----

| Manufacturer’sSerial Number |         | Previous AircraftMinor Model |         | Revised AircraftMinor Model |         | OriginalContractDelivery |         | Revised ContractDelivery |
|----------------------------------------|--------------|----------------------------------------|--------------|---------------------------------------|--------------|--------------------------|--------------|-------------------------------|
|                                   |         |                                   |         |                                  |         |                     |         |                          |
| 40799                                  |         | 767-300ER                              |         | 767-316F                              |         | Sep 2012                 |         | 2nd Qtr 2013                  |
|                                   |         |                                   |         |                                  |         |                     |         |                          |
| 40592                                  |         | 767-300ER                              |         | 767-316F                              |         | Oct 2012                 |         | 4th Qtr 2013                  |
|                                   |         |                                   |         |                                  |         |                     |         |                          |
| 40593                                  |    | 767-300ER                              |    | 767-316F                              |    | Nov 2012                 |    | 1st Qtr 2014                  |

----

----

| THE BOEING COMPANY |             | LAN AIRLINES S.A. |
|--------------------|------------------|-------------------|
|               |             |              |   |   |
| By:                |             |              | By: |   |
|               | Kathie S. Weibel |              |   | Mr. Roberto Alvo |
|               |             |              |   |   |
| Its                | Attorney-In-Fact |              | Its: | Sr. Vice President Strategic Planning & Corporate Development |
|               |             |              |   |   |
|               |             |              | By: |   |
|               |             |              |   | Mr. Alejandro de la Fuente |
|               |             |              |   |   |
|               |             |              | Its: | Chief Financial Officer |

----

----

|                  |   |                                                         |   | Supplemental |
|-----------------------|--------|--------------------------------------------------------------|--------|--------------|
|                  |   |                                                         |   | Agreement    |
| ARTICLES              |   |                                                         |   |         |
|   1.             |   | Quantity, Model and Description                              |   | 24           |
|   2.             |   | Delivery Schedule                                            |   | 24           |
|   3.             |   | Price                                                        |   | 24           |
|   4.             |   | Payment                                                      |   | 24           |
|   5.             |   | Miscellaneous                                                |   | 24           |
|   6.             |   | Confidentiality                                              |   | 24           |
|                  |   |                                                         |   |         |
| TABLE                 |   |                                                         |   |         |
|   1.             |   | Aircraft Information Table 767-300ER Aircraft – 1995$  |   | 1            |
|   2.             |   | Aircraft Information Table 767-300F Aircraft – 1997$   |   | 1            |
|   3.             |   | Aircraft Information Table 767-300F Aircraft – 1998$   |   | 8            |
|   4.             |   | Aircraft Information Table 767-300F Aircraft – 1999$   |   | 11           |
|   5.             |   | Aircraft Information Table 767-300F Aircraft – 2003$   |   | 18           |
|   6.             |   | Aircraft Information Table 767-316ER Aircraft – 2003$  |   | 21           |
|   7.             |   | Aircraft Information Table 767-300F Aircraft – 2004$   |   | 24           |
|   8.             |   | Aircraft Information Table 767-316ER Aircraft – 2004$  |   | 22           |
|   9.             |   | Aircraft Information Table 767-316ER Aircraft – 2005 $ |   | 22           |
| 10.                   |   | Aircraft Information Table 767-316ER Aircraft – 2006 $ |   | 25           |
| 11.                   |   | Aircraft Information Table 767-316ER Aircraft – 2008 $ |   | 28           |
| 12.                   |   | Aircraft Information Table 767-316F Aircraft – 2008$   |   | 28           |
|                  |   |                                                         |   |         |
| EXHIBITS              |   |                                                         |   |         |
| A.                    |   | Aircraft Configuration                                       |   |         |
| A-1                   |   | Aircraft Configuration                                       |   | 1            |
| A-2                   |   | Aircraft Configuration                                       |   | 5            |
| A-3                   |   | Aircraft Configuration                                       |   | 10           |
| A-4                   |   | Aircraft Configuration 767-316F Aircraft – 2003$       |   | 15           |
| A-5                   |   | Aircraft Configuration 767-316ER Aircraft – 2003$      |   | 17           |
| A-6                   |   | Aircraft Configuration 767-316ER Aircraft – 2004$      |   | 22           |
| A-7                   |   | Aircraft Configuration 767-316ER Aircraft – 2005$      |   | 22           |
| A-8                   |   | Aircraft Configuration 767-316ER Aircraft – 2006$      |   | 23           |
| A-9                   |   | Aircraft Configuration 767-316ER Aircraft – 2008$      |   | 24           |
| A-10                  |   | Aircraft Configuration 767-316F Aircraft – 2008$       |   | 28           |
| B.                    |   | Aircraft Delivery Requirements and Responsibilities          |   | 1            |
|                  |   |                                                         |   |         |
| SUPPLEMENTAL EXHIBITS |   |                                                         |
| BFE1.                 |   | BFE Variables                                                |   | 1            |
| CS1.                  |   | Customer Support Variables                                   |   | 1            |
| EE1.                  |   | Engine Escalation/Engine Warranty and Patent Indemnity       |   | 1            |
| EE1-1.                |   | Engine Escalation/Engine Warranty and Patent Indemnity       |   | 5            |
| EE1-2.                |   | Engine Escalation/Engine Warranty and Patent Indemnity       |   | 13           |
| EE1-2006$             |   | Engine Escalation, Engine Warranty & Patent Indemnity    |   | 26           |
| EE1-2008$             |   | Engine Escalation, Engine Warranty & Patent Indemnity    |   | 26           |
|                  |   |                                                         |   |         |
| SLP1.                 |   | Service Life Policy Components                               |   |         |
| AE1                   |   | Escalation adjustment - airframe and optional features       |   | 22           |
| AE1 2008$             |   | Escalation adjustment - airframe and optional features       |   | 24           |
|                  |   |                                                         |   |         |
| LETTER AGREEMENTS     |   |                                                         |
|                  |   |                                                         |   |         |
| 2126-1                |   | Seller Purchased Equipment                                   |   |         |
| 2126-2R1              |   | Cabin Systems Equipment                                      |   | 17           |
| 2126-3R4              |   | Option Aircraft                                              |   | 13           |

----

| 6-1162-DMH-350     | Performance Guarantees                                                                                                       |         |
|--------------------|------------------------------------------------------------------------------------------------------------------------------|--------------|
| 6-1162-DMH-351     | Promotion Support                                                                                                            |         |
| 6-1162-DMH-472     | Performance Guarantees                                                                                                       | 1            |
| 6-1162-DMH-475     | Configuration Matters                                                                                                        | 1            |
| [***]              | [***]                                                                                                                        | [***]        |
| 6-1162-LAJ-311     | Special Matters Relating to the July 2001 and September 2001 Aircraft                                                        | 11           |
| 6-1162-LAJ-956     | Special Matters Relating to four 2006 Delivery Aircraft (February 4, 2005)                                                   |         |
| 6-1162-LAJ-0895R6  | Business Considerations                                                                                                      | 23           |
| [***]              | [***]                                                                                                                        | [***]        |
| 6-1162-ILK-0381 R2 | Special Matters Letter Applicable to the 2011 Accelerated Aircraft and the Substitute 767 Freighter Aircraft                 | 28           |
| 6-1162-ILK-0382    | No longer applicable                                                                                                         | 26           |
| 6-1162-ILK-0383 R1 | Aircraft Model Substitution Relating to the 2011 Accelerated Aircraft and the Substitute 767 Freighter Aircraft              | 26           |
| 6-1162-ILK-0384 R2 | 16G Seats                                                                                                                    | 27           |
| 6-1162-ILK-0385 R2 | Performance Guarantees Relating to the 2011 Accelerated Aircraft; the 2012 Accelerated Aircraft and the Incremental Aircraft | 27           |
| 6-1162-ILK-0388    | Option Aircraft -deleted                                                                                                     | 28 (Art 6.2) |
| 6-1162-ILK-0412    | Special Matters Relating to Three Aircraft Originally Scheduled to Deliver in 2009                                           | 25           |
| [***]              | [***]                                                                                                                        | [***]        |
| 6-1162-KSW-6423    | Special Matters Letter Applicable to the Incremental Aircraft                                                                | 27           |
| 6-1162-KSW-6424    | Aircraft Model Substitution Relating to the Incremental Aircraft                                                             | 27           |
|               | RESTRICTED LETTER AGREEMENTS                                                                                                 |         |
|               | (continued)                                                                                                                  |         |
|               |                                                                                                                         |         |
| 6-1162-KSW-6456    | Performance Guarantees for Substitute 767 Freighter Aircraft                                                                 | 28           |

----

| Airframe Model/MTOW:                         | 767-300F    | 412000 pounds                         | Detail Specification:                              | D019T002LAN63F-1                      |
|----------------------------------------------|-------------|--------------------------------------------|----------------------------------------------------|---------------------------------------|
| Engine Model/Thrust:                         | CF6-80C2B6F | 60200 pounds                               | Airframe Price Base Year/Escalation Formula:  | Jul-08 ECI-MFG / CPI                  |
| Airframe Price:                              |        | [***]                                      | Engine Price Base Year/Escalation Formula:    | Jul-08 GE CF6-80 & GE90 (99 rev.) |
| Optional Features:                           |        | [***]                                      |                                               |                                  |   |
| Sub-Total of Airframe and Features:          | [***]       | Airframe Escalation Data:                  | (2Q09 Esc Fcst)                                    |
| Engine Price (Per Aircraft):                 |        | [***]                                      | Base Year Index (ECI):                             | 103.1                                 |
| Aircraft Basic Price (Excluding BFE/SPE):    | [***]       | Base Year Index (CPI):                     | 208.2                                              |
| Buyer Furnished Equipment (BFE) Estimate:    | [***]       | Engine Escalation Data:                    |                                               |                                  |
| Seller Purchased Equipment (SPE) Estimate:   | [***]       | Base Year Index (CPI):                     | 129.930                                            |
|                                         |        |                                       |                                               |
| Initial Payment/Aircraft at Proposal Accept: | [***]       | Escalation is not fixed for these aircraft |                                               |

|    |         |      |         | Escalation |         | Escalation |         |          |         | [***]  |         | [***]  |         |   |         |   |         |   |
|--------------|--------------|-----------|--------------|------------|--------------|------------|--------------|---------------|--------------|--------|--------------|--------|--------------|--------|--------------|--------|--------------|--------|
| Delivery     |         | Number of |         | Factor     |         | Factor     |         | Manufacturer  |         | [***]  |         | [***]  |         | [***]  |         | [***]  |         | [***]  |
| Date         |         | Aircraft  |         | (Airframe) |         | (Engine)   |         | Serial Number |         | [***]  |         | [***]  |         | [***]  |         | [***]  |         | [***]  |
| [***]        |         | 1         |         | 1.0964     |         | 1.1360     |         | 40799         |         | [***]  |         | [***]  |         | [***]  |         | [***]  |         | [***]  |
| [***]        |         | 1         |         | 1.1066     |         | 1.1510     |         | 40592         |         | [***]  |         | [***]  |         | [***]  |         | [***]  |         | [***]  |
| [***]        |         | 1         |         | 1.1146     |         | 1.1610     |         | 40593         |         | [***]  |         | [***]  |         | [***]  |         | [***]  |         | [***]  |
| Total        |    | 3         |    |       |    |       |    |          |    |   |    |   |    |   |    |   |    |   |

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

----

| Subject: | Special Matters Letter Applicable to the 2011 Accelerated Aircraft and the Substitute 767 Freighter Aircraft |
|----------|--------------------------------------------------------------------------------------------------------------|

| Reference: | Purchase Agreement No. 2126 (the Purchase Agreement) between The Boeing Company (Boeing) and LAN Airlines S.A. (Customer) relating to Model 767-316F, Model 767-38EF and Model 767-316ER aircraft (hereinafter referred to as "Aircraft") |
|------------|----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

|   | 1. |  Definitions. |
|--------|----|--------------------|

----

----

|   | 2. | Export License. |
|--------|----|-----------------|

|   | 3. | Warranty Modification. |
|--------|----|------------------------|

|   | 4. | Credit Memoranda for the 2011 Accelerated Aircraft and Substitute 767 Freighter Aircraft. |
|--------|----|-------------------------------------------------------------------------------------------|

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

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

----

|   | 5. | [***]. |
|--------|----|--------|

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

|   | 6. | Special Considerations for the Substitute Aircraft. |
|--------|----|-----------------------------------------------------|

----

|   | 6.5.1 | Article 5 of this Letter Agreement; and |
|--------|-------|-----------------------------------------|

|   | 6.5.2 | [***]. |
|--------|-------|--------|

|   | 7. | Intentionally Deleted. |
|--------|----|------------------------|

|   | 8. | Assignment. |
|--------|----|-------------|

|   | iii. | responding to a Customer request for proposals to provide financing of Aircraft pursuant to the Purchase Agreement, including pre-delivery payment financing |
|--------|------|--------------------------------------------------------------------------------------------------------------------------------------------------------------|

----

|   | 9. | 16G Seat Requirement Credit Memorandum. |
|--------|----|-----------------------------------------|

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

|   | 10. | Deferral of Payment Due at Signing of Supplemental Agreement 24 (SA-24). (This section is no longer applicable.) |
|--------|-----|------------------------------------------------------------------------------------------------------------------|

|   | 11. | [***]. |
|--------|-----|--------|

|   | 12. | Confidentiality. |
|--------|-----|------------------|

----

| THE BOEING COMPANY |
|--------------------|
|               |   |   |
| By:                |   |   |
|               | Kathie S. Weibel |   |
|               |   |   |
| Its:               | Attorney-In-Fact |   |

----

| ACCEPTED AND AGREED TO this 22 day of March 2010. |                                                    |
|---------------------------------------------------|---------------------------------------------------------|
|                                              |                                                    |
| LAN AIRLINES S.A.                                 |                                                    |
|                                              |                                                    |   |
| By:                                               |                                                    |   |
|                                              | Mr. Roberto Alvo                                        |   |
|                                              |                                                    |   |
| Its:                                              |   Sr. Vice President  Strategic Planning |   |
|                                              | & Corporate Development                             |   |
|                                              |                                                    |   |
| By:                                               |                                                    |   |
|                                              | Mr. Alejandro de la Fuente                              |   |
| Its:                                              | Chief Financial Officer                                 |   |

----

| Airframe Model/MTOW:                         | 767-300F    | 412000 pounds |                                       | Detail Specification:                              | D019T002LAN63F-1                      |
|----------------------------------------------|-------------|--------------------|--------------------------------------------|----------------------------------------------------|---------------------------------------|
| Engine Model/Thrust:                         | CF6-80C2B6F | 60200 pounds       |                                       | Airframe Price Base Year/Escalation Formula:  | Jul-08 ECI-MFG / CPI                  |
| Airframe Price:                              |        | ***                |                                       | Engine Price Base Year/Escalation Formula:    | Jul-08 GE CF6-80 & GE90 (99 rev.) |
| Optional Features:                           |        | ***                |                                       |                                               |                                  |   |
| Sub-Total of Airframe and Features:          | ***         |               | Airframe Escalation Data:                  | (4Q08 Esc Fcst)                                    |
| Engine Price (Per Aircraft):                 |        | ***                |                                       | Base Year Index (ECI):                             | 103.1                                 |
| Aircraft Basic Price (Excluding BFE/SPE):    | ***         |               | Base Year Index (CPI):                     | 208.2                                              |
| Buyer Furnished Equipment (BFE) Estimate:    | ***0        |               | Engine Escalation Data:                    |                                               |                                  |
| Seller Purchased Equipment (SPE) Estimate:   | ***         |               | Base Year Index (CPI):                     | 129.930                                            |
|                                         |        |               |                                       |                                               |
| Initial Payment/Aircraft at Proposal Accept: | ***         |               | Escalation is not fixed for these aircraft |                                               |

|    |         |      |         | Escalation |         | Escalation |         |          |         | Escalation Estimage   |        | ***          |   |         |   |         |   |         |
|--------------|--------------|-----------|--------------|------------|--------------|------------|--------------|---------------|--------------|----------------------------|-------------|--------------|--------|--------------|--------|--------------|--------|--------------|
| Delivery     |         | Number of |         | Factor     |         | Factor     |         | Manufacturer  |         | Adv Payment Base |        | ***          |   | ***          |   | ***          |   | ***          |
| Date         |         | Aircraft  |         | (Airframe) |         | (Engine)   |         | Serial Number |         | Price Per A/P    |        | ***          |   | ***          |   | ***          |   | ***          |
| Oct-2011     |         | 1         |         | 1.0622     |         | 1.0900     |         | 40590         |         | $                          | 171,309,000 |         | ***    |         | ***    |         | ***    |         | *** |
| Nov-2011     |         | 1         |         | 1.0633     |         | 1.0930     |         | 40591         |         | $                          | 171,529,000 |         | ***    |         | ***    |         | ***    |         | *** |
| Total        |    | 2         |    |       |    |       |    |          |    |                       |        |    |   |    |   |    |   |    |   |

----

|   | ***    |
|--------|--------|
|   |   |
| ***    | ***    |
|   |   |
| ***    | ***    |
|   |   |
| ***    | ***    |
|   |   |
| ***    | ***    |

