speech Interference Level (SIL)
shall be as follows: 
  

			
	 	  	Guarantee
	 SPL [dB(A)]
	  	[*CTR]
	 SIL [dB]
	  	[*CTR]

 Noise levels shall be measured at the Captain’s and First Officer’s seat position at
head level with normal cockpit air conditioning and ventilation in operation. 
  

	5.3.2	 Cabin 

At a pressure altitude of [*CTR] shall be as follows: 

 

					
	 	  	 	  	Guarantee
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
		  	SIL [dB]	  	[*CTR]
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
		  	SIL [dB]	  	[*CTR]

 Noise levels shall be measured at a height of [*CTR] above the passenger compartment floor on
the aisle center lines in the passenger seated area. 
  

	5.4	 Ramp Noise 

The APU noise during ground operation of the A319 NEO Aircraft [*CTR] 

[*CTR] 
  

	6	 GUARANTEE CONDITIONS 

  

	6.1	 The certification requirements for the A319 NEO Aircraft, except where otherwise noted, will be as stated in Section 02 of the Specification.

  

			
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	6.2	 For the determination of FAR take-off and landing performance [*CTR] 

When establishing take-off performance [*CTR] 
  

	6.3	 Climb, cruise and descent performance associated with the Guarantees will include [*CTR] 

Where applicable the Guarantees assume the use of an approved fuel having a density of [*CTR] 

Sound levels are to be specified in decibels (dB), at a reference pressure of [*CTR] 

The definition of dB(A) shall be that specified as the “A-scale” weighting given in [*CTR] 

The Speech Interference Level (SIL) is defined as the [*CTR] 

 

	7	 GUARANTEE COMPLIANCE 

  

	7.1	 Compliance with the Guarantees will be demonstrated [*CTR] 

 

	7.2	 Compliance with the take-off and landing elements of the Guarantees will be demonstrated [*CTR] 

 

	7.3	 Compliance [*CTR] will be demonstrated [*CTR] 

  

	7.4	 Compliance with the Manufacturer’s Weight Empty guarantee will be demonstrated [*CTR] 

 

	7.5	 The [*CTR] will be used to demonstrate compliance with the guarantees of certification noise levels. 

The A319 NEO Aircraft will have a [*CTR] 

Compliance with the interior noise and APU noise guarantees will be demonstrated [*CTR] 

[*CTR] 
  

	7.6	 Data [*CTR] will be adjusted as required [*CTR] accordance with established aeronautical practices to show compliance with the Guarantees.

  

	7.7	 The [*CTR] will be used to demonstrate compliance with the guarantee in Paragraph 5.2. 

 

	7.8	 The Seller undertakes to furnish the Buyer with [*CTR] demonstrating compliance with the Guarantees [*CTR] 

 

	8	 ADJUSTMENT OF GUARANTEES 

  

	8.1	 In the event of any change to any law, governmental regulation or requirement or interpretation thereof (“Rule Change”) by any
governmental agency made subsequent to the date of the Agreement and such Rule Change affects the A319 NEO Aircraft configuration or performance or both required to obtain certification the Guarantees will be appropriately modified to reflect the
effect of any such change. 

  

	8.2	 The Guarantees apply to the A319 NEO Aircraft as described in Paragraph 1 above and may be adjusted in the event of: 

 

	 	a)	 Any further configuration change which is the subject of an SCN 

  

			
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	 	b)	 Changes required to obtain certification which cause changes to the performance or weight of the A319 NEO Aircraft. 

 

	9	 EXCLUSIVE GUARANTEES 

The Guarantees are exclusive and are provided in lieu of any and all other performance and weight guarantees of any nature
which may be stated, referenced or incorporated in the Specification or any other document. 
  

	10	 UNDERTAKING REMEDIES 

Should the A319 NEO Aircraft fail to meet any of the Guarantees specified in this Letter Agreement the Seller will [*CTR] 

 

	10.1	 [*CTR] 

  

	 	(i)	 [*CTR] 

  

	 	(ii)	 [*CTR] 

  

	 	(iii)	 [*CTR] 

  

	 	(iv)	 [*CTR] 

  

	10.2	 [*CTR] 

  

	10.3	 The Seller’s maximum liability in respect of deficiency in performance of any A319 NEO Aircraft will be [*CTR] 

 

	11	 DUPLICATE REMEDIES 

Except as provided in Paragraph 10, the remedies provided to the Buyer under this Guarantee are not cumulative of any other
remedies provided to the Buyer under any other warranty or guarantee contained in the Agreement and the Buyer will not be entitled to duplicate remedies with respect to any single defect or costs incurred for any single defect. 

 

	12	 ASSIGNMENT 

This Letter Agreement and the rights and obligations of the parties will be subject to the provisions of Clause 21 of the
Agreement; provided, however, this Letter Agreement may not be assigned by the Buyer under either Clause 21.5 or 21.6 without the express written consent of the Seller, which the Seller may withhold in its sole discretion. 

 

	13	 CONFIDENTIALITY 

This Letter Agreement is subject to the terms and conditions of Clause 22.11 of the Agreement. 

 

	14	 COUNTERPARTS 

This Letter Agreement 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. 

  

			
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 If the foregoing correctly sets forth your understanding, please execute the original and one
(1) copy hereof in the space provided below and return a copy to the Seller. 
  

			
	 Very truly yours,
  

AIRBUS S.A.S.

		
	 By:
	 	 /s/ Airbus S.A.S.

		 	 Name: Airbus S.A.S.

		 	 Title: Senior Vice President Contracts

  

			
	 Accepted and Agreed
  

AMERICAN AIRLINES, INC.

		
	 By:
	 	 /s/ American Airlines, Inc.

		 	 Name: American Airlines, Inc.

		 	 Title: Vice President, Fleet Planning

  

			
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 APPENDIX A TO LETTER AGREEMENT NO. 11C 

 

			
	 Layout Number: [*CTR]
	  	 MTOW (lb): [*CTR]

	 Seating: [*CTR]
	  	 MLW (lb): [*CTR]

	 Total: [*CTR]
	  	 MZFW (lb): [*CTR]

  

			
	 	  	Weight (lb)
	 Preliminary Manufacturer’s Weight Empty based on Standard Specification [*CTR]
	  	[*CTR]
	 Manufacturer’s Weight Empty (MWE) for the purpose of Paragraph 4
	  	[*CTR]
		
	 Cabin changes
	  	[*CTR]
	 [*CTR]
	  	[*CTR]
	 Manufacturer’s [*CTR] equipment [*CTR] and cargo hold fire extinguishers)
	  	[*CTR]
		  	  

	 Customized MWE
		[*CTR]
		
	 Operator’s Items
		
	 Unusable fuel
		[*CTR]
	 Oil for engines, IDG and APU
		[*CTR]
	 Water
		[*CTR]
	 Water tank precharge
		[*CTR]
	 Aircraft documents and tool kit
		[*CTR]
	 Passenger seats and lifejackets
		[*CTR]
	 Galley structure
		[*CTR]
	 Fixed equipment
		[*CTR]
	 Catering and removable equipment
		[*CTR]
	 Emergency equipment
		[*CTR]
	 Crew and crew baggage
		[*CTR]
		  	  

	 Total Operator’s Items
		[*CTR]
		
	 Operating Weight Empty (OWE) for the purpose of Paragraph 3
		[*CTR]

  

			
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 LETTER AGREEMENT NO. 11C-1 

TO A320 FAMILY AIRCRAFT PURCHASE AGREEMENT 

Dated as of July 20, 2011 
 As
of November 25, 2014 
 American Airlines, Inc. 

4333 Amon Carter Boulevard 
 Fort
Worth, Texas 76155 
 Re: A319 NEO AIRCRAFT PERFORMANCE GUARANTEE – PW1124G-JM ENGINES 

Dear Ladies and Gentlemen, 

American Airlines, Inc. (the “Buyer”) and Airbus S.A.S. (the “Seller”) have entered into an A320 Family
Aircraft Purchase Agreement dated as of July 20, 2011 (as supplemented and amended by the other letter agreements, and as otherwise supplemented, amended or modified from time to time, the “Agreement”) which covers, among other
matters, the sale by the Seller and the purchase or lease by the Buyer of certain Aircraft, under the terms and conditions set forth in said Agreement. The Buyer and the Seller have agreed to set forth in this Letter Agreement No. 11C-1 (this
“Letter Agreement”) certain additional terms and conditions regarding the sale and lease of the Aircraft. 
 Capitalized
terms used herein and not otherwise defined in this Letter Agreement have the meanings assigned thereto in the Agreement. The terms “herein,” “hereof” and “hereunder” and words of similar import refer to this Letter
Agreement. 
 Both parties agree that this Letter Agreement will constitute an integral, nonseverable part of said Agreement, that the
provisions of said Agreement are hereby incorporated herein by reference, and that this Letter Agreement will be governed by the provisions of said Agreement, except that if the Agreement and this Letter Agreement have specific provisions which are
inconsistent, the specific provisions contained in this Letter Agreement will govern. 

  

			
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	1	 AIRCRAFT CONFIGURATION 

The guarantees defined in Paragraphs 2, 3, 4 and 5 below (the “Guarantees”) are applicable to the A319 NEO
Aircraft as described in the A319 Standard Specification [*CTR] for: 
  

	1.1	 Basic Configuration (not applicable to Paragraph 3.2) 

  

	 	i)	 [*CTR] 

  

	 	ii)	 [*CTR] 

  

	 	iii)	 [*CTR] 

  

	 	iv)	 the following design weights: 

  

			
	 Maximum Take-Off Weight (MTOW)
	  	[*CTR]
	 Maximum Landing Weight (MLW)
	  	[*CTR]
	 Maximum Zero Fuel Weight (MZFW)
	  	[*CTR]

  

	1.2	 Optional Configuration 

  

	 	i)	 [*CTR] 

  

	 	ii)	 [*CTR] 

  

	 	iii)	 [*CTR] 

  

	 	iv)	 the following design weights: 

  

			
	 Maximum Take-Off Weight (MTOW)
	  	[*CTR]
	 Maximum Landing Weight (MLW)
	  	[*CTR]
	 Maximum Zero Fuel Weight (MZFW)
	  	[*CTR]

 hereinafter referred to as the “Specification” without taking into account any
further changes thereto as provided in the Agreement. 
 The Guarantees are valid for the A319 NEO Aircraft [*CTR] 

 

	2	 GUARANTEED PERFORMANCE 

  

	2.1	 Take-Off 

  

	2.1.1	 Take-Off Field Length 

The FAR approved Take-Off Field Length at an A319 NEO Aircraft gross weight of [*CTR] at the start of ground run at sea level
pressure altitude in [*CTR] be not more than: 
  

					
	 Nominal: [*CTR]
	 	Tolerance: [*CTR]	 	Guarantee: [*CTR]

  

	2.1.2	 Take-Off Weight 

  

			
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 When the A319 NEO Aircraft is operated in departure airport conditions [*CTR] as
follows: 
  

					
	 Pressure altitude
	  	 	: [*CTR]	  
	 Temperature
	  	 	: [*CTR]	  
	 Take-Off Run Available (TORA)
	  	 	: [*CTR]	  
	 Take-Off Distance Available (TODA)
	  	 	: [*CTR]	  
	 Accelerate Stop Distance Available (ASDA)
	  	 	: [*CTR]	  
	 Slope
	  	 	: [*CTR]	  
	 Wind
	  	 	: [*CTR]	  
	 Obstacles
	  	 	: [*CTR]	  
	 (height and distance from beginning of TORA)
	  	 	: [*CTR]	  

 the FAR approved Take-Off Weight of the A319 NEO Aircraft at the start of ground run shall be
not less than: 
  

					
	 Nominal: [*CTR]
	 	Tolerance: [*CTR]	 	Guarantee: [*CTR]

  

	2.2	 Landing Field Length 

The FAR approved dry Landing Field Length at an A319 NEO Aircraft gross weight of [*CTR] at sea level pressure altitude shall
be not more than: 
  

					
	 Nominal: [*CTR]
	 	Tolerance: [*CTR]	 	Guarantee: [*CTR]

  

	3	 MISSION GUARANTEES 

  

	3.1	 Mission Payload [*CTR] 

The A319 NEO Aircraft will be capable of carrying a Payload of not less than 

 

					
	 Nominal: [*CTR]
	 	Tolerance: [*CTR]	 	Guarantee: [*CTR]

 [*CTR] 
  

	3.1.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.1.2	 An allowance of [*CTR] 

  

	3.1.3	 An allowance of [*CTR] 

  

	3.1.4	 [*CTR] 

  

	3.1.5	 An allowance of [*CTR] 

  

	3.1.6	 An allowance of [*CTR] 

  

	3.1.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

  

			
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	3.1.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.2	 Mission Payload [*CTR] 

The A319 NEO Aircraft will be capable of carrying a Payload of not less than 

 

					
	 Nominal: [*CTR]
	 	Tolerance: [*CTR]	 	Guarantee: [*CTR]

 [*CTR] 
  

	3.2.1	 The departure airport conditions [*CTR] are as follows: 

 

					
	 Pressure altitude
	  	 	: [*CTR]	  
	 Temperature
	  	 	: [*CTR]	  
	 Take-Off Run Available (TORA)
	  	 	: [*CTR]	  
	 Take-Off Distance Available (TODA)
	  	 	: [*CTR]	  
	 Accelerate-Stop Distance Available (ASDA)
	  	 	: [*CTR]	  
	 Slope
	  	 	: [*CTR]	  
	 Wind
	  	 	: [*CTR]	  
	 Obstacle
	  	 	: [*CTR]	  
	 (height and distance from beginning of TORA)
	  			

 The destination airport conditions are such as to allow the required Landing Weight to be used
without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.2.2	 An allowance of [*CTR] 

  

	3.2.3	 An allowance of [*CTR] 

  

	3.2.4	 [*CTR] 

  

	3.2.5	 An allowance of [*CTR] 

  

	3.2.6	 An allowance of [*CTR] 

  

	3.2.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.2.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

			
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	3.3	 Mission Block Fuel 

In carrying a fixed payload of [*CTR] of the A319 NEO Aircraft will be not more than 

 

					
	 Nominal: [*CTR]
	 	Tolerance: [*CTR]	 	Guarantee: [*CTR]

 when the A319 NEO Aircraft is operated as defined here below. 

 

	3.3.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.3.2	 An allowance of [*CTR] 

  

	3.3.3	 An allowance of [*CTR] 

  

	3.3.4	 [*CTR] 

  

	3.3.5	 An allowance of [*CTR] 

  

	3.3.6	 An allowance of [*CTR] 

  

	3.3.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.3.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.4	 The Mission Payload and Block Fuel guarantees are based on an estimated fixed Operating Weight Empty of [*CTR] (see Appendix A).

  

	4	 MANUFACTURER’S WEIGHT EMPTY GUARANTEE 

The Seller guarantees a Manufacturer’s Weight Empty of the A319 NEO Aircraft as defined in Paragraph 1 above of not more
than 
  

					
	 Nominal: [*CTR]
	 	Tolerance: [*CTR]	 	Guarantee: [*CTR]

 This is the Manufacturer’s Weight Empty of the A319 NEO Aircraft as defined in
Section 13-10 of the A319 Standard Specification as amended by the SCN’s defined in Paragraph 1 above and which will be derived from the weighing of the A319 NEO Aircraft and subject to adjustment as defined in the Paragraph 8 below. 

