Exhibit 4.39

Supplemental Agreement No. 7 (SA-7)

to

Purchase Agreement
No. 3158

between

The
Boeing Company

and

TAM
Linhas Aéreas S.A.

Relating to Boeing Model 777 Aircraft

THIS SUPPLEMENTAL AGREEMENT, entered into as of             , 2014, by and between
THE BOEING COMPANY (Boeing) and TAM LINHAS AÉREAS S.A. (Customer);

[***][***]

[***]

WHEREAS, the parties
have agreed to incorporate a new Exhibit A-4 for the 777F Aircraft configuration into the Agreement;

WHEREAS, Boeing and Customer have
mutually agreed to amend the Purchase Agreement to incorporate the effect of this and certain other changes.

AGREEMENT

NOW THEREFORE, and in consideration of the mutual covenants herein contained, the parties agree to amend the Purchase Agreement as follows:



|1. | Revision of Table of Contents and Aircraft Information Table to the Purchase Agreement:
|-- | ---------------------------------------------------------------------------------------

1.1. Table of Contents. [***]Tables. [***].



|2. | Exhibit A-4
|-- | -----------

2.1. A new Exhibit A-4 attached hereto is added to describe the
777F Aircraft.

[* * *] This information is subject to confidential treatment and has been omitted and filed separately with the commission.



---

|3. | Letter Agreements.
|-- | ------------------

3.1. [***].



|4. | Other Matters.
|-- | --------------

It is contemplated that Boeing and Customer will enter into an
assignment agreement assigning Customers rights to LATAM Airlines Group S.A. At such time as the assignment agreement is signed Boeing agrees to make Letter Agreement 6-1162-ILK-0277, entitled
777-FREIGHTER Performance Retention Commitment, to Purchase Agreement 3194 applicable to the two Table 3 Aircraft.



|5. | Confidential Treatment.
|-- | -----------------------

Boeing and Customer understand that the commercial and
financial information contained in this Supplemental Agreement is considered by the parties as confidential (Confidential Information) and both agree not to disclose such Confidential Information except as provided herein. In addition to the
parties respective officers, directors and employees who need to know the Confidential Information and who understand the obligation to keep it confidential, the parties may disclose Confidential Information (1) to the extent required by
law and (2) to its agents, auditors and advisors who need to know the Confidential Information for purposes of enabling each party to understand, perform its obligations under, or receive the benefits of, this Supplemental Agreement and who
have agreed not to use or disclose the Confidential Information for any other purpose without the other partys prior written consent. In the event that a party concludes that disclosure of Confidential Information contained in this
Supplemental Agreement is required by applicable law, the party will so advise the other party promptly in writing and endeavor to protect the confidentiality of such Confidential Information to the widest extent possible. In the event of a legal
dispute with Boeing, nothing herein will preclude Customer from sharing with its legal counsel information necessary for purposes of enabling counsel to advise or represent Customer provided that so long as Customer causes its legal counsel to
maintain the confidentiality of information that is the subject of this Article. This provision shall not apply to any Confidential Information that is in the public domain except that a party will be liable to the other for breach of its
obligations under this provision if the Confidential Information entered the public domain as a consequence of a wrongful act or omission on its part.

EXECUTED IN DUPLICATE as of the day and year first above written.

DATED AS OF this             day
of                                         of
2014

P.A. No. 3158

TAM

Boeing Proprietary

[* * *]
This information is subject to confidential treatment and has been omitted and filed separately with the commission.



---

|                       |  |                         |  |                    |  |      |  |                   
|---------------------- |  | ----------------------- |  | ------------------ |  | ---- |  | ------------------
|TAM LINHAS AÉREAS S.A. |  |                         |  | THE BOEING COMPANY
|                       |  |                         |  |                   
|By:                    |  |                         |  |                    |  | By:  |  | LOGO              
|                       |  |                         |  |                   
|                       |  |                         |  |                    |  |      |  | Mr. David J. Hilby
|                       |  | (Printed or Typed Name) |  |                    |  |      |  |                   
|                       |  |                         |  |                   
|Its:                   |  |                         |  |                    |  | Its: |  | Attorney in Fact  
|                       |  |                         |  |                   
|By:                    |  |                         |  |                    |  |      |  |                   
|                       |  |                         |  |                   
|                       |  |                         |  |                    |  |      |  |                   
|                       |  | (Printed or Typed Name) |  |                    |  |      |  |                   
|Its:                   |  |                         |  |                    |  |      |  |                   

P.A. No. 3158

TAM

Boeing Proprietary

[* * *]
This information is subject to confidential treatment and has been omitted and filed separately with the commission.



---

TABLE OF CONTENTS



|         |  |                                 |  |                             
|-------- |  | ------------------------------- |  | ----------------------------
|ARTICLES |  |                                 |  | SupplementalAgreement Number
|         |  |                                
|1.       |  | Quantity, Model and Description |  |                             
|2.       |  | Delivery Schedule               |  |                             
|3.       |  | Price                           |  |                             
|4.       |  | Payment                         |  |                             
|5.       |  | Miscellaneous                   |  |                             
|         |  |                                
|TABLE    |  |                                 |  |                             
|         |  |                                
|[***]    |  | [***]                           |  | [***]                       
|         |  |                                
|[***]    |  | [***]                           |  | [***]                       
|         |  |                                
|[***]    |  | [***]                           |  | [***]                       
|         |  |                                
|[***]    |  | [***]                           |  | [***]                       
|         |  |                                
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|         |  |                                
|[***]    |  | [***]                           |  | [***]                       
|         |  |                                
|[***]    |  | [***]                           |  | [***]                       
|         |  |                                
|[***]    |  | [***]                           |  | [***]                       
|         |  |                                
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|         |  |                                
|[***]    |  | [***]                           |  |                             
|         |  |                                
|[***]    |  | [***]                           |  | [***]                       
|         |  |                                
|[***]    |  | [***]                           |  | [***]                       
|         |  |                                
|[***]    |  | [***]                           |  |                             
|         |  |                                
|[***]    |  | [***]                           |  |                             
|         |  |                                
|[***]    |  | [***]                           |  |                             

[* * *] This information is subject to confidential treatment and has been omitted and filed separately with the
commission.