----

| 0110-000035 |   | MAJOR MODEL 767 AIRPLANE                                                                                                                                         |   | [***] |
|-------------|--------|------------------------------------------------------------------------------------------------------------------------------------------------------------------|--------|-------|
| 0110-000038 |   | MINOR MODEL 767-300F FREIGHTER AIRPLANE                                                                                                                          |   | [***] |
| 0110-000094 |   | MODEL 767-300 GENERAL MARKET FREIGHTER AIRPLANE                                                                                                                  |   | [***] |
| 0220-000040 |   | FAA TYPE CERTIFICATION                                                                                                                                           |   | [***] |
| 0220-000136 |   | 15 KNOT MAXIMUM TAKEOFF AND LANDING TAILWIND COMPONENT CERTIFICATION                                                                                             |   | [***] |
| 0221-000002 |   | DISPATCH WITH GEAR EXTENDED FOR REVENUE FLIGHT                                                                                                                   |   | [***] |
| 0221A251A19 |   | ENGINE INOPERATIVE TEN-MINUTE TAKEOFF THRUST OPERATION - CF6-80C2B6F THRUST RATING                                                                               |   | [***] |
| 0228-000032 |   | OPERATIONS MANUAL IN FAA FORMAT                                                                                                                                  |   | [***] |
| 0229A141A41 |   | PERFORMANCE - CERTIFICATION FOR OPERATION AT AIRPORT ALTITUDES OF 9500 FEET AND BELOW                                                                            |   | [***] |
| 0252-000014 |   | ENVIRONMENTAL CONTROL SYSTEM  -  TEMPERATURE INDICATIONS IN DEGREES CELSIUS                                                                  |   | [***] |
| 0252-000017 |   | INSTRUMENTATION WITH METRIC UNITS  -  MODEL 767                                                                                              |   | [***] |
| 0351A114C45 |   | TAKEOFF PERFORMANCE IMPROVEMENT - ALTERNATE FORWARD CENTER OF GRAVITY LIMITS                                                                                     |   | [***] |
| 0360B604F64 |   | MISCELLANEOUS WEIGHT COLLECTOR                                                                                                                                   |   | [***] |
| 1110B657K77 |   | MP - EXTERIOR COLOR SCHEME AND MARKINGS - REVISION - LAN 767-316F                                                                                                |   | [***] |
| 1110B657P08 |   | MP - EXTERIOR COLOR SCHEME AND MARKINGS - REVISION - LAN 767-316F                                                                                                |   | [***] |
| 1110C262A21 |   | EXTERIOR COLOR SCHEME AND MARKINGS - LAN 767-316F                                                                                                                |   | [***] |
| 1130-000344 |   | BOEING STANDARD MARKINGS - MAIN DECK CARGO COMPARTMENT                                                                                                           |   | [***] |
| 1130A931A06 |   | IATA STANDARD MARKINGS - LOWER LOBE CARGO COMPARTMENT                                                                                                            |   | [***] |
| 2145-000004 |   | BULK CARGO AREA HEATING AND VENTILATING FOR ANIMAL CARRIAGE                                                                                                      |   | [***] |
| 2210-000030 |   | AUTOFLIGHT - THREE DIGIT MACH NUMBER ON MODE CONTROL PANEL                                                                                                       |   | [***] |
| 2210-000031 |   | AUTOFLIGHT - AUTOMATIC AUTOPILOT CHANNEL SELECTION IN APPROACH MODE                                                                                              |   | [***] |
| 2210-000037 |   | AUTOFLIGHT - BANK ANGLE HOLD AT AUTOPILOT COMMAND ENGAGE                                                                                                         |   | [***] |
| 2210-000039 |   | AUTOFLIGHT - FULL TIME FLIGHT DIRECTOR                                                                                                                           |   | [***] |
| 2210-000151 |   | AUTOFLIGHT - ENABLE GLIDE SLOPE CAPTURE PRIOR TO LOCALIZER CAPTURE                                                                                               |   | [***] |
| 2210-000311 |   | AUTOFLIGHT - FLIGHT CONTROL COMPUTER (FCC) WITHOUT ONBOARD SOFTWARE LOADING CAPABILITY                                                                           |   | [***] |
| 2210A064A02 |   | AUTOFLIGHT - ALTITUDE ALERT - 300/900 FEET                                                                                                                       |   | [***] |
| 2210A811A40 |   | AUTOFLIGHT-REV-INHIBIT ILO ENABLE                                                                                                                                |   | [***] |
| 2210B403A07 |   | MODE CONTROL PANEL WITH BACKCOURSE SWITCH                                                                                                                        |   | [***] |
| 2230-000127 |   | AUTOTHROTTLE - SELECTION OF CLIMB DERATES                                                                                                                        |   | [***] |
| 2230-000133 |   | AUTOTHROTTLE - FIXED PERCENTAGE DERATE LEVELS OF 10% AND 20%                                                                                                     |   | [***] |
| 2230-000135 |   | AUTOTHROTTLE - CLIMB DERATE WASHOUT SCHEDULE - 10,000 TO 12,000 FEET                                                                                             |   | [***] |
| 2311-000122 |   | HF COMMUNICATIONS - DUAL GABLES HF CONTROL PANEL WITH SENSITIVITY CONTROL - P/N G7401-03 - BFE/SPE                                                               |   | [***] |
| 2311A213A84 |   | HF COMMUNICATIONS - DUAL ROCKWELL HF TRANSCEIVERS - P/N 822-0330-001 AND DIGITAL HF COUPLERS - P/N 822-0987-003 - BFE/SPE                                        |   | [***] |
| 2311B800D30 |   | MP - HIGH FREQUENCY (HF) COMMUNCIATIONS - ACTIVATION - DUAL ARINC 753 DATA LINK                                                                                  |   | [***] |
| 2311B800D40 |   | MP - HF COMMUNICATIONS - REPLACEMENT - DUAL GABLES HF CONTROL PANELS - P/N G7401-16 IN LIEU OF P/N G7401-03 - SPE                                                |   | [***] |
| 2311B800D41 |   | MP - HF COMMUNICATIONS - REPLACEMENT - DUAL ROCKWELL HF TRANSCEIVERS AND COUPLERS - 822-0990-004 AND 822-0987-004 IN LIEU OF 822-0330-001 AND 822-0987-003 - SPE |   | [***] |

----

| 2311C351C28 |   | MP - HF COMMUNICATIONS - REVISIONS - PARTIAL PROVISIONS FOR DUAL ARINC 753 HF DATALINK                                                                                     |   | [***] |
|-------------|--------|----------------------------------------------------------------------------------------------------------------------------------------------------------------------------|--------|-------|
| 2312-000432 |   | VHF COMMUNICATIONS - TRIPLE GABLES VHF TUNING PANELS (DUAL KNOB) - P/N G7400-27 - BFE/SPE                                                                                  |   | [***] |
| 2312-000703 |   | VHF COMMUNICATIONS - ACTIVATION OF 8.33 KHZ CHANNEL SPACING                                                                                                                |   | [***] |
| 2312-000786 |   | VHF COMMUNICATIONS - TRIPLE ROCKWELL ARINC 716/750 VHF-900B FM IMMUNE TRANSCEIVERS WITH 8.33 KHZ CHANNEL SPACING AND CMC INTERFACE CAPABILITY - P/N 822-1047-003 - BFE/SPE |   | [***] |
| 2312B800D42 |   | MP - VHF COMMUNICATIONS SYSTESM - REPLACEMENT - GABLES CONTROL PLANEL - G7400-227 IN LIEU OF G7400-27 - SPE                                                                |   | [***] |
| 2312B800D44 |   | MP - VHF COMMUNICATIONS - REPLACEMENT - ROCKWELL VHF TRANSCEIVERS - 822-1250-002 IN LIEU OF 822-1047-003 - SPE                                                             |   | [***] |
| 2315A213A67 |   | SATCOM - PARTIAL PROVISIONS FOR SATCOM SYSTEM AND TOP MOUNTED HIGH GAIN ANTENNA SYSTEM - MODEL 767                                                                         |   | [***] |
| 2315B800C72 |   | SATCOM - HF/SATCOM SELECT PANEL - INSTALLATION - FLIGHT DECK                                                                                                               |   | [***] |
| 2321B401A04 |   | SELCAL - AVTECH FIVE CHANNEL DECODER - P/N NA138-714C  - BFE/SPE                                                                                                 |   | [***] |
| 2322-000250 |   | ACARS - PARTIAL PROVISIONS FOR SINGLE ARINC 724B ACARS                                                                                                                     |   | [***] |
| 2322B800D45 |   | MP - ACARS - REVISION - ROCKWELL COLLINS ARINC 758 CMU (LEVEL AOA/VDL MODE 2 OPERATION) - SPE                                                                              |   | [***] |
| 2322B800D46 |   | MP - ACARS - INSTALLATION - ROCKWELL MULTIPURPOSE INTERACTIVE DISPLAY UNIT (MIDU) IN LIEU OF TELEDYNE INTERACTIVE DISPLAY UNIT (IDU) - SPE                                 |   | [***] |
| 2324B800D31 |   | MP - EMERGENCY LOCATOR TRANSMITTER (ELT) - ELTA 3-FREQUENCY AUTOMATIC - FIXED - P/N 95N6088 - SPE                                                                          |   | [***] |
| 2340B800C73 |   | CREW COMMUNICATION - PILOTS' CALL PANEL - SELCAL AND CARGO LOADING/GROUND CALL - 767 FREIGHTER                                                                             |   | [***] |
| 2350B800C71 |   | AUDIO INTEGRATING - AUDIO SELECTOR PANELS - FLIGHT DECK                                                                                                                    |   | [***] |
| 2351-000042 |   | CONTROL WHEEL PUSH TO TALK (PTT) SWITCH - STANDARD THREE POSITION                                                                                                          |   | [***] |
| 2351A138C64 |   | HAND HELD MICROPHONE - CAPTAIN, FIRST OFFICER AND FIRST OBSERVER -TELEPHONICS - P/N 107C800-22 - BFE/SPE                                                                   |   | [***] |
| 2351A213A33 |   | AUDIO INTEGRATION - INSTALLATION - TWO-PLUG AUDIO JACKS IN THE FLIGHT DECK                                                                                                 |   | [***] |
| 2351A213B77 |   | BOOM MICROPHONE HEADSETS - CAPTAIN AND FIRST OFFICER - TELEX AIRMAN 750 - P/N 64300-200 - BFE/SPE                                                                          |   | [***] |
| 2351A213B80 |   | HEADPHONE - FIRST OBSERVER - TELEX - P/N 64400-200 - BFE/SPE                                                                                                               |   | [***] |
| 2371-000009 |   | NO MONITOR JACK IN THE WHEEL WELL                                                                                                                                          |   | [***] |
| 2371-000017 |   | SOLID STATE VOICE RECORDER ED56A AND SOLID STATE MICROPHONE/MONITOR ED56A - ALLIEDSIGNAL - 2 HOUR RECORDING TIME - P/N 980-6022-001 AND P/N 980-6116-002 - BFE/SPE         |   | [***] |
| 2433-000021 |   | STANDBY POWER - EXTENDED TIME CAPABILITY - BATTERY PARALELLING                                                                                                             |   | [***] |
| 2511-000022 |   | MANUALLY OPERATED SEATS  -  CAPTAIN AND FIRST OFFICER                                                                                                  |   | [***] |
| 2513-000405 |   | SUNVISOR INSTALLATION - NUMBER 1 AND 2 WINDOWS - FLIGHT DECK - SFE                                                                                                         |   | [***] |
| 2527-000732 |   | CONVERSION OPTION - GALLEY/ENTRY AND LAVATORY MAT INSTALLATION - TARAFLEX - 767 FREIGHTER                                                                                  |   | [***] |
| 2530B604F65 |   | GALLEY INSERT PART NUMBERS - BFE/SPE                                                                                                                                       |   | [***] |

----

| 2550-000157 |   | DELIVERY CONFIGURATION - MAIN DECK - TRANSVERSE TYPE A (88" X 125 ") PALLETS                                                                          |   | [***] |
|-------------|--------|-------------------------------------------------------------------------------------------------------------------------------------------------------|--------|-------|
| 2550-000162 |   | ALTERNATE CARGO COMPARTMENT ARRANGEMENT - MAIN DECK - SIDE BY SIDE CONTOURED 88" X 125" TYPE A PALLETS                                                |   | [***] |
| 2550-000261 |   | CONVERSION OPTION - FIRST PALLET POSITION FOR ACCESS TO LIVE ANIMAL CARRIAGE OR HAZARDOUS MATERIAL CARRIAGE - 767 FREIGHTER                           |   | [***] |
| 2550-000263 |   | CONVERSION OPTION - ALTERNATE CARGO COMPARTMENT ARRANGEMENT - MAIN DECK - ADDITIONAL 96" X 196" PALLETS - FREIGHTER                                   |   | [***] |
| 2553-000044 |   | HARDWARE FOR CARRIAGE OF 88 X 125 AND 96 X 125 INCH PALLETS AND STANDARD CONTAINERS IN THE FORWARD CARGO COMPARTMENT                                  |   | [***] |
| 2555-000053 |   | CONVERSION OPTION - INSTALLATION OF ADDITIONAL NET AFT OF THE AFT CARGO DOOR                                                                          |   | [***] |
| 2560-000177 |   | HALON FIRE EXTINGUISHER - FLIGHT DECK - WALTER KIDDE                                                                                                  |   | [***] |
| 2560A141A86 |   | CREW LIFE VESTS - FLIGHT DECK - SWITLIK - P/N S-31850-6300-AAR001 - BFE/SPE                                                                           |   | [***] |
| 2560B599A35 |   | PROTECTIVE BREATHING EQUIPMENT - FLIGHT DECK - B/E AEROSPACE - BFE/SPE                                                                                |   | [***] |
| 2560C635A43 |   | MP - EMERGENCY EQUIPMENT - REVISION - FLIGHT DECK - LIFE VESTS - HOOVER IN LIEU OF SWITLIK - SPE                                                      |   | [***] |
| 2562A115D57 |   | EMERGENCY LOCATOR TRANSMITTER (RESCU 406) - INSTALLATION - BFE/SPE                                                                                    |   | [***] |
| 2564-000215 |   | CONVERSION OPTION - FIRST AID KIT - UPS - BFE/SPE                                                                                                     |   | [***] |
| 2610-000025 |   | KIDDE FIRE DETECTION SYSTEM  -  GE CF6-80C2 ENGINES AND APU                                                                       |   | [***] |
| 2618-000009 |   | SINGLE LOOP DUCT LEAK DETECTION SYSTEM - 3 ZONE                                                                                                       |   | [***] |
| 2622-000002 |   | FIRE BOTTLE COMMONALITY  -  CF6-80C2 ENGINES AND APU                                                                              |   | [***] |
| 2732-000001 |   | STALL WARNING COMPUTER SPEED TAPE ACTIVATION - INHIBIT DISPLAY OF MINIMUM MANEUVER SPEED ON TAKEOFF                                                   |   | [***] |
| 2844-000005 |   | FUEL MEASURING STICKS IN KILOGRAMS WITH CONVERSION TABLES IN KILOGRAMS                                                                                |   | [***] |
| 2911-000003 |   | AC MOTOR-DRIVEN HYDRAULIC PUMPS  -  VICKERS (P/N S270T201-7)                                                                      |   | [***] |
| 2911-000038 |   | ENGINE-DRIVEN HYDRAULIC PUMPS   -  VICKERS INC.   (60B00200-12)                                               |   | [***] |
| 3042-000003 |   | WINDSHIELD WIPERS - TWO SPEED - SINGLE SWITCH                                                                                                         |   | [***] |
| 3080-000006 |   | MANUAL ANTI-ICING SYSTEM - NO ICE DETECTION                                                                                                           |   | [***] |
| 3120-000011 |   | ELECTRONIC CLOCKS - WITHOUT TENTHS OF MINUTE DISPLAY - MAIN INSTRUMENT PANEL                                                                          |   | [***] |
| 3131-000143 |   | ACCELEROMETER  -  Honeywell  P/N 971-4193-001  -  BFE/SPE                                           |   | [***] |
| 3131-000187 |   | DIGITAL FLIGHT DATA RECORDER - ALLIEDSIGNAL - 256 WORDS PER SECOND MAXIMUM DATA RATE - P/N 980-4700-042 BFE/SPE                                       |   | [***] |
| 3131-000435 |   | INTEGRATED DISPLAY UNIT (IDU) INSTALLATION - BFE/SPE - TELEDYNE P/N 2229346-7                                                                         |   | [***] |
| 3131A218A57 |   | DIGITAL FLIGHT DATA ACQUISITION UNIT (DFDAU) WITH ACMS CAPABILITY AND INTERGRATED PCMCIA MEDIA INTERFACE-TELEDYNE CONTROLS-P/N 2233000-816-1 -BFE/SPE |   | [***] |
| 3131B800C90 |   | DIGITAL FLIGHT DATA ACQUISITION UNIT (DFDAU) WITH ACMS CAPABILITY AND INTERGRATED PCMCIA MEDIA INTERFACE-TELEDYNE CONTROLS-P/N 2233000-816-1 -BFE/SPE |   | [***] |
| 3131B800D34 |   | MP - FLIGHT DATA RECORDER SYSTEM - REPLACEMENT - DIGITAL FLIGHT DATA ACQUISITION UNIT (DFDAU) - TELEDYNE CONTROLS - SPE                               |   | [***] |
| 3132-000105 |   | PORTABLE DATA LOADER/RECORDER CONNECTOR IN FLIGHT DECK - ARINC 615 - SFE                                                                              |   | [***] |
| 3132-000117 |   | DATA LOADER SELECTOR SWITCH MODULE - 20 POSITION 3 WAY - SFE                                                                                          |   | [***] |