  

			
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	5	 NOISE GUARANTEE 

  

	5.1	 Noise Certification 

The A319 NEO Aircraft [*CTR] 

[*CTR] 
  

	5.2	 [*CTR] Noise 

The A319 NEO Aircraft [*CTR] 

This guarantee applies for the following conditions: 
  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

							
	 Station
	  	 Distance

from [*CTR]

threshold

(m)
	  	 Sideline Distance to

runway extended

centerline

(m)
	  	 Height

above
 ground

(m)

	 [*CTR]
	  	[*CTR]	  	[*CTR]	  	[*CTR]
	 [*CTR]
	  	[*CTR]	  	[*CTR]	  	[*CTR]

 This guarantee does not apply to the [*CTR] 

This guarantee is based on [*CTR] 
  

	5.3	 Interior Noise in Flight 

  

	5.3.1	 Cockpit 

At a pressure altitude of [*CTR] the guaranteed A-weighted Sound Pressure Level (SPL) and the Speech Interference Level (SIL)
shall be as follows: 
  

			
	 	  	Guarantee
	 SPL [dB(A)]
	  	[*CTR]
	 SIL [dB]
	  	[*CTR]

 Noise levels shall be measured at the Captain’s and First Officer’s seat position at
head level with normal cockpit air conditioning and ventilation in operation. 

  

			
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	5.3.2	 Cabin 

At a pressure altitude of [*CTR] shall be as follows: 

 

					
	 	  	 	  	Guarantee
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
		  	SIL [dB]	  	[*CTR]
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
		  	SIL [dB]	  	[*CTR]

 Noise levels shall be measured at a height of [*CTR] above the passenger compartment floor on
the aisle center lines in the passenger seated area. 
  

	5.4	 Ramp Noise 

The APU noise during ground operation of the A319 NEO Aircraft [*CTR] 

[*CTR] 
  

	6	 GUARANTEE CONDITIONS 

  

	6.1	 The certification requirements for the A319 NEO Aircraft, except where otherwise noted, will be as stated in Section 02 of the Specification.

  

	6.2	 For the determination of FAR take-off and landing performance [*CTR] 

When establishing take-off performance [*CTR] 
  

	6.3	 Climb, cruise and descent performance associated with the Guarantees will include [*CTR] 

 

	6.4	 Where applicable the Guarantees assume the use of an approved fuel having a density of [*CTR] 

 

	6.5	 Sound levels are to be specified in decibels (dB), at a reference pressure of [*CTR] 

The definition of dB(A) shall be that specified as the “A-scale” weighting given in [*CTR] 

The Speech Interference Level (SIL) is defined as the [*CTR] 

 

	7	 GUARANTEE COMPLIANCE 

  

	7.1	 Compliance with the Guarantees will be demonstrated [*CTR] 

 

	7.2	 Compliance with the take-off and landing elements of the Guarantees will be demonstrated [*CTR] 

 

	7.3	 Compliance [*CTR] will be demonstrated [*CTR] 

  

	7.4	 Compliance with the Manufacturer’s Weight Empty guarantee will be demonstrated [*CTR 

 

	7.5	 The [*CTR] will be used to demonstrate compliance with the guarantees of certification noise levels. 

  

			
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 The A319 NEO Aircraft will have a [*CTR] 

Compliance with the interior noise and APU noise guarantees will be demonstrated [*CTR] 

[*CTR] 

The [*CTR] will be used to demonstrate compliance with the guarantee in Paragraph 5.2. 

 

	7.6	 Data [*CTR] will be adjusted as required [*CTR] accordance with established aeronautical practices to show compliance with the Guarantees.

  

	7.7	 The Seller undertakes to furnish the Buyer with [*CTR] demonstrating compliance with the Guarantees [*CTR] 

 

	8	 ADJUSTMENT OF GUARANTEES 

  

	8.1	 In the event of any change to any law, governmental regulation or requirement or interpretation thereof (“Rule Change”) by any
governmental agency made subsequent to the date of the Agreement and such Rule Change affects the A319 NEO Aircraft configuration or performance or both required to obtain certification the Guarantees will be appropriately modified to reflect the
effect of any such change. 

  

	8.2	 The Guarantees apply to the A319 NEO Aircraft as described in Paragraph 1 above and may be adjusted in the event of: 

 

	 	a)	 Any further configuration change which is the subject of an SCN 

 

	 	b)	 Changes required to obtain certification which cause changes to the performance or weight of the A319 NEO Aircraft. 

 

	9	 EXCLUSIVE GUARANTEES 

The Guarantees are exclusive and are provided in lieu of any and all other performance and weight guarantees of any nature
which may be stated, referenced or incorporated in the Specification or any other document. 
  

	10	 UNDERTAKING REMEDIES 

Should the A319 NEO Aircraft fail to meet any of the Guarantees specified in this Letter Agreement the Seller will [*CTR] 

 

	10.1	 [*CTR] 

  

	 	(i)	 [*CTR] 

  

	 	(ii)	 [*CTR] 

  

	 	(iii)	 [*CTR] 

  

	 	(iv)	 [*CTR] 

  

			
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	10.2	 [*CTR] 

  

	10.3	 The Seller’s maximum liability in respect of deficiency in performance of any A319 NEO Aircraft will be [*CTR] 

 

	11	 DUPLICATE REMEDIES 

Except as provided in Paragraph 10, the remedies provided to the Buyer under this Guarantee are not cumulative of any other
remedies provided to the Buyer under any other warranty or guarantee contained in the Agreement and the Buyer will not be entitled to duplicate remedies with respect to any single defect or costs incurred for any single defect. 

 

	12	 ASSIGNMENT 

This Letter Agreement and the rights and obligations of the parties will be subject to the provisions of Clause 21 of the
Agreement; provided, however, this Letter Agreement may not be assigned by the Buyer under either Clause 21.5 or 21.6 without the express written consent of the Seller, which the Seller may withhold in its sole discretion. 

 

	13	 CONFIDENTIALITY 

This Letter Agreement is subject to the terms and conditions of Clause 22.11 of the Agreement. 

 

	14	 COUNTERPARTS 

This Letter Agreement 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. 

  

			
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 If the foregoing correctly sets forth your understanding, please execute the original and one
(1) copy hereof in the space provided below and return a copy to the Seller. 
  

									
		 		 	 Very truly yours,
  

AIRBUS S.A.S.

					
		 		 		 	 By:
	 	 /s/ Airbus S.A.S.

		 		 		 		 	 Name: Airbus S.A.S.

Title: Senior Vice President Contracts

  

			
	 Accepted and Agreed
  

AMERICAN AIRLINES, INC.

		
	 By:
	 	 /s/ American Airlines, Inc.

		 	 Name: American Airlines, Inc.

Title: Vice President, Fleet Planning

  

			
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 APPENDIX A TO LETTER AGREEMENT NO. 11C-1 

 

			
	 Layout Number: [*CTR]
	 	MTOW (lb): [*CTR]
	 Seating: [*CTR]
	 	MLW (lb): [*CTR]
	 Total: [*CTR]
	 	MZFW (lb): [*CTR]

  

			
	 	 	Weight (lb)
	 Preliminary Manufacturer’s Weight Empty based on Standard Specification [*CTR]
	 	[*CTR]
	 Manufacturer’s Weight Empty (MWE) for the purpose of Paragraph 4
	 	[*CTR]
		
	 Cabin changes
	 	[*CTR]
	 [*CTR]
	 	[*CTR]
	 Manufacturer’s [*CTR] equipment [*CTR] and cargo hold fire extinguishers)
	 	[*CTR]
		 	  

	 Customized MWE
		[*CTR]
		
	 Operator’s Items
		
	 Unusable fuel
		[*CTR]
	 Oil for engines, IDG and APU
		[*CTR]
	 Water
		[*CTR]
	 Water tank precharge
		[*CTR]
	 Aircraft documents and tool kit
		[*CTR]
	 Passenger seats and lifejackets
		[*CTR]
	 Galley structure
		[*CTR]
	 Fixed equipment
		[*CTR]
	 Catering and removable equipment
		[*CTR]
	 Emergency equipment
		[*CTR]
	 Crew and crew baggage
		[*CTR]
		 	  

	 Total Operator’s Items
		[*CTR]
		
	 Operating Weight Empty (OWE) for the purpose of Paragraph 3
		[*CTR]

  

			
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 AMENDED AND RESTATED 

LETTER AGREEMENT NO. 11D 
 TO A320
FAMILY AIRCRAFT PURCHASE AGREEMENT 
 Dated as of July 20, 2011 

As of November 25, 2014 

American Airlines, Inc. 
 4333
Amon Carter Boulevard 
 Fort Worth, Texas 76155 

Re: A319 NEO AIRCRAFT PERFORMANCE GUARANTEE – CFM LEAP-1A24 ENGINES 

Dear Ladies and Gentlemen, 

American Airlines, Inc. (the “Buyer”) and Airbus S.A.S. (the “Seller”) have entered into an A320 Family
Aircraft Purchase Agreement dated as of July 20, 2011 (as supplemented and amended by the other letter agreements, and as otherwise supplemented, amended or modified from time to time, the “Agreement”) which covers, among other
matters, the sale by the Seller and the purchase or lease by the Buyer of certain Aircraft, under the terms and conditions set forth in said Agreement. The Buyer and the Seller have agreed to set forth in this Amended and Restated Letter Agreement
No. 11D (this “Letter Agreement”) certain additional terms and conditions regarding the sale and lease of the Aircraft. Letter Agreement No. 11D dated as of July 20, 2011 to the Agreement is hereby amended and
restated to read in its entirety as set forth herein. 
 Capitalized terms used herein and not otherwise defined in this Letter Agreement
have the meanings assigned thereto in the Agreement. The terms “herein,” “hereof” and “hereunder” and words of similar import refer to this Letter Agreement. 

Both parties agree that this Letter Agreement will constitute an integral, nonseverable part of said Agreement, that the provisions of said
Agreement are hereby incorporated herein by reference, and that this Letter Agreement will be governed by the provisions of said Agreement, except that if the Agreement and this Letter Agreement have specific provisions which are inconsistent, the
specific provisions contained in this Letter Agreement will govern. 

  

			
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	1	 AIRCRAFT CONFIGURATION 

The guarantees defined in Paragraphs 2, 3, 4 and 5 below (the “Guarantees”) are applicable to the A319 NEO
Aircraft as described in the A319 Standard Specification [*CTR] for: 
  

	1.1	 Basic Configuration (not applicable to paragraph 3.2) 

  

	 	i)	 [*CTR] 

  

	 	ii)	 [*CTR] 

  

	 	iii)	 the following design weights: 

  

					
	 Maximum Take-Off Weight (MTOW)
	  	 	[*CTR]	  
	 Maximum Landing Weight (MLW)
	  	 	[*CTR]	  
	 Maximum Zero Fuel Weight (MZFW)
	  	 	[*CTR]	  

  

	1.2	 Optional Configuration 

  

	 	i)	 [*CTR] 

  

	 	ii)	 [*CTR] 

  

	 	iii)	 the following design weights: 

  

					
	 Maximum Take-Off Weight (MTOW)
	  	 	[*CTR]	  
	 Maximum Landing Weight (MLW)
	  	 	[*CTR]	  
	 Maximum Zero Fuel Weight (MZFW)
	  	 	[*CTR]	  

 hereinafter referred to as the “Specification” without taking into account any
further changes thereto as provided in the Agreement. 
  

	2	 GUARANTEED PERFORMANCE 

  

	2.1	 Take-Off 

  

	2.1.1	 Take-Off Field Length 

The FAR approved Take-Off Field Length at an A319 NEO Aircraft gross weight of [*CTR] at the start of ground run at sea level
pressure altitude in [*CTR] be not more than: 
  

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	2.1.2	 Take-Off Weight 

When the A319 NEO Aircraft is operated in departure airport conditions [*CTR] as follows: 

 

					
	 Pressure altitude
	  	 	: [*CTR]	  
	 Temperature
	  	 	: [*CTR]	  
	 Take-Off Run Available (TORA)
	  	 	: [*CTR]	  
	 Take-Off Distance Available (TODA)
	  	 	: [*CTR]	  
	 Accelerate Stop Distance Available (ASDA)
	  	 	: [*CTR]	  
	 Slope
	  	 	: [*CTR]	  
	 Wind
	  	 	: [*CTR]	  
	 Obstacles
	  	 	: [*CTR]	  
	 (height and distance from beginning of TORA)
	  	 	: [*CTR]	  

  

			
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 the FAR approved Take-Off Weight of the A319 NEO Aircraft at the start of ground
run shall be not less than: 
  

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	2.2	 Landing Field Length 

The FAR approved dry Landing Field Length at an A319 NEO Aircraft gross weight of [*CRT] at sea level pressure altitude shall
be not more than: 
  

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	3	 MISSION GUARANTEES 

  

	3.1	 Mission Payload [*CTR] 

The A319 NEO Aircraft will be capable of carrying a Payload of not less than 

 

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 [*CTR] 
  

	3.1.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.1.2	 An allowance of [*CTR] 

  

	3.1.3	 An allowance of [*CTR] 

  

	3.1.4	 [*CTR] 

  

	3.1.5	 An allowance of [*CTR] 

  

	3.1.6	 An allowance of [*CTR] 

  

	3.1.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.1.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.2	 Mission Payload [*CTR] 

The A319 NEO Aircraft will be capable of carrying a Payload of not less than 

 

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 [*CTR] 

  

			
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	3.2.1	 The departure airport conditions [*CTR] are as follows: 

 

					
	 Pressure altitude
	  	 	: [*CTR]	  
	 Temperature
	  	 	: [*CTR]	  
	 Take-Off Run Available (TORA)
	  	 	: [*CTR]	  
	 Take-Off Distance Available (TODA)
	  	 	: [*CTR]	  
	 Accelerate-Stop Distance Available (ASDA)
	  	 	: [*CTR]	  
	 Slope
	  	 	: [*CTR]	  
	 Wind
	  	 	: [*CTR]	  
	 Obstacle
	  	 	: [*CTR]	  
	 (height and distance from beginning of TORA)
	  			

 The destination airport conditions are such as to allow the required Landing Weight to be used
without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.2.2	 An allowance of [*CTR] 

  

	3.2.3	 An allowance of [*CTR] 

  

	3.2.4	 [*CTR] 

  

	3.2.5	 An allowance of [*CTR] 

  

	3.2.6	 An allowance of [*CTR] 

  

	3.2.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.2.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.3	 Mission Block Fuel 

In carrying a fixed payload of [*CTR] of the A319 NEO Aircraft will be not more than 

 

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 when the A319 NEO Aircraft is operated as defined here below. 