---

|                  |  |           |  |      
|----------------- |  | --------- |  | -----
|LETTER AGREEMENTS |  | SA Number
|                  |  |          
|[***]             |  | [***]     |  |      
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|[***]             |  | [***]     |  | [***]
|                  |  |          
|[***]             |  | [***]     |  | [***]

P.A. No. 3158

TAM

Boeing Proprietary



---

Table 3 To

Purchase Agreement No. PA-3158

Aircraft Delivery, Description, Price and Advance Payments

[***]

[* * *] The information in this table is
subject to confidential treatment and has been omitted and filed separately with the commission.



| |  |                    |  |       
| |  | ------------------ |  | ------
| |  | Boeing Proprietary |  | SA-7  
| |  |                    |  | Page 1



---

Exhibit A-4 To

Boeing Purchase Agreement



|            |  |                                                                                                                                                              |  |             
|----------- |  | ------------------------------------------------------------------------------------------------------------------------------------------------------------ |  | ------------
|CR          |  | Title                                                                                                                                                        |  | 2010 Dollars
|0110-000039 |  | MAJOR MODEL 777 AIRPLANE                                                                                                                                     |  | [***]       
|0110B750A90 |  |                                                                                                                                                              |  | [***]       
|0220-000040 |  | FAA TYPE CERTIFICATION                                                                                                                                       |  | [***]       
|0220C485B30 |  | TYPE CERTIFICATON & EXPORT CERTIFICATE OF AIRWORTHINESS FOR AIRPLANE DELIVERY - REQUIREMENT                                                                  |  | [***]       
|0221-000002 |  | DISPATCH WITH GEAR EXTENDED FOR REVENUE FLIGHT                                                                                                               |  | [***]       
|0221B401A43 |  | TAKEOFF AND LANDING WITH TAILWIND UP TO 15-KNOTS                                                                                                             |  | [***]       
|0221B401A44 |  | ENGINE INOPERATIVE TEN MINUTE TAKEOFF THRUST OPERATION                                                                                                       |  | [***]       
|0228-000032 |  | FLIGHT CREW OPERATIONS MANUAL IN FAA FORMAT                                                                                                                  |  | [***]       
|0228C485B24 |  | AIRPLANE FLIGHT MANUAL                                                                                                                                       |  | [***]       
|0229C677A10 |  | PERFORMANCE - CERTIFICATION FOR OPERATION AT AIRPORTS WITH PRESSURE ALTITUDES UP TO 9800 FEET                                                                |  | [***]       
|0252B299A36 |  | INSTRUMENTATION, AIRPLANE AND FUEL MEASURING STICK MANUALS IN METRIC UNITS - TEMPERATURE IN DEGREES CELSIUS                                                  |  | [***]       
|0315C485B25 |  | CERTIFIED OPERATIONAL WEIGHTS AND STRUCTURAL DESIGN WEIGHT- 777-FREIGHTER                                                                                    |  | [***]       
|0351C485B36 |  | TAKEOFF PERFORMANCE IMPROVEMENT - ALTERNATE FORWARD CENTER OF GRAVITY LIMITS                                                                                 |  | [***]       
|0352-000003 |  | AIRPLANE CUSTOMIZED LOADING SCHEDULE FOR WEIGHT AND BALANCE CONTROL - UNIVERSAL INDEX LOADING                                                                |  | [***]       
|1110C826G34 |  | ENGINE NACELLES BAC 7067 WHITE - EXTERIOR COLOR SCHEME AND MARKINGS                                                                                          |  | [***]       
|1110D121A74 |  | EXTERIOR COLOR SCHEME AND MARKINGS                                                                                                                           |  | [***]       
|1130C826G26 |  | BILINGUAL INTERIOR PLACARDS - SUPERNUMERARY COMPARTMENT                                                                                                      |  | [***]       
|1130D121A69 |  | REGISTRY PLACARD AND EXTERNAL DATA PLATE                                                                                                                     |  | [***]       
|1130D121A76 |  | INTERIOR PLACARDS - VERTICAL SIDEWALL LOWER LOBE COMPARTMENTS                                                                                                |  | [***]       
|1200C608C65 |  | SERVICE OPTION - ELECTRONIC FLIGHT BAG (EFB) SOFTWARE INSTALLATION - CUSTOMER ACCEPTANCE WALK AND CUSTOMER FLIGHTS                                           |  | [***]       
|2162C687A13 |  | AFT CARGO COMPARTMENT - INSTALLATION - CONDITIONED AIR SYSTEM                                                                                                |  | [***]       
|2210-000003 |  | AUTOFLIGHT - INHIBIT GLIDE SLOPE CAPTURE PRIOR TO LOCALIZER CAPTURE                                                                                          |  | [***]       
|2210-000030 |  | AUTOFLIGHT - THREE DIGIT MACH NUMBER ON MODE CONTROL PANEL                                                                                                   |  | [***]       
|2210-000037 |  | AUTOFLIGHT - BANK ANGLE HOLD AT AUTOPILOT COMMAND ENGAGE                                                                                                     |  | [***]       
|2210C594A11 |  | AUTOFLIGHT - ENABLE LNAV ENGAGEMENT ON TAKEOFF GO-AROUND                                                                                                     |  | [***]       
|2311-000137 |  | HF COMMUNICATIONS - PARTIAL PROVISIONS FOR DUAL ARINC 753 HF DATALINK                                                                                        |  | [***]       
|2311B401A39 |  | HF COMMUNICATIONS - EQUIPMENT INSTALLATION OF DUAL ROCKWELL HF VOICE/DATA TRANSCEIVERS - P/N 822-0990-004 AND DIGITAL HF COUPLERS - P/N 822-0987-004 BFE/SPE |  | [***]       
|2312-000703 |  | VHF COMMUNICATIONS - ACTIVATION OF 8.33 KHZ CHANNEL SPACING                                                                                                  |  | [***]       



|          |  |                    |  |      |  |       
|--------- |  | ------------------ |  | ---- |  | ------
|P.A. 3158 |  | BOEING PROPRIETARY |  | SA-7 |  | Page 1