----

| 3132B800D35 |   | MP - DATA AND RECORDER SYSTEMS - REVISION - ARINC 615 DATA LOADER IN ADDITION TO PORTABLE DATA LOADER CONNECTOR - SPE                                    |   | [***] |
|-------------|--------|----------------------------------------------------------------------------------------------------------------------------------------------------------|--------|-------|
| 3133-000057 |   | FULL FORMAT PRINTER - MILTOPE - ARINC 744 - P/N 706300-212 - BFE/SPE                                                                                     |   | [***] |
| 3133-000126 |   | ARINC 744 PRINTER PROVISIONS IN AN AISLESTAND EXTENSION IN THE 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                                                                                                               |   | [***] |
| 3161-000135 |   | HYDRAULIC PRESSURE ON EICAS STATUS PAGES                                                                                                                 |   | [***] |
| 3161-000137 |   | APU RPM ON EICAS STATUS PAGES                                                                                                                            |   | [***] |
| 3161-000139 |   | APU OIL QUANTITY LEVEL ON EICAS                                                                                                                          |   | [***] |
| 3161-000141 |   | ADDITIONAL ENVIRONMENTAL CONTROL SYSTEM (ECS) PARAMETERS - DISPLAY ON EICAS MAINTENANCE PAGE                                                             |   | [***] |
| 3161-000144 |   | GENERATOR OFF AND ENGINE OIL PRESSURE - EICAS ADVISORY LEVEL MESSAGES                                                                                    |   | [***] |
| 3161-000147 |   | ECS PRECOOLER OUTLET TEMPERATURE - (PW AND GE ENGINES) - DISPLAY ON EICAS                                                                                |   | [***] |
| 3161-000152 |   | BULK CARGO COMPARTMENT TEMPERATURE - DISPLAY ON EICAS                                                                                                    |   | [***] |
| 3161-000154 |   | RAM AIR OUTLET DOOR POSITION - DISPLAY ON EICAS                                                                                                          |   | [***] |
| 3161-000189 |   | ENGINE FUEL FLOW - FULL TIME DISPLAY - LOWER EICAS DISPLAY                                                                                               |   | [***] |
| 3162-000016 |   | FLIGHT MODE ANNUNCIATION AT TOP OF ADI                                                                                                                   |   | [***] |
| 3162-000021 |   | AIRSPEED TAPE - ROLLING DIGITS AND TREND VECTOR - ADI                                                                                                    |   | [***] |
| 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                                                                                                                     |   | [***] |
| 3162-000034 |   | RADIO ALTITUDE HEIGHT ALERT DISPLAY - 2500 FEET - ADI                                                                                                    |   | [***] |
| 3162-000054 |   | ILS DEVIATION WARNING - ADI                                                                                                                              |   | [***] |
| 3162-000059 |   | MAP MODE ORIENTATION - TRACK UP - NAVIGATION DISPLAY                                                                                                     |   | [***] |
| 3162-000066 |   | TRUE AIRSPEED AND GROUND SPEED - NAVIGATION DISPLAY                                                                                                      |   | [***] |
| 3162-000070 |   | WIND BEARING DIGITAL DISPLAY - NAVIGATION DISPLAY                                                                                                        |   | [***] |
| 3221-000011 |   | TORQUE ARM QUICK DISCONNECT  -  NOSE LANDING GEAR                                                                                    |   | [***] |
| 3242A114B69 |   | ANTISKID/AUTOBRAKE CONTROL UNIT (AACU) P/N 42-767-2 (S283T001-27)  - INSTALLATION                                                              |   | [***] |
| 3244-000022 |   | PARKING BRAKE REPEATER LIGHT - SINGLE LIGHT - NOSE LANDING GEAR AREA - LIGHT VISIBLE TO GROUND CREW                                                      |   | [***] |
| 3245-000230 |   | WHEELS AND TIRES - NOSE LANDING GEAR - WHEELS - ALLIEDSIGNAL - INSTALLATION WITH SFE 24 PR, 235 MPH TIRES                                                |   | [***] |
| 3245A298A12 |   | BRAKES - CARBON - MESSIER-BUGATTI                                                                                                                        |   | [***] |
| 3245A438A27 |   | OPERATIONAL TIRE SPEED LIMITS - 235MPH                                                                                                                   |   | [***] |
| 3245A438A28 |   | WHEELS AND TIRES - MAIN LANDING GEAR - HIGH GROSS WEIGHT WHEELS - MESSIER-BUGATTI - INSTALLATION WITH SFE 32 PR, 235 MPH TIRES.                          |   | [***] |
| 3246-000005 |   | BRAKE TEMPERATURE MONITORING SYSTEM                                                                                                                      |   | [***] |
| 3342-000009 |   | TAXI LIGHTS  -  NOSE GEAR MOUNTED  -  SPACE PROVISIONS                                                           |   | [***] |
| 3413-000027 |   | MACH/AIRSPEED INDICATOR - TWO KNOT GRADUATIONS BELOW 250 KNOTS                                                                                           |   | [***] |
| 3421-000042 |   | FAA MACH/AIRSPEED LIMITS AND OVERSPEED ALERTING                                                                                                          |   | [***] |
| 3423-000006 |   | STANDBY MAGNETIC COMPASS COMPENSATION FOR ELECTRICAL CIRCUITS (+/- 5 DEGREES)                                                                            |   | [***] |
| 3430-000187 |   | ILS/GPS MULTI-MODE RECEIVER (MMR) - ROCKWELL - P/N 822-1152-002 - BFE/SPE                                                                                |   | [***] |

----

| 3433-000032 |   | RADIO ALTIMETER (RA)  -  ROCKWELL INTERNATIONAL CORP  -  P/N 822-0334-002  -  BFE/SPE                      |   | [***] |
|-------------|--------|------------------------------------------------------------------------------------------------------------------------------------------------------------------------|--------|-------|
| 3443-000050 |   | DUAL WEATHER RADAR CONTROL PANEL - ROCKWELL P/N 622-5130-114 - BFE/SPE                                                                                                 |   | [***] |
| 3443A065A34 |   | DUAL WEATHER RADAR SYSTEM - WITH PREDICTIVE WINDSHEAR - ROCKWELL TRANSCEIVER P/N 622-5132-633 - BFE/SPE                                                                |   | [***] |
| 3443A141A90 |   | WEATHER RADAR INDICATOR ON FORWARD ELECTRONICS PANEL - ROCKWELL COLLINS - BFE/SPE                                                                                      |   | [***] |
| 3445A065A86 |   | TCAS SYSTEM - ROCKWELL COLLINS TCAS COMPUTER P/N 822-1293-002 - TCAS CHANGE 7 COMPLIANT - BFE/SPE                                                                      |   | [***] |
| 3446-000045 |   | STANDARD VOLUME FOR ALTITUDE CALLOUTS                                                                                                                                  |   | [***] |
| 3446-000048 |   | ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) - BANK ANGLE CALLOUT ENABLE                                                                                           |   | [***] |
| 3446-000050 |   | 500 SMART CALLOUT                                                                                                                                                      |   | [***] |
| 3446-000088 |   | GROUND PROXIMITY WARNING SYSTEM ALTITUDE CALLOUTS - 2500, 1000, 50, 40, 30, 20, 10, APPROACHING DECISION HEIGHT, MINIMUMS                                              |   | [***] |
| 3446B800A01 |   | MP - GROUND PROXIMTY WARNING SYSTEM (GPWS) - REVISION - 500 SMART CALL OUT - INHIBITED IN LIEU OF ENABLED                                                              |   | [***] |
| 3446C351C29 |   | MP - ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) - ACTIVATION - PEAKS AND OBSTACLES FEATURE                                                                       |   | [***] |
| 3451-000022 |   | VOR/MARKER BEACON - ROCKWELL RECEIVER P/N 822-0297-001 - BFE/SPE                                                                                                       |   | [***] |
| 3453B866A16 |   | ATC SYSTEM - ROCKWELL COLLINS ATC TRANSPONDER P/N 822-1338-003 - ELS/EHS/ES AND TCAS CHANGE 7 COMPLIANT - GABLES CONTROL PANEL P/N G6992-12 - BFE/SPE                  |   | [***] |
| 3455-000019 |   | DISTANCE MEASURING EQUIPMENT (DME) - ROCKWELL INTERROGATOR P/N 822-0329-001 - BFE/SPE                                                                                  |   | [***] |
| 3457-000212 |   | AUTOMATIC DIRECTION FINDER (ADF) - DUAL SYSTEM -  ROCKWELL ADF-900 SERIES - ADF RECEIVER P/N 822-0299-001;  ADF ANTENNA P/N 822-5404-001 - BFE/SPE |   | [***] |
| 3457-000219 |   | AUTOMATIC DIRECTION FINDER (ADF) - DUAL SYSTEM - ROCKWELL ADF-900/700 SERIES - ADF RECEIVER P/N 822-0299-001 - ADF ANTENNA P/N 622-5404-003 - BFE/SPE                  |   | [***] |
| 3457-000289 |   | DUAL ADF CONTROL PANEL - BOEING - 285T0557-2 - WITHOUT BFO OR TONE SWITCH - SFE                                                                                        |   | [***] |
| 3461A114D05 |   | MP - FLIGHT MANAGEMENT COMPUTING SYSTEM (FMCS) - REVISION - RUNWAY DISTANCE AND OFFSET POSITION SHIFT IN UNITS OF FEET                                                 |   | [***] |
| 3461A138D87 |   | FMCS-INSTALL-ACC DL-FANS FEATUREACTIVATION                                                                                                                             |   | [***] |
| 3461A138D88 |   | FMCS-INSTALL-PRINTER INTERFACE FANSFEATURE ACTIVATION                                                                                                                  |   | [***] |
| 3461A425A03 |   | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - OFFPATH DESCENT CIRCLES AND DISTANCE MEASURING EQUIPMENT RANGE RINGS DISPLAYED                                              |   | [***] |
| 3461A425A04 |   | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - SCANNING DME OPERATIONS - ENABLE                                                                                            |   | [***] |
| 3461A425A06 |   | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - RUNWAY DISTANCE AND OFFSET POSITION SHIFT IN UNITS OF METERS                                                                |   | [***] |
| 3461A425A10 |   | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - NAVIGATION DATABASE - CUSTOMER SUPPLIED                                                                                     |   | [***] |
| 3461B053A05 |   | FLT MGMT CPU SYS (FMCS) REV AIR TRAFFIC SERV DATA LINK                                                                                                                 |   | [***] |
| 3461C351C30 |   | MP - FLIGHT MANAGEMENT COMPUTING SYSTEM (FMCS) - REVISION - TAKEOFF DATA LINK - ENABLE IN LIEU OF INHIBIT                                                              |   | [***] |

----

| 3461C351C31  |         | MP - FLIGHT MANAGEMENT COMPUTING SYSTEM (FMCS) - INSTALLATION - AIRLINE MODIFIABLE INFORMATION (AMI) - CUSTOMER SUPPLIED          |         | [***] |
|--------------|--------------|-----------------------------------------------------------------------------------------------------------------------------------|--------------|-------|
| 3511B899B43  |         | CREW OXYGEN MASKS - DILUTER DEMAND REGULATORS  WITH SEPARATE SMOKE GOGGLES - CAPTAIN AND FIRST OFFICER - EROS - BFE/SPE |         | [***] |
| 3511B899B44  |         | CREW OXYGEN MASKS - DILUTER DEMAND TYPE REGULATORS WITH SEPARATE SMOKE GOGGLES - FIRST OBSERVER - EROS - BFE/SPE                  |         | [***] |
| 3611-000006  |         | ALLIEDSIGNAL INC.  -  INTERMEDIATE PRESSURE (IP) CHECK VALVES - GE\P&W ENGINES                            |         | [***] |
| 4970-000045  |         | APU HOURMETER  - FLIGHT DECK                                                                                            |         | [***] |
| 7200-000382  |         | STANDARD FAN SPINNER - GE ENGINES                                                                                                 |         | [***] |
| 7200-000412  |         | GE PROPULSION SYSTEM                                                                                                              |         | [***] |
| 7200-000459  |         | GENERAL ELECTRIC ENGINES - CF6-80C2-B6F - B6F RATING - WITH FADEC                                                                 |         | [***] |
| 7200A114C90  |         | ENG REPLACE GE ENG CF6-80C2-B6FSTAGE 1 HTP COATED BLADES                                                                          |         | [***] |
| 7830-000012  |         | MANUAL OPENING OF THRUST REVERSER ASSEMBLIES - GE CF6-80C2 ENGINES                                                                |         | [***] |
| 7900-000117  |         | LUBRICATING OIL - BP TURBO OIL 2380                                                                                               |         | [***] |
| 8011-000006  |         | HAMILTON STANDARD STARTERS AND STARTER VALVES  -  GE ENGINES                                                  |         | [***] |
| MISC FO      |         | FOLLOW ON EXH A VR259                                                                                                             |         | [***] |
| MISC/FAA4    |         | FLAME PROPAGATION - INSULATION BLANKETS                                                                                           |         | [***] |
|         |         |                                                                                                                              |         | [***] |
| OPTIONS: 171 |    | TOTAL:                                                                                                                            |    | [***] |

----

----

----

| 0110-000035 |   | MAJOR MODEL 767 AIRPLANE                                                                           |   | [***] |
|-------------|--------|----------------------------------------------------------------------------------------------------|--------|-------|
| 0110-000038 |   | MINOR MODEL 767-300F FREIGHTER AIRPLANE                                                            |   | [***] |
| 0110-000094 |   | MODEL 767-300 GENERAL MARKET FREIGHTER AIRPLANE                                                    |   | [***] |
| 0220-000040 |   | FAA TYPE CERTIFICATION                                                                             |   | [***] |
| 0220-000136 |   | 15 KNOT MAXIMUM TAKEOFF AND LANDING TAILWIND COMPONENT CERTIFICATION                               |   | [***] |
| 0221-000002 |   | DISPATCH WITH GEAR EXTENDED FOR REVENUE FLIGHT                                                     |   | [***] |
| 0221A251A19 |   | ENGINE INOPERATIVE TEN-MINUTE TAKEOFF THRUST OPERATION - CF6-80C2B6F THRUST RATING                 |   | [***] |
| 0228-000032 |   | OPERATIONS MANUAL IN FAA FORMAT                                                                    |   | [***] |
| 0229A141A41 |   | PERFORMANCE - CERTIFICATION FOR OPERATION AT AIRPORT ALTITUDES OF 9500 FEET AND BELOW              |   | [***] |
| 0252-000014 |   | ENVIRONMENTAL CONTROL SYSTEM  -  TEMPERATURE INDICATIONS IN DEGREES CELSIUS    |   | [***] |
| 0252-000017 |   | INSTRUMENTATION WITH METRIC UNITS  -  MODEL 767                                |   | [***] |
| 0351A114C45 |   | TAKEOFF PERFORMANCE IMPROVEMENT - ALTERNATE FORWARD CENTER OF GRAVITY LIMITS                       |   | [***] |
| 0360B604F64 |   | MISCELLANEOUS WEIGHT COLLECTOR                                                                     |   | [***] |
| 1110B657K77 |   | MP - EXTERIOR COLOR SCHEME AND MARKINGS - REVISION - LAN 767-316F                                  |   | [***] |
| 1110B657P08 |   | MP - EXTERIOR COLOR SCHEME AND MARKINGS - REVISION - LAN 767-316F                                  |   | [***] |
| 1110C262A21 |   | EXTERIOR COLOR SCHEME AND MARKINGS - LAN 767-316F                                                  |   | [***] |
| 1130-000344 |   | BOEING STANDARD MARKINGS - MAIN DECK CARGO COMPARTMENT                                             |   | [***] |
| 1130A931A06 |   | IATA STANDARD MARKINGS - LOWER LOBE CARGO COMPARTMENT                                              |   | [***] |
| 2145-000004 |   | BULK CARGO AREA HEATING AND VENTILATING FOR ANIMAL CARRIAGE                                        |   | [***] |
| 2210-000030 |   | AUTOFLIGHT - THREE DIGIT MACH NUMBER ON MODE CONTROL PANEL                                         |   | [***] |
| 2210-000031 |   | AUTOFLIGHT - AUTOMATIC AUTOPILOT CHANNEL SELECTION IN APPROACH MODE                                |   | [***] |
| 2210-000037 |   | AUTOFLIGHT - BANK ANGLE HOLD AT AUTOPILOT COMMAND ENGAGE                                           |   | [***] |
| 2210-000039 |   | AUTOFLIGHT - FULL TIME FLIGHT DIRECTOR                                                             |   | [***] |
| 2210-000151 |   | AUTOFLIGHT - ENABLE GLIDE SLOPE CAPTURE PRIOR TO LOCALIZER CAPTURE                                 |   | [***] |
| 2210-000311 |   | AUTOFLIGHT - FLIGHT CONTROL COMPUTER (FCC) WITHOUT ONBOARD SOFTWARE LOADING CAPABILITY             |   | [***] |
| 2210A064A02 |   | AUTOFLIGHT - ALTITUDE ALERT - 300/900 FEET                                                         |   | [***] |
| 2210A811A40 |   | AUTOFLIGHT-REV-INHIBIT ILO ENABLE                                                                  |   | [***] |
| 2210B403A07 |   | MODE CONTROL PANEL WITH BACKCOURSE SWITCH                                                          |   | [***] |
| 2230-000127 |   | AUTOTHROTTLE - SELECTION OF CLIMB DERATES                                                          |   | [***] |
| 2230-000133 |   | AUTOTHROTTLE - FIXED PERCENTAGE DERATE LEVELS OF 10% AND 20%                                       |   | [***] |
| 2230-000135 |   | AUTOTHROTTLE - CLIMB DERATE WASHOUT SCHEDULE - 10,000 TO 12,000 FEET                               |   | [***] |
| 2311-000122 |   | HF COMMUNICATIONS - DUAL GABLES HF CONTROL PANEL WITH SENSITIVITY CONTROL - P/N G7401-03 - BFE/SPE |   | [***] |

