Document:

EX-4.10.8

 Exhibit 4.10.8 

SUPPLEMENTAL AGREEMENT NO. 8 

to 
 Purchase Agreement
No. 3075 
 between 

THE BOEING COMPANY 
 and

 AEROVIAS DEL CONTINENTE AMERICANO S.A. AVIANCA 

Relating to Boeing Model 787-859 and 787-9 Aircraft 

THIS SUPPLEMENTAL AGREEMENT, is entered into as of the 3rd day of May 2018, by and
between THE BOEING COMPANY, a Delaware corporation with its principal offices in the City of Seattle, State of Washington, USA (Boeing), and AEROVIAS DEL CONTINENTE AMERICANO S.A. AVIANCA, a company organized under the laws of
the country of Columbia (Buyer); 
 Recitals 

1. Boeing and Buyer entered into Purchase Agreement No. PA-3075, dated 03 October 2006, as amended and supplemented
(the Agreement) relating to the purchase and sale of Boeing Model 787-859 and 787-9 aircraft (Aircraft). 

2. Pursuant to paragraph 2 of Letter Agreement AVI-PA-3075-LA-1704835 to the Agreement, titled “Open Configuration Matters 787-9”, Boeing is incorporating the Customer Configuration Changes
into the Agreement. 
  

	
	
	    

 Agreement 

The parties agree to amend the Agreement as follows: 

  

			
	 PA3075

SA-8
	  	 AVI

STA

	1.	 Table of Contents. 

Remove and replace the current Table of Contents with a new Table of Contents (attached hereto) to reflect the incorporation of this
Supplemental Agreement No. 8 (SA-8) to the Agreement. 
  

	
	
	    

  

	3.	 Exhibits. 

Remove and replace Exhibit A-1 with a new Exhibit A-1 (attached
hereto) to reflect incorporation of the Customer Configuration Changes to the Agreement. 
  

	
	
	    

 This SA-8 will expire if not signed by Buyer on or before May 18,
2018. 
 The Agreement, Pricing Tables, and Exhibits shall be deemed amended to the extent herein provided and as so amended shall continue
in full force and effect. In the event of any inconsistency between the above provisions and those provisions contained in the Agreement, the terms of this SA-8 will govern and control. 

  

			
	 PA3075

SA-8
	  	 AVI

STA

 EXECUTED IN DUPLICATE as of the date written above, 

 

			
	 THE BOEING COMPANY

			
		
	By  	 	 

			
	Its Attorney-In-Fact

  

	
	AEROVIAS DEL CONTINENTE AMERICANO S.A. AVIANCA
	
	 /s/ Roberto Held

	 Legal Representative

  

					
		 	
			
	Its  	 	 	 	 
		 		 	

  

			
	 PA3075

SA-8
	  	AVI

 TABLE OF CONTENTS 
  

							
	ARTICLES	  	 
 
	SA
 NUMBER
	 
  

			
	 1.
	 	Quantity, Model and Description	  			
	 2.
	 	Delivery Schedule	  			
	 3.
	 	Price	  			
	 4.
	 	Payment	  			
	 5.
	 	Miscellaneous	  			
			
	TABLE	 		  			
			
	 1-1
	 	Aircraft Information Table	  	 	SA-6	 
	 1-2
	 	Aircraft Information Table	  	 	SA-6	 
	 1-3
	 	Aircraft Information Table	  	 	SA-7	 
	 1-4
	 	Aircraft Information Table 787-9	  	 	SA-8	 
			
	EXHIBIT	 		  			
			
	 A.
	 	Aircraft Configuration	  	 	SA-5	 
			
	 A-1.
	 	Aircraft Configuration 787-9	  	 	SA-8	 
			
	 B.
	 	Aircraft Delivery Requirements and Responsibilities	  			
		
	SUPPLEMENTAL EXHIBITS	  			
			
	 AE1.
	 	Escalation Adjustment/Airframe and Optional Features	  			
			
	 BFE1
	 	Buyer Furnished Equipment Variables	  	 	SA-3	 
			
	 BFE1-1.
	 	Buyer Furnished Equipment Variables 787-9	  	 	SA-7	 
			
	 CS1.
	 	Buyer Support Document	  			
			
	 EE1.
	 	Engine Escalation/Engine Warranty and Patent Indemnity	  	 	SA-2	 
			
	 SLP1.
	 	Service Life Policy Components	  			

  

  

			
	 PA3075
 SA-8
	  	 AVI

STA

					
	 LETTER AGREEMENTS
	  	SA
NUMBER
			
	 3075-01
	 	 787 Open Configuration Matters
	  	
	 3075-02
	 	 787 Spare Parts Commitment
	  	
	 3075-03
	 	 787 Spare Parts Initial Provisioning
	  	
	 3075-04
	 	 Aircraft Model Substitution
	  	
	 3075-05
	 	 Demonstration Flight Waiver
	  	
	 3075-06
	 	 Schedule Reliability
	  	
	 3075-07
	 	 Spare Parts — Flight Crew Training
	  	
			
	 6-1162-DME-0895
	 	 AD Cost Materials
	  	
			
	 6-1162-DME-0896R1
	 	 Performance Guarantees and Attachments
	  	SA-6
			
	 6-1162-DME-0897
	 	 Alternate Engine Selection
	  	SA-2
			
	 6-1162-DME-0898
	 	 GEnx Performance Retention and
Attachment
	  	SA-2
			
	 6-1162-DME-0899
	 	 Trent Performance Retention and
Attachment
	  	
			
	 6-1162-DME-0900
	 	 Maintenance Cost Guarantees and
Attachment
	  	
			
	 6-1162-DME-0901R4
	 	 Advance Payment Matters and Attachments A & B
SA-7
	  	
			
	 6-1162-DME-0902
	 	 Promotional Support
	  	SA-1
			
	 6-1162-DME-0903R2
	 	 Purchase Rights
	  	SA-3
			
	 6-1162-DME-0904R1
	 	 Special Matters
	  	SA-6
			
	 6-1162-DME-0905R1
	 	 Escalation Risk Control Facility and Attachments A & B
	  	SA-3
			
	 6-1162-DME-0905-01
	 	 Fixed Escalation factors
	  	SA-3
			
	 6 1162 DME 0905 02
	 	 Process for Fixing Escalation Factors
	  	SA-3
			
	 6-1162-DME-0906R1
	 	 Customer Services Matters and
Attachment
	  	SA-2
			
	 6-1162-DME-0907
	 	 AGTA Matters
	  	
			
	
6-1162-DME-1089 
R1
	 	 Banded Fixed Escalation Program
	  	SA-3
			
	 6-1167-DME-1347
	 	 Additional Special Matters — Scheduled Month Aircraft
	  	SA-3
			
	 LA-1704594
	 	 Aircraft Performance Guarantees 787-9
	  	SA-7
			
	 LA-1704834
	 	 Special Matters 787-9
	  	SA-7
			
	 LA-1704835
	 	 Open Configuration Matters 787-9
	  	SA-7
			
	 LA-1704838
	 	 Advance Payment Matters 787-9
	  	SA-7
			
	 LA-1704897
	 	 Maintenance Cost Guarantees 787-9
	  	SA-7

 RECORD OF
SUPPLEMENTAL AGREEMENTS 
  

					
	 SA-1
	  	 28 March
	  	 2007

	 SA-2
	  	 21 November
	  	 2007

	 SA-3
	  	 26 September
	  	 2012

	 SA-4
	  	 11 January
	  	 2013

	 SA-5
	  	 15 April
	  	 2014

	 SA-6
	  	 25 July
	  	 2017

	 SA-7
	  	 19 September
	  	 2017

	 SA-8
	  	   3 May
	  	 2018

  

			
	 PA3075
 SA-8
	  	 AVI

STA

 Table 1-4 To 

Supplemental Agreement No. 8 Purchase Agreement No. PA-03075 

787-9 Aircraft Delivery, Description, Price and Advance Payments 

 

									
	 Airframe Model/MTOW: 
	  	 	787-9	 	  	 	545,000 pounds	 
	  
 Engine Model/Thrust:

	  	 	TRENT1000-N	 	  	 	76,000 pounds	 
	  
 Airframe
Price:
	  				  			
	  
 Optional
Features:
	 
  

	  
 Sub-Total of Airframe and Features:
	 
  

	  
 Engine Price
(Per Aircraft):
	 
  

	  
 Aircraft Basic
Price (Excluding BFE/SPE):
	 
  

	  
 Buyer
Furnished Equipment (BFE) Estimate:
	 
  

	  
 Fixed In-Flight Entertainment (IFE):
	 
  

	  
 Seller
Purchased Equipment (SPE) Estimate:
	 
  

	  
 Deposit per
Aircraft:
	  			

													
			 			
	  
 Airframe Price Base
Year/Escalation Formula:
	  	 	Jan-17	 	  				 	 	ECI-MFG/CPI	 
	  
 Engine Price Base
Year/Escalation Formula:
	  	 	Jan-17	 	  				 	 	787 ECI-MFG CPI Eng	 
	  
 Airframe Escalation
Data:
	  				  	 	    	 	 			
	  
 Base Year Index
(ECI):
	  				  				 			
	  
 Base Year Index
(CPI):
	  				 			
	  
 Engine Escalation
Data:
	  				 			
	  
 Base Year Index
(ECI):
	  				 			
	  
 Base Year Index
(CPI):
	  				 			

 
 

  

															
	 Delivery

Date
	 	Number of
Aircraft	 	Escalation
Factor
(Airframe)	 	Escalation
Factor
(Engine)	 	        	 	 	Escalation Estimate
Adv Payment Base
Price Per A/P	  	
Advance Payment Per Aircraft (Amts. Due/
Mos. Prior to Delivery):

	  	  

                 
                                         
                    
  

                 
                                         
              

	 May-2019
	 	1	 	                           
       	 				 	                 	  	                             
                                         
                                 
	 Aug-2019
	 	1	 	                           
       	 				 	                 	  	                             
                                         
                                 
	 0ct-2019
	 	1	 	                           
       	 				 	                 	  	                             
                                         
                                 
	 Total:
	 	3	 		 		 				 		  	

  

					
	AVI-PA-03075 109000-1F.txt	  	                             
                      	  	Page 1
	STA	  		  	

 AIRCRAFT CONFIGURATION 

between 
 THE BOEING
COMPANY 
 and 

AEROVIAS DEL CONTINENTE AMERICANO S.A. 