---

Exhibit A-4 To

Boeing Purchase Agreement



|            |  |                                                                                                                                                                                                     |  |             
|----------- |  | --------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |  | ------------
|CR          |  | Title                                                                                                                                                                                               |  | 2010 Dollars
|2312B401A87 |  | VHF COMMUNICATIONS - EQUIPMENT INSTALLATION OF TRIPLE ROCKWELL ARINC 750 VHF-2100 TRANSCEIVERS WITH 8.33 KHZ CHANNEL SPACING, VDL MODE 2, AND CMC INTERFACE CAPABILITY - P/N 822-1287-101 - BFE/SPE |  | [***]       
|2315C581A25 |  | SATCOM - AVIONICS EQUIPMENT INSTALLATION - ARINC 781 AERO-H+ AND SWIFTBROADBAND - THALES TOPFLIGHT SERIES - BFE/SPE                                                                                 |  | [***]       
|2315C594A56 |  | SATCOM - ANTENNA EQUIPMENT INSTALLATION - ARINC 781 COMPACT HIGH GAIN ANTENNA - CHELTON HGA-7001 WITH DIPLEXER P/N ###-##-#### - BFE/SPE                                                            |  | [***]       
|2321B401A04 |  | SELCAL - AVTECH FIVE CHANNEL DECODER - P/N NA138-714C - BFE/SPE                                                                                                                                     |  | [***]       
|2322C926A04 |  | AIRCRAFT COMMUNICATIONS ADDRESSING AND REPORTING SYSTEM (ACARS) - AIRPLANE INFORMATION MANAGEMENT SYSTEM (AIMS) ACTIVATION - VHF DATALINK MODE 2                                                    |  | [***]       
|2324B299A29 |  | EMERGENCY LOCATOR TRANSMITTER (ELT) - WULFSBERG ELECTRONICS AUTOMATIC FIXED WITH NAVIGATION INTERFACE UNIT (NIU) - MODE S BROADCAST - BFE/SPE                                                       |  | [***]       
|2351-000033 |  | HAND HELD MICROPHONE - CAPTAIN AND FIRST OFFICER - ELECTROVOICE - P/N 903-1342 - BFE/SPE                                                                                                            |  | [***]       
|2351-000035 |  | HAND HELD MICROPHONE - FIRST OBSERVER - ELECTROVOICE - P/N 903-1342 - BFE/SPE                                                                                                                       |  | [***]       
|2351-000042 |  | CONTROL WHEEL PUSH TO TALK (PTT) SWITCH - STANDARD THREE POSITION                                                                                                                                   |  | [***]       
|2351-000044 |  | AUDIO CONTROL PANEL - SECOND OBSERVER                                                                                                                                                               |  | [***]       
|2351A213B78 |  | BOOM MICROPHONE HEADSETS - CAPTAIN, FIRST OFFICER AND FIRST OBSERVER - TELEX AIRMAN 750 - P/N 64300-200 - BFE/SPE                                                                                   |  | [***]       
|2351A213B79 |  | BOOM MICROPHONE HEADSET - SECOND OBSERVER - TELEX AIRMAN 750 - P/N 64300-200 - BFE/SPE                                                                                                              |  | [***]       
|2371B628B36 |  | VOICE RECORDER, REMOTE MICROPHONE AND CONTROL PANEL - HONEYWELL - 2 HOUR RECORDING TIME - WITH DATALINK RECORDING CAPABILITY - P/N 980-6032-001, P/N 980-6115-001, P/N 980-6117-004 - BFE/SPE       |  | [***]       
|2371B628B42 |  | VOICE RECORDER - MANUAL ON/AUTO OFF SWITCH INSTALLATION - BACKUP POWER COMPATIBLE                                                                                                                   |  | [***]       
|2371C608G87 |  | VOICE RECORDER - AIRPLANE INFORMATION MANAGEMENT SYSTEM (AIMS) ACTIVATION - CONTROLLER-PILOT DATA LINK COMMUNICATIONS (CPDLC) DATA LINK MESSAGE RECORDING CAPABILITY                                |  | [***]       
|2431-000013 |  | NO BATTERY POWERED POSITION LIGHTS AND DC BACKUP POWER - TOWING OPERATION                                                                                                                           |  | [***]       
|2524C204D44 |  | OVERHEAD STOWAGE UNIT - CEILING MOUNTED                                                                                                                                                             |  | [***]       
|2525C204F43 |  | HIGH CAPACITY SEATING PROVISIONS - SUPERNUMERARY COMPARTMENT - 9 SEATS                                                                                                                              |  | [***]       
|2525C204F45 |  | ATTENDANT SEAT INSTALLATION - SUPERNUMERARY COMPARTMENT                                                                                                                                             |  | [***]       
|2527C204G19 |  | FLOOR COVERING - INSTALLATION - VINYL MAT THROUGHOUT THE SUPERNUMERARY AREA                                                                                                                         |  | [***]       
|2530C826G23 |  | GALLEY - SUPERNUMERARY COMPARTMENT                                                                                                                                                                  |  | [***]       
|2530C826G24 |  | GALLEY INSERTS - SUPERNUMERARY COMPARTMENT                                                                                                                                                          |  | [***]       



|          |  |                    |  |      |  |       
|--------- |  | ------------------ |  | ---- |  | ------
|P.A. 3158 |  | BOEING PROPRIETARY |  | SA-7 |  | Page 2



---

Exhibit A-4 To

Boeing Purchase Agreement



|            |  |                                                                                                                                                                                              |  |             
|----------- |  | -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- |  | ------------
|CR          |  | Title                                                                                                                                                                                        |  | 2010 Dollars
|2552-000318 |  | SLOPING SIDEWALL - FORWARD CARGO COMPARTMENT - 0.050-INCH-THICK BMS 8-223                                                                                                                    |  | [***]       
|2552-000319 |  | SLOPING SIDEWALL - AFT CARGO COMPARTMENT - 0.050-INCH-THICK BMS 8-223                                                                                                                        |  | [***]       
|2557C703A68 |  | AIRPLANE LOADING TIP ALARM SYSTEM INSTALLATION                                                                                                                                               |  | [***]       
|2557C703A73 |  | INSTALL SEAT-TRACK-TYPE IN LIEU OF SHACKLE-TYPE MOVEABLE TIE-DOWNS IN THE MAIN DECK CARGO HANDLING SYSTEM                                                                            |  | [***]       
|2558C703A75 |  | MAIN DECK CARGO RESTRAINTS - USE OF LBL AND RBL 48.2 RESTRAINT ANCHOR POINTS FOR TIE-DOWNS                                                                                                   |  | [***]       
|2558C756A03 |  | CENTERLINE LOADING OF THREE (3) LONGITUDINALLY-LOADED 16FT OR 20 FT ULDS IN THE MAIN DECK CARGO COMPARTMENT                                                                                  |  | [***]       
|2560-000207 |  | HALON FIRE EXTINGUISHER - FLIGHT DECK - WALTER KIDDE                                                                                                                                         |  | [***]       
|2560A075A10 |  | PROTECTIVE GLOVES - FLIGHT DECK - NORTH STAR - SFE                                                                                                                                           |  | [***]       
|2560C204E96 |  | PROTECTIVE BREATHING EQUIPMENT - FLIGHT DECK - B/E AEROSPACE                                                                                                                                 |  | [***]       
|2560C204H14 |  | FLASHLIGHTS WITH TAMPER SHIELD FOR TWO PILOTS - LED - FLIGHT DECK                                                                                                                            |  | [***]       
|2560D121A81 |  | CREW LIFE VESTS - FLIGHT DECK, WITH SECOND OBSERVER - EASTERN AERO MARINE - P01202-101C - BFE                                                                                                |  | [***]       
|2562C417D63 |  | EMERGENCY LOCATOR TRANSMITTER - PORTABLE                                                                                                                                                     |  | [***]       
|2562D121A80 |  | EASTERN AERO MARINE CREW LIFE VEST - OVERWATER SURVIVAL EQUIPMENT - SUPERNUMERARY COMPARTMENT - BFE                                                                                          |  | [***]       
|2564C204F03 |  | PROTECTIVE BREATHING EQUIPMENT - SUPERNUMERARY - B/E AEROSPACE                                                                                                                               |  | [***]       
|2564C204G43 |  | FIRST AID KIT - FAA                                                                                                                                                                          |  | [***]       
|2564D413D53 |  | OXYGEN BOTTLE WITH FULL-FACE MASK, ADDITIONAL - SUPERNUMERARY COMPARTMENT- SUPPLEMENTAL CEILING MOUNTED STOWAGE COMPARTMENT                                                                  |  | [***]       
|2622-000017 |  | ENGINE/APU FIRE EXTINGUISHER BOTTLES - COMMON BOTTLE                                                                                                                                         |  | [***]       
|2911-000003 |  | AC MOTOR-DRIVEN HYDRAULIC PUMPS - EATON (VICKERS) S270T201-7                                                                                                                                 |  | [***]       
|2911-000026 |  | ENGINE-DRIVEN HYDRAULIC PUMPS - PARKER (ABEX) S271W111                                                                                                                                       |  | [***]       
|3120-000013 |  | SIXTY MINUTE COUNT DOWN TIMER - INSTALLATION - FLIGHT DECK                                                                                                                                   |  | [***]       
|3131B628B16 |  | DIGITAL FLIGHT DATA RECORDER (DFDR) - HONEYWELL - 1024 WORDS PER SECOND MAXIMUM DATA RATE - P/N 980-4750-009 - BFE/SPE                                                                       |  | [***]       
|3135B628B47 |  | QUICK ACCESS RECORDER - TELEDYNE CONTROLS - GSM WIRELESS GROUNDLINK QUICK ACCESS RECORDER - P/N 2243800-81 - 512 MB PCMCIA FLASH MEMORY CARD RECORDING MEDIA - INSTALLATION - BFE            |  | [***]       
|3143-000013 |  | AIMS AIRPLANE MODIFIABLE (AMI) SOFTWARE - INSTALLATION AFTER DELIVERY AND BEFORE FLYAWAY                                                                                                     |  | [***]       
|3143C926A05 |  | AIRPLANE INFORMATION MANAGEMENT SYSTEM (AIMS) - OPERATIONAL PROGRAM CONFIGURATION FILE ACTIVATION - FLIGHT INFORMATION DATALINK COMMUNICATIONS MENU - ARINC 623 AIR TRAFFIC SERVICE MESSAGES |  | [***]       
|3150A213A18 |  | AURAL ADVISORY OF ALTITUDE APPROACH - FLIGHT DECK                                                                                                                                            |  | [***]       
|3151-000042 |  | FIREBELL AURAL WARNING - 1 SECOND ON, 9 SECONDS OFF                                                                                                                                          |  | [***]       
|3151-000046 |  | AUTOPILOT DISCONNECT - AURAL WARNING SIREN - AURAL WARNING AND MASTER WARNING LIGHT INHIBITED WHEN AUTOPILOT DISCONNECT SWITCH IS DOUBLE PRESSED QUICKLY                                     |  | [***]       
|3151A065A47 |  | RESETTABLE OVERSPEED AURAL WARNING - SIREN                                                                                                                                                   |  | [***]       