----

| 2311A213A84 |   | HF COMMUNICATIONS - DUAL ROCKWELL HF TRANSCEIVERS - P/N 822-0330-001 AND DIGITAL HF COUPLERS - P/N 822-0987-003 - BFE/SPE                                                  |   | [***] |
|-------------|--------|----------------------------------------------------------------------------------------------------------------------------------------------------------------------------|--------|-------|
| 2311B800D30 |   | MP - HIGH FREQUENCY (HF) COMMUNCIATIONS - ACTIVATION - DUAL ARINC 753 DATA LINK                                                                                            |   | [***] |
| 2311B800D40 |   | MP - HF COMMUNICATIONS - REPLACEMENT - DUAL GABLES HF CONTROL PANELS - P/N G7401-16 IN LIEU OF P/N G7401-03 - SPE                                                          |   | [***] |
| 2311B800D41 |   | MP - HF COMMUNICATIONS - REPLACEMENT - DUAL ROCKWELL HF TRANSCEIVERS AND COUPLERS - 822-0990-004 AND 822-0987-004 IN LIEU OF 822-0330-001 AND 822-0987-003 - SPE           |   | [***] |
| 2311C351C28 |   | MP - HF COMMUNICATIONS - REVISIONS - PARTIAL PROVISIONS FOR DUAL ARINC 753 HF DATALINK                                                                                     |   | [***] |
| 2312-000432 |   | VHF COMMUNICATIONS - TRIPLE GABLES VHF TUNING PANELS (DUAL KNOB) - P/N G7400-27 - BFE/SPE                                                                                  |   | [***] |
| 2312-000703 |   | VHF COMMUNICATIONS - ACTIVATION OF 8.33 KHZ CHANNEL SPACING                                                                                                                |   | [***] |
| 2312-000786 |   | VHF COMMUNICATIONS - TRIPLE ROCKWELL ARINC 716/750 VHF-900B FM IMMUNE TRANSCEIVERS WITH 8.33 KHZ CHANNEL SPACING AND CMC INTERFACE CAPABILITY - P/N 822-1047-003 - BFE/SPE |   | [***] |
| 2312B800D42 |   | MP - VHF COMMUNICATIONS SYSTESM - REPLACEMENT - GABLES CONTROL PLANEL - G7400-227 IN LIEU OF G7400-27 - SPE                                                                |   | [***] |
| 2312B800D44 |   | MP - VHF COMMUNICATIONS - REPLACEMENT - ROCKWELL VHF TRANSCEIVERS - 822-1250-002 IN LIEU OF 822-1047-003 - SPE                                                             |   | [***] |
| 2315A213A67 |   | SATCOM - PARTIAL PROVISIONS FOR SATCOM SYSTEM AND TOP MOUNTED HIGH GAIN ANTENNA SYSTEM - MODEL 767                                                                         |   | [***] |
| 2315B800C72 |   | SATCOM - HF/SATCOM SELECT PANEL - INSTALLATION - FLIGHT DECK                                                                                                               |   | [***] |
| 2321B401A04 |   | SELCAL - AVTECH FIVE CHANNEL DECODER - P/N NA138-714C  - BFE/SPE                                                                                                 |   | [***] |
| 2322-000250 |   | ACARS - PARTIAL PROVISIONS FOR SINGLE ARINC 724B ACARS                                                                                                                     |   | [***] |
| 2322B800D45 |   | MP - ACARS - REVISION - ROCKWELL COLLINS ARINC 758 CMU (LEVEL AOA/VDL MODE 2 OPERATION) - SPE                                                                              |   | [***] |
| 2322B800D46 |   | MP - ACARS - INSTALLATION - ROCKWELL MULTIPURPOSE INTERACTIVE DISPLAY UNIT (MIDU) IN LIEU OF TELEDYNE INTERACTIVE DISPLAY UNIT (IDU) - SPE                                 |   | [***] |
| 2324B800D31 |   | MP - EMERGENCY LOCATOR TRANSMITTER (ELT) - ELTA 3-FREQUENCY AUTOMATIC - FIXED - P/N 95N6088 - SPE                                                                          |   | [***] |
| 2340B800C73 |   | CREW COMMUNICATION - PILOTS' CALL PANEL - SELCAL AND CARGO LOADING/GROUND CALL - 767 FREIGHTER                                                                             |   | [***] |
| 2350B800C71 |   | AUDIO INTEGRATING - AUDIO SELECTOR PANELS - FLIGHT DECK                                                                                                                    |   | [***] |
| 2351-000042 |   | CONTROL WHEEL PUSH TO TALK (PTT) SWITCH - STANDARD THREE POSITION                                                                                                          |   | [***] |
| 2351A138C64 |   | HAND HELD MICROPHONE - CAPTAIN, FIRST OFFICER AND FIRST OBSERVER -TELEPHONICS - P/N 107C800-22 - BFE/SPE                                                                   |   | [***] |
| 2351A213A33 |   | AUDIO INTEGRATION - INSTALLATION - TWO-PLUG AUDIO JACKS IN THE FLIGHT DECK                                                                                                 |   | [***] |
| 2351A213B77 |   | BOOM MICROPHONE HEADSETS - CAPTAIN AND FIRST OFFICER - TELEX AIRMAN 750 - P/N 64300-200 - BFE/SPE                                                                          |   | [***] |
| 2351A213B80 |   | HEADPHONE - FIRST OBSERVER - TELEX - P/N 64400-200 - BFE/SPE                                                                                                               |   | [***] |
| 2371-000009 |   | NO MONITOR JACK IN THE WHEEL WELL                                                                                                                                          |   | [***] |

----

| 2371-000017 |   | SOLID STATE VOICE RECORDER ED56A AND SOLID STATE MICROPHONE/MONITOR ED56A - ALLIEDSIGNAL - 2 HOUR RECORDING TIME - P/N 980-6022-001 AND P/N 980-6116-002 - BFE/SPE |   | [***] |
|-------------|--------|--------------------------------------------------------------------------------------------------------------------------------------------------------------------|--------|-------|
| 2433-000021 |   | STANDBY POWER - EXTENDED TIME CAPABILITY - BATTERY PARALELLING                                                                                                     |   | [***] |
| 2511-000022 |   | MANUALLY OPERATED SEATS  -  CAPTAIN AND FIRST OFFICER                                                                                          |   | [***] |
| 2513-000405 |   | SUNVISOR INSTALLATION - NUMBER 1 AND 2 WINDOWS - FLIGHT DECK - SFE                                                                                                 |   | [***] |
| 2527-000732 |   | CONVERSION OPTION - GALLEY/ENTRY AND LAVATORY MAT INSTALLATION - TARAFLEX - 767 FREIGHTER                                                                          |   | [***] |
| 2530B604F65 |   | GALLEY INSERT PART NUMBERS - BFE/SPE                                                                                                                               |   | [***] |
| 2550-000157 |   | DELIVERY CONFIGURATION - MAIN DECK - TRANSVERSE TYPE A (88" X 125 ") PALLETS                                                                                       |   | [***] |
| 2550-000162 |   | ALTERNATE CARGO COMPARTMENT ARRANGEMENT - MAIN DECK - SIDE BY SIDE CONTOURED 88" X 125" TYPE A PALLETS                                                             |   | [***] |
| 2550-000261 |   | CONVERSION OPTION - FIRST PALLET POSITION FOR ACCESS TO LIVE ANIMAL CARRIAGE OR HAZARDOUS MATERIAL CARRIAGE - 767 FREIGHTER                                        |   | [***] |
| 2550-000263 |   | CONVERSION OPTION - ALTERNATE CARGO COMPARTMENT ARRANGEMENT - MAIN DECK - ADDITIONAL 96" X 196" PALLETS - FREIGHTER                                                |   | [***] |
| 2553-000044 |   | HARDWARE FOR CARRIAGE OF 88 X 125 AND 96 X 125 INCH PALLETS AND STANDARD CONTAINERS IN THE FORWARD CARGO COMPARTMENT                                               |   | [***] |
| 2555-000053 |   | CONVERSION OPTION - INSTALLATION OF ADDITIONAL NET AFT OF THE AFT CARGO DOOR                                                                                       |   | [***] |
| 2560-000177 |   | HALON FIRE EXTINGUISHER - FLIGHT DECK - WALTER KIDDE                                                                                                               |   | [***] |
| 2560A141A86 |   | CREW LIFE VESTS - FLIGHT DECK - SWITLIK - P/N S-31850-6300-AAR001 - BFE/SPE                                                                                        |   | [***] |
| 2560B599A35 |   | PROTECTIVE BREATHING EQUIPMENT - FLIGHT DECK - B/E AEROSPACE - BFE/SPE                                                                                             |   | [***] |
| 2560C635A43 |   | MP - EMERGENCY EQUIPMENT - REVISION - FLIGHT DECK - LIFE VESTS - HOOVER IN LIEU OF SWITLIK - SPE                                                                   |   | [***] |
| 2562A115D57 |   | EMERGENCY LOCATOR TRANSMITTER (RESCU 406) - INSTALLATION - BFE/SPE                                                                                                 |   | [***] |
| 2564-000215 |   | CONVERSION OPTION - FIRST AID KIT - UPS - BFE/SPE                                                                                                                  |   | [***] |
| 2610-000025 |   | KIDDE FIRE DETECTION SYSTEM  -  GE CF6-80C2 ENGINES AND APU                                                                                    |   | [***] |
| 2618-000009 |   | SINGLE LOOP DUCT LEAK DETECTION SYSTEM - 3 ZONE                                                                                                                    |   | [***] |
| 2622-000002 |   | FIRE BOTTLE COMMONALITY  -  CF6-80C2 ENGINES AND APU                                                                                           |   | [***] |
| 2732-000001 |   | STALL WARNING COMPUTER SPEED TAPE ACTIVATION - INHIBIT DISPLAY OF MINIMUM MANEUVER SPEED ON TAKEOFF                                                                |   | [***] |
| 2844-000005 |   | FUEL MEASURING STICKS IN KILOGRAMS WITH CONVERSION TABLES IN KILOGRAMS                                                                                             |   | [***] |
| 2911-000003 |   | AC MOTOR-DRIVEN HYDRAULIC PUMPS  -  VICKERS (P/N S270T201-7)                                                                                   |   | [***] |
| 2911-000038 |   | ENGINE-DRIVEN HYDRAULIC PUMPS   -  VICKERS INC.   (60B00200-12)                                                            |   | [***] |
| 3042-000003 |   | WINDSHIELD WIPERS - TWO SPEED - SINGLE SWITCH                                                                                                                      |   | [***] |
| 3080-000006 |   | MANUAL ANTI-ICING SYSTEM - NO ICE DETECTION                                                                                                                        |   | [***] |

----

| 3120-000011 |   | ELECTRONIC CLOCKS - WITHOUT TENTHS OF MINUTE DISPLAY - MAIN INSTRUMENT PANEL                                                                             |   | [***] |
|-------------|--------|----------------------------------------------------------------------------------------------------------------------------------------------------------|--------|-------|
| 3131-000143 |   | ACCELEROMETER  -  Honeywell  P/N 971-4193-001  -  BFE/SPE                                              |   | [***] |
| 3131-000187 |   | DIGITAL FLIGHT DATA RECORDER - ALLIEDSIGNAL - 256 WORDS PER SECOND MAXIMUM DATA RATE - P/N 980-4700-042 BFE/SPE                                          |   | [***] |
| 3131-000435 |   | INTEGRATED DISPLAY UNIT (IDU) INSTALLATION - BFE/SPE - TELEDYNE P/N 2229346-7                                                                            |   | [***] |
| 3131A218A57 |   | DIGITAL FLIGHT DATA ACQUISITION UNIT (DFDAU) WITH ACMS CAPABILITY AND INTERGRATED PCMCIA MEDIA INTERFACE-TELEDYNE CONTROLS-P/N 2233000-816-1 -BFE/SPE    |   | [***] |
| 3131B800C90 |   | DIGITAL FLIGHT DATA ACQUISITION UNIT (DFDAU) WITH ACMS CAPABILITY AND INTERGRATED PCMCIA MEDIA INTERFACE-TELEDYNE CONTROLS-P/N 2233000-816-1 -BFE/SPE    |   | [***] |
| 3131B800D34 |   | MP - FLIGHT DATA RECORDER SYSTEM - REPLACEMENT - DIGITAL FLIGHT DATA ACQUISITION UNIT (DFDAU) - TELEDYNE CONTROLS - SPE                                  |   | [***] |
| 3132-000105 |   | PORTABLE DATA LOADER/RECORDER CONNECTOR IN FLIGHT DECK - ARINC 615 - SFE                                                                                 |   | [***] |
| 3132-000117 |   | DATA LOADER SELECTOR SWITCH MODULE - 20 POSITION 3 WAY - SFE                                                                                             |   | [***] |
| 3132B800D35 |   | MP - DATA AND RECORDER SYSTEMS - REVISION - ARINC 615 DATA LOADER IN ADDITION TO PORTABLE DATA LOADER CONNECTOR - SPE                                    |   | [***] |
| 3133-000057 |   | FULL FORMAT PRINTER - MILTOPE - ARINC 744 - P/N 706300-212 - BFE/SPE                                                                                     |   | [***] |
| 3133-000126 |   | ARINC 744 PRINTER PROVISIONS IN AN AISLESTAND EXTENSION IN THE 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                                                                                                               |   | [***] |
| 3161-000135 |   | HYDRAULIC PRESSURE ON EICAS STATUS PAGES                                                                                                                 |   | [***] |
| 3161-000137 |   | APU RPM ON EICAS STATUS PAGES                                                                                                                            |   | [***] |
| 3161-000139 |   | APU OIL QUANTITY LEVEL ON EICAS                                                                                                                          |   | [***] |
| 3161-000141 |   | ADDITIONAL ENVIRONMENTAL CONTROL SYSTEM (ECS) PARAMETERS - DISPLAY ON EICAS MAINTENANCE PAGE                                                             |   | [***] |
| 3161-000144 |   | GENERATOR OFF AND ENGINE OIL PRESSURE - EICAS ADVISORY LEVEL MESSAGES                                                                                    |   | [***] |
| 3161-000147 |   | ECS PRECOOLER OUTLET TEMPERATURE - (PW AND GE ENGINES) - DISPLAY ON EICAS                                                                                |   | [***] |
| 3161-000152 |   | BULK CARGO COMPARTMENT TEMPERATURE - DISPLAY ON EICAS                                                                                                    |   | [***] |
| 3161-000154 |   | RAM AIR OUTLET DOOR POSITION - DISPLAY ON EICAS                                                                                                          |   | [***] |
| 3161-000189 |   | ENGINE FUEL FLOW - FULL TIME DISPLAY - LOWER EICAS DISPLAY                                                                                               |   | [***] |
| 3162-000016 |   | FLIGHT MODE ANNUNCIATION AT TOP OF ADI                                                                                                                   |   | [***] |
| 3162-000021 |   | AIRSPEED TAPE - ROLLING DIGITS AND TREND VECTOR - ADI                                                                                                    |   | [***] |
| 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                                                                                                                     |   | [***] |
| 3162-000034 |   | RADIO ALTITUDE HEIGHT ALERT DISPLAY - 2500 FEET - ADI                                                                                                    |   | [***] |