AVIANCA 
 EXHIBIT A to
PURCHASE AGREEMENT 
 NUMBER 

PA-03075 

  

					
	P.A. 3075-SA-8	  		  	Page 1
		  		  	STA

 EXHIBIT A 

AIRCRAFT CONFIGURATION 

DATED May 3, 2018 

relating to 
 BOEING
MODEL 787-9 AIRCRAFT 
 The Detail Specification is Boeing document number                                
   XXXXX (replace “XXXXX” by actual Aircraft manufacturer’s serial number), to be released approximately thirty (30) days prior to the scheduled Aircraft delivery. The
Detail Specification provides further description of Customer’s configuration set forth in this Exhibit A. Such Detail Specification will be comprised of Boeing configuration specification                                
                                         as amended to incorporate the optional features (Options) listed below, including the effects on Manufacturer’s Empty Weight (MEW) and Operating Empty Weight (OEW). As soon as
practicable, Boeing will furnish to Customer copies of the Detail Specification, which copies will reflect such Options. The Aircraft Basic Price reflects and includes all effects of such Options, except such Aircraft Basic Price does not include
the price effects of any Buyer Furnished Equipment or Seller Purchased Equipment. 

  

					
	P.A. 3075-SA-8	  		  	Page 2
		  		  	STA

 Exhibit A To 

Boeing Purchase Agreement 
  

					
	Customer Log:	  	                              
    
	Customer:	  	AVI-Avianca	  	
	Model:	  	787-9	  	
	Base Date:	  	JAN 2017
	Qty of A/C:	  	3

  

							
	 	  	 	 	2017$        	 
	 	  	 	 	3 A/P        	 
	 	  	 	 	Price        	 
	 CR
	  	 Title
	 	Per A/C $        	 
	 0110B750A60
	  	MAJOR MODEL 787 AIRPLANE	 			
	 0110B750A66
	  	MINOR MODEL 787-9 AIRPLANE	 			
	 0130E857W64
	  	INTERIOR ARRANGEMENT - 309 PASSENGERS - AVIANCA (AVI)	 			
	 0220E951B42
	  	TYPE CERTIFICATE & CERTIFICATE OF AIRWORTHINESS	 			
	 0221D047K94
	  	TAKEOFF AND LANDING WITH TAILWIND UP TO 15 KNOTS	 			
	 0221D047K95
	  	ENGINE INOPERATIVE TEN-MINUTE TAKEOFF THRUST OPERATION	 			
	 0222E951B33
	  	ALTERNATE FORWARD CENTER-OF-GRAVITY VALUES	 			
	 0228C512A10
	  	FLIGHT CREW OPERATIONS MANUAL DATA IN COMPLIANCE WITH FAA REQUIREMENTS	 			
	 0228E951B34
	  	AIRPLANE FLIGHT MANUAL	 			
	 0352C512A15
	  	CUSTOMIZED LOADING SCHEDULE FOR WEIGHT AND BALANCE CONTROL - UNIVERSAL INDEX LOADING	 			
	 0910C512A16
	  	AFT TOW FITTING - NOSE LANDING GEAR	 			
	 1110E556A56
	  	NON-STANDARD NACELLES COLOR	 			
	 1110E857U82
	  	EXTERIOR COLOR SCHEME AND MARKING	 			
	 1130C171N57
	  	FOREIGN REGULATORY AIRPLANE REGISTRY PLACARD	 			
	 1130E176C10
	  	EXTERNAL DATA PLATE	 			
	 1130E857U83
	  	INTERIOR PASSENGER COMPARTMENT PLACARDS AND MARKINGS	 			
	 1130E857U87
	  	LEASING/OWNERSHIP NAMEPLATES	 			
	 1200D047F19
	  	SERVICE OPTION - ENHANCED AIRBORNE FLIGHT RECORDER (EAFR) STATEMENT OF COMPLIANCE LETTER	 			
	 2120D047G27
	  	PERSONAL AIR OUTLET (PAO) FOR PASSENGER	 			
	 2154C512B72
	  	FORWARD CARGO COMPARTMENT AIR-CONDITIONING SYSTEM	 			
	 2170C512A18
	  	FLIGHT DECK HUMIDIFICATION SYSTEM	 			
	 2324E556C53
	  	FIXED EMERGENCY LOCATOR TRANSMITTER (ELT) - ANTENNA & CONTROL PANEL, SERIAL USER PROTOCOL WITH AIRCRAFT 24-BIT ADDRESS	 			
	 2327C512H95
	  	ATN DATALINK	 			
	 2351E556B30
	  	FLIGHT INTERPHONE - HAND-HELD MICROPHONES AND HOLDER - CAPTAIN, FIRST OFFICER	 			
	 2351E556B31
	  	FLIGHT INTERPHONE - HAND-HELD MICROPHONES AND HOLDER - FIRST OBSERVER	 			

  

					
	P.A. 3075-SA-8	  		  	Page 3
		  	                             
                      	  	
		  		  	STA

							
	 2375C512B73
	  	FLIGHT DECK ENTRY VIDEO SURVEILLANCE SYSTEM (FDEVSS)	  	 	                    	 
	 2523E857U91
	  	PASSENGER SERVICE UNIT (PSU) & OXYGEN MASK LOCATION ARRANGEMENT INSTALLATION	  			
	 2524E857W03
	  	CLOSET - FULL HEIGHT - C1F-1L	  			
	 2524E857W07
	  	CURTAIN - CREW REST ENCLOSURE - ROW 40 CENTERLINE	  			
	 2524E857W08
	  	PARTITION - OUTBOARD - DOOR 4L FWD	  			
	 2524E857W09
	  	PARTITION - OUTBOARD - DOOR 4R FWD	  			
	 2524E857W10
	  	CURTAIN - DR1 CTR	  			
	 2524E857W11
	  	CURTAIN - DOOR 1L - AFT	  			
	 2524E857W12
	  	CURTAIN - DOOR 1R-AFT	  			
	 2524E857W13
	  	CURTAIN - DOOR 1L - AFT - 2	  			
	 2524E857W14
	  	CURTAIN - DOOR 1R - AFT - 2	  			
	 2524E857W15
	  	CURTAIN - DOOR 2L - FWD	  			
	 2524E857W16
	  	CURTAIN - DOOR 2R - FWD	  			
	 2524E857W17
	  	CURTAIN - DOOR 2L - AFT	  			
	 2524E857W18
	  	CURTAIN - DOOR 2R - AFT	  			
	 2524E857W21
	  	CURTAIN - DOOR 4L - CROSS-AISLE	  			
	 2524E857W22
	  	CURTAIN - DOOR 4R - CROSS-AISLE	  			
	 2524E857X25
	  	CURTAIN - DOOR 2L - AFT - 2	  			
	 2524E857X26
	  	CURTAIN - DOOR 2R - AFT - 2	  			
	 2524E939K70

2524E939K71
	  	 CURTAIN - CREW REST ENCLOSURE - ROW 41 CENTERLINE

TBS3 - BUSINESS CLASS FRONT ROW MONUMENTS - ZAII - BFE
	  			
	 2525E857U93
	  	PASSENGER SEAT INSTALLATION - BUSINESS CLASS - ZSUS - CIRRUS III-28 PAX-BFE	  			
	 2525E939K83
	  	ECONOMY CLASS SEAT - ZODIAC SEATS US - 5751 - 9 ABREAST SEATING (3-3-3)	  			
	 2525E951B35
	  	TAMPER EVIDENT LIFE VEST SEALS	  			
	 2526E857W01
	  	CABIN ATTENDANT PANEL	  			
	 2526E857W02
	  	VIDEO CONTROL STATION (VCS) - WALL MOUNTED	  			
	 2526E857W23
	  	ATTENDANT SEAT - STANDARD - DOOR 1L FWD - AS1F-1L	  			
	 2526E857W24
	  	ATTENDANT SEAT - STANDARD - DOOR 1L AFT - AS1A-1L	  			
	 2526E857W25
	  	ATTENDANT SEAT - STANDARD - DOOR 1R AFT - AS1A-1R	  			
	 2526E857W26
	  	ATTENDANT SEAT - STANDARD - DOOR 2L FWD - AS2F-1L	  			
	 2526E857W27
	  	ATTENDANT SEAT - STANDARD - DOOR 2R FWD - AS2F-1R	  			
	 2526E857W28
	  	ATTENDANT SEAT - STANDARD - DOOR 2L AFT - AS2A-1L	  			
	 2526E857W29
	  	ATTENDANT SEAT - STANDARD - DOOR 2R AFT - AS2A-1R	  			
	 2526E857W30
	  	ATTENDANT SEAT - STANDARD - DOOR 3L FWD - AS3F-1L	  			
	 2526E857W31
	  	ATTENDANT SEAT - STANDARD - DOOR 3R FWD - AS3F-1R	  			
	 2526E857W32
	  	ATTENDANT SEAT - HIGH COMFORT - DOOR 4 LEFT CTR - AS4A-1LC	  			
	 2526E857W33
	  	ATTENDANT SEAT - HIGH COMFORT - DOOR 4 RIGHT CTR - AS4A-1RC	  			
	 2526E857X27
	  	ATTENDANT SEAT - STANDARD - DOOR 4L AFT - AS4A-1L	  			
	 2526E857X28
	  	ATTENDANT SEAT - STANDARD - DOOR 4R AFT - AS4A-1R	  			
	 2527E095A67
	  	TBS3 - GALLEY & ENTRY FLOOR MAT - NON-ICO COLOR	  			
	 2527E857U98
	  	FLOOR COVERING COLLECTOR	  			
	 2528C512F39
	  	DOOR 4 OVERHEAD CEILING STOWAGE	  			