|          |  |                    |  |      |  |       
|--------- |  | ------------------ |  | ---- |  | ------
|P.A. 3158 |  | BOEING PROPRIETARY |  | SA-7 |  | Page 3



---

Exhibit A-4 To

Boeing Purchase Agreement



|            |  |                                                                                                                                                                                            |  |             
|----------- |  | ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ |  | ------------
|CR          |  | Title                                                                                                                                                                                      |  | 2010 Dollars
|3161-000002 |  | DOOR SYNOPTIC AND EICAS MESSAGE - PASSENGER DOOR SLIDE/RAFT ARMING HANDLE POSITION INDICATION - AUTO, MANUAL AND AUTO/MANUAL MESSAGES                                                      |  | [***]       
|3161-000167 |  | ANNUNCIATION FOR LOSS OF RIGHT OR LEFT FMCS - EICAS ADVISORY MESSAGE                                                                                                                       |  | [***]       
|3161-000168 |  | FLIGHT DECK COMMUNICATIONS FUNCTION (FDCF) AUTOMATIC RESET - ACTIVATION                                                                                                                    |  | [***]       
|3161-000169 |  | ANNUNCIATION FOR SATELLITE VOICE COMMUNICATION CAPABILITY - EICAS                                                                                                                          |  | [***]       
|3161-000170 |  | ANNUNCIATION FOR DATALINK AVAILABILITY - EICAS                                                                                                                                             |  | [***]       
|3161A425A45 |  | VMO/MMO OVERSPEED EICAS STATUS MESSAGE AND VFE OVERSPEED EICAS STATUS MESSAGE WITH FLAP/SLAT POSITION SNAPSHOT - FLIGHT DECK                                                               |  | [***]       
|3162-000022 |  | FLIGHT DIRECTOR COMMAND DISPLAY - SPLIT AXIS - ADI                                                                                                                                         |  | [***]       
|3162-000026 |  | DISPLAY OF ROUND DIAL AND DIGITAL RADIO ALTITUDE - ADI                                                                                                                                     |  | [***]       
|3162-000030 |  | RISING RUNWAY - DISPLAYED ON THE ADI                                                                                                                                                       |  | [***]       
|3162-000036 |  | LANDING ALTITUDE REFERENCE BAR - PRIMARY FLIGHT DISPLAY                                                                                                                                    |  | [***]       
|3162-000040 |  | BARO MINIMUMS POINTER - DISPLAYED ON SELECTION OF RADIO ALTITUDE MINIMUMS - PRIMARY FLIGHT DISPLAY                                                                                         |  | [***]       
|3162-000044 |  | TCAS RESOLUTION ADVISORY - VSI                                                                                                                                                             |  | [***]       
|3162-000051 |  | ILS LOCALIZER DEVIATION EXPANDED SCALE - AUTOPILOT OR FLIGHT DIRECTOR MODE                                                                                                                 |  | [***]       
|3162-000059 |  | MAP MODE ORIENTATION - TRACK UP - NAVIGATION DISPLAY                                                                                                                                       |  | [***]       
|3162-000062 |  | GRID HEADING - NAVIGATION DISPLAY                                                                                                                                                          |  | [***]       
|3162-000084 |  | TCAS 3 NM RANGE RING - NAVIGATION DISPLAY                                                                                                                                                  |  | [***]       
|3162-000211 |  | VREF AND SELECTED FLAP POSITION - PRIMARY FLIGHT DISPLAY                                                                                                                                   |  | [***]       
|3162-000218 |  | GROUND SPEED - DISPLAYED BELOW AIRSPEED TAPE WHEN MACH NUMBER IS NOT DISPLAYED - PRIMARY FLIGHT DISPLAY                                                                                    |  | [***]       
|3162C594A07 |  | NAVIGATION PERFORMANCE SCALES (NPS) AND REQUIRED NAVIGATION PERFORMANCE (RNP) ENHANCEMENTS - AIRPLANE INFORMATION MANAGEMENT SYSTEM (AIMS) - PRIMARY FLIGHT DISPLAY AND NAVIGATION DISPLAY |  | [***]       
|3245B047A08 |  | BRAKES - CARBON - HIGH CAPACITY - MESSIER-BUGATTI                                                                                                                                          |  | [***]       
|3245B047A09 |  | WHEELS AND TIRES - MAIN LANDING GEAR - HIGH GROSS WEIGHT WHEELS - MESSIER - BUGATTI - INSTALLATION WITH SFE 36 PR, 235 MPH RADIAL TIRES.                                                   |  | [***]       
|3245B047A10 |  | WHEELS AND TIRES - NOSE LANDING GEAR - WHEELS - MESSIER - BUGATTI- INSTALLATION WITH SFE 32 PR, 235 MPH RADIAL TIRES                                                                       |  | [***]       
|3324C198A28 |  | PASSENGER INFORMATION SIGNS - NO SMOKING SIGN - PERMANENT ILLUMINATION AND NO SMOKING FLIGHT DECK SELECTOR SWITCH REMOVAL                                                                  |  | [***]       
|3430B866A33 |  | ILS/GPS MULTI-MODE RECEIVER (MMR) - ROCKWELL COLLINS - P/N 822-1821-001 - BFE/SPE                                                                                                          |  | [***]       
|3433-000032 |  | RADIO ALTIMETER (RA) - ROCKWELL INTERNATIONAL CORP - P/N 822-0334-002 - BFE/SPE                                                                                                            |  | [***]       
|3443A065B20 |  | DUAL WEATHER RADAR CONTROL PANEL - WITH MULTISCAN FUNCTIONALITY - ROCKWELL COLLINS P/N 622-5130-801 - BFE/SPE                                                                              |  | [***]       
|3443C594A20 |  | DUAL WEATHER RADAR SYSTEM - WITH PREDICTIVE WINDSHEAR AND MULTISCAN CAPABILITY - ROCKWELL COLLINS WRT-2100 TRANSCEIVER - P/N 822-1710-002 - BFE/SPE                                        |  | [***]       