 

	3.3.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.3.2	 An allowance of [*CTR] 

  

			
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	3.3.3	 An allowance of [*CTR] 

  

	3.3.4	 [*CTR] 

  

	3.3.5	 An allowance of [*CTR] 

  

	3.3.6	 An allowance of [*CTR] 

  

	3.3.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.3.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.4	 The Mission Payload and Block Fuel guarantees are based on an estimated fixed Operating Weight Empty of [*CTR] (see Appendix A).

  

	4	 MANUFACTURER’S WEIGHT EMPTY GUARANTEE 

The Seller guarantees a Manufacturer’s Weight Empty of the A319 NEO Aircraft as defined in Paragraph 1 above of not more
than 
  

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 This is the Manufacturer’s Weight Empty of the A319 NEO Aircraft as defined in
Section 13-10 of the A319 Standard Specification as amended by the SCN’s defined in Paragraph 1 above and which will be derived from the weighing of the A319 NEO Aircraft and subject to adjustment as defined in the Paragraph 8 below. 

 

	5	 NOISE GUARANTEE 

  

	5.1	 Noise Certification 

The A319 NEO Aircraft [*CTR] 

[*CTR] 
  

	5.2	 [*CTR] Noise 

The A319 NEO Aircraft [*CTR] 

This guarantee applies for the following conditions: 
  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

			
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 [*CTR]=[CONFIDENTIAL PORTION OMITTED AND FILED SEPARATELY WITH THE COMMISSION
PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] 

							
	 Station
	  	 Distance

from
 [*CTR]

threshold

(m)
	  	 Sideline Distance to

runway extended

centerline

(m)
	  	 Height

above
 ground

(m)

	 [*CTR]
	  	[*CTR]	  	[*CTR]	  	[*CTR]
	 [*CTR]
	  	[*CTR]	  	[*CTR]	  	[*CTR]

 This guarantee does not apply to the [*CTR] 

This guarantee is based on [*CTR] 
  

	5.3	 Interior Noise in Flight 

  

	5.3.1	 Cockpit 

At a pressure altitude of [*CTR] the guaranteed A-weighted Sound Pressure Level (SPL) and the Speech Interference Level (SIL)
shall be as follows: 
  

			
	 	  	Guarantee
	 SPL [dB(A)]
	  	[*CTR]
	 SIL [dB]
	  	[*CTR]

 Noise levels shall be measured at the Captain’s and First Officer’s seat position at
head level with normal cockpit air conditioning and ventilation in operation. 
  

	5.3.2	 Cabin 

At a pressure altitude of [*CTR] the guaranteed A-weighted Sound Pressure Level (SPL) and the Speech Interference Level (SIL)
shall be as follows: 
  

					
	 	  	 	  	Guarantee
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
		  	SIL [dB]	  	[*CTR]
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
		  	SIL [dB]	  	[*CTR]

 Noise levels shall be measured at a height of [*CTR] above the passenger compartment floor on
the aisle center lines in the passenger seated area. 
  

	5.4	 Ramp Noise 

The APU noise during ground operation of the A319 NEO Aircraft [*CTR] 

[*CTR] 
  

	6	 GUARANTEE CONDITIONS 

  

	6.1	 The certification requirements for the A319 NEO Aircraft, except where otherwise noted, will be as stated in Section 02 of the Specification.

  

			
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	6.2	 For the determination of FAR take-off and landing performance [*CTR] 

When establishing take-off performance [*CTR] 
  

	6.3	 Climb, cruise and descent performance associated with the Guarantees will include [*CTR] 

 

	6.4	 Where applicable the Guarantees assume the use of an approved fuel having a density of [*CTR] 

 

	6.5	 Sound levels are to be specified in decibels (dB), at a reference pressure of [*CTR] 

The definition of dB(A) shall be that specified as the “A-scale” weighting given in [*CTR] 

The Speech Interference Level (SIL) is defined as the [*CTR] 

 

	7	 GUARANTEE COMPLIANCE 

  

	7.1	 Compliance with the Guarantees will be demonstrated [*CTR] 

 

	7.2	 Compliance with the take-off and landing elements of the Guarantees will be demonstrated [*CTR] 

 

	7.3	 Compliance [*CTR] will be demonstrated [*CTR] 

  

	7.4	 Compliance with the Manufacturer’s Weight Empty guarantee will be demonstrated [*CTR] 

 

	7.5	 The [*CTR] will be used to demonstrate compliance with the guarantees of certification noise levels. 

The A319 NEO Aircraft will have a [*CTR] 

Compliance with the interior noise and APU noise guarantees will be demonstrated [*CTR] 

[*CTR] 
  

	7.6	 Data [*CTR] will be adjusted as required [*CTR] accordance with established aeronautical practices to show compliance with the Guarantees.

  

	7.7	 The [*CTR] will be used to demonstrate compliance with the guarantee in Paragraph 5.2 

 

	7.8	 The Seller undertakes to furnish the Buyer with [*CTR] demonstrating compliance with the Guarantees [*CTR] 

 

	8	 ADJUSTMENT OF GUARANTEES 

  

	8.1	 In the event of any change to any law, governmental regulation or requirement or interpretation thereof (“Rule Change”) by any
governmental agency made subsequent to the date of the Agreement and such Rule Change affects the A319 NEO Aircraft configuration or performance or both required to obtain certification the Guarantees will be appropriately modified to reflect the
effect of any such change. 

  

	8.2	 The Guarantees apply to the A319 NEO Aircraft as described in Paragraph 1 above and may be adjusted in the event of: 

 

	 	a)	 Any further configuration change which is the subject of an SCN 

  

			
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	 	b)	 Changes required to obtain certification which cause changes to the performance or weight of the A319 NEO Aircraft. 

 

	9	 EXCLUSIVE GUARANTEES 

The Guarantees are exclusive and are provided in lieu of any and all other performance and weight guarantees of any nature
which may be stated, referenced or incorporated in the Specification or any other document. 
  

	10	 UNDERTAKING REMEDIES 

Should the A319 NEO Aircraft fail to meet any of the Guarantees specified in this Letter Agreement the Seller will [*CTR] 

 

	10.1	 [*CTR] 

  

	 	(i)	 [*CTR] 

  

	 	(ii)	 [*CTR] 

  

	 	(iii)	 [*CTR] 

  

	 	(iv)	 [*CTR] 

  

	10.2	 [*CTR] 

  

	10.3	 The Seller’s maximum liability in respect of deficiency in performance of any A319 NEO Aircraft will be [*CTR] 

 

	11	 DUPLICATE REMEDIES 

Except as provided in Paragraph 10, the remedies provided to the Buyer under this Guarantee are not cumulative of any other
remedies provided to the Buyer under any other warranty or guarantee contained in the Agreement and the Buyer will not be entitled to duplicate remedies with respect to any single defect or costs incurred for any single defect. 

 

	12	 ASSIGNMENT 

This Letter Agreement and the rights and obligations of the parties will be subject to the provisions of Clause 21 of the
Agreement; provided, however, this Letter Agreement may not be assigned by the Buyer under either Clause 21.5 or 21.6 without the express written consent of the Seller, which the Seller may withhold in its sole discretion. 

 

	13	 CONFIDENTIALITY 

This Letter Agreement is subject to the terms and conditions of Clause 22.11 of the Agreement. 

 

	14	 COUNTERPARTS 

This Letter Agreement 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. 

  

			
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 If the foregoing correctly sets forth your understanding, please execute the original and one
(1) copy hereof in the space provided below and return a copy to the Seller. 
  

			
	 Very truly yours,
  

AIRBUS S.A.S.

		
	 By:
	 	 /s/ Airbus S.A.S

		 	 Name: Airbus S.A.S.

		 	 Title: Senior Vice President Contracts

  

			
	 Accepted and Agreed
  

AMERICAN AIRLINES, INC.

		
	 By:
	 	 /s/ American Airlines, Inc.

		 	 Name: American Airlines, Inc.

		 	 Title: Vice President, Fleet Planning

  

			
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 APPENDIX A TO LETTER AGREEMENT NO. 11D 

 

			
	 Layout Number: [*CTR]
	  	 MTOW (lb): [*CTR]

	 Seating: [*CTR]
	  	 MLW (lb): [*CTR]

	 Total: [*CTR]
	  	 MZFW (lb): [*CTR]

  

					
	 	  	Weight (lb)	 
	 Preliminary Manufacturer’s Weight Empty based on Standard Specification [*CTR]
	  	 	[*CTR]	  
	 Manufacturer’s Weight Empty (MWE) for the purpose of Paragraph 4
	  	 	[*CTR]	  
		
	 Cabin changes
	  	 	[*CTR]	  
	 [*CTR]
	  	 	[*CTR]	  
	 Manufacturer’s [*CTR] equipment [*CTR] and cargo hold fire extinguishers)
	  	 	[*CTR]	  
		  	  
	  
	 
	 Customized MWE
		 	[*CTR]	  
		
	 Operator’s Items
				
	 Unusable fuel
		 	[*CTR]	  
	 Oil for engines, IDG and APU
		 	[*CTR]	  
	 Water
		 	[*CTR]	  
	 Water tank precharge
		 	[*CTR]	  
	 Aircraft documents and tool kit
		 	[*CTR]	  
	 Passenger seats and lifejackets
		 	[*CTR]	  
	 Galley structure
		 	[*CTR]	  
	 Fixed equipment
		 	[*CTR]	  
	 Catering and removable equipment
		 	[*CTR]	  
	 Emergency equipment
		 	[*CTR]	  
	 Crew and crew baggage
		 	[*CTR]	  
		  	  
	  
	 
	 Total Operator’s Items
		 	[*CTR]	  
		
	 Operating Weight Empty (OWE) for the purpose of Paragraph 3
		 	[*CTR]	  

  

			
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 AMENDED AND RESTATED 

LETTER AGREEMENT NO. 11J 
 TO A320
FAMILY AIRCRAFT PURCHASE AGREEMENT 
 Dated as of July 20, 2011 

As of November 25, 2014 

American Airlines, Inc. 
 4333
Amon Carter Boulevard 
 Fort Worth, Texas 76155 

Re: A321 AIRCRAFT PERFORMANCE GUARANTEE – IAE V2533-A5 ENGINES 

Dear Ladies and Gentlemen, 

American Airlines, Inc. (the “Buyer”) and Airbus S.A.S. (the “Seller”) have entered into an A320 Family
Aircraft Purchase Agreement dated as of July 20, 2011 (as supplemented and amended by the other letter agreements, and as otherwise supplemented, amended or modified from time to time, the “Agreement”) which covers, among other
matters, the sale by the Seller and the purchase or lease by the Buyer of certain Aircraft, under the terms and conditions set forth in said Agreement. The Buyer and the Seller have agreed to set forth in this Amended and Restated Letter Agreement
No. 11J (this “Letter Agreement”) certain additional terms and conditions regarding the sale and lease of the Aircraft. Letter Agreement No. 11J dated as of July 20, 2011 to the Agreement is hereby amended and
restated to read in its entirety as set forth herein. 
 Capitalized terms used herein and not otherwise defined in this Letter Agreement
have the meanings assigned thereto in the Agreement. The terms “herein,” “hereof” and “hereunder” and words of similar import refer to this Letter Agreement. 

Both parties agree that this Letter Agreement will constitute an integral, nonseverable part of said Agreement, that the provisions of said
Agreement are hereby incorporated herein by reference, and that this Letter Agreement will be governed by the provisions of said Agreement, except that if the Agreement and this Letter Agreement have specific provisions which are inconsistent, the
specific provisions contained in this Letter Agreement will govern. 

  

			
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	1	 AIRCRAFT CONFIGURATION 

The guarantees defined in Paragraphs 2, 3, 4 and 5 below (the “Guarantees”) are applicable to the A321
Aircraft as described in the A321 Standard Specification [*CTR] for: 
  

	 	i)	 [*CTR] 

  

	 	ii)	 [*CTR] 

  

	 	iii)	 the following design weights: 

  

					
	 Maximum Take-Off Weight (MTOW)
	  	 	[*CTR]	  
	 Maximum Landing Weight (MLW)
	  	 	[*CTR]	  
	 Maximum Zero Fuel Weight (MZFW)
	  	 	[*CTR]	  

  

	 	iv)	 [*CTR] 

hereinafter referred to as the “Specification” without taking into account any further changes thereto as
provided in the Agreement. 
  

	2	 GUARANTEED PERFORMANCE 

  

	2.1	 Take-Off 

  

	2.1.1	 Take-Off Field Length 

The FAR approved Take-Off Field Length at an A321 Aircraft gross weight of [*CTR] at the start of ground run at sea level
pressure altitude in [*CTTR] be not more than: 
  

					
	 Nominal: [*CTR]
	 	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	2.1.2	 Take-Off Weight 

When the A321 Aircraft is operated in departure airport conditions [(*CTR)] as follows: 

 

					
	 Pressure altitude
	  	 	: [*CTR]	  
	 Temperature
	  	 	: [*CTR]	  
	 Take-Off Run Available (TORA)
	  	 	: [*CTR]	  
	 Take-Off Distance Available (TODA)
	  	 	: [*CTR]	  
	 Accelerate Stop Distance Available (ASDA)
	  	 	: [*CTR]	  
	 Slope
	  	 	: [*CTR]	  
	 Wind
	  	 	: [*CTR]	  
	 Obstacles
	  	 	: [*CTR]	  
	 (height and distance from beginning of TORA)
	  	 	: [*CTR]	  

 the FAR approved Take-Off Weight of the A321 Aircraft at the start of ground run shall be not
less than: 
  

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	2.2	 Landing Field Length 

  

			
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 The FAR approved dry Landing Field Length at an A321 Aircraft gross weight of
[*CTR] at sea level pressure altitude shall be not more than: 
  

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	3	 MISSION GUARANTEES 

  

	3.1	 Mission Payload [*CTR] 

The A321 Aircraft will be capable of carrying a Payload of not less than 

 

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 [*CTR] 
  

	3.1.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.1.2	 An allowance of [*CTR] 

  

	3.1.3	 An allowance of [*CTR] 

  

	3.1.4	 [*CTR] 

  

	3.1.5	 An allowance of [*CTR] 

  

	3.1.6	 An allowance of [*CTR] 

  

	3.1.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CRT] 

 

	3.1.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.2	 Mission Payload [*CTR] 

The A321 Aircraft will be capable of carrying a Payload of not less than 

 

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 [*CTR] 

  

			
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	3.2.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.2.2	 An allowance of [*CTR] 

  

	3.2.3	 An allowance of [*CTR] 

  

	3.2.4	 [*CTR] 

  

	3.2.5	 An allowance of [*CTR] 

  

	3.2.6	 An allowance of [*CTR] 

  

	3.2.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.2.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.3	 Mission Payload [*CTR] 

The A321 Aircraft will be capable of carrying a Payload of not less than 

 

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 [*CTR] 
  

	3.3.1	 The departure airport conditions [*CTR] are as follows: 

 

					
	 Pressure altitude
	  	 	: [*CTR]	  
	 Temperature
	  	 	: [*CTR]	  
	 Take-Off Run Available (TORA)
	  	 	: [*CTR]	  
	 Take-Off Distance Available (TODA)
	  	 	: [*CTR]	  
	 Accelerate-Stop Distance Available (ASDA)
	  	 	: [*CTR]	  
	 Slope
	  	 	: [*CTR]	  
	 Wind
	  	 	: [*CTR]	  
	 Obstacle
	  	 	: [*CTR]	  
	 (height and distance from beginning of TORA)
	  			

 The destination airport conditions are such as to allow the required Landing Weight to be used
without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.3.2	 An allowance of [*CTR] 

  

			
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	3.3.3	 An allowance of [*CTR] 

  

	3.3.4	 [*CTR] 

  

	3.3.5	 An allowance of [*CTR] 

  

	3.3.6	 An allowance of [*CTR] 

  

	3.3.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.3.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.4	 Mission Block Fuel 

In carrying a fixed payload of [*CTR] of the A321 Aircraft will be not more than 

 

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 when the A321 Aircraft is operated as defined here below. 