  

					
	P.A. 3075-SA-8	  		  	Page 4
		  	                             
                      	  	
		  		  	STA

					
	2528E857W34	 	LITERATURE POCKETS	  	                    
	2528E857W38	 	OVERHEAD STOWAGE BINS	  	
	2528E857W40	 	ATTENDANT MODULES (AMODS)	  	
	2528E857W41	 	FLOOR MOUNTED STOWAGE UNIT - DOOR 3C FWD	  	
	2528E857W42	 	FLOOR MOUNTED STOWAGE UNIT - DOOR 3L FWD	  	
	2528E857W43	 	FLOOR MOUNTED STOWAGE UNIT - DOOR 3R FWD	  	
	2528E857W44	 	FLOOR MOUNTED STOWAGE UNIT - DOOR 4C FWD	  	
	2528E857W45	 	FLOOR MOUNTED STOWAGE UNIT - DOOR 4L FWD	  	
	2528E857W46	 	FLOOR MOUNTED STOWAGE UNIT - DOOR 4R FWD	  	
	2529C171K37	 	OVERHEAD FLIGHT CREW REST (OFCR) - 58” SINGLE SEAT - STABLE SYSTEMS, EQUIPMENT AND MODULES	  	
	2529E857W47	 	MEDICAL ELECTRICAL OUTLETS	  	
	2529E857W48	 	OVERHEAD FLIGHT CREW REST (OFCR) - 58-INCH SINGLE SEAT ENCLOSURE SELECTABLES	  	
	2530E095B62	 	TBS3 - GALLEY G1F-1C - DOOR 1 FWD CENTER - DUST BAG HOLDER	  	
	2530E857W66	 	TBS3 - CUSTOMER SPECIFIED STANDARD CONTAINERS - CERTIFICATION	  	
	2530E857W68	 	GALLEY - FAMILY 1 - G1F-1C	  	
	2530E857W69	 	GALLEY - FAMILY 5A- G2F-1C	  	
	2530E857W70	 	GALLEY - FAMILY 6E - G2A-1C	  	
	2530E857W73	 	GALLEY - FAMILY 50 - G4A-1C	  	
	2530E857X33	 	GALLEY - FAMILY 21A - G4F-1C	  	
	2530E857X44	 	GALLEY - FAMILY 33 - G2F-1L	  	
	2530E857X45	 	GALLEY - FAMILY 33 - G2F-1R	  	
	2530E939K98	 	GALLEY - INSERT PART NUMBERS - ELECTRICAL - AVI	  	
	2530E939K99	 	TBS3 - CUSTOMER SPECIFIED GALLEY CARTS - CERTIFICATION	  	
	2540E095A72	 	TBS3 - LAVATORIES - FLOOR MAT - NON-ICO COLOR - AVI	  	
	2540E857W74	 	TBS3 - LAVATORIES - SANITARY WIPE DISPENSER HOLDER INSTALLATION	  	
	2540E857W75	 	TBS3 - LAVATORIES - TOILET SEAT COVER DISPENSER HOLE COVER	  	
	2540E857W81	 	LAVATORY - FAMILY 11 - L1A-1L	  	
	2540E857W82	 	LAVATORY - FAMILY 12 - L1A-1R	  	
	2540E857X34	 	LAVATORY - FAMILY 95 - L3F-1LC	  	
	2540E857X35	 	LAVATORY - FAMILY 96 - L3F-1RC	  	
	2540E857X36	 	LAVATORY - FAMILY 11 - L2A-1L	  	
	2540E857X39	 	LAVATORY - FAMILY 12 - L2A-1R	  	
	2540E857X40	 	LAVATORY - FAMILY 11 - L3F-1L	  	
	2540E857X41	 	LAVATORY - FAMILY 12 - L3F-1R	  	
	2560C171H74	 	PROTECTIVE BREATHING EQUIPMENT- FLIGHT DECK - AVOX - P/N 802300-14	  	
	2560E951B36	 	CREW LIFE VESTS - FLIGHT DECK - NON-STANDARD - BFE	  	
	2560F079J39	 	TBS3 - PORTABLE FIRE EXTINGUISHER - CLEAN AGENT - INSTALLATION - FLIGHT DECK - KIDDE	  	
	2562E857W49	 	OVERWATER EMERGENCY EQUIPMENT	  	
	2564E857W50	 	DETACHABLE EMERGENCY EQUIPMENT	  	

  

					
	P.A. 3075-SA-8	  		  	Page 5
		  	                             
                      	  	STA

					
	2566C512A88	 	ESCAPE SYSTEM, PASSENGER CAPACITY UP TO 355 WITH SLIDE/RAFTS AT ALL DOORS (C-A-A-A)	  	                    
	3245C513A04	 	WHEELS AND CARBON BRAKES - MESSIER-BUGATTI	  	
	3350E939K72	 	TBS3 - EMERGENCY ESCAPE PATH LIGHTING - FLOOR MOUNTED - PHOTOLUMINESCENT - LUFTHANSA TECHNIK - BFE	  	
	3520C513A10	 	PASSENGER OXYGEN MEDIUM CAPACITY DESCENT	  	
	3810C512A56	 	POTABLE WATER STORAGE CAPACITY INCREASE - 270 GALLONS	  	
	3810C512C10	 	POTABLE WATER PRE-SELECT AT ATTENDANT CONTROL PANEL	  	
	4420C512G92	 	WALL-MOUNTED VIDEO CONTROL STATION (VCS) EQUIPMENT - PANASONIC	  	
	4420D047L04	 	THREE CONTENT SERVERS TWO NETWORK CONTROLLERS CONFIGURATION E-2 RACK INSTALLATIONS (-9 ONLY) - PANASONIC	  	
	 4420D942A62
 4420D985A07
	 	ACARS ACTIVATION - PANASONIC	  	
	 	TBS3 - INFLIGHT ENTERTAINMENT SYSTEM - INSTALLATION - ECO 11 INCH DISPLAY - OVERHEAD FLIGHT CREW REST	  	
	4420F163B36	 	PANASONIC IN-SEAT VIDEO EQUIPMENT - ECONOMY CLASS SEATS	  	
	4420F163B43	 	PANASONIC IN-SEAT VIDEO EQUIPMENT - BUSINESS CLASS SEATS -16” ELITE	  	
	4420F163B50	 	OVERHEAD FLIGHT CREW REST IFE EQUIPMENT INSTALLATION - PANASONIC	  	
	4420F163B53	 	INFLIGHT ENTERTAINMENT SYSTEM - COLOR DEFINITION - PANASONIC	  	
	4611C512A60	 	SECOND MAINTENANCE SYSTEMS FILE SERVER MODULE	  	
	4611C947B61	 	AIRLINE FILE SERVER MODULE (AFSM)	  	
	4611D855A30	 	TERMINAL CELLULAR SYSTEM	  	
	5621E857X42	 	WINDOW PLUGS	  	
	7200B750A70	 	ROLLS-ROYCE PROPULSION SYSTEM	  	
	7200E951B37	 	ROLLS-ROYCE TRENT 1000 THRUST RATINGS - TRENT 1000-N	  	
	7900E556C05	 	LUBRICATING OIL - EASTMAN 2197	  	
	MISC	 	INTERIOR ALLOWANCE	  	
	SUBTOTAL OPTIONS SUBJECT TO ESCALATION	  	
			
	2120D047G27ADJ	 	 PERSONAL AIR OUTLET (PAO) FOR PASSENGER
                                  

	  	
	TOTAL OPTIONS SUBJECT TO ESCALATION	  	
			
		 	FIXED PRICE OPTIONS:	  	
	4420AVIP309	 	AVI - PANASONIC IFE SYSTEM PRICE	  	
	TOTAL FIXED PRICE OPTIONS	  	

  

					
	P.A. 3075-SA-8	  		  	Page 6
		  	                             
                      	  	STAEX-4.10.9

 Exhibit 4.10.9 

SUPPLEMENTAL AGREEMENT NO. 9 

to 
 Purchase Agreement
No. 3075 
 between 

THE BOEING COMPANY 
 and

 AEROVIAS DEL CONTINENTE AMERICANO S.A. AVIANCA 

Relating to Boeing Model
787-8     and 787-9 Aircraft 

THIS SUPPLEMENTAL AGREEMENT, is entered into as of the 26th day of February 2019, by and between THE BOEING
COMPANY, a Delaware corporation with its principal offices in the City of Seattle, State of Washington, USA (Boeing), and Aerovias del Continente Americano S.A. AVIANCA, a company organized under the laws of the country of Colombia
(Buyer); 
 Recitals 

1. Boeing and Buyer entered into Purchase Agreement No. 3075, dated 03 October 2006, as amended and supplemented (the Agreement)
relating to the purchase and sale of Boeing Model 787-8     and 787-9 aircraft (Aircraft). 
 2. Boeing and Buyer now wish to amend the Agreement to:
(i) update the configuration of one (1) model 787-9 aircraft; (ii) reschedule the delivery dates of two (2) model 787-9 aircraft (together Aircraft in (i) and (ii) are the Re-Contracted Aircraft); and (iii) update the performance guarantees. 