|          |  |                    |  |      |  |       
|--------- |  | ------------------ |  | ---- |  | ------
|P.A. 3158 |  | BOEING PROPRIETARY |  | SA-7 |  | Page 4



---

Exhibit A-4 To

Boeing Purchase Agreement



|             |  |                                                                                                                                                       |  |             
|------------ |  | ----------------------------------------------------------------------------------------------------------------------------------------------------- |  | ------------
|CR           |  | Title                                                                                                                                                 |  | 2010 Dollars
|3445C594B04  |  | TCAS SYSTEM - ROCKWELL COLLINS TCAS COMPUTER P/N 822-1293-033 - TCAS CHANGE 7.1 COMPLIANT - BFE/SPE                                                   |  | [***]       
|3446-000050  |  | 500 SMART CALLOUT                                                                                                                                     |  | [***]       
|3446-000088  |  | GROUND PROXIMITY WARNING SYSTEM ALTITUDE CALLOUTS - 2500, 1000, 50, 40, 30, 20, 10, APPROACHING DECISION HEIGHT, MINIMUMS                             |  | [***]       
|3446C174A14  |  | ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) - BANK ANGLE CALLOUT (VARIABLE CALLOUT BELOW 130 FT) - ENABLE                                        |  | [***]       
|3451-000022  |  | VOR/MARKER BEACON - ROCKWELL RECEIVER P/N 822-0297-001 - BFE/SPE                                                                                      |  | [***]       
|3453D197A15  |  | ATC SYSTEM - ROCKWELL COLLINS ATC TRANSPONDER P/N 822-1338-005 - ELS/EHS/ES AND TCAS CHANGE 7 COMPLIANT - GABLES CONTROL PANEL P/N G7131-03 - BFE/SPE |  | [***]       
|3455-000019  |  | DISTANCE MEASURING EQUIPMENT (DME) - ROCKWELL INTERROGATOR P/N 822-0329-001 - BFE/SPE                                                                 |  | [***]       
|3457-000214  |  | AUTOMATIC DIRECTION FINDER (ADF) - DUAL SYSTEM - ROCKWELL ADF-900 SERIES - ADF RECEIVER P/N 822-0299-001; ADF ANTENNA P/N 822-5404-003 - BFE/SPE      |  | [***]       
|3461A213A10  |  | FMCS - ENHANCED FIX PAGE CAPABILITIES                                                                                                                 |  | [***]       
|3461A213A11  |  | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - GPS APPROACHES WITH VERTICAL ANGLES                                                                        |  | [***]       
|3461A213A12  |  | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS)- DISPLAY OF VERTICAL BEARING, FLIGHT PATH ANGLE (FPA) AND VERTICAL SPEED                                     |  | [***]       
|3461A425A05  |  | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - RUNWAY DISTANCE AND OFFSET POSITION SHIFT IN UNITS OF FEET                                                 |  | [***]       
|3461A425A08  |  | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - FLIGHT CREW ALERTNESS MONITORING - ENABLE                                                                  |  | [***]       
|3461A425A10  |  | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - NAVIGATION DATABASE - CUSTOMER SUPPLIED                                                                    |  | [***]       
|3461A425A23  |  | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS)- QUICK REFERENCE HANDBOOK (QRH) - TAKEOFF SPEEDS- DISPLAYED                                                  |  | [***]       
|3461C739A08  |  | FMCS - PROVIDE REQUIRED NAVIGATION PERFORMANCE (RNP) VALUES WITH 0.3 NM APPROACH                                                                      |  | [***]       
|3511B899B48  |  | CREW OXYGEN MASKS - AUTOMATIC PRESSURE BREATHING TYPE WITH SEPARATE SMOKE GOGGLES - CAPTAIN AND FIRST OFFICER - AVOX - BFE/SPE                        |  | [***]       
|3511B899B49  |  | CREW OXYGEN MASKS - AUTOMATIC PRESSURE BREATHING TYPE WITH SEPARATE SMOKE GOGGLES - FIRST OBSERVER - AVOX - BFE/SPE                                   |  | [***]       
|3511B899B50  |  | CREW OXYGEN MASKS - AUTOMATIC PRESSURE BREATHING TYPE WITH SEPARATE SMOKE GOGGLES - SECOND OBSERVER - AVOX - BFE/SPE                                  |  | [***]       
|4610B872A04  |  | ELECTRONIC FLIGHT BAG (EFB) - INSTALLATION                                                                                                            |  | [***]       
|4610C164A11  |  | CUSTOMER UNIQUE ELECTRONIC FLIGHT BAG (EFB) SOFTWARE INSTALLATION - AFTER DELIVERY AND BEFORE FLYAWAY                                                 |  | [***]       
|4610C594A09  |  | ELECTRONIC FLIGHT BAG (EFB) SYSTEM - AIRPLANE INFORMATION MANAGEMENT SYSTEM (AIMS) - ACTIVATION OF ARINC 724B ACARS INTERFACE                         |  | [***]       
|4900-000016  |  | MUFFLER IN APU EXHAUST SYSTEM                                                                                                                         |  | [***]       
|7200-000412  |  | GE PROPULSION SYSTEM                                                                                                                                  |  | [***]       
|7200A519A02  |  | GENERAL ELECTRIC ENGINES - GE90-110B1L THRUST RATING                                                                                                  |  | [***]       
|7900B753B83  |  | LUBRICATING OIL - BP TURBO OIL 2197                                                                                                                   |  | [***]       
|             |  |                                                                                                                                                       |  | [***]       
|OPTIONS: 131 |  | TOTALS:                                                                                                                                               |  | [***]       





|          |  |                    |  |      |  |       
|--------- |  | ------------------ |  | ---- |  | ------
|P.A. 3158 |  | BOEING PROPRIETARY |  | SA-7 |  | Page 5



---

|     |  |  |  |  |  |                                                        
|---- |  |  |  |  |  | -------------------------------------------------------
|LOGO |  |  |  |  |  | The Boeing Company P.O. Box 3707
Seattle, WA 98124-2207





6-1161-DJH-1298

TAM Linhas Aereas S.A.