 

	3.4.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.4.2	 An allowance of [*CTR] 

  

	3.4.3	 An allowance of [*CTR] 

  

	3.4.4	 [*CTR] 

  

	3.4.5	 An allowance of [*CTR] 

  

	3.4.6	 An allowance of [*CTR] 

  

	3.4.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.4.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

			
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	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.5	 The Mission Payload and Block Fuel guarantees are based on an estimated fixed Operating Weight Empty of [*CTR] (see Appendix A).

  

	4	 MANUFACTURER’S WEIGHT EMPTY GUARANTEE 

The Seller guarantees a Manufacturer’s Weight Empty of the A321 Aircraft as defined in Paragraph 1 above of not more than

  

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 This is the Manufacturer’s Weight Empty of the A321 Aircraft as defined in
Section 13-10 of the A321 Standard Specification as amended by the SCN’s defined in Paragraph 1 above and which will be derived from the weighing of the A321 Aircraft and subject to adjustment as defined in the Paragraph 8 below. 

 

	5	 NOISE GUARANTEE 

  

	5.1	 Noise Certification 

The A321 Aircraft [*CTR] 

[*CTR] 
  

	5.2	 [*CTR] Noise 

The A321 Aircraft [*CTR] 

This guarantee applies for the following conditions: 
  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

							
	 Station
	  	 Distance from
[*CTR] threshold

(m)
	  	 Sideline Distance to
runway extended

centerline

(m)
	  	 Height above ground

(m)

	 [*CTR ]
	  	[*CTR]	  	[*CTR]	  	[*CTR]
	 [*CTR]
	  	[*CTR]	  	[*CTR]	  	[*CTR]

 This guarantee does not apply to the [*CTR]. 

This guarantee is based on [*CTR]. 

  

			
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	5.3	 Interior Noise in Flight 

  

	5.3.1	 Cockpit 

At a pressure altitude of [*CTR], the guaranteed A-weighted Sound Pressure Level (SPL) and the Speech Interference Level (SIL)
shall be as follows: 
  

					
	 	  	Guarantee	 
	 SPL [dB(A)]
	  	 	[*CTR]	  
	 SIL [dB]
	  	 	[*CTR]	  

 Noise levels shall be measured at the Captain’s and First Officer’s seat position at
head level with normal cockpit air conditioning and ventilation in operation. 
  

	5.3.2	 Cabin 

At a pressure altitude of [*CTR] shall be as follows: 

 

					
	 	  	 	  	Guarantee
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
		  	SIL [dB]	  	[*CTR]
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
		  	SIL [dB]	  	[*CTR]

 Noise levels shall be measured at a height of [*CTR] above the passenger compartment floor on
the aisle center lines in the passenger seated area. 
  

	5.4	 Ramp Noise 

The APU noise during ground operation of the A321 Aircraft [*CTR] 

[*CTR] 
  

	6	 GUARANTEE CONDITIONS 

  

	6.1	 The certification requirements for the A321 Aircraft, except where otherwise noted, will be as stated in Section 02 of the Specification.

  

	6.2	 For the determination of FAR take-off and landing performance [*CTR] 

When establishing take-off performance [*CTR] 
  

	6.3	 Climb, cruise and descent performance associated with the Guarantees will include [*CTR] 

Cruise performance at [*CTR] 
  

	6.4	 Where applicable the Guarantees assume the use of an approved fuel having a density of [*CTR] 

  

			
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	6.5	 Sound levels are to be specified in decibels (dB), at a reference pressure of [*CTR] 

The definition of dB(A) shall be that specified as the “A-scale” weighting given in [*CTR] 

The Speech Interference Level (SIL) is defined as the [*CTR] 

 

	7	 GUARANTEE COMPLIANCE 

  

	7.1	 Compliance with the Guarantees will be demonstrated [*CTR] 

 

	7.2	 Compliance with the take-off and landing elements of the Guarantees will be demonstrated [*CTR] 

 

	7.3	 Compliance [*CTR] will be demonstrated [*CTR] 

  

	7.4	 Compliance with the Manufacturer’s Weight Empty guarantee will be demonstrated [*CTR] 

 

	7.5	 The [*CTR] will be used to demonstrate compliance with the guarantees of certification noise levels. 

The A321 Aircraft will have a [*CTR] 

Compliance with the interior noise and APU noise guarantees will be demonstrated [*CTR] 

[*CTR] 

The [*CTR] will be used to demonstrate compliance with the guarantee in Paragraph 5.2. 

 

	7.6	 Data [*CTR] will be adjusted as required [*CTR] accordance with established aeronautical practices to show compliance with the Guarantees.

  

	7.7	 The Seller undertakes to furnish the Buyer with [*CTR] demonstrating compliance with the Guarantees [*CTR] 

 

	8	 ADJUSTMENT OF GUARANTEES 

  

	8.1	 In the event of any change to any law, governmental regulation or requirement or interpretation thereof (“Rule Change”) by any
governmental agency made subsequent to the date of the Agreement and such Rule Change affects the A321 Aircraft configuration or performance or both required to obtain certification the Guarantees will be appropriately modified to reflect the effect
of any such change. 

  

	8.2	 The Guarantees apply to the A321 Aircraft as described in Paragraph 1 above and may be adjusted in the event of: 

 

	 	a)	 Any further configuration change which is the subject of an SCN 

 

	 	b)	 Changes required to obtain certification which cause changes to the performance or weight of the A321 Aircraft. 

  

			
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	9	 EXCLUSIVE GUARANTEES 

The Guarantees are exclusive and are provided in lieu of any and all other performance and weight guarantees of any nature
which may be stated, referenced or incorporated in the Specification or any other document. 
  

	10	 UNDERTAKING REMEDIES 

Should the A321 Aircraft fail to meet any of the Guarantees specified in this Letter Agreement the Seller will [*CTR] 

 

	10.1	 [*CTR] 

  

	 	(i)	 [*CTR] 

  

	 	(ii)	 [*CTR] 

  

	 	(iii)	 [*CTR] 

  

	10.2	 [*CTR] 

  

	10.3	 The Seller’s maximum liability in respect of deficiency in performance of any A321 Aircraft will be [*CTR] 

 

	11	 DUPLICATE REMEDIES 

Except as provided in Paragraph 10, the remedies provided to the Buyer under this Guarantee are not cumulative of any other
remedies provided to the Buyer under any other warranty or guarantee contained in the Agreement and the Buyer will not be entitled to duplicate remedies with respect to any single defect or costs incurred for any single defect. 

 

	12	 ASSIGNMENT 

This Letter Agreement and the rights and obligations of the parties will be subject to the provisions of Clause 21 of the
Agreement; provided, however, this Letter Agreement may not be assigned by the Buyer under either Clause 21.5 or 21.6 without the express written consent of the Seller, which the Seller may withhold in its sole discretion. 

 

	13	 CONFIDENTIALITY 

This Letter Agreement is subject to the terms and conditions of Clause 22.11 of the Agreement. 

 

	14	 COUNTERPARTS 

This Letter Agreement 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. 

  

			
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PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] 

 If the foregoing correctly sets forth your understanding, please execute the original and one
(1) copy hereof in the space provided below and return a copy to the Seller. 
  

			
	 Very truly yours,
  

AIRBUS S.A.S.

		
	 By:
	 	 /s/ Airbus S.A.S.

		 	 Name: Airbus S.A.S.

		 	 Title: Senior Vice President Contracts

  

			
	 Accepted and Agreed
  

AMERICAN AIRLINES, INC.

		
	 By:
	 	 /s/ American Airlines, Inc.

		 	 Name: Airbus S.A.S.

		 	 Title: Vice President, Fleet Planning.

  

			
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 APPENDIX A TO AMENDED AND RESTATED LETTER AGREEMENT NO. 11J 

 

			
	 Layout Number: [*CTR]
	  	 MTOW (lb): [*CTR]

	 Seating: [*CTR]
	  	 MLW (lb): [*CTR]

	 Total: [*CTR]
	  	 MZFW (lb): [*CTR]

  

					
	 	  	Weight (lb)	 
	 Manufacturer’s Weight Empty Standard Specification [*CTR]
	  	 	[*CTR]	  
	 [*CTR]
	  	 	[*CTR]	  
	 [*CTR]
	  	 	[*CTR]	  
	 [*CTR]
	  	 	[*CTR]	  
	 [*CTR]
	  	 	[*CTR]	  
	 Manufacturer’s Weight Empty (MWE) for the purpose of Paragraph 4
	  	 	[*CTR]	  
		
	 Cabin changes
	  	 	[*CTR]	  
	 [*CTR]
	  	 	[*CTR]	  
	 Manufacturer’s [*CTR] equipment [*CTR] and cargo hold fire extinguishers)
	  	 	[*CTR]	  
		  	  
	  
	 
	 Customized MWE [*CTR]
		 	[*CTR]	  
		
	 Operator’s Items
				
	 Unusable fuel
		 	[*CTR]	  
	 Oil for engines, IDG and APU
		 	[*CTR]	  
	 Water
		 	[*CTR]	  
	 Water tank precharge
		 	[*CTR]	  
	 Aircraft documents and tool kit
		 	[*CTR]	  
	 Passenger seats and lifejackets
		 	[*CTR]	  
	 Galley structure
		 	[*CTR]	  
	 Fixed equipment
		 	[*CTR]	  
	 Catering and removable equipment
		 	[*CTR]	  
	 Emergency equipment
		 	[*CTR]	  
	 Crew and crew baggage
		 	[*CTR]	  
		  	  
	  
	 
	 Total Operator’s Items
		 	[*CTR]	  
		
	 Operating Weight Empty (OWE) for the purpose of Paragraph 3
		 	[*CTR]	  

  

			
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 AMENDED AND RESTATED 

LETTER AGREEMENT NO. 11K 
 TO A320
FAMILY AIRCRAFT PURCHASE AGREEMENT 
 Dated as of July 20, 2011 

As of November 25, 2014 

American Airlines, Inc. 
 4333
Amon Carter Boulevard 
 Fort Worth, Texas 76155 

Re: A321 NEO AIRCRAFT PERFORMANCE GUARANTEE – PW1133G-JM ENGINES 

Dear Ladies and Gentlemen, 

American Airlines, Inc. (the “Buyer”) and Airbus S.A.S. (the “Seller”) have entered into an A320 Family
Aircraft Purchase Agreement dated as of July 20, 2011 (as supplemented and amended by the other letter agreements, and as otherwise supplemented, amended or modified from time to time, the “Agreement”) which covers, among other
matters, the sale by the Seller and the purchase or lease by the Buyer of certain Aircraft, under the terms and conditions set forth in said Agreement. The Buyer and the Seller have agreed to set forth in this Amended and Restated Letter Agreement
No. 11K (this “Letter Agreement”) certain additional terms and conditions regarding the sale and lease of the Aircraft. Letter Agreement No. 11K dated as of July 20, 2011 to the Agreement is hereby amended and
restated to read in its entirety as set forth herein. 
 Capitalized terms used herein and not otherwise defined in this Letter Agreement
have the meanings assigned thereto in the Agreement. The terms “herein,” “hereof” and “hereunder” and words of similar import refer to this Letter Agreement. 

Both parties agree that this Letter Agreement will constitute an integral, nonseverable part of said Agreement, that the provisions of said
Agreement are hereby incorporated herein by reference, and that this Letter Agreement will be governed by the provisions of said Agreement, except that if the Agreement and this Letter Agreement have specific provisions which are inconsistent, the
specific provisions contained in this Letter Agreement will govern. 

  

			
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	1	 AIRCRAFT CONFIGURATION 

The guarantees defined in Paragraphs 2, 3, 4 and 5 below (the “Guarantees”) are applicable to the A321 NEO
Aircraft as described in the A321 Standard Specification [*CTR] for: 
  

	 	i)	 [*CTR] 

  

	 	ii)	 [*CTR] 

  

	 	iii)	 the following design weights: 

  

					
	 Maximum Take-Off Weight (MTOW)
	  	 	[*CTR]	  
	 Maximum Landing Weight (MLW)
	  	 	[*CTR]	  
	 Maximum Zero Fuel Weight (MZFW)
	  	 	[*CTR]	  

  

	 	iv)	 [*CTR] 

hereinafter referred to as the “Specification” without taking into account any further changes thereto as
provided in the Agreement. 
  

	2	 GUARANTEED PERFORMANCE 

  

	2.1	 Take-Off 

  

	2.1.1	 Take-Off Field Length 

The FAR approved Take-Off Field Length at an A321 NEO Aircraft gross weight of [*CTR] at the start of ground run at sea level
pressure altitude in [*CTR] be not more than: 
  

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	2.1.2	 Take-Off Weight 

When the A321 NEO Aircraft is operated in departure airport conditions [*CTR] as follows: 

 

					
	 Pressure altitude
	  	 	[:*CTR]	  
	 Temperature
	  	 	[:*CTR]	  
	 Take-Off Run Available (TORA)
	  	 	[:*CTR]	  
	 Take-Off Distance Available (TODA)
	  	 	[:*CTR]	  
	 Accelerate Stop Distance Available (ASDA)
	  	 	[:*CTR]	  
	 Slope
	  	 	[:*CTR]	  
	 Wind
	  	 	[:*CTR]	  
	 Obstacles
	  	 	[:*CTR]	  
	 (height and distance from beginning of TORA)
	  	 	[:*CTR]	  

 the FAR approved Take-Off Weight of the A321 NEO Aircraft at the start of ground run shall be
not less than: 
  

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

			
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	2.2	 Landing Field Length 

The FAR approved dry Landing Field Length at an A321 NEO Aircraft gross weight of [*CTR] at sea level pressure altitude shall
be not more than: 
  

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	3	 MISSION GUARANTEES 

  

	3.1	 Mission Payload [*CTR] 

The A321 NEO Aircraft will be capable of carrying a Payload of not less than 

 

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 [*CTR] 
  

	3.1.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.1.2	 An allowance of [*CTR] 

  

	3.1.3	 An allowance of [*CTR] 

  

	3.1.4	 [*CTR] 

  

	3.1.5	 An allowance of [*CTR] 

  

	3.1.6	 An allowance of [*CTR] 

  

	3.1.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.1.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.2	 Mission Payload [*CTR] 

The A321 NEO Aircraft will be capable of carrying a Payload of not less than 

 

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 [*CTR] 

  

			
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	3.2.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.2.2	 An allowance of [*CTR] 

  

	3.2.3	 An allowance of [*CTR] 

  

	3.2.4	 [*CTR] 

  

	3.2.5	 An allowance of [*CTR] 

  

	3.2.6	 An allowance of [*CTR] 

  

	3.2.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.2.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.3	 Mission Payload [*CTR] 

The A321 NEO Aircraft will be capable of carrying a Payload of not less than 

 

					
	 Nominal: [*CTR]
	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 [*CTR] 
  

	3.3.1	 The departure airport conditions (assumed representative of LGA runway 04) are as follows: 

 

					
	 Pressure altitude
	  	 	:[*CTR]	  
	 Temperature
	  	 	:[*CTR]	  
	 Take-Off Run Available (TORA)
	  	 	:[*CTR]	  
	 Take-Off Distance Available (TODA)
	  	 	:[*CTR]	  
	 Accelerate Stop Distance Available (ASDA)
	  	 	:[*CTR]	  
	 Slope
	  	 	:[*CTR]	  
	 Wind
	  	 	:[*CTR]	  
	 Obstacles
	  	 	:[*CTR]	  
	 (height and distance from beginning of TORA)
	  			

 The destination airport conditions are such as to allow the required Landing Weight to be used
without restriction. Pressure altitude is [*CTR] at destination airport. 