Agreement 
 The parties
agree to amend the Agreement as follows: 
  

	 	1.	 Table of Contents. 

Remove and replace the Table of Contents with a new Table of Contents (attached hereto) to reflect the incorporation of this
Supplemental Agreement No. 9 (SA-9) into the Agreement. 
  

  

			
	 PA3075
 SA-9
	  	AVI

	 	2.	 Pricing Tables. 

2.1 Table 1-4 is hereby deleted in its entirety and replaced with Table 1-4 (attached hereto) to: (i) replace the TRENT1000-N engine model with TRENT1000-K engine model; and (ii) remove two
(2) of the Re-Contracted Aircraft. 
 2.2 Table
1-5 (attached hereto) is hereby added to the Agreement to reflect the rescheduled delivery dates of two (2) of the Re-Contracted Aircraft. 

 

	 	3.	 Letter Agreements. 

3.1 Letter Agreement AVI-PA-3075-LA-1704594, titled “Aircraft Performance Guarantees 787-9” is hereby cancelled and replaced with Letter Agreement AVI-PA-3075-LA-1704594R1, titled “Aircraft Performance Guarantees 787-9” (attached hereto). 
 3.2 Letter Agreement AVI-PA-3075-LA-1809416, titled “Aircraft Configuration Matters 787-9”
(attached hereto) is hereby added to the Agreement. 
  

	 	4.	 Miscellaneous. 

 

			
		
		 	

 4.3 The Agreement shall be deemed amended to the extent herein provided and as so amended shall
continue in full force and effect. In the event of any inconsistency between the above provisions and those provisions contained in the Agreement, the terms of this SA-9 will govern and control. 

[Signatures on the following page] 

  

			
	 PA3075
 SA-9
	  	AVI

 EXECUTED IN DUPLICATE as of the date written above, 

THE BOEING COMPANY 
  

			
		
	By	 	  

	Its	 	

 AEROVIAS DEL CONTINENTE AMERICANO S.A. AVIANCA 

			
		
	By	 	 /s/ Renato Covelo

	Its	 	 Secretary General/Officer

  

			
	 PA3075
 SA-9
	  	AVI

 EXECUTED IN DUPLICATE as of the date written above, 

THE BOEING COMPANY 
  

			
	By	 	                               
     
	Its	 	                               
     

 AEROVIAS DEL CONTINENTE AMERICANO S.A. AVIANCA 

			
		
	By	 	 /s/ Renato Covelo

	Its	 	Secretary General/Officer

  

			
	 PA3075
 SA-9
	  	AVI

 TABLE OF CONTENTS 
  

							
	ARTICLES	  	 
	SA
NUMBER	 
 
			
	 1.
	 	Quantity, Model and Description	  			
	 2.
	 	Delivery Schedule	  			
	 3.
	 	Price	  			
	 4.
	 	Payment	  			
	 5.
	 	Miscellaneous	  			
			
	TABLE	 		  			
			
	 1-1
	 	Aircraft Information Table	  	 	SA-6	 
	 1-2
	 	Aircraft Information Table	  	 	SA-6	 
	 1-3
	 	Aircraft Information Table	  	 	SA-7	 
	 1-4
	 	Aircraft Information Table 787-9	  	 	SA-9	 
	 1-5
	 	Aircraft Information Table 787-9	  	 	SA-9	 
		
	EXHIBIT	  			
			
	 A.
	 	Aircraft Configuration	  	 	SA-5	 
			
	 A-1.
	 	Aircraft Configuration 787-9	  	 	SA-8	 
			
	 B.
	 	Aircraft Delivery Requirements and Responsibilities	  			
		
	SUPPLEMENTAL EXHIBITS	  			
			
	 AE1.
	 	Escalation Adjustment/Airframe and Optional Features	  			
			
	 BFE1
	 	Buyer Furnished Equipment Variables	  	 	SA-3	 
			
	 BFE1-1.
	 	Buyer Furnished Equipment Variables 787-9	  	 	SA-7	 
			
	 CS1.
	 	Buyer Support Document	  			
			
	 EE1.
	 	Engine Escalation/Engine Warranty and Patent Indemnity	  	 	SA-2	 
			
	 SLP1.
	 	Service Life Policy Components	  			

  

			
	 PA3075
 SA-9
	  	AVI

					
	 LETTER AGREEMENTS
	  	SA
 NUMBER

			
	 3075-01
	 	 787 Open Configuration Matters
	  	
	 3075-02
	 	 787 Spare Parts Commitment
	  	
	 3075-03
	 	 787 Spare Parts Initial Provisioning
	  	
	 3075-04
	 	 Aircraft Model Substitution
	  	
	 3075-05
	 	 Demonstration Flight Waiver
	  	
	 3075-06
	 	 Schedule Reliability
	  	
	 3075-07
	 	 Spare Parts – Flight Crew Training
	  	
			
	 6-1162-DME-0895
	 	 AD Cost Materials
	  	
	 6-1162-DME-0896R1
	 	 Performance Guarantees and Attachments
	  	SA-6
	 6-1162-DME-0897
	 	 Alternate Engine Selection
	  	SA-2
	 6-1162-DME-0898
	 	 GEnx Performance Retention and Attachment
	  	SA-2
	 6-1162-DME-0899
	 	 Trent Performance Retention and Attachment
	  	
	 6-1162-DME-0900
	 	 Maintenance Cost Guarantees and Attachment
	  	
	 6-1162-DME-0901R4
	 	 Advance Payment Matters and Attachments A & B
	  	SA-7
	 6-1162-DME-0902
	 	 Promotional Support
	  	SA-1
	 6-1162-DME-0903R2
	 	 Purchase Rights
	  	SA-3
	 6-1162-DME-0904R1
	 	 Special Matters
	  	SA-6
	 6-1162-DME-0905R1
	 	 Escalation Risk Control Facility and Attachments A & B
	  	SA-3
	 6-1162-DME-0905-01
	 	 Fixed Escalation factors
	  	SA-3
	 6-1162-DME-0905-02
	 	 Process for Fixing Escalation Factors
	  	SA-3
	 6-1162-DME-0906R1
	 	 Customer Services Matters and Attachment
	  	SA-2
	 6-1162-DME-0907
	 	 AGTA Matters
	  	
	 6-1162-DME-1089-R1
	 	 Banded Fixed Escalation Program
	  	SA-3
	 6-1167-DME-1347
	 	 Additional Special Matters – Scheduled Month Aircraft
	  	SA-3
	 LA-1704594R1
	 	 Aircraft Performance Guarantees 787-9
	  	SA-9
	 LA-1704834
	 	 Special Matters 787-9
	  	SA-7
	 LA-1704835
	 	 Open Configuration Matters 787-9
	  	SA-7
	 LA-1704838
	 	 Advance Payment Matters 787-9
	  	SA-7
	 LA-1704897
	 	 Maintenance Cost Guarantees 787-9
	  	SA-7
	 LA-1809416
	 	 Aircraft Configuration Matters 787-9
	  	SA-9

 RECORD OF SUPPLEMENTAL AGREEMENTS 

 

					
	 SA-1
	  	 28 March
	  	 2007

	 SA-2
	  	 21 November
	  	 2007

	 SA-3
	  	 26 September
	  	 2012

	 SA-4
	  	 11 January
	  	 2013

	 SA-5
	  	 15 April
	  	 2014

	 SA-6
	  	 25 July
	  	 2017

	 SA-7
	  	 19 September
	  	 2017

	 SA-8
	  	 3 May
	  	 2018

	 SA-9
	  	
                  
      
	  	 2019

  

			
	 PA3075
 SA-9
	  	AVI

  

 Table 1-4 To 

Supplemental Agreement No. 9 Purchase Agreement No. PA-03015 

Aircraft Delivery, Description, Price and Advance Payments 

 

					
	Airframe Model/MTOW:	 	787-9	 	545,000 pounds
			
	Engine Model/Thrust:	 	TRENT1000-K	 	74,400 pounds
			
	Airframe Price:	 		 	              
			
	Optional Features:	 		 	            
			
	Fixed In-Flight Entertainment (IFE):	 		 	            
		 		 	  

			
	Sub-Total of Airframe and Features:	 		 	              
			
	Engine Price (Per Aircraft):	 		 	            
			
	Aircraft Basic Price (Excluding BFE/SPE):	 		 	              
		 		 	  

			
	Buyer Furnished Equipment (BFE) Estimate:	 		 	            
			
	Seller Purchased Equipment (SPE) Estimate:	 		 	        
			
	Deposit per Aircraft:	 		 	          
			
		 		 	

					
	                	 	                        
			
	Airframe Price Base Year/Escalation Formula:	 	Jan-17	 	ECI-MFG/CPI
			
	Engine Price Base Year/Escalation Formula:	 	Jan-17	 	787 ECI-MFG CPI Eng
			
	Airframe Escalation Data:	 		 	
			
	Base Year Index (ECI):	 		 	    
			
	Base Year Index (CPI):	 		 	    
			
	Engine Escalation Data:	 		 	
			
	Base Year Index (ECI):	 		 	    
			
	Base Year Index (CPI):	 		 	    

 
 

  

																			
	 Delivery

Date
	  	Number of
Aircraft	  	Escalation
Factor
(Airframe)	  	Escalation
Factor
(Engine)	  	 
	  	Escalation Estimate
Adv Payment Base
Price Per A/P	  	Advance Payment Per Aircraft (Amts.
Due/Mos. Prior to Delivery):
	  	At Signing
1%	  	24 Mos.
4%	  	21/18/12/9/6
Mos.	  	    
    