Rua General Pantaleao Teles, 210

Sao Paulo - SP

04355-040

Brazil



|Subject: | Aircraft Performance Guarantees for Table 3 Aircraft
|-------- | ----------------------------------------------------



|Reference: | Purchase Agreement No. 3158 (Purchase Agreement) between The Boeing Company (Boeing) and TAM Linhas Aereas S.A. (Customer) relating to Model Model 777 aircraft (777F 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. | Confidential Treatment.
|-- | -----------------------

Boeing and Customer understand that the commercial and financial information
contained in this Letter Agreement is considered by the parties as confidential (Confidential Information) and both agree not to disclose such Confidential Information except as provided herein. In addition to the parties respective
officers, directors and employees who need to know the Confidential Information and who understand the obligation to keep it confidential, the parties may disclose Confidential Information (1) to the extent required by law and (2) to its
agents, auditors and advisors who need to know the Confidential Information for purposes of enabling each party to understand, perform its obligations under, or receive the benefits of, this Letter Agreement and who have agreed not to use or
disclose the Confidential Information for any other purpose without the other partys prior written consent. In the event that a party concludes that disclosure of Confidential Information contained in this Letter Agreement is required by
applicable law, the party will so advise the other party promptly in writing and endeavor to protect the confidentiality of such Confidential Information to the widest extent possible. In the event of a legal dispute with Boeing, nothing herein will
preclude Customer from sharing with its legal counsel information necessary for purposes of enabling counsel to advise or represent Customer provided that so long as Customer causes its legal counsel to maintain the confidentiality of information
that is the subject of this Article. This provision shall not apply to any



|                                |  |  |  |       
|------------------------------- |  |  |  | ------
|PA-3158                         |  |  |  | SA-7  
|Aircraft Performance Guarantees |  |  |  | Page 1

BOEING PROPRIETARY

[* * *] This information is subject to confidential treatment and has been omitted and filed separately with the commission.



---

LOGO





Confidential Information that is in the public domain except that a party will be liable to the other for breach of its obligations under this provision if the Confidential Information entered
the public domain as a consequence of a wrongful act or omission on its part.

Very truly yours,



|                            |  |      
|--------------------------- |  | -----
|THE BOEING COMPANY         
|                            | 
|[***]                       |  |      
|                            | 
|[***]                       |  | [***]
|                           
|ACCEPTED AND AGREED TO this
|                            | 
|Date:                       |  |      
|                           
|TAM Linhas Aereas S.A.     
|                            | 
|By                          |  |      
|                            | 
|Its                         |  |      



|                       |  | 
|---------------------- |  | 
|TAM Linhas Aereas S.A.
|                       | 
|By                     |  | 
|                       | 
|Its                    |  | 



|                                |  |  |  |       
|------------------------------- |  |  |  | ------
|PA-3158                         |  |  |  | SA-7  
|Aircraft Performance Guarantees |  |  |  | Page 1

BOEING PROPRIETARY

[* * *] This information is subject to confidential treatment and has been omitted and filed separately with the commission.



---

|     |  |  |  |                                                        
|---- |  |  |  | -------------------------------------------------------
|LOGO |  |  |  | The Boeing Company P.O. Box 3707
Seattle, WA 98124-2207





TPR-PA-3158-LA-1103768R1

TAM Linhas Aereas S.A.

Rua General Pantaleao Teles, 210

Sao Paulo - SP

04355-040

Brazil



|           |  |                                                                                                                                                                              
|---------- |  | -----------------------------------------------------------------------------------------------------------------------------------------------------------------------------
|Subject:   |  | Table 3 Aircraft Special Matters                                                                                                                                             
|           | 
|Reference: |  | Purchase Agreement No. PA-3158 (Purchase Agreement) between The Boeing Company (Boeing) and TAM Linhas Aereas S.A. (Customer) relating to Model 777F aircraft (777F Aircraft)

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

1. [***]

2. [***]

3. [***]

4. [***]

[***]



|1. | Confidentiality
|-- | ---------------

Boeing and Customer understand that the commercial and financial
information contained in this Letter Agreement is considered by the parties as confidential (Confidential Information) and both agree not to disclose such Confidential Information except as provided herein. In addition to the parties
respective officers, directors and employees who need to know the Confidential Information and who understand the obligation to keep it confidential, the parties may disclose Confidential Information (1) to the extent required by law and
(2) to its agents, auditors and advisors who need to know the Confidential Information for purposes of enabling each party to understand, perform its obligations under, or receive the benefits of, this Letter Agreement and who have agreed not
to use or disclose the Confidential Information for any other purpose without the other partys prior written consent. In the event that a party concludes that disclosure of Confidential Information contained in this Letter Agreement is
required by applicable law, the party will so advise the other party promptly in writing and endeavor





[* * *] This information is
subject to confidential treatment and has been omitted and filed separately with the commission.

BOEING PROPRIETARY



---

LOGO

to protect the confidentiality of such Confidential Information to the widest extent possible. In the event of a legal dispute with Boeing, nothing herein will preclude Customer from sharing with
its legal counsel information necessary for purposes of enabling counsel to advise or represent Customer provided that so long as Customer causes its legal counsel to maintain the confidentiality of information that is the subject of this Article.
This provision shall not apply to any Confidential Information that is in the public domain except that a party will be liable to the other for breach of its obligations under this provision if the Confidential Information entered the public domain
as a consequence of a wrongful act or omission on its part.

Very truly yours,



|                            |  |                 
|--------------------------- |  | ----------------
|THE BOEING COMPANY         
|                            | 
|By                          |  | LOGO            
|                            | 
|Its                         |  | Attorney-In-Fact
|                           
|ACCEPTED AND AGREED TO this
|                            | 
|Date:                       |  |                 
|                           
|TAM Linhas Aereas S.A.     
|                            | 
|By                          |  |                 
|                            | 
|Its                         |  |                 
|                           
|TAM Linhas Aereas S.A.     
|                            | 
|By                          |  |                 
|                            | 
|Its                         |  |                 



[* * *] This information is
subject to confidential treatment and has been omitted and filed separately with the commission.