----

| 3162-000054 |   | ILS DEVIATION WARNING - ADI                                                                                                                           |   | [***] |
|-------------|--------|-------------------------------------------------------------------------------------------------------------------------------------------------------|--------|-------|
| 3162-000059 |   | MAP MODE ORIENTATION - TRACK UP - NAVIGATION DISPLAY                                                                                                  |   | [***] |
| 3162-000066 |   | TRUE AIRSPEED AND GROUND SPEED - NAVIGATION DISPLAY                                                                                                   |   | [***] |
| 3162-000070 |   | WIND BEARING DIGITAL DISPLAY - NAVIGATION DISPLAY                                                                                                     |   | [***] |
| 3221-000011 |   | TORQUE ARM QUICK DISCONNECT  -  NOSE LANDING GEAR                                                                                 |   | [***] |
| 3242A114B69 |   | ANTISKID/AUTOBRAKE CONTROL UNIT (AACU) P/N 42-767-2 (S283T001-27)  - INSTALLATION                                                           |   | [***] |
| 3244-000022 |   | PARKING BRAKE REPEATER LIGHT - SINGLE LIGHT - NOSE LANDING GEAR AREA - LIGHT VISIBLE TO GROUND CREW                                                   |   | [***] |
| 3245-000230 |   | WHEELS AND TIRES - NOSE LANDING GEAR - WHEELS - ALLIEDSIGNAL - INSTALLATION WITH SFE 24 PR, 235 MPH TIRES                                             |   | [***] |
| 3245A298A12 |   | BRAKES - CARBON - MESSIER-BUGATTI                                                                                                                     |   | [***] |
| 3245A438A27 |   | OPERATIONAL TIRE SPEED LIMITS - 235MPH                                                                                                                |   | [***] |
| 3245A438A28 |   | WHEELS AND TIRES - MAIN LANDING GEAR - HIGH GROSS WEIGHT WHEELS - MESSIER-BUGATTI - INSTALLATION WITH SFE 32 PR, 235 MPH TIRES.                       |   | [***] |
| 3246-000005 |   | BRAKE TEMPERATURE MONITORING SYSTEM                                                                                                                   |   | [***] |
| 3342-000009 |   | TAXI LIGHTS  -  NOSE GEAR MOUNTED  -  SPACE PROVISIONS                                                        |   | [***] |
| 3413-000027 |   | MACH/AIRSPEED INDICATOR - TWO KNOT GRADUATIONS BELOW 250 KNOTS                                                                                        |   | [***] |
| 3421-000042 |   | FAA MACH/AIRSPEED LIMITS AND OVERSPEED ALERTING                                                                                                       |   | [***] |
| 3423-000006 |   | STANDBY MAGNETIC COMPASS COMPENSATION FOR ELECTRICAL CIRCUITS (+/- 5 DEGREES)                                                                         |   | [***] |
| 3430-000187 |   | ILS/GPS MULTI-MODE RECEIVER (MMR) - ROCKWELL - P/N 822-1152-002 - BFE/SPE                                                                             |   | [***] |
| 3433-000032 |   | RADIO ALTIMETER (RA)  -  ROCKWELL INTERNATIONAL CORP  -  P/N 822-0334-002  -  BFE/SPE     |   | [***] |
| 3443-000050 |   | DUAL WEATHER RADAR CONTROL PANEL - ROCKWELL P/N 622-5130-114 - BFE/SPE                                                                                |   | [***] |
| 3443A065A34 |   | DUAL WEATHER RADAR SYSTEM - WITH PREDICTIVE WINDSHEAR - ROCKWELL TRANSCEIVER P/N 622-5132-633 - BFE/SPE                                               |   | [***] |
| 3443A141A90 |   | WEATHER RADAR INDICATOR ON FORWARD ELECTRONICS PANEL - ROCKWELL COLLINS - BFE/SPE                                                                     |   | [***] |
| 3445A065A86 |   | TCAS SYSTEM - ROCKWELL COLLINS TCAS COMPUTER P/N 822-1293-002 - TCAS CHANGE 7 COMPLIANT - BFE/SPE                                                     |   | [***] |
| 3446-000045 |   | STANDARD VOLUME FOR ALTITUDE CALLOUTS                                                                                                                 |   | [***] |
| 3446-000048 |   | ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) - BANK ANGLE CALLOUT ENABLE                                                                          |   | [***] |
| 3446-000050 |   | 500 SMART CALLOUT                                                                                                                                     |   | [***] |
| 3446-000088 |   | GROUND PROXIMITY WARNING SYSTEM ALTITUDE CALLOUTS - 2500, 1000, 50, 40, 30, 20, 10, APPROACHING DECISION HEIGHT, MINIMUMS                             |   | [***] |
| 3446B800A01 |   | MP - GROUND PROXIMTY WARNING SYSTEM (GPWS) - REVISION - 500 SMART CALL OUT - INHIBITED IN LIEU OF ENABLED                                             |   | [***] |
| 3446C351C29 |   | MP - ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) - ACTIVATION - PEAKS AND OBSTACLES FEATURE                                                      |   | [***] |
| 3451-000022 |   | VOR/MARKER BEACON - ROCKWELL RECEIVER P/N 822-0297-001 - BFE/SPE                                                                                      |   | [***] |
| 3453B866A16 |   | ATC SYSTEM - ROCKWELL COLLINS ATC TRANSPONDER P/N 822-1338-003 - ELS/EHS/ES AND TCAS CHANGE 7 COMPLIANT - GABLES CONTROL PANEL P/N G6992-12 - BFE/SPE |   | [***] |

----

| 3455-000019 |   | DISTANCE MEASURING EQUIPMENT (DME) - ROCKWELL INTERROGATOR P/N 822-0329-001 - BFE/SPE                                                                                  |   | [***] |
|-------------|--------|------------------------------------------------------------------------------------------------------------------------------------------------------------------------|--------|-------|
| 3457-000212 |   | AUTOMATIC DIRECTION FINDER (ADF) - DUAL SYSTEM -  ROCKWELL ADF-900 SERIES - ADF RECEIVER P/N 822-0299-001;  ADF ANTENNA P/N 822-5404-001 - BFE/SPE |   | [***] |
| 3457-000219 |   | AUTOMATIC DIRECTION FINDER (ADF) - DUAL SYSTEM - ROCKWELL ADF-900/700 SERIES - ADF RECEIVER P/N 822-0299-001 - ADF ANTENNA P/N 622-5404-003 - BFE/SPE                  |   | [***] |
| 3457-000289 |   | DUAL ADF CONTROL PANEL - BOEING - 285T0557-2 - WITHOUT BFO OR TONE SWITCH - SFE                                                                                        |   | [***] |
| 3461A114D05 |   | MP - FLIGHT MANAGEMENT COMPUTING SYSTEM (FMCS) - REVISION - RUNWAY DISTANCE AND OFFSET POSITION SHIFT IN UNITS OF FEET                                                 |   | [***] |
| 3461A138D87 |   | FMCS-INSTALL-ACC DL-FANS FEATUREACTIVATION                                                                                                                             |   | [***] |
| 3461A138D88 |   | FMCS-INSTALL-PRINTER INTERFACE FANSFEATURE ACTIVATION                                                                                                                  |   | [***] |
| 3461A425A03 |   | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - OFFPATH DESCENT CIRCLES AND DISTANCE MEASURING EQUIPMENT RANGE RINGS DISPLAYED                                              |   | [***] |
| 3461A425A04 |   | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - SCANNING DME OPERATIONS - ENABLE                                                                                            |   | [***] |
| 3461A425A06 |   | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - RUNWAY DISTANCE AND OFFSET POSITION SHIFT IN UNITS OF METERS                                                                |   | [***] |
| 3461A425A10 |   | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - NAVIGATION DATABASE - CUSTOMER SUPPLIED                                                                                     |   | [***] |
| 3461B053A05 |   | FLT MGMT CPU SYS (FMCS) REV AIR TRAFFIC SERV DATA LINK                                                                                                                 |   | [***] |
| 3461C351C30 |   | MP - FLIGHT MANAGEMENT COMPUTING SYSTEM (FMCS) - REVISION - TAKEOFF DATA LINK - ENABLE IN LIEU OF INHIBIT                                                              |   | [***] |
| 3461C351C31 |   | MP - FLIGHT MANAGEMENT COMPUTING SYSTEM (FMCS) - INSTALLATION - AIRLINE MODIFIABLE INFORMATION (AMI) - CUSTOMER SUPPLIED                                               |   | [***] |
| 3511B899B43 |   | CREW OXYGEN MASKS - DILUTER DEMAND REGULATORS  WITH SEPARATE SMOKE GOGGLES - CAPTAIN AND FIRST OFFICER - EROS - BFE/SPE                                      |   | [***] |
| 3511B899B44 |   | CREW OXYGEN MASKS - DILUTER DEMAND TYPE REGULATORS WITH SEPARATE SMOKE GOGGLES - FIRST OBSERVER - EROS - BFE/SPE                                                       |   | [***] |
| 3611-000006 |   | ALLIEDSIGNAL INC.  -  INTERMEDIATE PRESSURE (IP) CHECK VALVES - GE\P&W ENGINES                                                                 |   | [***] |
| 4970-000045 |   | APU HOURMETER  - FLIGHT DECK                                                                                                                                 |   | [***] |
| 7200-000382 |   | STANDARD FAN SPINNER - GE ENGINES                                                                                                                                      |   | [***] |
| 7200-000412 |   | GE PROPULSION SYSTEM                                                                                                                                                   |   | [***] |
| 7200-000459 |   | GENERAL ELECTRIC ENGINES - CF6-80C2-B6F - B6F RATING - WITH FADEC                                                                                                      |   | [***] |
| 7200A114C90 |   | ENG REPLACE GE ENG CF6-80C2-B6FSTAGE 1 HTP COATED BLADES                                                                                                               |   | [***] |
| 7830-000012 |   | MANUAL OPENING OF THRUST REVERSER ASSEMBLIES - GE CF6-80C2 ENGINES                                                                                                     |   | [***] |
| 7900-000117 |   | LUBRICATING OIL - BP TURBO OIL 2380                                                                                                                                    |   | [***] |
| 8011-000006 |   | HAMILTON STANDARD STARTERS AND STARTER VALVES  -  GE ENGINES                                                                                       |   | [***] |

----

| MISC FO      |         | FOLLOW ON EXH A VR259                   |         | [***] |
|--------------|--------------|-----------------------------------------|--------------|-------|
| MISC/FAA4    |         | FLAME PROPAGATION - INSULATION BLANKETS |         | [***] |
|         |         |                                    |         | [***] |
| OPTIONS: 171 |    | TOTAL:                                  |    | [***] |

----

| Airframe Model/MTOW:                         | 767-300F    | 412000 pounds |                                       | Detail Specification:                              | D019T002LAN63F-1                      |
|----------------------------------------------|-------------|--------------------|--------------------------------------------|----------------------------------------------------|---------------------------------------|
| Engine Model/Thrust:                         | CF6-80C2B6F | 60200 pounds       |                                       | Airframe Price Base Year/Escalation Formula:  | Jul-08 ECI-MFG / CPI                  |
| Airframe Price:                              |        | ***                |                                       | Engine Price Base Year/Escalation Formula:    | Jul-08 GE CF6-80 & GE90 (99 rev.) |
| Optional Features:                           |        | ***                |                                       |                                               |                                  |   |
| Sub-Total of Airframe and Features:          | [***]       |               | Airframe Escalation Data:                  | (4Q08 Esc Fcst)                                    |
| Engine Price (Per Aircraft):                 |        | [***]              |                                       | Base Year Index (ECI):                             | 103.1                                 |
| Aircraft Basic Price (Excluding BFE/SPE):    | [***]       |               | Base Year Index (CPI):                     | 208.2                                              |
| Buyer Furnished Equipment (BFE) Estimate:    | [***]       |               | Engine Escalation Data:                    |                                               |                                  |
| Seller Purchased Equipment (SPE) Estimate:   | [***]       |               | Base Year Index (CPI):                     | 129.930                                            |
|                               |        |               |                                       |                                               |
| Initial Payment/Aircraft at Proposal Accept: | [***]       |               | Escalation is not fixed for these aircraft |                                               |

|    |         |      |         | Escalation |         | Escalation |         |          |         | [***]  |         | [***]  |         | [***]  |         | [***]  |         | [***]  |
|--------------|--------------|-----------|--------------|------------|--------------|------------|--------------|---------------|--------------|--------|--------------|--------|--------------|--------|--------------|--------|--------------|--------|
| Delivery     |         | Number of |         | Factor     |         | Factor     |         | Manufacturer  |         | [***]  |         | [***]  |         | [***]  |         | [***]  |         | [***]  |
| Date         |         | Aircraft  |         | (Airframe) |         | (Engine)   |         | Serial Number |         | [***]  |         | [***]  |         | [***]  |         | [***]  |         | [***]  |
| Oct-2011     |         | 1         |         | 1.0622     |         | 1.0900     |         | 40590         |         | [***]  |         | [***]  |         | [***]  |         | [***]  |         | [***]  |
| Nov-2011     |         | 1         |         | 1.0633     |         | 1.0930     |         | 40591         |         | [***]  |         | [***]  |         | [***]  |         | [***]  |         | [***]  |
| Total        |    | 2         |    |       |    |       |    |          |    |   |    |   |    |   |    |   |    |   |

| P. A. No. 2126 | Boeing Proprietary |   |
|----------------|--------------------|--------|
| Attachment A   |               | Page 1 |

----

----

| Very truly yours,           |
|-----------------------------|
|                        |
| THE BOEING COMPANY          |
|                        |   |
| By                          |   |
| Its                         | Attorney-In-Fact |
|                        |   |
| ACCEPTED AND AGREED TO this |
| Date: March 22, 2010        |
|                        |
| LAN AIRLINES S.A.           |
|                        |   |
| By                          |   |
|                        | Mr. Roberto Alvo |
|                        |   |
| Its                         | Sr. Vice President Strategic |
|                        | Planning & Corporate Planning |
|                        |   |
| By                          |   |
|                        | Mr. Alejandro de la Fuente |
|                        |   |
| Its                         | Chief Financial Officer |

----

| 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         |

----

| 1 | AIRCRAFT MODEL APPLICABILITY |
|---|------------------------------|

| 2 | FLIGHT PERFORMANCE |
|---|--------------------|

| 2.1 | [***] |
|-----|-------|

| 2.2 | [***] |
|-----|-------|

| 2.3 | [***] |
|-----|-------|

| 3 | MANUFACTURER'S EMPTY WEIGHT |
|---|-----------------------------|

| 4 | AIRCRAFT CONFIGURATION |
|---|------------------------|

| 4.1 | The guarantees contained in this Attachment are based on the Aircraft configuration as defined in Detail Specification D019T002LAN63F-2 (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. |
|-----|------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

| 4.2 | The Manufacturer's Empty Weight guarantee of Section 3 will be adjusted by Boeing for the following in its evidence of compliance with the guarantees: |
|-----|--------------------------------------------------------------------------------------------------------------------------------------------------------|

| 5 | GUARANTEE CONDITIONS |
|---|----------------------|

| 5.1 | All guaranteed performance data are based on the International Standard Atmosphere (ISA) and specified variations therefrom; altitudes are pressure altitudes. |
|-----|----------------------------------------------------------------------------------------------------------------------------------------------------------------|

| 5.2 | The Federal Aviation Administration (FAA) regulations referred to in this Attachment are, unless otherwise specified, the 767-300 Certification Basis regulations specified in the Type Certificate Data Sheet A1NM, Revision 23, dated May 10, 2004. |
|-----|-------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

| 5.3 | 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 5.2, 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 shall be appropriately modified to reflect any such change. |
|-----|---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

----

| 5.4 | The takeoff and landing guarantees are based on hard surface, level and dry runways with no wind or obstacles, no clearway or stopway, 225 mph tires, with Category D brakes and anti-skid operative, and with the Aircraft center of gravity at the most forward limit unless otherwise specified.  The takeoff performance is based on no engine bleed for air conditioning or thermal anti-icing and the Auxiliary Power Unit (APU) turned off unless otherwise specified.  The improved climb performance procedure will be used for takeoff as required.  The landing performance is based on the use of automatic spoilers. |
|-----|-----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

| 5.5 | The cruise fuel mileage guarantee includes allowances for normal power extraction and engine bleed for normal operation of the air conditioning system.  Normal electrical power extraction shall be defined as not less than a 140 kilowatts total electrical load.  Normal operation of the air conditioning system shall be defined as pack switches in the "Auto" position, the temperature control switches in the "Auto" position that results in a nominal cabin temperature of 75°F, and all air conditioning systems operating normally.  This operation allows a maximum cabin pressure differential of 8.6 pounds per square inch at higher altitudes, with a nominal Aircraft cabin ventilation rate of 1,600 cubic feet per minute including passenger cabin recirculation (nominal recirculation is 0 percent).  The APU is turned off unless otherwise specified. |
|-----|-------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

| 5.6 | The cruise fuel mileage guarantee is based on an Aircraft center of gravity location of 17 percent of the mean aerodynamic chord. |
|-----|-----------------------------------------------------------------------------------------------------------------------------------|

| 5.7 | Performance, where applicable, is based on a fuel Lower Heating Value (LHV) of 18,580 BTU per pound. |
|-----|------------------------------------------------------------------------------------------------------|

| 6 | GUARANTEE COMPLIANCE |
|---|----------------------|

| 6.1 | Compliance with the guarantees of Sections 2 and 3 shall be based on the conditions specified in those sections, the Aircraft configuration of Section 4 and the guarantee conditions of Section 5. |
|-----|-----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

| 6.2 | Compliance with the takeoff and landing guarantees shall be based on the FAA approved Airplane Flight Manual for the Model 767-300F. |
|-----|--------------------------------------------------------------------------------------------------------------------------------------|

| 6.3 | Compliance with the cruise fuel mileage guarantee shall be established by calculations based on flight test data obtained from an aircraft in a configuration similar to that defined by the Detail Specification. |
|-----|--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

| 6.4 | Compliance with the Manufacturer's Empty Weight guarantee shall be based on information in the "Weight and Balance Control and Loading Manual - Aircraft Report." |
|-----|-------------------------------------------------------------------------------------------------------------------------------------------------------------------|

| 6.5 | The data derived from tests shall be adjusted as required by conventional methods of correction, interpolation or extrapolation in accordance with established engineering practices to show compliance with these guarantees. |
|-----|--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

| 6.6 | Compliance shall be based on the performance of the airframe and engines in combination, and shall not be contingent on the engine meeting its manufacturer's performance specification. |
|-----|------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

| 7 | EXCLUSIVE GUARANTEES |
|---|----------------------|

----

| 1. | Table of Contents, Articles, Tables, Exhibits and Supplemental Exhibits: |
|----|--------------------------------------------------------------------------|