	 May-2019
	  	1	  	        	  	        	  		  	                	  	            	  	            	  	            	  	            
	 Total:
	  	1	  		  		  		  		  		  		  		  	

  

					
	AVI-PA-03015 112452-IF.txt	  		  	SA-9
		  	PROPRIETARY	  	

  

 Table 1-5 To 

Supplemental Agreement No. 9 Purchase Agreement No. PA-03075 

Aircraft Delivery, Description, Price and Advance Payments 

 

					
	Airframe Model/MTOW:	 	787-9	 	545,000 pounds
			
	Engine Model/Thrust:	 	TRENT1000-N	 	76,000 pounds
			
	Airframe Price:	 		 	              
			
	Optional Features:	 		 	            
			
	Fixed In-Flight Entertainment (IFE):	 		 	            
		 		 	  

			
	Sub-Total of Airframe and Features:	 		 	              
			
	Engine Price (Per Aircraft):	 		 	            
			
	Aircraft Basic Price (Excluding BFE/SPE):	 		 	              
		 		 	  

			
	Buyer Furnished Equipment (BFE) Estimate:	 		 	            
			
	Seller Purchased Equipment (SPE) Estimate:	 		 	        
			
	Deposit per Aircraft:	 		 	            

					
		
	                    	 	                            

			
	Airframe Price Base Year/Escalation Formula:	 	Jan-17	 	ECI-MFG/CPI
			
	Engine Price Base Year/Escalation Formula:	 	Jan-17	 	787 ECI-MFG CPI Eng
			
	Airframe Escalation Data:	 		 	
			
	Base Year Index (ECI):	 		 	    
			
	Base Year Index (CPI):	 		 	    
			
	Engine Escalation Data:	 		 	
			
	Base Year Index (ECI):	 		 	    
			
	Base Year Index (CPI):	 		 	    

 
 

  

																			
	 Delivery

Date
	  	Number of
Aircraft	  	Escalation
Factor
(Airframe)	  	Escalation
Factor
(Engine)	  	 
	  	Escalation Estimate
Adv Payment Base
Price Per A/P	  	Advance Payment Per Aircraft (Amts.
Due/Mos. Prior to Delivery):
	  	At Signing
1%	  	24 Mos.
4%	  	21/18/12/9/6
Mos.	  	    
    

	 Jan-2021
	  	1	  	        	  	        	  		  	                	  	            	  	            	  	            	  	            
	 Jun-2021
	  	1	  	        	  	        	  		  	                	  	            	  	            	  	            	  	            
	 Total:
	  	2	  		  		  		  		  		  		  		  	

  

					
	AVI-PA-03075 112225-IF.txt	  		  	SA-9
		  	Boeing Proprietary	  	

			
	 

	 	 The Boeing Company     

P.O. Box 3707                

Seattle, WA 98124 2207

 AVI-PA-3075-LA-1704594R1 
 Aerovias del Continente Americano S.A. Avianca 

Centro Administrativo 
 Avenida El Dorado - No. 92-30 
 Bogota 

Colombia 
  

	Subject:	 Aircraft Performance Guarantees 787-9 

 

	Reference:	 Purchase Agreement No. PA-3075 (Purchase Agreement)
between The Boeing Company (Boeing) and Aerovias del Continente Americano S.A. Avianca (Customer) relating to Model 787-9 aircraft (Aircraft) 

This letter agreement (Letter Agreement) amends and supplements the Purchase Agreement. All terms used but not defined in this Letter
Agreement will have the same meaning as in the Purchase Agreement. 
  

			
	        	 	
		
		 	
		 	

  

	1.	 Assignment. 

Notwithstanding any other provisions of the Purchase Agreement, the rights and obligations described in this Letter Agreement are provided to
Customer in consideration of Customer becoming the operator of the Aircraft and cannot be assigned, in whole or in part, without the prior written consent of Boeing. 
  

	2.	 Confidentiality. 

Customer understands that certain commercial and financial information contained in this Letter Agreement is considered by Boeing as confidential. Customer
agrees that it will treat this Letter Agreement and the information contained herein as confidential and will not, without the prior written consent of Boeing, disclose this Letter Agreement or any information contained herein to any other person or
entity. Customer understands that certain commercial and financial information contained in this Letter Agreement is considered by Boeing as confidential. Customer agrees that it
will treat this Letter Agreement and the information contained herein as confidential and will not, without the prior written consent of Boeing, disclose this Letter Agreement or any information contained herein to any other person or entity. 

  

					
		 		 	SA-9 Page 1
		 	BOEING PROPRIETARY	 	

 

 
 Customer agrees not to disclose this Letter Agreement,
attachments, or any other information related to this Letter Agreement without prior written consent by Boeing.Customer agrees not to disclose this Letter Agreement, attachments, or any other information related to this Letter Agreement without
prior written consent by Boeing. 
 Customer agrees not to disclose this Letter
Agreement, attachments, or any other information related to this Letter Agreement without prior written consent by Boeing. 
 Very truly yours, 

 

			
		
	 THE
	 	
		
	 By
	 	
	 Its
	 	

			
	
	 ACCEPTED AND AGREED TO this

	
	 Date:   February 26, 2019

	
	AEROVIAS DEL CONTINENTE AMERICANO S.A. AVIANCA

			
		
	 By
	 	 /s/ Renato Covelo

	 Its
	 	 Secretary General/Officer

  

					
	AVI-PA-3075-LA-1704594R1	 		 	SA-9 Page 2
		 	BOEING PROPRIETARY	 	

 

 
 Customer agrees not to disclose this Letter Agreement,
attachments, or any other information related to this Letter Agreement without prior written consent by Boeing.Customer agrees not to disclose this Letter Agreement, attachments, or any other information related to this Letter Agreement without
prior written consent by Boeing. 
 Customer agrees not to disclose this Letter
Agreement, attachments, or any other information related to this Letter Agreement without prior written consent by Boeing. 
  

	
	 Very truly yours,

	
	 THE BOEING COMPANY

			
		
	 By
	 	 /s/ Shane T Anderson

	 Its 
                            

			
	
	 ACCEPTED AND AGREED TO this

		
	Date:	 	                                      
                                    
	
	 AEROVIAS DEL CONTINENTE AMERICANO S.A. AVIANCA

			
		
	 By
	 	 /s/ Renato Covelo

	 Its
	 	 Secretary General/Officer

  

					
	AVI-PA-3075-LA-1704594R1	 		 	SA-9 Page 2
		 	BOEING PROPRIETARY	 	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 1 
  

 MODEL 787-9 PERFORMANCE GUARANTEES 

FOR AEROVIAS DEL CONTINENTE AMERICANO S.A. AVIANCA 
  

					
	 	 	SECTION	  	CONTENTS
			
		 	1	  	 AIRCRAFT MODEL APPLICABILITY

			
		 	2	  	 FLIGHT PERFORMANCE

			
		 	3	  	
            
                                         
           

			
		 	4	  	
            
                    

			
		 	5	  	 AIRCRAFT CONFIGURATION

			
		 	6	  	 GUARANTEE CONDITIONS

			
		 	7	  	 GUARANTEE COMPLIANCE

			
		 	8	  	 EXCLUSIVE GUARANTEES

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 2 
  

	1	 AIRCRAFT MODEL APPLICABILITY 

The guarantees contained in this Attachment (the “Performance Guarantees”) are applicable to the
787-9 Aircraft with a maximum takeoff weight of              kilograms, a maximum landing weight of              kilograms, and a maximum zero fuel weight of              kilograms, and equipped with Boeing furnished Trent 1000-N (TEN BoM) engines. 
  