PA 3158

|                                 |  |            
|-------------------------------- |  | -----------
|Table 3 Aircraft Special Matters |  | SA-7 Page 2

| |  |                    |  | 
| |  | ------------------ |  | 
| |  |                   
| |  | BOEING PROPRIETARY |  | 



---

Attachment to Letter Agreement

No. 6-1161-DJH-1298

GE90-110B1L Engines

Page 1

MODEL 777 FREIGHTER PERFORMANCE
GUARANTEES

FOR TAM LINHAS AEREAS S.A.



|        |  |                             
|------- |  | ----------------------------
|SECTION |  | CONTENTS                    
|        | 
|1       |  | AIRCRAFT MODEL APPLICABILITY
|        | 
|2       |  | FLIGHT PERFORMANCE          
|        | 
|3       |  | MANUFACTURERS EMPTY WEIGHT 
|        | 
|4       |  | AIRCRAFT CONFIGURATION      
|        | 
|5       |  | GUARANTEE CONDITIONS        
|        | 
|6       |  | GUARANTEE COMPLIANCE        
|        | 
|7       |  | EXCLUSIVE GUARANTEES        



|                      |  |  |  |          
|--------------------- |  |  |  | ---------
|P.A. No. 3158         |  |  |  |          
|AERO-B-BBA4-M14-0074B |  |  |  | SS14-0059

BOEING PROPRIETARY

[* * *] This information is subject to confidential treatment and has been omitted and filed separately with the commission.



---

Attachment to Letter Agreement

No. 6-1161-DJH-1298

GE90-110B1L Engines

Page 2



1 [***] [Information in this and the next three pages has been omitted]



|                      |  |  |  |          
|--------------------- |  |  |  | ---------
|P.A. No. 3158         |  |  |  |          
|AERO-B-BBA4-M14-0074B |  |  |  | SS14-0059

BOEING PROPRIETARY

[* * *] This information is subject to confidential treatment and has been omitted and filed separately with the commission.



---

AIRCRAFT CONFIGURATION  777F Aircraft

between

THE BOEING COMPANY

and

TAM LINHAS AÉREAS
S.A.

Exhibit A-4 to Purchase Agreement Number 3158



|              |  |     |  |      
|------------- |  | --- |  | -----
|P.A. No. 3158 |  | A-4 |  | SA-07

BOEING PROPRIETARY

[* * *] This information is subject to confidential treatment and has been omitted and filed separately with the commission.



---

AIRCRAFT CONFIGURATION

Dated

relating to

BOEING MODEL 777-F
AIRCRAFT

[***]



|              |  |    |  |      
|------------- |  | -- |  | -----
|P.A. No. 3158 |  | A1 |  | SA-07

BOEING PROPRIETARY

[* * *] This information is subject to confidential treatment and has been omitted and filed separately with the commission.



---

|     |  |  |  |                                                        
|---- |  |  |  | -------------------------------------------------------
|LOGO |  |  |  | The Boeing Company P.O. Box 3707
Seattle, WA 98124-2207



6-1161-DJH-1295

TAM Linhas Aereas S.A.

Rua General Pantaleao Teles, 210

Sao Paulo - SP

04355-040

Brazil



|           |  |                                                                                                                                                                             
|---------- |  | ----------------------------------------------------------------------------------------------------------------------------------------------------------------------------
|Subject:   |  | May 2017 777F Aircraft Model Substitution Rights                                                                                                                            
|           | 
|Reference: |  | Purchase Agreement No. PA-3158 (Purchase Agreement) between The Boeing Company (Boeing) and TAM Linhas Aereas S.A. (Customer) relating to Model 777 aircraft (777F Aircraft)

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

[***]:



|1. | Customers Written Notice.
|-- | --------------------------

[***]



|2. | Boeings Production Capability.
|-- | -------------------------------

2.1 Customers substitution right is
conditioned upon Boeing having production capability for the Substitute Aircraft in the same scheduled delivery month as [***] Aircraft for which it will be substituted. Boeing will provide a written response to Customers notice of intent
indicating [***].

2.2 If Boeing is unable to manufacture the Substitute Aircraft in the same scheduled delivery month as [***] for which
it will be substituted, then Boeing shall [***] acceptance within thirty days of such offer.

2.3 All of Boeings quoted delivery
positions for Substitute Aircraft shall be considered preliminary until such time as the parties enter into a definitive agreement in accordance with paragraph 4 below.



|3. | Auxiliary Fuel Tanks (for 737MAX-9 Aircraft).
|-- | ---------------------------------------------

[***]



|                                                 |  |        |  |     
|------------------------------------------------ |  | ------ |  | ----
|PA-3158                                          |  |        |  | SA-7
|May 2017 777F Aircraft Model Substitution Rights |  | Page 1

BOEING PROPRIETARY

[* * *] This information is subject to confidential treatment and has been omitted and filed separately with the commission.



---

LOGO



|4. | Definitive Agreement.
|-- | ---------------------

Customers substitution right and Boeings obligation
in this Letter Agreement are further conditioned upon Customers and Boeings executing a definitive agreement for the purchase of the Substitute Aircraft within thirty (30) days of Customers receipt of a draft of such
definitive agreement. Boeing shall provide Customer with a draft of the definitive agreement as soon as reasonably practicable following receipt of Customers notice of intent or, as the case may be, Customers acceptance of an alternative
delivery month. The parties shall negotiate the definitive agreement in good faith.



|5. | Price and Advance Payments.
|-- | ---------------------------

5.1 [***].



|6. | Assignment.
|-- | -----------

[***]



|7. | Confidential Treatment.
|-- | -----------------------

Boeing and Customer understand that the commercial and
financial information contained in this Letter Agreement is considered by the parties as confidential (Confidential Information) and both agree not to disclose such Confidential Information except as provided herein. In addition to the
parties respective officers, directors and employees who need to know the Confidential Information and who understand the obligation to keep it confidential, the parties may disclose Confidential Information (1) to the extent required by
law and (2) to its agents, auditors and advisors who need to know the Confidential Information for purposes of enabling each party to understand, perform its obligations under, or receive the benefits of, this Letter Agreement and who have
agreed not to use or disclose the Confidential Information for any other purpose without the other partys prior written consent. In the event that a party concludes that disclosure of Confidential Information contained in this Letter Agreement
is required by applicable law, the party will so advise the other party promptly in writing and endeavor to protect the confidentiality of such Confidential Information to the widest extent possible. In the event of a legal dispute with Boeing,
nothing herein will preclude Customer from sharing with its legal counsel information necessary for purposes of enabling counsel to advise or represent Customer provided that so long as Customer causes its legal counsel to maintain the
confidentiality of information that is the subject of this Article. This provision shall not apply to any Confidential Information that is in the public domain except that a party will be liable to the other for breach of its obligations under this
provision if the Confidential Information entered the public domain as a consequence of a wrongful act or omission on its part.



PA-3158

|                                                 |  |     
|------------------------------------------------ |  | ----
|May 2017 777F Aircraft Model Substitution Rights |  | SA-7

| |  |                    |  |       
| |  | ------------------ |  | ------
| |  |                    |  | Page 2
| |  | BOEING PROPRIETARY |  |       

[* * *] This information is subject to confidential treatment and has been omitted and filed separately with
the commission.