----

| 2. | Restricted Letter Agreements. |
|----|-------------------------------|

| 3. | Payment Due at Effective Date of this Supplemental Agreement. |
|----|---------------------------------------------------------------|

| Computation  of amount due upon signing of SA-29:           |   |
|-----------------------------------------------------------------------|--------|
| [***]                                                                 |   |
| [***]                                                                 | [***]  |
| [***]                                                                 | [***]  |
| [***]                                                                 | [***]  |
|                                                                  |   |
| Subtotal                                                              | [***]  |
|                                                                  |   |
| Less:  Creditable amount from Substituted 767-316F Aircraft | [***]  |

----

| Total amount due upon signing SA-29                                                                                     | [***]  |
|-------------------------------------------------------------------------------------------------------------------------|--------|
|                                                                                                                    |   |
| +-in accordance with delivery terms specified in the Special Matters Letter Applicable to the 2012 Accelerated Aircraft |   |

| 4. | Confidentiality. |
|----|------------------|

----

| THE BOEING COMPANY  |             | LAN AIRLINES S.A. |
|---------------------|------------------|-------------------|
|                |             |              |
| By:                 |             |              | By: |   |
| Ms. Irma L. Krueger |             | Mr. Roberto Alvo  |
|                |             |              |
| Its                 | Attorney-In-Fact |              | Its: | Sr. Vice President Strategic Planning & |
|                |             |              |   | Corporate Development |

|   | By:                             |                    |
|--------|---------------------------------|-------------------------|
|   | Mr. Alejandro de la Fuente Goic |
|   |                            |
|   | Its:                            | Chief Financial Officer |

----

----

|     |                            |   | Supplemental |   |
|----------|---------------------------------|--------|--------------|--------|
| ARTICLES |                            |   | Agreement    |   |
| 1.       | Quantity, Model and Description |   |         | 24     |   |
| 2.       | Delivery Schedule               |   |         | 24     |   |
| 3.       | Price                           |   |         | 24     |   |
| 4.       | Payment                         |   |         | 24     |   |
| 5.       | Miscellaneous                   |   |         | 24     |   |
| 6.       | Confidentiality                 |   |         | 24     |   |

| TABLE |                                                                |   |   |   |
|-------|---------------------------------------------------------------------|--------|--------|--------|
| 1.    | Aircraft Information Table 767 300ER Aircraft – 1995$         |   |   | 1      |   |
| 2.    | Aircraft Information Table 767 300F Aircraft – 1997$          |   |   | 1      |   |
| 3.    | Aircraft Information Table 767 300F Aircraft – 1998$          |   |   | 8      |   |
| 4.    | Aircraft Information Table 767 300F Aircraft – 1999$          |   |   | 11     |   |
| 5.    | Aircraft Information Table 767 300F Aircraft – 2003$          |   |   | 18     |   |
| 6.    | Aircraft Information Table 767 316ER Aircraft – 2003$         |   |   | 21     |   |
| 7.    | Aircraft Information Table 767 300F Aircraft – 2004$          |   |   | 24     |   |
| 8.    | Aircraft Information Table 767 316ER Aircraft – 2004$         |   |   | 22     |   |
| 9.    | Aircraft Information Table 767 316ER Aircraft – 2005 $        |   |   | 22     |   |
| 10.   | Aircraft Information Table 767-316ER Aircraft – 2006 $        |   |   | 25     |   |
| 11.   | Aircraft Information Table 767-316ER Aircraft – 2008 $        |   |   | 28     |   |
| 12.   | Aircraft Information Table 767-316F Aircraft – 2008 $:DELETED |   |   | 29     |   |
| 13.   | Aircraft Information Table 767-316ER Aircraft – 2010 $        |   |   | 29     |   |

| EXHIBITS |                                                           |   |   |   |
|----------|----------------------------------------------------------------|--------|--------|--------|
| A.       | Aircraft Configuration                                         |   |   |   |
| A-1      | Aircraft Configuration                                         |   |   | 1      |   |
| A-2      | Aircraft Configuration                                         |   |   | 5      |   |
| A-3      | Aircraft Configuration                                         |   |   | 10     |   |
| A-4      | Aircraft Configuration 767-316F Aircraft – 2003$         |   |   | 15     |   |
| A-5      | Aircraft Configuration 767-316ER Aircraft – 2003$        |   |   | 17     |   |
| A-6      | Aircraft Configuration 767-316ER Aircraft – 2004$        |   |   | 22     |   |
| A-7      | Aircraft Configuration 767-316ER Aircraft – 2005$        |   |   | 22     |   |
| A-8      | Aircraft Configuration 767-316ER Aircraft – 2006$        |   |   | 23     |   |
| A-9      | Aircraft Configuration 767-316ER Aircraft – 2008$        |   |   | 24     |   |
| A-10     | Aircraft Configuration 767-316F Aircraft – 2008$:DELETED |   |   | 29     |   |
| A-11     | Aircraft Configuration 767-316ER Aircraft – 2010$        |   |   | 29     |   |
| B.       | Aircraft Delivery Requirements and Responsibilities            |   |   | 1      |   |

|                       |                                                      | Supplemental       |   |
|----------------------------|-----------------------------------------------------------|--------------------|--------|
| SUPPLEMENTAL EXHIBITS |                                                      | Agreement (s) |   |
|                       |                                                      |               |   |   |   |
| BFE1.                      | BFE Variables                                             |               |   | 1 |   |
| CS1.                       | Customer Support Variables                                |               |   | 1 |   |
| EE1.                       | Engine Escalation/Engine Warranty and Patent Indemnity    |               |   | 1 |   |
| EE1-1.                     | Engine Escalation/Engine Warranty and Patent Indemnity    |               |   | 5 |   |
| EE1-2.                     | Engine Escalation/Engine Warranty and Patent Indemnity    |               |   | 13 |   |
| EE1-2006$                  | Engine Escalation, Engine Warranty & Patent Indemnity |               |   | 26 |   |
| EE1-2008$                  | Engine Escalation, Engine Warranty & Patent Indemnity |               |   | 26 |   |
| EE1-2010$                  | Engine Escalation, Engine Warranty & Patent Indemnity |               |   | 29 |   |
| SLP1.                      | Service Life Policy Components                            |               |   |   |   |
| AE1                        | Escalation adjustment-airframe and optional features      |               |   | 22 |   |
| AE1 2008$                  | Escalation adjustment-airframe and optional features      |               |   | 24 |   |
| AE1 2010$                  | Escalation adjustment-airframe and optional features      |               |   | 29 |   |

----

| LETTER AGREEMENTS |                       |   |   |   |
|------------------------|----------------------------|--------|--------|--------|
|                   |                       |   |   |   |
| 2126-1                 | Seller Purchased Equipment |   |   |   |
| 2126-2R1               | Cabin Systems Equipment    |   |   | 17     |   |
| 2126-3R4               | Option Aircraft            |   |   | 13     |   |

| RESTRICTED LETTER AGREEMENTS                                         |                                                                                                         |
|--------------------------------------------------------------------------------|--------------------------------------------------------------------------------------------------------------|
|                                                                           |                                                                                                         |   |
|           6-1162-DMH-350     | Performance Guarantees                                                                                       |   |
|           6-1162-DMH-351     | Promotion Support                                                                                            |   |
|           6-1162-DMH-472     | Performance Guarantees                                                                                       | 1 |
|           [***]              | [***]                                                                                                        | 1 |
|           [***]              | [***]                                                                                                        | 9 |
|           6-1162-LAJ-311     | Special Matters Relating to the July 2001 and September 2001 Aircraft                                        | 11 |
|           6-1162-LAJ-956     | Special Matters Relating to four 2006 Delivery Aircraft (February 4, 2005)                                   |   |
|           6-1162-LAJ-0895R6  | Business Considerations                                                                                      | 23 |
|           [***]              | [***]                                                                                                        | 21 |
|           6-1162-ILK-0381 R2 | Special Matters Letter Applicable to the 2011 Accelerated Aircraft and the Substitute 767 Freighter Aircraft | 29DELETED |
|           6-1162-ILK-0382    | No longer applicable                                                                                         | 26 |
|           [***]              | [***]                                                                                                        | 26 |

|                                                                           |                                                                                                                         |               | Supplemental |
|--------------------------------------------------------------------------------|------------------------------------------------------------------------------------------------------------------------------|--------------------|--------------|
| RESTRICTED LETTER AGREEMENTS, continued                         |                                                                                                                         | Agreement (s) |
|                                                                           |                                                                                                                         |               |         |
|           6-1162-ILK-0384 R2 | 16G Seats                                                                                                                    |               | 27           |
|           6-1162-ILK-0385 R2 | Performance Guarantees Relating to the 2011 Accelerated Aircraft; the 2012 Accelerated Aircraft and the Incremental Aircraft |               | 27           |
|           6-1162-ILK-0388    | Option Aircraft – DELETED                                                                                              |               | 28(Art 6.2)  |
|           6-1162-ILK-0412    | Special Matters Relating to Three Aircraft Originally Scheduled to Deliver in 2009                                           |               | 25           |
|           [***]              | [***]                                                                                                                        |               | 25           |
|           6-1162-KSW-6423    | Special Matters Letter Applicable to the  Incremental Aircraft                                                     |               | 27           |
|           6-1162-KSW-6424    | Aircraft Model Substitution Relating to the Incremental Aircraft                                                             |               | 27           |
|           6-1162-KSW-6456    | Performance Guarantees for Substitute 767 Freighter Aircraft:  DELETED                                             |               | 29           |
|           6-1162-ILK-0450    | Special Matters Letter Applicable to the 2012 Accelerated Aircraft                                                           |               | 29           |

----

----

| Airframe Model/MTOW:                       | 767-300ER   | 412000 pounds |                                       | Detail Specification:                        | D019T001-L (2/10/2010)         |        |
|--------------------------------------------|-------------|---------------|--------------------------------------------|----------------------------------------------|--------------------------------|-------------|
| Engine Model/Thrust:                       | CF6-80C2B6F | 60200 pounds  |                                       | Airframe Price Base Year/Escalation Formula: | Jul-10          | ECI-MFG/CPI |
| Airframe Price:                            | [***]       |          | Engine Price Base Year/Escalation Formula: | Jul-10                        | GE CF6-80 & GE90 (99 rev.) |
| Optional Features:                         | [***]       |          |                                       |                                         |                           |
| Sub-Total of Airframe and Features:        | [***]       |          | Airframe Escalation Data:                  |                                         |                           |
| Engine Price (Per Aircraft):               | [***]       |          | Base Year Index (ECI):                     | 106.8                                        |                           |
| Aircraft Basic Price (Excluding BFE/SPE):  | [***]       |          | Base Year Index (CPI):                     | 215.6                                        |                           |
| Buyer Furnished Equipment (BFE) Estimate:  | [***]       |          | Engine Escalation Data:                    |                                         |                           |
| Seller Purchased Equipment (SPE) Estimate: | [***]       |          | Base Year Index (CPI):                     | 133.190                                      |                           |
|                                       |        |          |                                       |                                         |                           |
| [***]                                      | [***]       |          |                                       |                                         |                           |

|    |         |           |         | Escalation |   | Escalation |         |               |         | Escalation Estimate   |         | Advance Payment Per Aircraft (Amts. Due/Mos. Prior to Delivery): |
|--------------|--------------|----------------|--------------|------------|--------|------------|--------------|--------------------|--------------|----------------------------|--------------|-----------------------------------------------------------------------------------------------------|
| Delivery     |         | Number of |         | Factor     |   | Factor     |         | Manufacturer       |         | Adv Payment Base |         | [***]                                                                                               |   | [***] |   | [***] |   | Total |
| Date         |         | Aircraft       |         | (Airframe) |   | (Engine)   |         | Serial Number |         | Price Per A/P    |         | [***]                                                                                               |   | [***] |   | [***] |   | [***] |
| Jun-2012     |         | 1              |         | 1.0391     |   | 1.081      |         | 40799              |         | [***]                      |         | [***]                                                                                               |   | [***] |   | $8,538,100 |   | [***] |
| Jul-2012     |         | 1              |         | 1.0405     |   | 1.084      |         | 40592              |         | [***]                      |         | [***]                                                                                               |   | [***] |   | $8,551,450 |   | [***] |
| Oct-2012     |         | 1              |         | 1.0455     |   | 1.093      |         | 40593              |         | [***]                      |         | [***]                                                                                               |   | [***] |   | $8,596,950 |   | [***] |
| Total:       |    | 3              |    |       |   |       |    |               |    |                       |    |                                                                                                |    |   |    |   |    |   |

----

----

----

| 0110-000035 | MAJOR MODEL 767 AIRPLANE                                                                                                      | [***] |
|-------------|-------------------------------------------------------------------------------------------------------------------------------|-------|
| 0110-000037 | MINOR MODEL 767-300 PASSENGER AIRPLANE                                                                                        | [***] |
| 0110-000092 | MODEL 767-300ER PASSENGER AIRPLANE                                                                                            | [***] |
| 0110A276A30 | NEW LOOK INTERIOR - 767-300ER                                                                                                 | [***] |
| 0130B657J85 | MP - INTERIOR ARRANGEMENT - REVISION                                                                                          | [***] |
| 0130B657L12 | MP - BUSINESS CLASS PASSENGER SEATS - REVISION - PASSENGER CABIN                                                              | [***] |
| 0130B657L60 | MP - INTERIOR ARRANGEMENT - REVISION                                                                                          | [***] |
| 0130B657L79 | MP - RELOCATION OF MONUMENT MOUNTED LCD MONITORS,  LITERATURE POCKETS AND BASSINET FITTINGS - PASSENGER CABIN - SPE | [***] |
| 0220B604D37 | TYPE CERTIFICATON & EXPORT CERTIFICATE OF AIRWORTHINESS FOR AIRPLANE DELIVERY - REQUIREMENT - LAN 767-300ER               | [***] |
| 0221-000002 | DISPATCH WITH GEAR EXTENDED FOR REVENUE FLIGHT                                                                                | [***] |
| 0221A251A19 | ENGINE INOPERATIVE TEN-MINUTE TAKEOFF THRUST OPERATION - CF6-80C2B6F THRUST RATING                                            | [***] |
| 0221B401A43 | TAKEOFF AND LANDING WITH TAILWIND UP TO 15-KNOTS                                                                              | [***] |
| 0224-000024 | EXTENDED RANGE TWIN ENGINE OPERATIONS  (ETOPS)                                                                      | [***] |
| 0228-000001 | FLIGHT MANUALS IN FAA FORMAT                                                                                                  | [***] |
| 0228-000032 | OPERATIONS MANUAL IN FAA FORMAT                                                                                               | [***] |
| 0229A141A41 | PERFORMANCE - CERTIFICATION FOR OPERATION AT AIRPORT ALTITUDES OF 9500 FEET AND BELOW                                         | [***] |
| 0252-000014 | ENVIRONMENTAL CONTROL SYSTEM  -  TEMPERATURE INDICATIONS IN DEGREES CELSIUS                               | [***] |
| 0252-000017 | INSTRUMENTATION WITH METRIC UNITS  -  MODEL 767                                                           | [***] |
| 0254-000003 | USPHS CERTIFICATE OF SANITARY CONSTRUCTION                                                                                    | [***] |
| 0315C417A53 | CERTIFIED OPERATIONAL AND STRUCTURAL DESIGN WEIGHTS 767-300ER                                                                 | [***] |
| 0351B523A03 | TEMPLATE - TAKEOFF PERFORMANCE IMPROVEMENT - ALTERNATE FORWARD CENTER OF GRAVITY LIMITS                                       | [***] |
| 0351C417B92 | MP - CENTER-OF-GRAVITY LIMITS - REPLACE - TEMPLATE OPTION                                                                     | [***] |
| 0360C417A60 | MISCELLANEOUS WEIGHT COLLECTOR                                                                                                | [***] |
| 1110B657G71 | EXTERIOR COLOR SCHEME AND MARKINGS                                                                                            | [***] |
| 1110B657M33 | MP - BFE - PREMASK - VERTICAL STABILIZER - EXTERIOR COLOR SCHEMES AND MARKINGS                                                | [***] |
| 1120-000019 | MAINTENANCE MARKINGS - ACCESS PANELS - ENGINE STRUT AND COWLS                                                                 | [***] |
| 1130A931A06 | IATA STANDARD MARKINGS - LOWER LOBE CARGO COMPARTMENT                                                                         | [***] |
| 1130B657G72 | INTERIOR PASSENGER COMPARTMENT PLACARDS AND MARKINGS                                                                          | [***] |
| 1130B657J09 | SEAT ROW MARKERS -  PASSENGER CABIN                                                                                 | [***] |
| 1130B657L11 | MP - ECONOMY CLASS SEAT ROW MARKERS REVISION - INTERIOR PLACARDS                                                              | [***] |
| 1130B657P19 | MP - INTERIOR PLACARDS - REVISION - PASSENGER CABIN                                                                           | [***] |