	2	 FLIGHT PERFORMANCE 

 

	2.1	
            

  

	2.1.1	
                
                                         
                                         
                                         
                                         
                    
                                         
                                         
                                         
                                         
                                    
                                         
                                         
                                         
                                         
                             and using the conditions defined below, will not be less than
the following guarantee value: 

  

					
	 NOMINAL:
	 	
             
   
	  	     kilograms

	 TOLERANCE:
	 	
             
   
	  	     kilograms

	 GUARANTEE:
	 	
             
   
	  	     kilograms

 Conditions: 
  

            
                                         
                                         
                                         
                                         
                 
  

            
                                         
                                         
                                         
                                         
             
  

            
                                         
                                         
                                         
                                         
             
  

            
                                         
                                         
                                         
                                         
                   

            
         
  

            
                                         
                                         
                                         
                                         
                     

            
         
  

            
                                         
                                         
                                         
                                         
         
  

            
                                         
                                         
                               

 

            
                                         
                                         
                               

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 3 
  

 The following obstacle definition is based on a straight-out
departure where obstacle height and distance are specified with reference to the liftoff end of the runway: Height Distance 
  

					
		  	 Height    
	  	 Distance

	1.    	  	                    	  	                            

  

	2.1.2	
                 
                                         
                                         
                                         
                                         
                   
                                         
                                         
                                         
                                         
                                    
                                         
                                         
                                         
                                         
                                 nd using the conditions defined below, will not be
less than the following guarantee value: 

  

					
	 NOMINAL:
	 	
             
   
	  	     kilograms

	 TOLERANCE:
	 	
             
   
	  	     kilograms

	 GUARANTEE:
	 	
             
   
	  	     kilograms

 Conditions: 
  

            
                                         
                                         
                                         
                                         
                 
  

            
                                         
                                         
                                         
                                         
             
  

            
                                         
                                         
                                         
                                         
             
  

            
                                         
                                         
                                         
                                         
                   

            
         
  

            
                                         
                                         
                                         
                                         
                     

            
         
  

            
                                         
                                         
                                         
                                         
         
  

            
                                         
                                         
                               

 

            
                                         
                                         
                               

The following obstacle definition is based on a straight-out departure where obstacle height and
distance are specified with reference to the liftoff end of the runway: 
  

					
		  	 Height    
	  	 Distance

	1.    	  	                    	  	                            

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 4 
  

	2.2	
                
                                         
                                         
               

                                
                                         
                                         
                                         
                                         
     
                                         
                                         
                                         
                                         
                                    
                                         
                                         
                                         
                                         
                                    
                                         
                                         
                                         
                                         
     will not be less than the following guarantee value: 
  

					
	 NOMINAL:
	 	
             
   
	  	     feet

	 TOLERANCE:
	 	
             
   
	  	     feet

	 GUARANTEE:
	 	
             
   
	  	     feet

  

	2.3	
                
                                         
                                         
               

                       
                                         
                                         
                                         
                                         
             
                              
                                         
                                         
                                         
                                         
      
                                         
                                         
                                         
                                         
                                    
                                         
                                         
                                         
                          will not be less than the following guarantee
value: 
  

					
	 NOMINAL:
	 	
             
   
	  	     feet

	 TOLERANCE:
	 	
             
   
	  	     feet

	 GUARANTEE:
	 	
             
   
	  	     feet

 Conditions: 
  

	 	1)	
                 
                                         
                                         
                                         
                                         
       
                                         
                                         
                                         
                                     

  

	 	2)	
                 
                                         
                                         
                                         
                                         
       
                                         
                                         
                                         
                                         
                                         

  

	 	3)	
                 
                                         
                                         
                                         
                                         
        

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 5 
  

	2.4	 Cruise Range 

The still air range at an initial cruise altitude of
             feet on an                  day at          Mach number, starting at a gross weight of              kilograms and consuming              kilograms of fuel, and using not more than maximum cruise thrust
(except maximum climb thrust may be used during a step climb) and using the conditions and operating rules defined below, will not be less than the following guarantee value: 

 

					
	 NOMINAL:
	 	
             
   
	  	     nautical miles

	 TOLERANCE:
	 	
             
   
	  	     nautical miles

	 GUARANTEE:
	 	
             
   
	  	     nautical miles

 Conditions and operating rules: 

A step climb or multiple step climbs of
             feet altitude may be used when beneficial to maximize range.

  

	2.5	 Mission 

  

	2.5.1	 Mission Payload 

The payload for a stage length of
           nautical miles in still air (representative of a
                                         
           ) using the conditions and operating rules defined below, will not be less than the following guarantee value: 

 

					
	 NOMINAL:
	 	
             
   
	  	     kilograms

	 TOLERANCE:
	 	
             
   
	  	     kilograms

	 GUARANTEE:
	 	
             
   
	  	     kilograms

 Conditions and operating rules: 

 

					
	   	 	Stage	  	The stage length is defined as the sum of the
		 	Length:	  	distances for the climb, cruise, and descent.

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 6 
  

							
	Takeoff:	  	                              
                                         
                                         
                        
		
		  	                              
                                         
                                         
        
		
		  	
                    
                                         
                                         
                                         
 

                    

		
		  	
                    
                                         
                                         
                                         
 

                    
                

		
		  	                                                 
                                  
                                  
                            

                    
                                    

		
		  	
                    
                                         
                                         
                                         
 

                    
                                

		
		  	
                    
                                         
                                         
                                         
 

                    
    

		
		  	                              
                                         
                                         
                        
		
		  	The following obstacle definition is based on a straight out departure where obstacle height and distance are specified with reference to the liftoff end of the runway:
				
		  		  	Height  	 	Distance
		  	        1.	  	              	 	                        
		
		  	 Takeoff performance is based on an alternate forward center of gravity limit of
       percent of the mean aerodynamic chord.
  

Maximum takeoff thrust is used for the takeoff.
  

The takeoff gross weight will conform to FAA Regulations.

		
	Climbout Maneuver:	  	
                    
                                         
                                         
                                  
                                   
                                         
                                         
                   
                                   
                                         
                                         
                   
                                   
                                         
                                         
                   
                     

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 7 
  

  

			
	 Climb:
	 	
             
                                         
                                         
                                         

             
                                         
                                         
                                         

             
                                   

		
		 	
             
                                         
                                         
                                         

             
                                         
                                         
                                         

             
                                         
                                  

		
		 	
             
                                         
                                         
                                         

             
                                         
                                         
                                         

             
                                   

		
		 	
             
                                         
                                         
                         

		
		 	
             
                                         
                                         
                             

		
	 Cruise:
	 	
             
                                         
                                         
                         

		
		 	
             
                                         
                                         
                                         

             
                                         
              

		
		 	
             
                                         
                                         
                         

		
		 	
             
                                         
                                         
                                         

             
                                         
                                         
                                         

             
                                         
                                         
                         

		
	 Descent:
	 	
             
                                         
                                         
                                         

             
                                         
                                         
                                         

             
                                         
                                         
                         

		
		 	
             
                                         
                                         
                                         

             
                                         
                                         
                                         

             
                                         
                                         
                                         

		
		 	
             
                                         
                                         
                                         

		
	 Approach and Landing

Maneuver:
	 	
             
                                         
                                         
                                         

             
                                         
                                         
                                         

             
                                       

		
		 	
             
                                         
                                         
                             

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 8 
  

			
	Fixed Allowances:	  	 For the purpose of this guarantee and for the purpose of establishing compliance with this guarantee, the following will be used as fixed
quantities and allowances:
  

Taxi-Out:

		  	
               
                                 

		
		  	Takeoff and Climbout Maneuver:
		  	
               
                                 

		
		  	Approach and Landing Maneuver:
		  	
               
                                 

		
		  	Taxi-In (will be consumed from the reserve fuel):
		  	
               
                                 

		
		  	Usable reserve fuel remaining upon completion of the approach and landing maneuver:
                    
		
		  	For information purposes, the reserve fuel is based on an              day temperature and a) a contingency fuel allowance
equivalent to      percent of the flight fuel required to fly to the redispatch point (representative of
       of the track distance from the origin airport to the final destination airport), starting at the end of mission cruise at a LRC Mach number, b) a missed approach and
flight to a          nautical mile alternate, c) and includes
             kilograms of hold and emergency fuel and an additional 
         kg of fuel for international routes per customer rules.

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 9 
  

	2.5.2	 Mission Payload 

The payload for a stage length of
             nautical miles in              (representative of
a
                             
           ) using the conditions and operating rules defined below, will not be less than the following guarantee value: 

 

							
		 	 NOMINAL:
	  	
            

	  	 kilograms

		 	 TOLERANCE:
	  	          
  
	  	 kilograms

		 	GUARANTEE:	  	            	  	kilograms

 Conditions and operating rules: 

 

			
	Stage Length:	  	The stage length is defined as the sum of the distances for the climb, cruise, and descent.
		
	Takeoff:	  	                                
                                         
               
		
		  	                                
                                        

		
		  	
                    
                                         
                               

                

		
		  	
                    
                                         
                               

                    
    

		
		  	                                       
                           
                           

                    
                

		
		  	
                    
                                         
                               

                    
                

		
		  	
                    
                                         
                               

                    

		
		  	                                
                                         
           
		
		  	The following obstacle definition is based on a straight out departure where obstacle height and distance are specified with reference to the liftoff end of the runway:

 
							
				
		  		  	  Height    	  	    Distance    
		  	         1.
	  	              	  	                      

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 10 
  

			
		  	Takeoff performance is based on an alternate forward center of gravity limit      of percent of the mean aerodynamic chord.
		
		  	Maximum takeoff thrust is used for the takeoff.
		  	The takeoff gross weight will conform to FAA Regulations.
		