---

LOGO



Very truly yours,



|                            |  |                 
|--------------------------- |  | ----------------
|THE BOEING COMPANY         
|                            | 
|By                          |  | LOGO            
|                            | 
|Its                         |  | Attorney-In-Fact
|                           
|ACCEPTED AND AGREED TO this
|                            | 
|Date:                       |  |                 
|                           
|TAM Linhas Aereas S.A.     
|                            | 
|By                          |  |                 
|                            | 
|Its                         |  |                 
|                           
|TAM Linhas Aereas S.A.     
|                            | 
|By                          |  |                 
|                            | 
|Its                         |  |                 



PA-3158

|                                                 |  |     
|------------------------------------------------ |  | ----
|May 2017 777F Aircraft Model Substitution Rights |  | SA-7

| |  |                    |  |       
| |  | ------------------ |  | ------
| |  |                    |  | Page 3
| |  | BOEING PROPRIETARY |  |       

[* * *] This information is subject to confidential treatment and has been omitted and filed separately with
the commission.



---

|     |  |  |  |                                                        
|---- |  |  |  | -------------------------------------------------------
|LOGO |  |  |  | The Boeing Company P.O. Box 3707
Seattle, WA 98124-2207





TPR-PA-3158-LA-1103767R-1

TAM Linhas Aereas S.A.

Rua General Pantaleao Teles, 210

Sao Paulo - SP

04355-040

Brazil



|           |  |                                                                                                                                                                              
|---------- |  | -----------------------------------------------------------------------------------------------------------------------------------------------------------------------------
|Subject:   |  | Table 3 Aircraft Banded Fixed Escalation Program                                                                                                                             
|           | 
|Reference: |  | Purchase Agreement No. PA-3158 (Purchase Agreement) between The Boeing Company (Boeing) and TAM Linhas Aereas S.A. (Customer) relating to Model 777-300ER aircraft (Aircraft)

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

[* * *]

[The information in the next ten pages has been omitted].



|                                |  |                    |  |          
|------------------------------- |  | ------------------ |  | ---------
|TPR-PA-3158-LA-1103767R-1       |  |                    |  |          
|Escalation-Banded Fixed Program |  |                    |  | LA Page 1
|                                |  | BOEING PROPRIETARY |  | SA-7     

[* * *] This information is subject to confidential treatment and has been omitted and filed
separately with the commission.



---

LOGO



|      |  |  |  |      
|----- |  |  |  | -----
|[***] |  |  |  |      
|      |  | 
|[***] |  |  |  |      
|      |  | 
|[***] |  |  |  | LOGO 
|      |  | 
|[***] |  |  |  | [***]
|      |  | 
|[***] |  |  |  |      
|      |  | 
|[***] |  |  |  |      
|      |  | 
|[***] |  |  |  |      
|      |  | 
|[***] |  |  |  |      
|      |  | 
|[***] |  |  |  |      
|      |  | 
|[***] |  |  |  |      
|      |  | 
|[***] |  |  |  |      
|      |  | 
|[***] |  |  |  |      



TPR-PA-3158-LA-1103767R-1

|                                |  |          
|------------------------------- |  | ---------
|Escalation-Banded Fixed Program |  | LA Page 2

| |  |                    |  |     
| |  | ------------------ |  | ----
| |  | BOEING PROPRIETARY |  | SA-7

[* * *] This information is subject to confidential treatment and has been omitted and filed
separately with the commission.



---

LOGO

[***]



|      |  |       |  |      
|----- |  | ----- |  | -----
|[***] |  | [***] |  | [***]
|[***] |  | [***] |  | [***]
|[***] |  | [***] |  | [***]
|[***] |  | [***] |  | [***]
|[***] |  | [***] |  | [***]
|[***] |  | [***] |  | [***]
|[***] |  | [***] |  | [***]
|[***] |  | [***] |  | [***]
|[***] |  | [***] |  | [***]
|[***] |  | [***] |  | [***]
|[***] |  | [***] |  | [***]
|[***] |  | [***] |  | [***]
|[***] |  | [***] |  | [***]
|[***] |  | [***] |  | [***]





TPR-PA-3158-LA-1103767R-1

|                                |  |          
|------------------------------- |  | ---------
|Escalation-Banded Fixed Program |  | LA Page 3

| |  |                    |  |     
| |  | ------------------ |  | ----
| |  | BOEING PROPRIETARY |  | SA-7

[* * *] This information is subject to confidential treatment and has been omitted and filed
separately with the commission.



---

LOGO

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TPR-PA-3158-LA-1103767R-1

|                                |  |          
|------------------------------- |  | ---------
|Escalation-Banded Fixed Program |  | LA Page 4

| |  |                    |  |     
| |  | ------------------ |  | ----
| |  | BOEING PROPRIETARY |  | SA-7

[* * *] This information is subject to confidential treatment and has been omitted and filed
separately with the commission.



---

LOGO



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TPR-PA-3158-LA-1103767R-1

|                                |  |          
|------------------------------- |  | ---------
|Escalation-Banded Fixed Program |  | LA Page 5

| |  |                    |  |     
| |  | ------------------ |  | ----
| |  | BOEING PROPRIETARY |  | SA-7

[* * *] This information is subject to confidential treatment and has been omitted and filed
separately with the commission.



---

LOGO



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|[***] |  | [***] |  | [***] |  | [***]





TPR-PA-3158-LA-1103767R-1

|                                |  |          
|------------------------------- |  | ---------
|Escalation-Banded Fixed Program |  | LA Page 6

| |  |                    |  |     
| |  | ------------------ |  | ----
| |  | BOEING PROPRIETARY |  | SA-7

[* * *] This information is subject to confidential treatment and has been omitted and filed
separately with the commission.



---

LOGO



|      |  |       |  |       |  |      
|----- |  | ----- |  | ----- |  | -----
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|[***] |  | [***] |  | [***] |  | [***]





TPR-PA-3158-LA-1103767R-1

|                                |  |          
|------------------------------- |  | ---------
|Escalation-Banded Fixed Program |  | LA Page 7

| |  |                    |  |     
| |  | ------------------ |  | ----
| |  | BOEING PROPRIETARY |  | SA-7

[* * *] This information is subject to confidential treatment and has been omitted and filed
separately with the commission.



---

LOGO



|      |  |       |  |       |  |      
|----- |  | ----- |  | ----- |  | -----
|[***] |  | [***] |  | [***] |  | [***]
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TPR-PA-3158-LA-1103767R-1

|                                |  |          
|------------------------------- |  | ---------
|Escalation-Banded Fixed Program |  | LA Page 8

| |  |                    |  |     
| |  | ------------------ |  | ----
| |  | BOEING PROPRIETARY |  | SA-7

[* * *] This information is subject to confidential treatment and has been omitted and filed
separately with the commission.