  

			
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	3.3.2	 An allowance of [*CTR] 

  

	3.3.3	 An allowance of [*CTR] 

  

	3.3.4	 [*CTR] 

  

	3.3.5	 An allowance of [*CTR] 

  

	3.3.6	 An allowance of [*CTR] 

  

	3.3.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.3.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.4	 Mission Block Fuel 

In carrying a fixed payload of [*CTR] 
  

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 when the A321 NEO Aircraft is operated as defined here below. 

 

	3.4.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.4.2	 An allowance of [*CTR] 

  

	3.4.3	 An allowance of [*CTR] 

  

	3.4.4	 [*CTR] 

  

	3.4.5	 An allowance of [*CTR] 

  

	3.4.6	 An allowance of [*CTR] 

  

	3.4.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.4.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

			
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	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.5	 The Mission Payload and Block Fuel guarantees are based on an estimated fixed Operating Weight Empty of [*CTR] (see Appendix A).

  

	4	 MANUFACTURER’S WEIGHT EMPTY GUARANTEE 

The Seller guarantees a Manufacturer’s Weight Empty of the A321 NEO Aircraft as defined in Paragraph 1 above of not more
than 
  

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 This is the Manufacturer’s Weight Empty of the A321 NEO Aircraft as defined in
Section 13-10 of the A321 Standard Specification as amended by the SCNs defined in Paragraph 1 above and which will be derived from the weighing of the A321 NEO Aircraft and subject to adjustment as defined in the Paragraph 8 below. 

 

	5	 NOISE GUARANTEE 

  

	5.1	 Noise Certification 

The A321 NEO Aircraft [*CTR] 

[*CTR] 
  

	5.2	 [*CTR] Noise 

The A321 NEO Aircraft [*CTR] 

This guarantee applies for the following conditions: 
  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

							
	 Station
	  	 Distance from

[*CTR] threshold

(m)
	  	 Sideline Distance

to runway extended
centerline

(m)
	  	 Height above

ground

(m)

	 [*CTR]
	  	[*CTR]	  	[*CTR]	  	[*CTR]
	 [*CTR]
	  	[*CTR]	  	[*CTR]	  	[*CTR]

 This guarantee does not apply [*CTR] This guarantee is based [*CTR] 

  

			
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	5.3	 Interior Noise in Flight 

  

	5.3.1	 Cockpit 

At a pressure altitude of [*CTR] the guaranteed A-weighted Sound Pressure Level (SPL) and the Speech Interference Level (SIL)
shall be as follows: 
  

					
	 	  	Guarantee	 
	 SPL [dB(A)]
	  	 	[*CTR]	  
	 SIL [dB]
	  	 	[*CTR]	  

 Noise levels shall be measured at the Captain’s and First Officer’s seat position at
head level with normal cockpit air conditioning and ventilation in operation. 
  

	5.3.2	 Cabin 

At a pressure altitude of [*CTR] shall be as follows: 

 

					
	 	  	 	  	Guarantee
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
		  	SIL [dB]	  	[*CTR]
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
		  	SIL [dB]	  	[*CTR]

 Noise levels shall be measured at a height of [*CTR] above the passenger compartment floor on
the aisle center lines in the passenger seated area. 
  

	5.4	 Ramp Noise 

The APU noise during ground operation of the A321 NEO Aircraft [*CTR] 

[*CTR] 
  

	6	 GUARANTEE CONDITIONS 

  

	6.1	 The certification requirements for the A321 NEO Aircraft, except where otherwise noted, will be as stated in Section 02 of the Specification.

  

	6.2	 For the determination of FAR take-off and landing performance [*CTR] 

When establishing take-off performance [*CTR] 
  

	6.3	 Climb, cruise and descent performance associated with the Guarantees will include [*CTR] 

 

	6.4	 Where applicable the Guarantees assume the use of an approved fuel having a density of [*CTR] 

 

	6.5	 Sound levels are to be specified in decibels (dB), at a reference pressure of [*CTR] 

  

			
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 The definition of dB(A) shall be that specified as the “A-scale”
weighting given in [*CTR] 
 The Speech Interference Level (SIL) is defined as the [*CTR] 

 

	7	 GUARANTEE COMPLIANCE 

  

	7.1	 Compliance with the Guarantees will be demonstrated [*CTR] 

 

	7.2	 Compliance with the take-off and landing elements of the Guarantees will be demonstrated [*CTR] 

 

	7.3	 Compliance [*CTR] will be demonstrated [*CTR] 

  

	7.4	 Compliance with the Manufacturer’s Weight Empty guarantee will be demonstrated [*CTR] 

 

	7.5	 The [*CTR] will be used to demonstrate compliance with the guarantees of certification noise levels. 

The A321 NEO Aircraft will have a [*CTR] 

Compliance with the interior noise and APU noise guarantees will be demonstrated [*CTR] 

[*CTR] 

The [*CTR] will be used to demonstrate compliance with the guarantee in Paragraph 5.2. 

 

	7.6	 Data [*CTR] will be adjusted as required [*CTR] accordance with established aeronautical practices to show compliance with the Guarantees.

  

	7.7	 The Seller undertakes to furnish the Buyer with [*CTR] demonstrating compliance with the Guarantees [*CTR] 

 

	8	 ADJUSTMENT OF GUARANTEES 

  

	8.1	 In the event of any change to any law, governmental regulation or requirement or interpretation thereof (“Rule Change”) by any
governmental agency made subsequent to the date of the Agreement and such Rule Change affects the A321 NEO Aircraft configuration or performance or both required to obtain certification the Guarantees will be appropriately modified to reflect the
effect of any such change. 

  

	8.2	 The Guarantees apply to the A321 NEO Aircraft as described in Paragraph 1 above and may be adjusted in the event of: 

 

	 	a)	 Any further configuration change which is the subject of an SCN 

 

	 	b)	 Changes required to obtain certification which cause changes to the performance or weight of the A321 NEO Aircraft. 

 

	9	 EXCLUSIVE GUARANTEES 

The Guarantees are exclusive and are provided in lieu of any and all other performance and weight guarantees of any nature
which may be stated, referenced or incorporated in the Specification or any other document with the exception of the A320 Family NEO Aircraft Performance Retention Guarantee. 

  

			
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	10	 UNDERTAKING REMEDIES 

Should the A321 NEO Aircraft fail to meet any of the Guarantees specified in this Letter Agreement the Seller will [*CTR] 

 

	10.1	 [*CTR] 

  

	 	(i)	 [*CTR] 

  

	 	(ii)	 [*CTR] 

  

	 	(iii)	 [*CTR] 

  

	10.2	 [*CTR] 

  

	10.3	 The Seller’s maximum liability in respect of deficiency in performance of any A321 NEO Aircraft will be [*CTR] 

 

	11	 DUPLICATE REMEDIES 

Except as provided in Paragraph 10, the remedies provided to the Buyer under this Guarantee are not cumulative of any other
remedies provided to the Buyer under any other warranty or guarantee contained in the Agreement and the Buyer will not be entitled to duplicate remedies with respect to any single defect or costs incurred for any single defect. 

 

	12	 ASSIGNMENT 

This Letter Agreement and the rights and obligations of the parties will be subject to the provisions of Clause 21 of the
Agreement; provided, however, this Letter Agreement may not be assigned by the Buyer under either Clause 21.5 or 21.6 without the express written consent of the Seller, which the Seller may withhold in its sole discretion. 

 

	13	 CONFIDENTIALITY 

This Letter Agreement is subject to the terms and conditions of Clause 22.11 of the Agreement. 

 

	14	 COUNTERPARTS 

This Letter Agreement 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. 

  

			
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 If the foregoing correctly sets forth your understanding, please execute the original and one
(1) copy hereof in the space provided below and return a copy to the Seller. 
  

			
	 Very truly yours,

	
	 AIRBUS S.A.S.

		
	 By:
	 	 /s/ Airbus S.A.S

		 	 Name: Airbus S.A.S.

		 	 Title: Senior Vice President Contracts

 Accepted and Agreed 
  

			
	 AMERICAN AIRLINES, INC.

		
	 By:
	 	 /s/ American Airlines, Inc.

		 	 Name: American Airlines, Inc.

		 	 Title: Vice President, Fleet Planning

  

			
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 APPENDIX A TO AMENDED AND RESTATED LETTER AGREEMENT NO. 11K 

 

			
	 Layout Number: [*CTR]

Seating: [*CTR]
 Total:
[*CTR]
	  	 MTOW (lb): [*CTR]

MLW (lb): [*CTR]
 MZFW (lb):
[*CTR]

  

			
	 	  	Weight (lb)
	 Preliminary Manufacturer’s Weight Empty based on Standard Specification [*CTR]
	  	[*CTR]
	 [*CTR]
	  	[*CTR]
	 [*CTR]
	  	[*CTR]
	 Manufacturer’s Weight Empty (MWE) for the purpose of Paragraph 4
	  	[*CTR]
		
	 Cabin changes
	  	[*CTR]
	 [*CTR]
	  	[*CTR]
	 Manufacturer’s [*CTR] equipment [*CTR] and cargo hold fire extinguishers)
	  	[*CTR]
		  	  

	 Customized MWE [*CTR]
		[*CTR]
		
	 Operator’s Items
		
	 Unusable fuel
		[*CTR]
	 Oil for engines, IGG and APU
		[*CTR]
	 Water
		[*CTR]
	 Water tank precharge
		[*CTR]
	 Aircraft documents and tool kit
		[*CTR]
	 Passenger seats and lifejackets
		[*CTR]
	 Galley structure
		[*CTR]
	 Fixed equipment
		[*CTR]
	 Catering and removable equipment
		[*CTR]
	 Emergency equipment
		[*CTR]
	 Crew and crew baggage
		[*CTR]
		  	  

	 Total Operator’s Items
		[*CTR]
		
	 Operating Weight Empty (OWE) for the purpose of Paragraph 3
		[*CTR]

  

			
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 LETTER AGREEMENT NO. 11K-1 

TO A320 FAMILY AIRCRAFT PURCHASE AGREEMENT 

Dated as of July 20, 2011 
 As
of November 25, 2014 
 American Airlines, Inc. 

4333 Amon Carter Boulevard 
 Fort
Worth, Texas 76155 
 Re: A321 NEO AIRCRAFT PERFORMANCE GUARANTEE – PW1133G-JM ENGINES 

Dear Ladies and Gentlemen, 

American Airlines, Inc. (the “Buyer”) and Airbus S.A.S. (the “Seller”) have entered into an A320 Family
Aircraft Purchase Agreement dated as of July 20, 2011 (as supplemented and amended by the other letter agreements, and as otherwise supplemented, amended or modified from time to time, the “Agreement”) which covers, among other
matters, the sale by the Seller and the purchase or lease by the Buyer of certain Aircraft, under the terms and conditions set forth in said Agreement. The Buyer and the Seller have agreed to set forth in this Letter Agreement No. 11K-1 (this
“Letter Agreement”) certain additional terms and conditions regarding the sale and lease of the Aircraft. 
 Capitalized
terms used herein and not otherwise defined in this Letter Agreement have the meanings assigned thereto in the Agreement. The terms “herein,” “hereof” and “hereunder” and words of similar import refer to this Letter
Agreement. 
 Both parties agree that this Letter Agreement will constitute an integral, nonseverable part of said Agreement, that the
provisions of said Agreement are hereby incorporated herein by reference, and that this Letter Agreement will be governed by the provisions of said Agreement, except that if the Agreement and this Letter Agreement have specific provisions which are
inconsistent, the specific provisions contained in this Letter Agreement will govern. 