	 Climbout
 Maneuver:
	  	
                    
                                         
                                         
                                         
         

                    
                                         
                                         
                                         
         

                    
                                         
                                         
                                         
         

                    

		
	Climb:	  	
                    
                                         
                                         
                                         
         

                    
                                         
                                         
                                         
         

                    
        

		
		  	
                    
                                         
                                         
                                         
         

                    
                                         
                                         
                                         
         

                    
                                         
               

		
		  	
                    
                                         
                                         
                                         
         

                    
                                         
                                         
                                         
         

                    

		
		  	                                
                                         
                                         
                                      
		
	Cruise:	  	
                    
                                         
                                         
                                         
         
  
                                     
                                         
                                         
                                  

		
		  	
                    
                                         
                                         
                                         
         

                    
                    

		
		  	                                
                                         
                                         
                                      
		
		  	
                    
                                         
                                         
                                         
         

                    
                                         
                                         
                                         
         

                    
                                         
                                  
             

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 11 
  

			
		
	Descent:	  	The Aircraft descends from the final cruise
		  	
                    
                                         
                                         
                                         
         

                    
                                         
                                         
                          

		
		  	
                    
                                         
                                         
                                         
         

                    
                                         
                                         
                                         
         

                    
                                         
                                         
                                         
         

		
		  	                                
                                         
                                         
                                      
		
	 Approach and Landing
 Maneuver:
	  	
                    
                                         
                                         
                                         
         

                    
                                         
                                         
                                         
         

                    
                                         
                   

		
		  	                                
                                         
                                         
          
		
	Fixed Allowances:	  	For the purpose of this guarantee and for the purpose of establishing compliance with this guarantee, the following will be used as fixed quantities and allowances:
		
		  	Taxi-Out:
		  	         
                                   
             

		
		  	Takeoff and Climbout Maneuver:
		  	         
                                   
             

		
		  	Approach and Landing Maneuver:
		  	         
                                   
             

		
		  	Taxi-In (will be consumed from the reserve fuel):
		
		  	         
                                   
             

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 12 
  

			
		  	Usable reserve fuel remaining upon completion of the approach and landing maneuver:              kilograms
		
		  	For information purposes, the reserve fuel is based on
                         day temperature and a) a contingency fuel allowance
equivalent to      percent of the flight fuel required to fly to the redispatch point (representative of
         of the track distance from the origin airport to the final destination airport), starting at the end of mission cruise at a LRC Mach number, b) a missed
approach and flight to a          nautical mile alternate, c) and includes
             kilograms of hold and emergency fuel and an additional
       kg of fuel for international routes per customer rules.

  

	2.5.3	 Mission Block Fuel 

The block fuel for a stage length of
         nautical miles in              (representative of                              route with             
flight time from             ) with a              kilogram payload using the conditions and operating rules defined
below, will not be more than the following guarantee value: 
  

			
	 NOMINAL:
	  	
            
  kilograms

	 TOLERANCE:         
	  	
            
  kilograms

	GUARANTEE:	  	              kilograms

 Conditions and operating rules: 
  

					
	            	 	Stage Length:	  	The stage length is defined as the sum of the distances for the climb, cruise, and descent.
			
		 	Block Fuel:	  	The block fuel is defined as the sum of the fuel used for taxi-out, takeoff and climbout maneuver, climb, cruise, descent, approach and landing maneuver, and
taxi-in.

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 13 
  

									
			
	            	 	Takeoff:	  	                              
                                         
                                  
                                       

			
		 		  	                              
                                  
                                  
              
			
		 		  	
                    
                                         
                                  
                                  
                       

            

			
		 		  	
                    
                                         
                                  
                                  
                       

                    
        

			
		 		  	                                                                         
                                                                
                
                                     
       

			
		 		  	
                    
                                         
                                  
                                                         

                    
                

			
		 		  	
                    
                                         
                                  
                                                         

                

			
		 		  	                              
                                  
                          
                          
                                  
  
			
		 		  	The following obstacle definition is based on a straight out departure where obstacle height and distance are specified with reference to the liftoff end of the runway:
					
		 		  		    	Height	  	Distance      
		 		  	        1.	    	                	  	                            
			
		 		  	Takeoff performance is based on an alternate forward center of gravity limit of      percent of the mean aerodynamic chord.
			
		 		  	Maximum takeoff thrust is used for the takeoff.
			
		 		  	The takeoff gross weight will conform to FAA Regulations.
			
		 	Climbout	  	                              
                                         
                                         
                                        

		 	Maneuver:	  	                              
                                         
                                  
                                         
      
		 		  	                              
                                         
                                  
                                         
      
		 		  	                              
                                         
                                  
                                         
      
		 		  	                              
      

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 14 
  

			
	 Climb:
	 	
             
                                         
                  
                                         
                               

             
                                         
                  
                                         
                               

             
                       

		
		 	
             
                                         
                                  
                                         
               
                                     
                                    
                                         
                               

             
                                                       

		
		 	
             
                                         
                                  
                                         
               
                                     
                                                                        
                                    

             
           

		
		 	
             
                                         
                                  
                                         
               

		
		 	
             
                                         
                                  
                                         
               

		
	 Cruise:
	 	
             
                                         
                                  
                                         
               

		 	
		 	
             
                                         
                                         
                                         
        

             
                                         
                                         
                                         
        

             
                           

		
		 	
             
                                         
                                  
                                         
               

		
		 	
             
                                         
                                  
                                         
               
                                     
                                                                        
                                    

             
                                         
                                         
                                 

		 	
		
	 Descent:
	 	
             
                                         
                                  
                                         
               
                                     
                                         
                                         
                          

             
                                         
                                         
                                         

		
		 	
             
                                         
                                  
                                         
               
                                     
                                                                        
                                    

             
                                         
                                  
                                         
               

		
		 	
             
                                         
                                  
                                         
               

		
	 Approach and Landing

Maneuver:
	 	
             
                                         
                                  
                                         
               
                                     
                                         
                                         
                          

             
                                         
                          

		 	
		 	
             
                                         
                                         
         

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 15 
  

			
	Fixed Allowances:	  	For the purpose of this guarantee and for the purpose of establishing compliance with this guarantee, the following will be used as fixed quantities and allowances:
		
		  	Taxi-Out:
		  	
               
                     

		
		  	Takeoff and Climbout Maneuver:
		  	
               
                     

		
		  	Approach and Landing Maneuver:
		  	
               
                     

		
		  	Taxi-In (will be consumed from the reserve fuel):
		  	
               
                     

		
		  	Usable reserve fuel remaining upon completion of the approach and landing
maneuver:                        
		
		  	For information purposes, the reserve fuel is based on
                         day temperature for the climb and descent segments and              day for the cruise segment and a) a contingency fuel allowance equivalent to   
percent of the flight fuel from takeoff through the completion of the approach and landing maneuver at the destination airport, b) a missed approach and flight to a
         nautical mile alternate, c) and includes
             kilograms of hold and emergency fuel and an additional
         kg of fuel for international routes per customer rules.

  

	2.5.4	 Operational Empty Weight Basis 

The Operational Empty Weight (OEW) derived in paragraph 2.5.5 is the basis for the mission guarantees of paragraphs 2.5.1 through 2.5.3. 

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 16 
  

 2.5.5 787-9 Weight Summary - Aerovias del Continente Americano S.A. Avianca 

 

					
	 	  	Kilograms	 
	Standard Model Specification Manufacturer’s Empty Weight (MEW)	  	 	            	 
	
             
                                         
              
	  			
	
             
                           
	  			
	
             
                                         
                                      
	  	 	    	 
	
             
                               
	  			
	
             
               
	  			
	
             
                                       
	  			
	
             
                               
	  			

  

					
	Changes for Aerovias del Continente Americano S.A. Avianca *	  	 	 
	
             
                                         
                              
	  	 	         	 
	
             
                       
	  			
	
             
                       
	  	 	  	 
	
             
                                         
                                  
	  	 	    	 
	
             
                                         
                                         
         
	  	 	  	 
	
             
                                         
                                         
          
	  	 	  	 
	
             
       
	  	 	        	 
	
             
                           
	  	 	        	 

  

					
	Aerovias del Continente Americano S.A. Avianca Manufacturer’s Empty Weight (MEW)	  	 	            	 
	 Standard and Operational Items Allowance (Paragraph 2.5.6)
	  	 	          	 
	Aerovias del Continente Americano S.A. Avianca Operational Empty Weight (OEW)	  	 	            	 

  

													
	 	  	Quantity	 	  	Kilograms	 	  	Kilograms	 
	 * Seat Weight Included
	  				  				  	 	            	 
				
	 Business Class
            
	  	 	    	 	  	 	            	 	  			
	 Business Class
                    
	  	 	  	 	  	 	    	 	  			
	 Economy Class
        
	  	 	    	 	  	 	            	 	  			
	 Economy Class
            
	  	 	  	 	  	 	         	 	  			

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 17 
  

	2.5.6	 Standard and Operational Items Allowance 

 

									
	 	  	 Quantity
	  	 Kilograms
	  	 Kilograms
	  	 Kilograms

	 Standard Items Allowance
	  		  		  		  	        
	
             
         
	  		  		  	        	  	
	     
	  		  		  	    	  	
	
             
                 
	  		  		  	    	  	
	
             
                           
	  		  		  	    	  	
	
             
                                         
  
	  		  		  	            	  	
					
	 Operational Items Allowance
	  		  		  		  	        
	
             
                       
	  		  		  	            	  	
	
             
                           
	  	  	  	        	  		  	
	
             
                               
	  	    	  	        	  		  	
	
             
                       
	  	    	  	        	  		  	
	
             
                                       
	  	  	  	    	  		  	
	
             
                                         
  
	  		  		  	            	  	
	
             
       
	  	    	  	        	  		  	
	
             
         
	  	        	  	          	  		  	
	
             
                           
	  		  		  	        	  	
	