----

| 1130B657P39 | INTERIOR PLACARDS - REVISION - ADDITIONAL SEAT ROW MARKERS - CENTER OVERHEAD BINS INTERIOR                                                                                                                   | [***] |
|-------------|--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|-------|
| 2145-000004 | BULK CARGO AREA HEATING AND VENTILATING FOR ANIMAL CARRIAGE                                                                                                                                                  | [***] |
| 2158A071A11 | IN-FLIGHT ENTERTAINMENT EQUIPMENT COOLING SYSTEM, FWD OF DOOR 2 - 200 CFM INSTALLATION                                                                                                                       | [***] |
| 2210-000003 | AUTOFLIGHT - INHIBIT GLIDE SLOPE CAPTURE PRIOR TO LOCALIZER CAPTURE                                                                                                                                          | [***] |
| 2210-000030 | AUTOFLIGHT - THREE DIGIT MACH NUMBER ON MODE CONTROL PANEL                                                                                                                                                   | [***] |
| 2210-000031 | AUTOFLIGHT - AUTOMATIC AUTOPILOT CHANNEL SELECTION IN APPROACH MODE                                                                                                                                          | [***] |
| 2210-000037 | AUTOFLIGHT - BANK ANGLE HOLD AT AUTOPILOT COMMAND ENGAGE                                                                                                                                                     | [***] |
| 2210-000039 | AUTOFLIGHT - FULL TIME FLIGHT DIRECTOR                                                                                                                                                                       | [***] |
| 2210-000311 | AUTOFLIGHT - FLIGHT CONTROL COMPUTER (FCC) WITHOUT ONBOARD SOFTWARE LOADING CAPABILITY                                                                                                                       | [***] |
| 2210A064A02 | AUTOFLIGHT - ALTITUDE ALERT - 300/900 FEET                                                                                                                                                                   | [***] |
| 2210B403A08 | MODE CONTROL PANEL WITHOUT BACKCOURSE SWITCH                                                                                                                                                                 | [***] |
| 2230-000127 | AUTOTHROTTLE - SELECTION OF CLIMB DERATES                                                                                                                                                                    | [***] |
| 2230-000133 | AUTOTHROTTLE - FIXED PERCENTAGE DERATE LEVELS OF 10% AND 20%                                                                                                                                                 | [***] |
| 2230-000135 | AUTOTHROTTLE - CLIMB DERATE WASHOUT SCHEDULE - 10,000 TO 12,000 FEET                                                                                                                                         | [***] |
| 2311-000124 | HF COMMUNICATIONS - DUAL GABLES HF CONTROL PANELS WITH SENSITIVITY AND DATALINK CONTROL - P/N G7401-16 - BFE/SPE                                                                                             | [***] |
| 2311-000137 | HF COMMUNICATIONS - PARTIAL PROVISIONS FOR DUAL ARINC 753 HF DATALINK                                                                                                                                        | [***] |
| 2311B401A29 | DUAL HF DATA RADIO - ARINC 753 - ACTIVATION - AIRLINE DATA LINK COMMUNICATIONS ONLY                                                                                                                          | [***] |
| 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                                                                                                                                                  | [***] |
| 2312B401A16 | VHF COMMUNICATIONS - EQUIPMENT INSTALLATION OF TRIPLE ROCKWELL ARINC 750 VHF-920 FM IMMUNE TRANSCEIVERS WITH 8.33 KHZ CHANNEL SPACING, VDL MODE 2, AND CMC INTERFACE CAPABILITY - P/N 822-1250-002 - BFE/SPE | [***] |
| 2312B800D19 | VHF COMMUNICATIONS - TRIPLE GABLES VHF TUNING PANELS (DUAL KNOB) - P/N G7400-227 - BFE/SPE                                                                                                                   | [***] |
| 2321B401A04 | SELCAL - AVTECH FIVE CHANNEL DECODER - P/N NA138-714C  - BFE/SPE                                                                                                                                   | [***] |
| 2322A213B76 | CMU - INSTALLATION OF PARTIAL PROVISIONS FOR SINGLE CMU ACCORDANCE WITH ARINC 758                                                                                                                            | [***] |
| 2322B401A31 | CMU - INSTALLATION OF ROCKWELL COLLINS ARINC 758 LEVEL AOA CMU - P/N 822-1239-151  - BFE / SPE                                                                                                     | [***] |

----

| 2322B800A68 | AIRCRAFT COMMUNICATIONS ADDRESSING AND REPORTING SYSTEM (ACARS) - LARGE FORMAT MULTIPURPOSE INTERACTIVE DISPLAY UNIT (MIDU) - ROCKWELL - P/N 822-1626-105 -  BFE/SPE | [***] |
|-------------|--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|-------|
| 2324B800D31 | MP - EMERGENCY LOCATOR TRANSMITTER (ELT) - ELTA 3-FREQUENCY AUTOMATIC - FIXED - P/N 95N6088 - SPE                                                                              | [***] |
| 2324C485B12 | MP - EMERGENCY LOCATOR TRANSMITTER (ELT) - INSTALLATION - ELTA 3 - FREQUENCY AUTOMATIC - FIXED - P/N 01N65900 - SPE                                                            | [***] |
| 2331B702M61 | PASSENGER ADDRESS (PA) SYSTEM - TWO CLASS -  ROCKWELL COLLINS                                                                                                        | [***] |
| 2332A324A38 | IN-FLIGHT ENTERTAINMENT SYSTEM POWER CONTROL SWITCH - HEAD END                                                                                                                 | [***] |
| 2332A324A39 | IN-FLIGHT ENTERTAINMENT SYSTEM POWER CONTROL SWITCH - SEAT AND AREA DISTRIBUTION                                                                                               | [***] |
| 2332A324A40 | IN-FLIGHT ENTERTAINMENT SYSTEM POWER CONTROL SWITCH - MASTER                                                                                                                   | [***] |
| 2332B702M66 | IN-FLIGHT ENTERTAINMENT - PARTIAL PROVISIONS - THALES - 767                                                                                                                    | [***] |
| 2332B702N44 | IN-FLIGHT ENTERTAINMENT SYSTEM - THALES - WITH OVERHEAD VIDEO - FULL CABIN PC POWER - FUL CABIN AVOD - PAX - CSE                                                               | [***] |
| 2332B702N67 | MP - PASSENGER ENTERTAINMENT SYSTEM - PARTIAL PROVISIONS - PARTITION RELOCATION - MOBILE FRONTIER                                                                              | [***] |
| 2332B702P67 | MP - PASSENGER ENTERTAINMENT SYSTEM - VIDEO - REVISION - THALES - CSE                                                                                                          | [***] |
| 2332C417B98 | MP - PASSENGER ENTERTAINMENT SYSTEM - REPLACEMENT - THALES 15" MONITOR IN LIEU OF JAMCO 15" MONITOR - THALES - SPE                                                             | [***] |
| 2332C522A02 | MP - PASSENGER ENTERTAINMENT SYSTEM - REVISION - TPCU HANDSET - THALES - SPE                                                                                                   | [***] |
| 2332C817F17 | MP - PASSENGER ENTERTAINMENT SYSTEM - VIDEO - REVISION - SOFTWARE PART NUMBERS - THALES - SPE                                                                                  | [***] |
| 2340B800D47 | CREW COMMUNICATIONS - PILOTS' CALL PANEL - FLIGHT DECK                                                                                                                         | [***] |
| 2342-000016 | CABIN INTERPHONE SYSTEM - CABIN INTERPHONE HANDSET - FLIGHT COMPARTMENT                                                                                                        | [***] |
| 2350B800C71 | AUDIO INTEGRATING - AUDIO SELECTOR PANELS - FLIGHT DECK                                                                                                                        | [***] |
| 2350C164D44 | MP - AUDIO SELECTOR PANEL (ASP) & PILOT'S CALL PLANEL - REPLACEMENT - SFE ASP WITH INTEGRATED SELCAL AND CREW CALL FUNCTIONS - 3 VHF/2 HF/2 SATCOM (P/N 285T0022-51)       | [***] |
| 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                                                                                                              | [***] |

----

| 2351A213A33 | AUDIO INTEGRATION - INSTALLATION - TWO-PLUG AUDIO JACKS IN THE FLIGHT DECK                                                                                         | [***] |
|-------------|--------------------------------------------------------------------------------------------------------------------------------------------------------------------|-------|
| 2351A213B77 | BOOM MICROPHONE HEADSETS - CAPTAIN AND FIRST OFFICER - TELEX AIRMAN 750 - P/N 64300-200 - BFE/SPE                                                                  | [***] |
| 2351A213B80 | HEADPHONE - FIRST OBSERVER - TELEX - P/N 64400-200 - BFE/SPE                                                                                                       | [***] |
| 2351A213B81 | HEADPHONE - SECOND OBSERVER - TELEX - P/N 64400-200 - BFE/SPE                                                                                                      | [***] |
| 2371-000009 | NO MONITOR JACK IN THE WHEEL WELL                                                                                                                                  | [***] |
| 2371-000017 | SOLID STATE VOICE RECORDER ED56A AND SOLID STATE MICROPHONE/MONITOR ED56A - ALLIEDSIGNAL - 2 HOUR RECORDING TIME - P/N 980-6022-001 AND P/N 980-6116-002 - BFE/SPE | [***] |
| 2432-000002 | AUXILIARY POWER UNIT (APU) - ADDITIONAL STARTING CAPABILITY                                                                                                        | [***] |
| 2433-000021 | STANDBY POWER - EXTENDED TIME CAPABILITY - BATTERY PARALELLING                                                                                                     | [***] |
| 2451-000002 | 90 KVA GALLEY POWER SUPPLY                                                                                                                                         | [***] |
| 2501A611A19 | FORWARD MONUMENT COMPLEX 4                                                                                                                                         | [***] |
| 2504A611A14 | AFT MONUMENT COMPLEX 3                                                                                                                                             | [***] |
| 2511-000022 | MANUALLY OPERATED SEATS  -  CAPTAIN AND FIRST OFFICER                                                                                          | [***] |
| 2511-000026 | FIRST OBSERVER'S SEAT - WALL MOUNTED                                                                                                                               | [***] |
| 2511B806J86 | MP - SECOND OBSERVER STSATION WITH ARMRESTS - ADDITION                                                                                                             | [***] |
| 2513-000405 | SUNVISOR INSTALLATION - NUMBER 1 AND 2 WINDOWS - FLIGHT DECK - SFE                                                                                                 | [***] |
| 2520B657G80 | INTERIOR COLOR AND MATERIAL - STANDARD OFFERING                                                                                                                    | [***] |
| 2520B657J42 | UNIQUE DECORATIVE TEDLAR LAMINATE (DTL) - MONUMENTS - INTERIOR COLOR AND MATERIAL - SFE                                                                            | [***] |
| 2520B657K41 | MP - BFE RAW CARPET, CURTAIN AND FLOOR MAT MATERIAL                                                                                                                | [***] |
| 2520B657M19 | MP - INTERIOR DECOR - REVISION - PASSENGER CABIN                                                                                                                   | [***] |
| 2520B657M35 | MP - DECORATIVE TEDLAR LAMINATE (DTL) - REVISION - MONUMENT MOUNTED - INTERIOR COLOR AND MATERIAL - SFE                                                            | [***] |
| 2520B657M56 | MP - DECORATIVE TEDLAR LAMINATE (DTL) - REVISION - MONUMENT MOUNTED - INTERIOR COLOR AND MATERIAL - SFE                                                            | [***] |
| 2523B657J10 | ADDITIONAL PASSENGER SERVICE UNITS -                                                                                                                               | [***] |
| 2523B657J31 | PASSENGER SERVICE UNITS                                                                                                                                            | [***] |
| 2524B657G86 | SPE - FULL HEIGHT CENTERLINE CLOSET - STA 353 - STA 379                                                                                                            | [***] |
| 2524B657G99 | CURTAIN AND TRACK INSTALLATION - DOOR 1 LEFT AFT                                                                                                                   | [***] |
| 2524B657H01 | CURTAIN AND TRACK INSTALLATION - DOOR 1 RIGHT AFT                                                                                                                  | [***] |
| 2524B657H04 | CURTAIN AND TRACK INSTALLATION - DOOR 4                                                                                                                            | [***] |
| 2524B657H95 | UNDERBIN CENTERLIN CLASS DIVIDER - SPE                                                                                                                             | [***] |
| 2524B657H96 | LH UNDERBIN OUTBOARD CLASS DIVIDER - SPE                                                                                                                           | [***] |

----

| 2524B657H97 | RH UNDERBIN OUTBOARD CLASS DIVIDER - SPE                                                                                                                         | [***] |
|-------------|------------------------------------------------------------------------------------------------------------------------------------------------------------------|-------|
| 2524B657J00 | CURTAIN AND TRACK INSTALLATION                                                                                                                                   | [***] |
| 2524B657J01 | CURTAIN AND TRACK INSTALLATION - BETWEEN BUSINESS CLASS AND ECONOMY CLASS                                                                                        | [***] |
| 2524B657J13 | LH UNDERBIN OUTBOARD CLASS DIVIDER - SPE                                                                                                                         | [***] |
| 2524B657J15 | RH UNDERBIN OUTBOARD CLASS DIVIDER - SPE                                                                                                                         | [***] |
| 2524B657J40 | SPE - CLOSET WITH INTEGRAL STOWAGE UNIT AND WALL MOUNTED ATTENDANT SEAT PROVISIONS - LH UNDERBIN - ECONOMY CLASS - FORWARD DOOR 4                                | [***] |
| 2524B657J41 | SPE - CLOSET WITH INTEGRAL STOWAGE UNIT AND WALL MOUNTED ATTENDANT SEAT PROVISIONS - RH UNDERBIN - ECONOMY CLASS - FORWARD DOOR 4                                | [***] |
| 2524B657K50 | MP - CLOSETS, PARTITION & CLASS DIVIDERS - REVISION - FULL HEIGHT CENTERLINE STA 344 - STA 366 - SPE                                                         | [***] |
| 2524B657P10 | MP - CURTAINS - REVISION - CURTAIN AND CURTAIN TRACK - PASSENGER CABIN                                                                                           | [***] |
| 2524B657P16 | MP - CLASS DIVIDERS - REPLACEMENT - BUSINESS CLASS - SPE                                                                                                         | [***] |
| 2524C417C49 | MP - CURTAINS - REVISION - CURTAIN AND CURTAIN TRACK - PASSENGER CABIN                                                                                           | [***] |
| 2524C707A33 | MP - CLOSETS, PARTITION & CLASS DIVIDERS - REVISION - FULL HEIGHT SEAT TRACK MOUNTED CLOSETS - STA 1465.95 - STA 1478.95 AND STA 1467.95 - STA 1478.95 - SPE | [***] |
| 2524C826C28 | MP - CURTAINS - REVISION - BFE CURTAIN MATERIAL                                                                                                                  | [***] |
| 2524C826R50 | MP - CLOSETS, PARTITIONS AND CLASS DIVIDERS - REVISION - CURTAIN MATERIAL - NEO-TEX - BFE                                                                        | [***] |
| 2525B657H05 | BUSINESS CLASS SEATS                                                                                                                                             | [***] |
| 2525B657H07 | ECONOMY CLASS SEATS                                                                                                                                              | [***] |
| 2525B657J37 | ATTENDANT SEATS FOR 767-300                                                                                                                                      | [***] |
| 2525B657L13 | MP - ECONOMY CLASS PASSENGER SEATS - REVISION                                                                                                                    | [***] |
| 2525B657N74 | MP - BUSINESS CALSS SEATS - REVISION - REVIEW AND APPROVE SUPPLIER DATA - SPE                                                                                    | [***] |
| 2525C485B41 | MP - PASSENGER SEATS - REVISION - BUSINESS CLASS SEAT PART NUMBER REVISION - PASSENGER COMPARTMENT - SPE                                                         | [***] |
| 2526B657H11 | SPE - IF-1C VIDEO CONTROL CENTER - FORWARD COMPARTMENT OF THE F2 GALLEY                                                                                          | [***] |
| 2527B657H12 | ENTRYWAY FLOOR COVERING                                                                                                                                          | [***] |
| 2527B657H98 | FLOOR COVERING - SPE                                                                                                                                             | [***] |
| 2527B657K59 | MP - SEAT TRACK COVES AND RACEWAYS - REVISION - BFE IN LIEU OF SFE - ECONOMY CLASS                                                                               | [***] |
| 2527B657L92 | MP - FLOOR COVERING - REVISION - FLOOR MAT MATERIAL - SCHNELLER - BFE                                                                                            | [***] |
| 2527B657N98 | MP - FLOOR COVERING - REVISION - BUSINESS CLASS CARPET AND FLOOR MOUNTED EMERGENCY ESCAPE PATH LIGHTING SYSTEM                                                   | [***] |
| 2527C006A05 | FLOOR COVERING - CARPET, SERGED EDGES                                                                                                                            | [***] |
| 2528B657H13 | OVERHEAD STOWAGE BINS                                                                                                                                            | [***] |
| 2528B657H21 | LITERATURE POCKETS                                                                                                                                               | [***] |