  

			
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	1	 AIRCRAFT CONFIGURATION 

The guarantees defined in Paragraphs 2, 3, 4 and 5 below (the “Guarantees”) are applicable to the A321 NEO
Aircraft as described in the A321 Standard Specification [*CTR] for: 
  

	 	i)	 [*CTR] 

  

	 	ii)	 [*CTR] 

  

	 	iii)	 [*CTR] 

  

	 	iv)	 the following design weights: 

  

			
	 Maximum Take-Off Weight (MTOW)
	  	[*CTR]
	 Maximum Landing Weight (MLW)
	  	[*CTR]
	 Maximum Zero Fuel Weight (MZFW)
	  	[*CTR]

  

	 	v)	 [*CTR] 

hereinafter referred to as the “Specification” without taking into account any further changes thereto as
provided in the Agreement. 
 The Guarantees are valid for the A321 NEO Aircraft [*CTR] 

 

	2	 GUARANTEED PERFORMANCE 

  

	2.1	 Take-Off 

  

	2.1.1	 Take-Off Field Length 

The FAR approved Take-Off Field Length at an A321 NEO Aircraft gross weight of [*CTR] at the start of ground run at sea level
pressure altitude in [*CTR] be not more ]than: 
  

					
	Nominal: [*CTR]	 	Tolerance: [*CTR]	 	Guarantee: [*CTR]

  

	2.1.2	 Take-Off Weight 

When the A321 NEO Aircraft is operated in departure airport conditions [*CTR] as follows: 

 

					
	 Pressure altitude
	  	 	: [*CTR]	  
	 Temperature
	  	 	: [*CTR]	  
	 Take-Off Run Available (TORA)
	  	 	: [*CTR]	  
	 Take-Off Distance Available (TODA)
	  	 	: [*CTR]	  
	 Accelerate Stop Distance Available (ASDA)
	  	 	: [*CTR]	  
	 Slope
	  	 	: [*CTR]	  
	 Wind
	  	 	: [*CTR]	  
	 Obstacles
	  	 	: [*CTR]	  
	 (height and distance from beginning of TORA)
	  	 	: [*CTR]	  

 the FAR approved Take-Off Weight of the A321 NEO Aircraft at the start of ground run shall be
not less than: 
  

					
	Nominal: [*CTR]	 	Tolerance: [*CTR]	 	Guarantee: [*CTR]

  

			
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	2.2	 Landing Field Length 

The FAR approved dry Landing Field Length at an A321 NEO Aircraft gross weight of [*CTR] at sea level pressure altitude shall
be not more than: 
  

					
	Nominal: [*CTR]	 	Tolerance: [*CTR]	 	Guarantee: [*CTR]

  

	3	 MISSION GUARANTEES 

  

	3.1	 Mission Payload [*CTR] 

The A321 NEO Aircraft will be capable of carrying a Payload of not less than 

 

					
	Nominal: [*CTR]	 	Tolerance: [*CTR]	 	Guarantee: [*CTR]

 [*CTR] 
  

	3.1.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.1.2	 An allowance of [*CTR] 

  

	3.1.3	 An allowance of [*CTR] 

  

	3.1.4	 [*CTR] 

  

	3.1.5	 An allowance of [*CTR] 

  

	3.1.6	 An allowance of [*CTR] 

  

	3.1.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.1.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.2	 Mission Payload [*CTR] 

The A321 NEO Aircraft will be capable of carrying a Payload of not less than 

 

					
	Nominal: [*CTR]	 	Tolerance: [*CTR]	 	Guarantee: [*CTR]

 [*CTR] 

  

			
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	3.2.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.2.2	 An allowance of [*CTR] 

  

	3.2.3	 An allowance of [*CTR] 

  

	3.2.4	 [*CTR] 

  

	3.2.5	 An allowance of [*CTR] 

  

	3.2.6	 An allowance of [*CTR] 

  

	3.2.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.2.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.3	 Mission Payload [*CTR] 

The A321 NEO Aircraft will be capable of carrying a Payload of not less than 

 

					
	Nominal: [*CTR]	 	Tolerance: [*CTR]	 	Guarantee: [*CTR]

 [*CTR] 
  

	3.3.1	 The departure airport conditions (assumed representative of LGA runway 04) are as follows: 

 

					
	 Pressure altitude
	  	 	: [*CTR]	  
	 Temperature
	  	 	: [*CTR]	  
	 Take-Off Run Available (TORA)
	  	 	: [*CTR]	  
	 Take-Off Distance Available (TODA)
	  	 	: [*CTR]	  
	 Accelerate Stop Distance Available (ASDA)
	  	 	: [*CTR]	  
	 Slope
	  	 	: [*CTR]	  
	 Wind
	  	 	: [*CTR]	  
	 Obstacles
	  	 	: [*CTR]	  
	 (height and distance from beginning of TORA)
	  			

  

			
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 The destination airport conditions are such as to allow the required Landing
Weight to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.3.2	 An allowance of [*CTR] 

  

	3.3.3	 An allowance of [*CTR] 

  

	3.3.4	 [*CTR] 

  

	3.3.5	 An allowance of [*CTR] 

  

	3.3.6	 An allowance of [*CTR] 

  

	3.3.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.3.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.4	 Mission Block Fuel 

In carrying a fixed payload of [*CTR] 
  

					
	Nominal: [*CTR]	 	Tolerance: [*CTR]	 	Guarantee: [*CTR]

 when the A321 NEO Aircraft is operated as defined here below. 

 

	3.4.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.4.2	 An allowance of [*CTR] 

  

	3.4.3	 An allowance of [*CTR] 

  

	3.4.4	 [*CTR] 

  

	3.4.5	 An allowance of [*CTR] 

  

	3.4.6	 An allowance of [*CTR] 

  

	3.4.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

  

			
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	3.4.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.5	 The Mission Payload and Block Fuel guarantees are based on an estimated fixed Operating Weight Empty of [*CTR] (see Appendix A).

  

	4	MANUFACTURER’S WEIGHT EMPTY GUARANTEE 

 The Seller guarantees a
Manufacturer’s Weight Empty of the A321 NEO Aircraft as defined in Paragraph 1 above of not more than 
  

					
	Nominal: [*CTR]	 	Tolerance: [*CTR]	 	Guarantee: [*CTR]

 This is the Manufacturer’s Weight Empty of the A321 NEO Aircraft as defined in
Section 13-10 of the A321 Standard Specification as amended by the SCNs defined in Paragraph 1 above and which will be derived from the weighing of the A321 NEO Aircraft and subject to adjustment as defined in the Paragraph 8 below. 

 

	5	NOISE GUARANTEE 

  

	5.1	 Noise Certification 

The A321 NEO Aircraft [*CTR] 

[*CTR] 
  

	5.2	 [*CTR] Noise 

The A321 NEO Aircraft [*CTR] 

This guarantee applies for the following conditions: 
  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

							
	 Station
	  	 Distance from

[*CTR]
 threshold

(m)
	  	 Sideline Distance

to runway
 extended

centerline

(m)
	  	 Height

above
 ground

(m)

	 [*CTR]
	  	[*CTR]	  	[*CTR]	  	[*CTR]
	 [*CTR]
	  	[*CTR]	  	[*CTR]	  	[*CTR]

  

			
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 This guarantee does not apply to the [*CTR] 

This guarantee is based on [*CTR] 
  

	5.3	 Interior Noise in Flight 

  

	5.3.1	 Cockpit 

At a pressure altitude of [*CTR] the guaranteed A-weighted Sound Pressure Level (SPL) and the Speech Interference Level (SIL)
shall be as follows: 
  

			
	 	  	Guarantee
	 SPL [dB(A)]
	  	[*CTR]
	 SIL [dB]
	  	[*CTR]

 Noise levels shall be measured at the Captain’s and First Officer’s seat position at
head level with normal cockpit air conditioning and ventilation in operation. 
  

	5.3.2	 Cabin 

At a pressure altitude of [*CTR] shall be as follows: 

 

					
	 	  	 	  	Guarantee
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
		  	SIL [dB]	  	[*CTR]
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
		  	SIL [dB]	  	[*CTR]

 Noise levels shall be measured at a height of [*CTR] above the passenger compartment floor on
the aisle center lines in the passenger seated area. 
  

	5.4	 Ramp Noise 

The APU noise during ground operation of the A321 NEO Aircraft [*CTR] 

[*CTR] 
  

	6	GUARANTEE CONDITIONS 

  

	6.1	 The certification requirements for the A321 NEO Aircraft, except where otherwise noted, will be as stated in Section 02 of the Specification.

  

	6.2	 For the determination of FAR take-off and landing performance [*CTR] 

When establishing take-off performance [*CTR] 
  

	6.3	 Climb, cruise and descent performance associated with the Guarantees will include [*CTR] 

  

			
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	6.4	 Where applicable the Guarantees assume the use of an approved fuel having a density of [*CTR] 

 

	6.5	 Sound levels are to be specified in decibels (dB), at a reference pressure of [*CTR] 

The definition of dB(A) shall be that specified as the “A-scale” weighting given in [*CTR] 

The Speech Interference Level (SIL) is defined as the [*CTR] 

 

	7	GUARANTEE COMPLIANCE 

  

	7.1	 Compliance with the Guarantees will be demonstrated [*CTR] 

 

	7.2	 Compliance with the take-off and landing elements of the Guarantees will be demonstrated [*CTR] 

 

	7.3	 Compliance [*CTR] will be demonstrated [*CTR] 

  

	7.4	 Compliance with the Manufacturer’s Weight Empty guarantee will be demonstrated [*CTR] 

 

	7.5	 The [*CTR] will be used to demonstrate compliance with the guarantees of certification noise levels. 

The A321 NEO Aircraft will have a [*CTR] 

Compliance with the interior noise and APU noise guarantees will be demonstrated [*CTR] 

[*CTR] 

The [*CTR] program will be used to demonstrate compliance with the guarantee in Paragraph 5.2. 

 

	7.6	 Data [*CTR] will be adjusted as required [*CTR] accordance with established aeronautical practices to show compliance with the Guarantees.

  

	7.7	 The Seller undertakes to furnish the Buyer with [*CTR] demonstrating compliance with the Guarantees [*CTR] 

 

	8	ADJUSTMENT OF GUARANTEES 

  

	8.1	 In the event of any change to any law, governmental regulation or requirement or interpretation thereof (“Rule Change”) by any
governmental agency made subsequent to the date of the Agreement and such Rule Change affects the A321 NEO Aircraft configuration or performance or both required to obtain certification the Guarantees will be appropriately modified to reflect the
effect of any such change. 

  

	8.2	 The Guarantees apply to the A321 NEO Aircraft as described in Paragraph 1 above and may be adjusted in the event of: 

 

	 	a)	 Any further configuration change which is the subject of an SCN 

 

	 	b)	 Changes required to obtain certification which cause changes to the performance or weight of the A321 NEO Aircraft. 

  

			
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	9	 EXCLUSIVE GUARANTEES 

The Guarantees are exclusive and are provided in lieu of any and all other performance and weight guarantees of any nature
which may be stated, referenced or incorporated in the Specification or any other document with the exception of the A320 Family NEO Aircraft Performance Retention Guarantee. 
  

	10	 UNDERTAKING REMEDIES 

Should the A321 NEO Aircraft fail to meet any of the Guarantees specified in this Letter Agreement the Seller will [*CTR] 

 

	10.1	 [*CTR] 

  

	 	(i)	 [*CTR] 

  

	 	(ii)	 [*CTR] 

  

	 	(iii)	 [*CTR] 

  

	10.2	 [*CTR] 

  

	10.3	 The Seller’s maximum liability in respect of deficiency in performance of any A321 NEO Aircraft will be [*CTR] 

 

	11	 DUPLICATE REMEDIES 

Except as provided in Paragraph 10, the remedies provided to the Buyer under this Guarantee are not cumulative of any other
remedies provided to the Buyer under any other warranty or guarantee contained in the Agreement and the Buyer will not be entitled to duplicate remedies with respect to any single defect or costs incurred for any single defect. 

 

	12	 ASSIGNMENT 

This Letter Agreement and the rights and obligations of the parties will be subject to the provisions of Clause 21 of the
Agreement; provided, however, this Letter Agreement may not be assigned by the Buyer under either Clause 21.5 or 21.6 without the express written consent of the Seller, which the Seller may withhold in its sole discretion. 

 

	13	 CONFIDENTIALITY 

This Letter Agreement is subject to the terms and conditions of Clause 22.11 of the Agreement. 

 

	14	 COUNTERPARTS 

This Letter Agreement 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. 

  

			
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 If the foregoing correctly sets forth your understanding, please execute the original and one
(1) copy hereof in the space provided below and return a copy to the Seller. 
  

			
	 Very truly yours,
  

AIRBUS S.A.S.

		
	 By:
	 	 /s/ Airbus S.A.S

		 	 Name: Airbus S.A.S.

Title: Senior Vice President Contracts

 Accepted and Agreed 
  

			
	 AMERICAN AIRLINES, INC.

		
	 By:
	 	 /s/ American Airlines, Inc.

		 	 Name: American Airlines, Inc.

Title: Vice President, Fleet Planning

  

			
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 APPENDIX A TO LETTER AGREEMENT NO. 11K-1 

 

			
	 Layout Number: [*CTR]
	  	 MTOW (lb): [*CTR]

	 Seating: [*CTR]
	  	 MLW (lb): [*CTR]

	 Total: [*CTR]
	  	 MZFW (lb): [*CTR]

  

					
	 	  	Weight (lb)	 
	 Preliminary Manufacturer’s Weight Empty based on Standard Specification [*CTR]
	  	 	[*CTR]	  
	 [*CTR]
	  	 	[*CTR]	  
	 [*CTR]
	  	 	[*CTR]	  
	 Manufacturer’s Weight Empty (MWE) for the purpose of Paragraph 4
	  	 	[*CTR]	  
		
	 Cabin changes
	  	 	[*CTR]	  
	 [*CTR]
	  	 	[*CTR]	  
	 Manufacturer’s [*CTR] equipment [*CTR] and cargo hold fire extinguishers)
	  	 	[*CTR]	  
		  	  
	  
	 
	 Customized MWE [*CTR]
		 	[*CTR]	  
		
	 Operator’s Items
				
	 Unusable fuel
		 	[*CTR]	  
	 Oil for engines, IGG and APU
		 	[*CTR]	  
	 Water
		 	[*CTR]	  
	 Water tank precharge
		 	[*CTR]	  
	 Aircraft documents and tool kit
		 	[*CTR]	  
	 Passenger seats and lifejackets
		 	[*CTR]	  
	 Galley structure
		 	[*CTR]	  
	 Fixed equipment
		 	[*CTR]	  
	 Catering and removable equipment
		 	[*CTR]	  
	 Emergency equipment
		 	[*CTR]	  
	 Crew and crew baggage
		 	[*CTR]	  
		  	  
	  
	 
	 Total Operator’s Items
		 	[*CTR]	  
		
	 Operating Weight Empty (OWE) for the purpose of Paragraph 3
		 	[*CTR]	  

  

			
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 AMENDED AND RESTATED 

LETTER AGREEMENT NO. 11L 
 TO A320
FAMILY AIRCRAFT PURCHASE AGREEMENT 
 Dated as of July 20, 2011 

As of November 25, 2014 

American Airlines, Inc. 
 4333
Amon Carter Boulevard 
 Fort Worth, Texas 76155 

Re: A321 NEO AIRCRAFT PERFORMANCE GUARANTEE – CFM LEAP-1A32 ENGINES 

Dear Ladies and Gentlemen, 

American Airlines, Inc. (the “Buyer”) and Airbus S.A.S. (the “Seller”) have entered into an A320 Family
Aircraft Purchase Agreement dated as of July 20, 2011 (as supplemented and amended by the other letter agreements, and as otherwise supplemented, amended or modified from time to time, the “Agreement”) which covers, among other
matters, the sale by the Seller and the purchase or lease by the Buyer of certain Aircraft, under the terms and conditions set forth in said Agreement. The Buyer and the Seller have agreed to set forth in this Amended and Restated Letter Agreement
No. 11L (this “Letter Agreement”) certain additional terms and conditions regarding the sale and lease of the Aircraft. Letter Agreement No. 11L dated as of July 20, 2011 to the Agreement is hereby amended and
restated to read in its entirety as set forth herein. 
 Capitalized terms used herein and not otherwise defined in this Letter Agreement
have the meanings assigned thereto in the Agreement. The terms “herein,” “hereof” and “hereunder” and words of similar import refer to this Letter Agreement. 

Both parties agree that this Letter Agreement will constitute an integral, nonseverable part of said Agreement, that the provisions of said
Agreement are hereby incorporated herein by reference, and that this Letter Agreement will be governed by the provisions of said Agreement, except that if the Agreement and this Letter Agreement have specific provisions which are inconsistent, the
specific provisions contained in this Letter Agreement will govern. 

  

			
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	1	 AIRCRAFT CONFIGURATION 

The guarantees defined in Paragraphs 2, 3, 4 and 5 below (the “Guarantees”) are applicable to the A321 NEO
Aircraft as described in the A321 Standard Specification [*CTR] for: 
  

	 	i)	 [*CTR] 

  

	 	ii)	 [*CTR] 

  

	 	iii)	 the following design weights: 

  

			
	 Maximum Take-Off Weight (MTOW)
	  	[*CTR]
	 Maximum Landing Weight (MLW)
	  	[*CTR]
	 Maximum Zero Fuel Weight (MZFW)
	  	[*CTR]

  

	 	iv)	 [*CTR] 

hereinafter referred to as the “Specification” without taking into account any further changes thereto as
provided in the Agreement. 
  