             
                       
	  		  		  	  	  	
	
             
                                         
              
	  		  		  	        	  	
	
             
           
	  		  		  	            	  	
	
             
                       
	  		  	        	  		  	
	
             
                               
	  		  	            	  		  	
					
	 Total Standard and Operational Items Allowance
	  		  		  		  	        

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 18 
  

	3	
                
                                         
                                         
                   

  

			
		
		  	
	                	  	

  

	4	
                
                                         
                                

 

	4.1	
                
                                         
                    

  

	 	
                
                                         
                                         
                                         
                      

	 	
                
                                         
                                         
                                         
                      

  

	 	
                
                                         
                                       
                                         
                    

 

	 	
               
                                       
                                         
                                         
                         

	 	
                
                                        
                                 
                                        
                               

	 	
                
                            

	 	
                
                               

 

	 	
               
                                       
                                         
                                         
                         

	 	
                
                                        
                                 
                                        
                               

	 	
                
                            

	 	
                
                               

 

	 	
               
                                       
                                         
                                         
                         

	 	
                
                                        
                                 
                                        
                               

	 	
                
                            

	 	
                
                               

 

	5	 AIRCRAFT CONFIGURATION 

 

	5.1	 The guarantees contained in this Attachment are based on the Aircraft configuration as defined in Boeing
Document                 
                 , “787 Airplane Configuration Specification”,
dated                         , plus any changes mutually agreed to or otherwise
allowed by the Purchase Agreement to be incorporated into the original release of the Customer’s Detail Specification (hereinafter referred to as the Detail Specification). Appropriate adjustment shall be made for changes in such Detail
Specification approved by the Customer and Boeing or otherwise allowed by the Purchase Agreement which cause changes to the flight performance and/or weight and balance of the Aircraft. Such adjustment shall be accounted for by Boeing in its
evidence of compliance with the guarantees. 

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 19 
  

	5.2	 The guarantee payloads of paragraphs 2.5.1 and 2.5.2, and the specified payload of the paragraph 2.5.3 block
fuel guarantee will be adjusted by Boeing for the effect of the following on OEW and
                             guarantee of Section 3 will
be adjusted by Boeing for the following in its evidence of compliance with the guarantees: 

  

	 	(1)	 Changes to the Detail Specification or any other changes mutually agreed upon between the Customer and Boeing
or otherwise allowed by the Purchase Agreement. 

  

	 	(2)	 The difference between the component weight allowances given in Appendix E of the Detail Specification and the
actual weights. 

  

	6	 GUARANTEE CONDITIONS 

 

	6.1	 All guaranteed performance data are based on the International Standard Atmosphere (ISA) and specified
variations therefrom; altitudes are pressure altitudes. 

  

	6.2	 The Federal Aviation Administration (FAA) regulations referred to in this Attachment are, unless
otherwise specified, Code of Federal Regulations 14, Part 25 amended by Amendments 25-1 through 25-128, subject to the approval of the Federal Aviation Administration.

  

	6.3	 In the event a change is made to any law, governmental regulation or requirement, or in the
interpretation of any such law, governmental regulation or requirement that affects the certification basis for the Aircraft as described in Paragraph 6.2, and as a result thereof, a change is made to the configuration and/or the performance of the
Aircraft in order to obtain certification, the guarantees set forth in this Attachment will be appropriately modified to reflect any such change. 

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 20 
  

  

	6.4	
                
                                         
                                         
                                         
                                         
            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                 
                                    
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
             

  

	6.5	
                
                                         
                                         
                                         
                                         
            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
    

  

	6.6	
                
                                         
                                         
                                         
                                         
            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
    

  

	6.7	
                
                                         
                                         
                                         
                                         
            
                                         
                                         
                                         
                                         
                            
                                 

 

	6.8	
                
                                         
                                         
                                         
                                         
            
                                         
                                         
                                         
                                         
                            
                             

 

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 21 
  

	6.9	
                
                                         
                                         
                                         
                                         
            
                                         
                                         
                                         
                                         
                            
                                
                                  
                                  
                                  
                                  
                        
                                         
                                         
                                         
                                         
                            
                                        
                                  
                                         
                                         
                                    
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                      

  

	6.10	
                
                                         
                                         
                                         
                                         
            
                                         
                                         
                                         
                                         
                            
                           
                                 
                            
                                  
                                   
                                  
 
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
             

  

	7	 GUARANTEE COMPLIANCE 

 

	7.1	 Compliance with the guarantees of Section 2, 3 and 4 will be based on the conditions specified in
those sections, the Aircraft configuration of Section 5 and the guarantee conditions of Section 6. 

  

	7.2	
                
                                         
                                         
                                         
                                         
            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                   

  

	    	                                   
                           
                                         
                                         
                                        
                                         
    
                           
                                         
                                         
                                         
                                         
   
                                   
                                        
   
                                         
                                         
                                  
                           
                                         
                                         
                                         
                                        
    
                           
                                         
                                         
                                         
                                        
    
                                         
                                         
                                         
                                         
                                  
                       

  

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 22 
  

	7.3	
                
                                         
                                         
                                         
                                         
            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
             

  

	7.4	
                
                                         
                                         
                                         
                                         
            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
      

  

	7.5	
                
                                         
                                         
                                         
                                         
            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                                
                                         
                                         
       

  

	7.6	 The OEW used for compliance with the mission guarantees will be the actual MEW plus the Standard and
Operational Items Allowance in Appendix E of the Detail Specification. 

  

	7.7	
                
                                         
                                         
                                         
                                         
            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                      

  

	7.8	 The data derived from tests will be adjusted as required by conventional methods of correction,
interpolation or extrapolation in accordance with established engineering practices to show compliance with these guarantees. 

  

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

 Attachment to Letter Agreement 

No. AVI-PA-3075-LA-1704594R1 
 Trent 1000-N Engines 

Page 23 
  

	7.9	
              
                                         
                                         
                                         
                                         
              
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                         
                                 
                                    
                                         
                                         
                                         
                                         
                            
                                         
                                         
                                   

 

	7.10	 Compliance will be based on the performance of the airframe and engines in combination, and will not be
contingent on the engine meeting its manufacturer’s performance specification. 

  

	8	 EXCLUSIVE GUARANTEES 

 

	    	 The only performance guarantees applicable to the Aircraft are those set forth in this Attachment.

  

  

					
	 P.A. No. 3075
 AERO-B-BBA4-M17-0656C
	  	  
	  	SS17-0471
		  	                                
        	  	

							
	

	 		 	 The Boeing Company
 P.O. Box 3707

Seattle, WA 98124 2207

AVI-3075-LA-1809416 

Aerovias del Continente Americano S.A. Avianca 
 Centro
Administrativo 
 Avenida El Dorado – No. 92-30 

Bogota 
 Columbia 

 

			
	Subject:	  	Aircraft Configuration Matters 787-9
		
	Reference:	  	Purchase Agreement No. 3075 (Purchase Agreement) between The Boeing Company (Boeing) and Aerovias del Continente Americano S.A. Avianca (Customer) relating to Model
787-9 aircraft (Aircraft)

 This letter agreement (Letter Agreement) amends and supplements the Purchase Agreement. All
terms used but not defined in this Letter Agreement will have the same meaning as in the Purchase Agreement. 
 As reflected in Table 1-4 of the Purchase Agreement, Boeing has initiated a change to the configuration of the Aircraft identified in Table 1-4 via Master Change Number                      to revise the
engineering required to install Rolls Royce Trent 1000-K engines in lieu of Rolls Royce Trent 1000-N engines. Master Change Number                      will be provided
for acceptance to Customer and will appear as a part of the Aircraft’s final invoice at delivery. 
 The Aircraft identified in
Table 1-5 will retain the Trent 1000-N engines as reflected in Exhibit A-1 of the Purchase Agreement, so no additional change to
the configuration of Customer’s Aircraft in Exhibit A-1 is required. 
 [signatures on the
following page] 

  

					
		  	  
	  	 Page 1

SA-9

		  	                                
        	  	

  

  
 

 
  

			
	THE BOEING COMPANY

			
		
	 By
  

 
 Its
	 	
                    
                                        
            

                    
                                        
            

                    
                                        
            

                    
                                        
            

	
	ACCEPTED AND AGREED TO this
	
	Date: February 26, 2019
	
	AEROVIAS DEL CONTINENTE AMERICANO S.A. AVIANCA
		
	By	 	 /s/ Renato Covelo

	Its	 	 Secretary General/Officer

  

					
	 AVI-3075-LA-1809416
 Aircraft Configuration
Matters 787-9
	  	  
	  	 Page 2

SA-9

		  	                                
        	  	

 

 
  

			
	THE BOEING COMPANY

			
		
	By	  	                              
                                         
                             
	Its	  	                              
                                         
                             
	
	ACCEPTED AND AGREED TO this

			
	
	 Dat

	
	AEROVIAS DEL CONTINENTE AMERICANO S.A. AVIANCA

			
		
	 By
	 	 /s/ Renato Covelo

	 Its
	 	 Secretary General/Officer

  

					
	 AVI-3075-LA-1809416
 Aircraft Configuration
Matters 787-9
	  	  
	  	 Page 2

SA-9

Source: [{"source": "alea-institute/alea-institute/kl3m-data-edgar-agreements/train-00295-of-00352.parquet"}, [{"source": "alea-institute/alea-institute/kl3m-data-edgar-agreements/train-00295-of-00352.parquet"}]]