	2	GUARANTEED PERFORMANCE 

  

	2.1	 Take-Off 

  

	2.1.1	 Take-Off Field Length 

The FAR approved Take-Off Field Length at an A321 NEO Aircraft gross weight of [*CTR] at the start of ground run at sea level
pressure altitude in [*CTR] shall be not more than: 
  

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	2.1.2	 Take-Off Weight 

When the A321 NEO Aircraft is operated in departure airport conditions [*CTR] as follows: 

 

			
	 Pressure altitude
	  	: [*CTR]
	 Temperature
	  	: [*CTR]
	 Take-Off Run Available (TORA)
	  	: [*CTR]
	 Take-Off Distance Available (TODA)
	  	: [*CTR]
	 Accelerate Stop Distance Available (ASDA)
	  	: [*CTR]
	 Slope
	  	: [*CTR]
	 Wind
	  	: [*CTR]
	 Obstacles
	  	: [*CTR]
	 (height and distance from beginning of TORA)
	  	: [*CTR]

 the FAR approved Take-Off Weight of the A321 NEO Aircraft at the start of ground run shall be
not less than: 
  

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

	2.2	 Landing Field Length 

The FAR approved dry Landing Field Length at an A321 NEO Aircraft gross weight of [*CTR] at sea level pressure altitude shall
be not more than: 
  

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

			
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	3	 MISSION GUARANTEES 

  

	3.1	 Mission Payload [*CTR] 

The A321 NEO Aircraft will be capable of carrying a Payload of not less than 

 

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 [*CTR] 
  

	3.1.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.1.2	 An allowance of [*CTR] 

  

	3.1.3	 An allowance of [*CTR] 

  

	3.1.4	 [*CTR] 

  

	3.1.5	 An allowance of [*CTR] 

  

	3.1.6	 An allowance of [*CTR] 

  

	3.1.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.1.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.2	 Mission Payload [*CTR] 

The A321 NEO Aircraft will be capable of carrying a Payload of not less than 

 

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 [*CTR] 
  

	3.2.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.2.2	 An allowance of [*CTR] 

  

			
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	3.2.3	 An allowance of [*CTR] 

  

	3.2.4	 [*CTR] 

  

	3.2.5	 An allowance of [*CTR] 

  

	3.2.6	 An allowance of [*CTR] 

  

	3.2.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.2.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.3	 Mission Payload [*CTR] 

The A321 NEO Aircraft will be capable of carrying a Payload of not less than 

 

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 [*CTR] 
  

	3.3.1	 The departure airport conditions [*CTR] are as follows: 

 

			
	 Pressure altitude
	  	: [*CTR]
	 Temperature
	  	: [*CTR]
	 Take-Off Run Available (TORA)
	  	: [*CTR]
	 Take-Off Distance Available (TODA)
	  	: [*CTR]
	 Accelerate Stop Distance Available (ASDA)
	  	: [*CTR]
	 Slope
	  	: [*CTR]
	 Wind
	  	: [*CTR]
	 Obstacles
	  	: [*CTR]
	 (height and distance from beginning of TORA)
	  	

 The destination airport conditions are such as to allow the required Landing Weight to be used
without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.3.2	 An allowance of [*CTR] 

  

	3.3.3	 An allowance of [*CTR] 

  

	3.3.4	 [*CTR] 

  

	3.3.5	 An allowance of [*CTR] 

  

	3.3.6	 An allowance of [*CTR] 

  

	3.3.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

  

			
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	3.3.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.4	 Mission Block Fuel 

In carrying a fixed payload of [*CTR] of the A321 NEO Aircraft will be not more than 

 

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

 when the A321 NEO Aircraft is operated as defined here below. 

 

	3.4.1	 The departure airport conditions are such as to allow the required Take-Off Weight to be used without restriction. Pressure altitude is [*CTR] at
departure airport. 

 The destination airport conditions are such as to allow the required Landing Weight
to be used without restriction. Pressure altitude is [*CTR] at destination airport. 
  

	3.4.2	 An allowance of [*CTR] 

  

	3.4.3	 An allowance of [*CTR] 

  

	3.4.4	 [*CTR] 

  

	3.4.5	 An allowance of [*CTR] 

  

	3.4.6	 An allowance of [*CTR] 

  

	3.4.7	 Stage distance is defined as the distance [*CTR] Block fuel is defined as the fuel [*CTR] 

 

	3.4.8	 At the end of approach and landing [*CTR] of fuel will remain in the tanks. This represents the estimated fuel required for: 

 

	 	a)	 [*CTR] 

  

	 	b)	 [*CTR] 

  

	 	c)	 [*CTR] 

  

	 	d)	 [*CTR] 

  

	 	e)	 [*CTR] 

  

	3.5	 The Mission Payload and Block Fuel guarantees are based on an estimated fixed Operating Weight Empty of [*CTR] (see Appendix A).

  

	4	MANUFACTURER’S WEIGHT EMPTY GUARANTEE 

 The Seller guarantees a
Manufacturer’s Weight Empty of the A321 NEO Aircraft as defined in Paragraph 1 above of not more than 
  

					
	Nominal: [*CTR]	  	Tolerance: [*CTR]	  	Guarantee: [*CTR]

  

			
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 This is the Manufacturer’s Weight Empty of the A321 NEO Aircraft as defined
in Section 13-10 of the A321 Standard Specification as amended by the SCNs defined in Paragraph 1 above and which will be derived from the weighing of the A321 NEO Aircraft and subject to adjustment as defined in the Paragraph 8 below. 

 

	5	NOISE GUARANTEE 

  

	5.1	 Noise Certification 

The A321 NEO Aircraft [*CTR] 

[*CTR] 
  

	5.2	 [*CTR] Noise 

The A321 NEO Aircraft [*CTR] 

This guarantee applies for the following conditions: 
  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

	 	•	 	 [*CTR] 

  

							
	 Station
	  	 Distance from
[*CTR] threshold

(m)
	  	 Sideline Distance to
runway extended

centerline

(m)
	  	 Height

above
 ground

(m)

	 [*CTR]
	  	[*CTR]	  	[*CTR]	  	[*CTR]
	 [*CTR]
	  	[*CTR]	  	[*CTR]	  	[*CTR]

 This guarantee does not apply to the [*CTR] 

This guarantee is based on [*CTR] 
  

	5.3	 Interior Noise in Flight 

  

	5.3.1	 Cockpit 

At a pressure altitude of [*CTR] the guaranteed A-weighted Sound Pressure Level (SPL) and the Speech Interference Level (SIL)
shall be as follows: 
  

			
	 	  	 Guarantee

	 SPL [dB(A)]
	  	[*CTR]
	 SIL [dB]
	  	[*CTR]

 Noise levels shall be measured at the Captain’s and First Officer’s seat position at
head level with normal cockpit air conditioning and ventilation in operation. 

  

			
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	5.3.2	 Cabin 

At a pressure altitude of [*CTR] the guaranteed A-weighted Sound Pressure Level (SPL) and the Speech Interference Level (SIL)
shall be as follows: 
  

					
	 	  	 	  	Guarantee
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
		  	SIL [dB]	  	[*CTR]
	 [*CTR]
	  	SPL [dB(A)]	  	[*CTR]
		  	SIL [dB]	  	[*CTR]

 Noise levels shall be measured at a height of [*CTR] above the passenger compartment floor on
the aisle center lines in the passenger seated area. 
  

	5.4	 Ramp Noise 

The APU noise during ground operation of the A321 NEO Aircraft [*CTR] 

[*CTR] 
  

	6	GUARANTEE CONDITIONS 

  

	6.1	 The certification requirements for the A321 NEO Aircraft, except where otherwise noted, will be as stated in Section 02 of the Specification.

  

	6.2	 For the determination of FAR take-off and landing performance [*CTR] 

When establishing take-off performance [*CTR] 
  

	6.3	 Climb, cruise and descent performance associated with the Guarantees will include [*CTR] 

 

	6.4	 Where applicable the Guarantees assume the use of an approved fuel having a density of [*CTR] 

 

	6.5	 Sound levels are to be specified in decibels (dB), at a reference pressure of [*CTR] 

The definition of dB(A) shall be that specified as the “A-scale” weighting given in [*CTR] 

The Speech Interference Level (SIL) is defined as the [*CTR] 

 

	7	GUARANTEE COMPLIANCE 

  

	7.1	 Compliance with the Guarantees will be demonstrated [*CTR] 

 

	7.2	 Compliance with the take-off and landing elements of the Guarantees will be demonstrated [*CTR] 

 

	7.3	 Compliance [*CTR] will be demonstrated [*CTR] 

  

	7.4	 Compliance with the Manufacturer’s Weight Empty guarantee will be demonstrated [*CTR] 

 

	7.5	 The [*CTR] will be used to demonstrate compliance with the guarantees of certification noise levels. 

The A321 NEO Aircraft will have a [*CTR] 

Compliance with the interior noise and APU noise guarantees will be demonstrated [*CTR] 

[*CTR] 

  

			
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	7.6	 Data [*CTR] will be adjusted as required [*CTR] accordance with established aeronautical practices to show compliance with the Guarantees.

  

	7.7	 The [*CTR] will be used to demonstrate compliance with the guarantee in Paragraph 5.2. 

 

	7.8	 The Seller undertakes to furnish the Buyer with [*CTR] demonstrating compliance with the Guarantees [*CTR] 

 

	8	ADJUSTMENT OF GUARANTEES 

  

	8.1	 In the event of any change to any law, governmental regulation or requirement or interpretation thereof (“Rule Change”) by any
governmental agency made subsequent to the date of the Agreement and such Rule Change affects the A321 NEO Aircraft configuration or performance or both required to obtain certification the Guarantees will be appropriately modified to reflect the
effect of any such change. 

  

	8.2	 The Guarantees apply to the A321 NEO Aircraft as described in Paragraph 1 above and may be adjusted in the event of: 

 

	 	a)	 Any further configuration change which is the subject of an SCN 

 

	 	b)	 Changes required to obtain certification which cause changes to the performance or weight of the A321 NEO Aircraft. 

 

	9	 EXCLUSIVE GUARANTEES 

The Guarantees are exclusive and are provided in lieu of any and all other performance and weight guarantees of any nature
which may be stated, referenced or incorporated in the Specification or any other document with the exception of the A320 Family NEO Aircraft Performance Retention Guarantee. 
  

	10	UNDERTAKING REMEDIES 

 Should the A321 NEO Aircraft fail to meet any of
the Guarantees specified in this Letter Agreement the Seller will [*CTR] 
  

	10.1	 [*CTR] 

  

	 	(i)	 [*CTR] 

  

	 	(ii)	 [*CTR] 

  

	 	(iii)	 [*CTR] 

  

	10.2	 [*CTR] 

  

	10.3	 The Seller’s maximum liability in respect of deficiency in performance of any A321 NEO Aircraft will be [*CTR] 

 

	11	DUPLICATE REMEDIES 

 Except as provided in Paragraph 10, the remedies
provided to the Buyer under this Guarantee are not cumulative of any other remedies provided to the Buyer under any other warranty or guarantee contained in the Agreement and the Buyer will not be entitled to duplicate remedies with respect to any
single defect or costs incurred for any single defect. 

  

			
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	12	 ASSIGNMENT 

This Letter Agreement and the rights and obligations of the parties will be subject to the provisions of Clause 21 of the
Agreement; provided, however, this Letter Agreement may not be assigned by the Buyer under either Clause 21.5 or 21.6 without the express written consent of the Seller, which the Seller may withhold in its sole discretion. 

 

	13	 CONFIDENTIALITY 

This Letter Agreement is subject to the terms and conditions of Clause 22.11 of the Agreement. 

 

	14	 COUNTERPARTS 

This Letter Agreement 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. 

  

			
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COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT] 

 If the foregoing correctly sets forth your understanding, please execute the original and one
(1) copy hereof in the space provided below and return a copy to the Seller. 
  

			
	 Very truly yours,
  

AIRBUS S.A.S.

		
	 By:
	 	 /s/ Airbus S.A.S.

		 	 Name: Airbus S.A.S

Title: Senior Vice President Contracts

  

			
	 Accepted and Agreed
  

AMERICAN AIRLINES, INC.

		
	 By:
	 	 /s/ American Airlines, Inc.

		 	 Name: American Airlines, Inc.

Title: Vice President, Fleet Planning

  

			
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 APPENDIX A TO LETTER AGREEMENT NO. 11L 

 

			
	 Layout Number: [*CTR]
	  	 MTOW (lb): [*CTR]

	 Seating: [*CTR]
	  	 MLW (lb): [*CTR]

	 Total: [*CTR]
	  	 MZFW (lb): [*CTR]

  

			
	 	  	Weight (lb)
	 Preliminary Manufacturer’s Weight Empty based on Standard Specification [*CTR]
	  	[*CTR]
	 [*CTR]
	  	[*CTR]
	 [*CTR]
	  	[*CTR]
	 Manufacturer’s Weight Empty (MWE) for the purpose of Paragraph 4
	  	[*CTR]
		
	 Cabin changes
	  	[*CTR]
	 [*CTR]
	  	[*CTR]
	 Manufacturer’s [*CTR] equipment [*CTR] and cargo hold fire extinguishers)
	  	[*CTR]
		  	  

	 Customized MWE [*CTR]
		[*CTR]
		
	 Operator’s Items
		
	 Unusable fuel
		[*CTR]
	 Oil for engines, IGG and APU
		[*CTR]
	 Water
		[*CTR]
	 Water tank precharge
		[*CTR]
	 Aircraft documents and tool kit
		[*CTR]
	 Passenger seats and lifejackets
		[*CTR]
	 Galley structure
		[*CTR]
	 Fixed equipment
		[*CTR]
	 Catering and removable equipment
		[*CTR]
	 Emergency equipment
		[*CTR]
	 Crew and crew baggage
		[*CTR]
		  	  

	 Total Operator’s Items
		[*CTR]
		
	 Operating Weight Empty (OWE) for the purpose of Paragraph 3
		[*CTR]

  

			
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COMMISSION PURSUANT TO A REQUEST FOR CONFIDENTIAL TREATMENT]GCI-EX10.6.9_2014.12.28-10K

Exhibit 10-6-9

AWARD AGREEMENT

STOCK UNITS

The Executive Compensation Committee of the Gannett Board of Directors has approved an award of Restricted Stock Units (referred to herein as “Stock Units”) to you under the 2001 Omnibus Incentive Compensation Plan (Amended and Restated as of May 4, 2010), as set forth below.

This Award Agreement and the enclosed Terms and Conditions effective as of ________, ____, constitute the formal agreement governing this award.

Please sign both copies of this Award Agreement to evidence your agreement with the terms hereof.  Keep one copy and return the other to the undersigned.

Please keep the enclosed Terms and Conditions for future reference. 

____________________________________________________________________________________________________

Director:                        
Grant Date:    __/__/__

Stock Unit Commencement Date:    __/__/__

		
	Stock Unit Vesting Schedule:
	25% of the Stock Units shall vest on August 1, 20__ [year of Grant Date]

25% of the Stock Units shall vest on November 1, 20__ [year of Grant Date]
25% of the Stock Units shall vest on February 1, 20__ [year following Grant Date]
25% of the Stock Units shall vest on earlier of May 1, 20__ [year following Grant Date] or the date of the 20__ Annual Meeting [year following Grant Date]

Number of Stock Units:    
______________________________________________________________________________________________________
Gannett Co., Inc.

	
				
	 
	 
	By:
	 

	Director's Signature
	 
	 
	Kevin E. Lord

	 
	 
	 
	Senior Vice President/Human Resources

STOCK UNITS
TERMS AND CONDITIONS
Under the
Gannett Co., Inc.
2001 Omnibus Incentive Compensation Plan (Amended and Restated as of May 4, 2010)

These Terms and Conditions, dated ______, ____, govern the grant of Restricted Stock Units (referred to herein as “Stock Units”) to the director (the “Director”) designated in the Award Agreement dated coincident with these Terms and Conditions.  The Stock Units are granted under, and are subject to, the Gannett Co., Inc. (the “Company”) 2001 Omnibus Incentive Compensation Plan (Amended and Restated as of May 4, 2010) (the "Plan").  Terms used herein that are defined in the Plan shall have the meaning ascribed to them in the Plan.  If there is any inconsistency between these Terms and Conditions and the terms of the Plan, the Plan’s terms shall supersede and replace the conflicting terms herein.
1.    Grant of Stock Units.  Pursuant to the provisions of (i) the Plan, (ii) the individual Award Agreement governing the grant, and (iii) these Terms and Conditions, the Company has granted to the Director the number of Stock Units set forth on the applicable Award Agreement.  Each Stock Unit shall entitle the Director to receive from the Company one share of the Company's common stock ("Common Stock") upon the Director’s separation from service.  
2.    Vesting Schedule.  Except as otherwise provided in Sections 6, 13 and 14 below, the Stock Units shall vest in accordance with the Vesting Schedule specified in the Award Agreement; provided that the Director continues as a director of the Company until the dates specified in the Vesting Schedule.
3.    Dividend Units.  Dividend units shall be credited to the Director with regard to the Stock Units.  Dividend units shall be calculated based on the dividends paid on shares of Common Stock.  Dividend units shall be deemed to be reinvested in shares of Common Stock as of the date dividends are paid on Common Stock, shall be paid to the Director at the same time and in the same form as Stock Units are paid to the Director and are subject to the same terms and conditions as the Stock Units, including, without limitation, the same vesting requirements.  The Spin-Off described in Section 14 shall not be treated as an event that triggers the crediting of a dividend unit.

4.    Delivery of Shares.  The Company shall deliver to the Director a certificate or certificates, or at the election of the Company make an appropriate book-entry, for the number of shares of Common Stock equal to the number of vested Stock Units as soon as administratively practicable after the Director separates from service, but no later than 30 days from that date.  A Director shall have no further rights with regard to the Stock Units once the underlying shares of Common Stock have been delivered.
5.    Cancellation of Stock Units.  Except as provided in Sections 6, 13 and 14 below, all unvested Stock Units granted to the Director shall automatically be cancelled upon the Director’s separation from service, and in such event the Director shall not be entitled to receive any shares of Common Stock in respect thereof.
6.    Death, Disability or Retirement.  In the event that the Director separates from service on or prior to the Stock Unit Vesting Date due to death, Disability or the age of service limitations set forth in the Company’s Bylaws, the Director (or in the case of the Director's death, the Director's estate or designated beneficiary) shall be entitled to receive at the time of the Director’s death or separation from service the total number of shares of Common Stock in respect of such Stock Units which the Director would have been entitled to receive had the Director continued employment until the Stock Unit Vesting Date.  For purposes of this Award Agreement, Disability shall mean the Director is unable to engage in any substantial gainful activity by reason of any medically determinable physical or mental impairment that can be expected to result in death or can be expected to last for a continuous period of not less than 12 months.
7.    Non-Assignability.  Stock Units may not be transferred, assigned, pledged or hypothecated, whether by operation of law or otherwise, nor may the Stock Units be made subject to execution, attachment or similar process.  
8.    Rights as a Shareholder.  The Director shall have no rights as a shareholder by reason of the Stock Units.
9.    Discretionary Plan; Employment.  The Plan is discretionary in nature and may be suspended or terminated by the Company at any time. With respect to the Plan, (a) each grant of Stock Units is a one-

time benefit which does not create any contractual or other right to receive future grants of Stock Units, or benefits in lieu of Stock Units; (b) all determinations with respect to any such future grants, including, but not limited to, the times when the Stock Units shall be granted, the number of Stock Units, and the Vesting Schedule, will be at the sole discretion of the Company; (c) the Director’s participation in the Plan is voluntary; and (d) the future value of the Stock Units is unknown and cannot be predicted with certainty.
10.    Effect of Plan and these Terms and Conditions.  The Plan is hereby incorporated by reference into these Terms and Conditions, and these Terms and Conditions are subject in all respects to the provisions of the Plan, including without limitation the authority of the Executive Compensation Committee of the Company (the "Committee") in its sole discretion to adjust awards and to make interpretations and other determinations with respect to all matters relating to the applicable Award Agreements, these Terms and Conditions, the Plan and awards made pursuant thereto.  These Terms and Conditions shall apply to the grant of Stock Units made to the Director on the date hereof and shall not apply to any future grants of Stock Units made to the Director.
11.    Notices.  Notices hereunder shall be in writing and if to the Company shall be addressed to the Secretary of the Company at 7950 Jones Branch Drive, McLean, Virginia 22107, and if to the Director shall be addressed to the Director at his or her address as it appears on the Company's records.
12.    Successors and Assigns.  The applicable Award Agreement and these Terms and Conditions shall be binding upon and inure to the benefit of the successors and assigns of the Company and, to the extent provided in Section 6 hereof, to the estate or designated beneficiary of the Director.
13.    Change in Control Provisions.
Notwithstanding anything to the contrary in these Terms and Conditions, the following provisions shall apply to all Stock Units granted under the attached Award Agreement.

(a)    Definitions.  
As used in Article 15 of the Plan and in these Terms and Conditions, a “Change in Control” shall mean the first to occur of the following:
(i)    the acquisition by any individual, entity or group (within the meaning of Section 13(d)(3) or 14(d)(2) of the Exchange Act) (a “Person”) of beneficial ownership (within the meaning of Rule 13d‐3 promulgated under the Exchange Act) of 20% or more of either (A) the then-outstanding shares of common stock of the Company (the “Outstanding Company Common Stock”) or (B) the combined voting power of the then-outstanding voting securities of the Company entitled to vote generally in the election of directors (the “Outstanding Company Voting Securities”); provided, however, that, for purposes of this Section, the following acquisitions shall not constitute a Change in Control:  (i) any acquisition directly from the Company, (ii) any acquisition by the Company, (iii) any acquisition by any employee benefit plan (or related trust) sponsored or maintained by the Company or one of its affiliates or (iv) any acquisition pursuant to a transaction that complies with Sections 13(a)(iii)(A), 13(a)(iii)(B) and 13(a)(iii)(C);
(ii)    individuals who, as of the date hereof, constitute the Board (the “Incumbent Board”) cease for any reason to constitute at least a majority of the Board; provided, however, that any individual becoming a director subsequent to the date hereof whose election or nomination for election by the Company’s stockholders was approved by a vote of at least a majority of the directors then comprising the Incumbent Board shall be considered as though such individual were a member of the Incumbent Board, but excluding, for this purpose, any such individual whose initial assumption of office occurs as a result of an actual or threatened election contest with respect to the election or removal of directors or other actual or threatened solicitation of proxies or consents by or on behalf of a Person other than the Board;
(iii)    consummation of a reorganization, merger, statutory share exchange or consolidation or similar corporate transaction involving the Company or any of its subsidiaries, a sale or other disposition of all or substantially all of the assets of the Company, or the acquisition of assets or stock of another entity by the Company or any of its subsidiaries (each, a “Business Combination”), in each case, 

unless, following such Business Combination, (A) all or substantially all of the individuals and entities that were the beneficial owners of the Outstanding Company Common Stock and the Outstanding Company Voting Securities immediately prior to such Business Combination beneficially own, directly or indirectly, more than 50% of the then-outstanding shares of common stock and the combined voting power of the then-outstanding voting securities entitled to vote generally in the election of directors, as the case may be, of the corporation or entity resulting from such Business Combination (including, without limitation, a corporation or entity that, as a result of such transaction, owns the Company or all or substantially all of the Company’s assets either directly or through one or more subsidiaries) in substantially the same proportions as their ownership immediately prior to such Business Combination of the Outstanding Company Common Stock and the Outstanding Company Voting Securities, as the case may be, (B) no Person (excluding any employee benefit plan (or related trust) of the Company or any corporation or entity resulting from such Business Combination) beneficially owns, directly or indirectly, 20% or more of, respectively, the then-outstanding shares of common stock of the corporation or entity resulting from such Business Combination or the combined voting power of the then-outstanding voting securities of such corporation or entity, except to the extent that such ownership existed prior to the Business Combination, and (C) at least a majority of the members of the board of directors of the corporation or entity resulting from such Business Combination were members of the Incumbent Board at the time of the execution of the initial agreement or of the action of the Board providing for such Business Combination; or 
(iv)    approval by the stockholders of the Company of a complete liquidation or dissolution of the Company.
(b)    Acceleration Provisions.  In the event of the occurrence of a Change in Control, the vesting of the Stock Units shall be accelerated and, if such Change in Control constitutes a “change in control event” within the meaning of Section 409A of the Code, there shall be paid out to the Director within thirty (30) days following the effective date of the Change in Control, the full number of shares of Common Stock subject to the Stock Units.  In the event of the occurrence of a Change in Control that is not a “change in 

control event” within the meaning of Section 409A of the Code, the vesting of the Stock Units shall be accelerated and the Stock Units shall be paid out at the Director’s separation from service.
(c)  Legal Fees.  The Company shall pay all legal fees, court costs, fees of experts and other costs and expenses when incurred by Director in connection with any actual, threatened or contemplated litigation or legal, administrative or other proceedings involving the provisions of this Section 13, whether or not initiated by the Director.  The Company agrees to pay such amounts within 10 days following the Company’s receipt of an invoice from the Director, provided that the Director shall have submitted an invoice for such amounts at least 30 days before the end of the calendar year next following the calendar year in which such fees and disbursements were incurred.
14.    Spin-Off.  The Company has announced its intention to create a new subsidiary for its newspaper and publishing businesses (“SpinCo”) and to distribute the stock of SpinCo to its existing shareholders (the “Spin-Off”).  With respect to Stock Units that are vested on the date of the Spin-Off (“Vested Stock Units”), each Vested Stock Unit will represent the right to receive one share of Common Stock of the Company and a number of shares of common stock of SpinCo equal to the number received for each share of Common Stock in the Spin-Off.  
With respect to Stock Units that are unvested on the date of the Spin-Off (“Unvested Stock Units”), each Unvested Stock Unit granted under this Award Agreement shall be adjusted if the Director continues service as a director of the Company in conjunction with the Spin-Off, as follows:

		
	•
	The number of Unvested Stock Units under this Award Agreement will be adjusted by multiplying such number by the “RemainCo Stock Conversion Ratio”.  The RemainCo Stock Conversion Ratio is equal to (i) divided by (ii) where: (i) is the value of one share of the Company’s Common Stock immediately before the Spin-Off; and (ii) is the value of one share of the Company’s Common Stock immediately after the Spin-Off.  Such conversion shall be effected in a manner intended generally to prevent the dilution or enlargement of rights under this Award Agreement, provided that all determinations in connection therewith (including the methodology for determining the value of a share for the RemainCo Stock Conversion Ratio) shall be made by the Committee in its sole discretion. 

		
	•
	Except as set forth above, the terms of the Award Agreement shall remain in effect.

In the event of the Spin-Off, if the Director becomes a director of SpinCo in conjunction with the Spin-Off:
		
	•
	As of the date of the Spin-Off, the Unvested Stock Units under this Award Agreement will be converted into an award agreement to receive stock units denominated in common shares of SpinCo.  The number of stock units under the SpinCo award agreement will be calculated by multiplying the number of Unvested Stock Units under this Award Agreement by the “SpinCo Stock Conversion Ratio”.  The SpinCo Stock Conversion Ratio is equal to (i) divided by (ii) where: (i) is the value of one share of the Company’s Common Stock immediately before the Spin-Off; and (ii) is the value of one share of SpinCo’s common stock immediately after the Spin-Off.  Such conversion shall be effected in a manner intended generally to prevent the dilution or enlargement of rights under this Award Agreement, provided that all determinations in connection therewith (including the methodology for determining the value of a share for the SpinCo Stock Conversion Ratio) shall be made by the Committee in its sole discretion.  

		
	•
	The Director’s termination as a director of the Company and commencement as a director of SpinCo in conjunction with the Spin-Off shall not be treated as an event that cancels the Director’s rights under Section 5 or a termination of employment under Section 6.  For all Stock Units granted under this Award Agreement, a Change in Control under Section 13 shall refer to a Change in Control of SpinCo.

		
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	Except as set forth above and for appropriate conforming changes (e.g., references to the Company shall instead refer to SpinCo, references to Common Shares shall refer to common stock of SpinCo, references to the Committee shall refer to the committee appointed by SpinCo, a Change in Control under Section 13 shall refer to a Change in Control of SpinCo, etc.), the SpinCo award agreement shall have terms and conditions that are substantially the same as the terms and conditions set forth herein.

15.    Applicable Laws and Consent to Jurisdiction.  The validity, construction, interpretation and enforceability of this Agreement shall be determined and governed by the laws of the State of Delaware without giving effect to the principles of conflicts of law.  For the purpose of litigating any dispute that arises under this Agreement, the parties hereby consent to exclusive jurisdiction in Virginia and agree that such litigation shall be conducted in the courts of Fairfax County, Virginia or the federal courts of the United States for the Eastern District of Virginia.
16.    Compliance with Section 409A.  This Award is intended to comply with the requirements of Section 409A, and shall be interpreted and administered in accordance with that intent (e.g., the definition of “separates from service” or “separation from service” (or similar term used herein) shall have the meaning ascribed to “separation from service” under Section 409A).  If any provision of these Terms and Conditions would otherwise conflict with or frustrate this intent, the provision shall not apply. Solely to the extent required 

by Section 409A of the Internal Revenue Code of 1986, as amended (the “Code”), if the Director is a “specified employee” (within the meaning of Code Section 409A and the regulations and guidance issued thereunder (“Section 409A”)) and if delivery of shares is being made in connection with the Director’s separation from service other than by reason of the Director’s death, delivery of the shares shall be delayed until six months and one day after the Director’s separation from service with the Company (or, if earlier than the end of the six-month period, the date of the Director’s death).

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