----

| 2528B657J03 | CENTERLINE FLOOR MOUNTED STOWAGE UNIT - SPE                                                                                                                                | [***] |
|-------------|----------------------------------------------------------------------------------------------------------------------------------------------------------------------------|-------|
| 2528B657J23 | MAGAZINE STOWAGE - MONUMENT MOUNTED                                                                                                                                        | [***] |
| 2528B657J29 | LH OUTBOARD FLOOR MOUNTED STOWAGE UNIT - SPE                                                                                                                               | [***] |
| 2528B657J30 | RH OUTBOARD FLOOR MOUNTED STOWAGE UNIT - SPE                                                                                                                               | [***] |
| 2528B657J59 | BIN FAIRING AND CLOSEOUT PANEL - OUTBAOARD OVERHEAD STOWAGE  BINS                                                                                                | [***] |
| 2528B657K02 | MP - STOWAGE COMPARTMENTS - REVISION - BUSTLE IN LIEU OF MAGAZINE BUSTLE - 4F-2LC AND 4F-2RC LAVATORIES                                                                    | [***] |
| 2529B657H43 | CURTAIN AND CURTAIN TRACK INSTALLATION - IN-FLIGHT CREW REST - FORWARD OF DOOR 4R                                                                                          | [***] |
| 2529B657N61 | MP - PASSENGER AND CABIN ATTENDANTS' ACCOMODATIONS - INSTALLATION - CURTAINS AND CURTAIN TRACK - IN-FLIGHT CREW REST ENCLOSURE - BUSINESS CLASS - AFT RH                   | [***] |
| 2529B657R29 | MP - PASSENGER AND CABIN ATTENDANTS ACCOMODATIONS - REVISION - LONGITUDINAL CURTAIN TRACK TO BIN SUPPORT FITTINGS - IN-FLIGHT CREW REST ENCLOSURE- BUSINESS CLASS - RH AFT | [***] |
| 2529C417A72 | ATTENDANT WORKSTATION                                                                                                                                                      | [***] |
| 2530B657H31 | F1 GALLEY                                                                                                                                                                  | [***] |
| 2530B657H33 | F2 GALLEY                                                                                                                                                                  | [***] |
| 2530B657H35 | F3 GALLEY                                                                                                                                                                  | [***] |
| 2530B657H37 | A1 GALLEY                                                                                                                                                                  | [***] |
| 2530B657H39 | A2 GALLEY                                                                                                                                                                  | [***] |
| 2530B657H40 | A3 GALLEY                                                                                                                                                                  | [***] |
| 2530B657H41 | GALLEY PART NUMBERS - BFE/SPE                                                                                                                                              | [***] |
| 2530B657H42 | GALLEY INSERT PART NUMBERS - BFE/SPE                                                                                                                                       | [***] |
| 2530B657J92 | MP - BUFFETS/GALLEYS - REPLACEMENT - F3 GALLEY WITH INTEGRAL CHILLER IN LIEU OF F3 GALLEY WITHOUT INTEGRAL CHILLER - SPE                                                   | [***] |
| 2530B657N79 | MP - BUFFET/GALLEY - REVISION - F3 GALLEY - SPE                                                                                                                            | [***] |
| 2530B657N82 | MP - BUFFET/GALLEY - REVISION - ALTERNATE GALLEY CART PART NUMBER - F2 GALLEY - SPE                                                                                        | [***] |
| 2530C485B69 | MP - GALLEY - REVISION - OVEN PART NUMBER - SPE                                                                                                                            | [***] |
| 2530C635A24 | MP - GALLEY - REVISION - CHILLER - BE AEROSPACE - SPE                                                                                                                      | [***] |
| 2530C826R54 | MP - GALLEY - REVISION - WATER BOILER - B.E. AEROSPACE - SPE                                                                                                               | [***] |
| 2531B657H99 | PARTIAL PROVISIONS FOR NON-STANDARD A4 GALLEY - SPE                                                                                                                        | [***] |
| 2533A798A01 | CHILLERS (6800 BTUH) - THREE - GALLEY  -  FORWARD AND AFT  -  BFE/SPE - P/N 267-100                                                | [***] |
| 2540B657H46 | 1F-1L LAVATORY                                                                                                                                                             | [***] |
| 2540B657H54 | 4F-2LC LAVATORY                                                                                                                                                            | [***] |
| 2540B657H56 | 4F-2RC LAVATORY                                                                                                                                                            | [***] |
| 2540B657H60 | 1A-1L LAVATORY                                                                                                                                                             | [***] |
| 2540B657J34 | 2F-9L LAVATORY                                                                                                                                                             | [***] |
| 2540B657J36 | 2F-9R LAVATORY                                                                                                                                                             | [***] |

----

| 2540B657K45 | MP - LAVATORIES - REVISION - ADDITONAL MIRROR IN 2F-9L AND 2F-9R LAVATORIES                                             | [***] |
|-------------|-------------------------------------------------------------------------------------------------------------------------|-------|
| 2540B657L09 | MP - LAVATORY REVISION - BABY CARE TABLE                                                                                | [***] |
| 2540B657P32 | MP - LAVATORY EQUIPMENT - REVISION - 1A-1L LAVATORY MIRROR                                                              | [***] |
| 2550-000040 | NO PROVISIONS FOR LOADING LONG LIGHTWEIGHT ITEMS - FORWARD CARGO COMPARTMENT                                            | [***] |
| 2552-000135 | CARGO COMPARTMENTS - PARTIAL FLOOR                                                                                      | [***] |
| 2552-000223 | FABRIC STA 744 ENDWALL                                                                                                  | [***] |
| 2552A931A07 | SLOPING SIDEWALL - CARGO COMPARTMENTS - .020 THICKNESS OVERALL  AND .030 THICKNESS AT CARGO DOORS - BMS 8-223 | [***] |
| 2553-000036 | HARDWARE FOR STANDARD CONTAINERS IN THE AFT CARGO COMPARTMENT                                                           | [***] |
| 2553-000042 | NO SPOOL-TYPE LOADER INDEX FITTINGS - AFT CARGO COMPARTMENT                                                             | [***] |
| 2553-000044 | HARDWARE FOR CARRIAGE OF 88 X 125 AND 96 X 125 INCH PALLETS AND STANDARD CONTAINERS IN THE FORWARD CARGO COMPARTMENT    | [***] |
| 2553-000085 | REMOTELY OPERATED CONTAINER ROLLOUT STOPS - AFT CARGO COMPARTMENT DOORWAY                                               | [***] |
| 2555-000022 | STANDARD BULK CARGO AREA FLOOR                                                                                          | [***] |
| 2555-000024 | BULK CARGO DOOR PROTECTOR - NET                                                                                         | [***] |
| 2560-000175 | HALON FIRE EXTINGUISHER - FLIGHT DECK - WALTER KIDDE                                                                    | [***] |
| 2560-000200 | PROTECTIVE BREATHING EQUIPMENT - FLIGHT DECK - SCOTT AVIATION - P/N 802300-14 - BFE/SPE                                 | [***] |
| 2560B800A79 | CREW LIFE VESTS - FLIGHT DECK - AIR CRUISER - P/N D21344-101 - BFE/SPE                                                  | [***] |
| 2561A931A10 | FORWARD ESCAPE HATCH POSITION FOR ESCAPE STRAP                                                                          | [***] |
| 2562B657J43 | OVERWATER EMERGENCY EQUIPMENT                                                                                           | [***] |
| 2562C826P97 | MP - OVERWATER SURVIVAL EQUIPMENT - REVISION - PORTABLE EMERGENCY LOCATOR TRANSMITTER (ELT) - SPE                       | [***] |
| 2562C826R66 | MP - OVERWATER SURVIVAL EQUIPMENT - REPLACEMENT - LIFE VEST - SPE                                                       | [***] |
| 2564B657J49 | DETACHABLE EMERGENCY EQUIPMENT - PASSENGER COMPARTMENT                                                                  | [***] |
| 2564B657K19 | MP - DETACHABLE EMERGENCY EQUIPMENT - REVISION - PASSENGER COMPARTMENT - SPE                                            | [***] |
| 2564B657L23 | MP - DETACHABLE EMERGENCY EQUIPMENT - REVISION - PASSENGER COMPARTMENT                                                  | [***] |
| 2564B657M21 | MP - DETACHABLE EMERGENCY EQUIPMENT - REVISION - PASSENGER COMPARTMENT                                                  | [***] |
| 2564B657M45 | MP - DETACHABLE EMERGENCY EQUIPMENT - NON-RECHARGEABLE FLASHLIGHT IN LIEU OF RECHARGEABLE FLASHLIGHT - SPE              | [***] |
| 2564B657N93 | MP - DETACHABLE EMERGENCY EQUIPMENT - REVISION - PASSENGER COMPARTMENT - SPE                                            | [***] |
| 2564B657P30 | MP - DETACHABLE EMERGENCY EQUIPMENT - REVISION - PASSENGER COMPARTMENT                                                  | [***] |

----

| 2564C826A13 | MP - DETACHABLE EMERGENCY EQUIPMENT - REVISION -  PORTABLE OXYGEN BOTTLE RELOCATION - PASSENGER COMPARTMENT                                                                       | [***] |
|-------------|---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|-------|
| 2566A649A46 | ESCAPE SLIDE - DUAL LANE - TYPE III EXIT WITH VISUAL GUIDANCE                                                                                                                               | [***] |
| 2566C522A04 | MP - ESCAPE SLIDE - DUALLANE - TYPE 111 EXIT WITH VISUAL GUIDANCE                                                                                                                           | [***] |
| 2610-000025 | KIDDE FIRE DETECTION SYSTEM  -  GE CF6-80C2 ENGINES AND APU                                                                                                             | [***] |
| 2613B657G91 | LAVATORY SMOKE DETECTORS  -  767                                                                                                                                        | [***] |
| 2618-000009 | SINGLE LOOP DUCT LEAK DETECTION SYSTEM - 3 ZONE                                                                                                                                             | [***] |
| 2622-000004 | FIRE BOTTLE COMMONALITY - CF6-80C2 ENGINES AND DUAL APU FIRE EXTINGUISHING SYSTEM                                                                                                           | [***] |
| 2732-000002 | STALL WARNING COMPUTER SPEED TAPE ACTIVATION - DISPLAY MINIMUM MANEUVER SPEED ON TAKEOFF                                                                                                    | [***] |
| 2811-000021 | EXTENDED RANGE (ER) FUEL TANK AND FUEL JETTISON SYSTEMS                                                                                                                                     | [***] |
| 2844-000005 | FUEL MEASURING STICKS IN KILOGRAMS WITH CONVERSION TABLES IN KILOGRAMS                                                                                                                      | [***] |
| 2911-000003 | AC MOTOR-DRIVEN HYDRAULIC PUMPS  -  EATON (VICKERS) S270T201-7                                                                                                          | [***] |
| 2911-000038 | ENGINE-DRIVEN HYDRAULIC PUMPS   -  VICKERS INC.   (60B00200-12)                                                                                     | [***] |
| 3042-000003 | WINDSHIELD WIPERS - TWO SPEED - SINGLE SWITCH                                                                                                                                               | [***] |
| 3080-000006 | MANUAL ANTI-ICING SYSTEM - NO ICE DETECTION                                                                                                                                                 | [***] |
| 3120-000011 | ELECTRONIC CLOCKS - WITHOUT TENTHS OF MINUTE DISPLAY - MAIN INSTRUMENT PANEL                                                                                                                | [***] |
| 3131-000143 | ACCELEROMETER  -  Honeywell  P/N 971-4193-001  -  BFE/SPE                                                                                 | [***] |
| 3131-000187 | DIGITAL FLIGHT DATA RECORDER - ALLIEDSIGNAL - 256 WORDS PER SECOND MAXIMUM DATA RATE - P/N 980-4700-042 BFE/SPE                                                                             | [***] |
| 3131A715A01 | DIGITAL FLIGHT DATA ACQUISITION UNIT (DFDAU) WITH ACMS CAPABILITY AND INTERGRATED PCMCIA MEDIA INTERFACE-TELEDYNE CONTROLS-P/N 2233000-816-1 -BFE/SPE                                       | [***] |
| 3132-000095 | AIRBORNE DATA LOADER/RECORDER - ARINC 615 - ALLIEDSIGNAL - 964-0401-006 - BFE/SPE                                                                                                           | [***] |
| 3132-000117 | DATA LOADER SELECTOR SWITCH MODULE - 20 POSITION 3 WAY - SFE                                                                                                                                | [***] |
| 3132A887A01 | DUAL ARINC 615 DATA LOADER/RECORDER INTERFACE TO THE THREE WAY, TWENTY POSITION SYSTEM SELECTOR SWITCH - PORTABLE DATA LOADER/RECORDER CONNECTOR INSTALLATION IN P61 RIGHT SIDE PANEL - SFE | [***] |
| 3133-000057 | FULL FORMAT PRINTER - MILTOPE - ARINC 744 - P/N 706300-212 - BFE/SPE                                                                                                                        | [***] |
| 3133-000125 | ARINC 744 PRINTER PROVISIONS IN THE FLIGHT DECK AISLESTAND                                                                                                                                  | [***] |
| 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                                                                                                               | [***] |
| 3161-000135 | HYDRAULIC PRESSURE ON EICAS STATUS PAGES                                                                                                                 | [***] |
| 3161-000137 | APU RPM ON EICAS STATUS PAGES                                                                                                                            | [***] |
| 3161-000139 | APU OIL QUANTITY LEVEL ON EICAS                                                                                                                          | [***] |
| 3161-000141 | ADDITIONAL ENVIRONMENTAL CONTROL SYSTEM (ECS) PARAMETERS - DISPLAY ON EICAS MAINTENANCE PAGE                                                             | [***] |
| 3161-000144 | GENERATOR OFF AND ENGINE OIL PRESSURE - EICAS ADVISORY LEVEL MESSAGES                                                                                    | [***] |
| 3161-000147 | ECS PRECOOLER OUTLET TEMPERATURE - (PW AND GE ENGINES) - DISPLAY ON EICAS                                                                                | [***] |
| 3161-000152 | BULK CARGO COMPARTMENT TEMPERATURE - DISPLAY ON EICAS                                                                                                    | [***] |
| 3161-000154 | RAM AIR OUTLET DOOR POSITION - DISPLAY ON EICAS                                                                                                          | [***] |
| 3161-000189 | ENGINE FUEL FLOW - FULL TIME DISPLAY - LOWER EICAS DISPLAY                                                                                               | [***] |
| 3162-000016 | FLIGHT MODE ANNUNCIATION AT TOP OF ADI                                                                                                                   | [***] |
| 3162-000021 | AIRSPEED TAPE - ROLLING DIGITS AND TREND VECTOR - ADI                                                                                                    | [***] |
| 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                                                                                                                     | [***] |
| 3162-000034 | RADIO ALTITUDE HEIGHT ALERT DISPLAY - 2500 FEET - ADI                                                                                                    | [***] |
| 3162-000054 | ILS DEVIATION WARNING - ADI                                                                                                                              | [***] |
| 3162-000059 | MAP MODE ORIENTATION - TRACK UP - NAVIGATION DISPLAY                                                                                                     | [***] |
| 3162-000066 | TRUE AIRSPEED AND GROUND SPEED - NAVIGATION DISPLAY                                                                                                      | [***] |
| 3162-000070 | WIND BEARING DIGITAL DISPLAY - NAVIGATION DISPLAY                                                                                                        | [***] |
| 3162-000081 | ADF POINTER(S) - NAVIGATION DISPLAY                                                                                                                      | [***] |
| 3221-000011 | TORQUE ARM QUICK DISCONNECT  -  NOSE LANDING GEAR                                                                                    | [***] |
| 3242A114B69 | ANTISKID/AUTOBRAKE CONTROL UNIT (AACU) P/N 42-767-2 (S283T001-27)  - INSTALLATION                                                              | [***] |
| 3245-000230 | WHEELS AND TIRES - NOSE LANDING GEAR - WHEELS - ALLIEDSIGNAL - INSTALLATION WITH SFE 24 PR, 235 MPH TIRES                                                | [***] |
| 3245A298A12 | BRAKES - CARBON - MESSIER-BUGATTI                                                                                                                        | [***] |
| 3245A438A27 | OPERATIONAL TIRE SPEED LIMITS - 235MPH                                                                                                                   | [***] |
| 3245A438A28 | WHEELS AND TIRES - MAIN LANDING GEAR - HIGH GROSS WEIGHT WHEELS - MESSIER-BUGATTI - INSTALLATION WITH SFE 32 PR, 235 MPH TIRES.                          | [***] |
| 3246-000005 | BRAKE TEMPERATURE MONITORING SYSTEM                                                                                                                      | [***] |

----

| 3320B657N77 | MP - PASSENGER COMPARTMENT - REVISION - OUTBOARD OVERHEAD CLOSEOUT PANEL AREA LIGHT - LH/RH STA 792 - STA 813-95                                      | [***] |
|-------------|-------------------------------------------------------------------------------------------------------------------------------------------------------|-------|
| 3324-000117 | NO-SMOKING LIGHT ON - HARD WIRE                                                                                                                       | [***] |
| 3324B657H92 | OVER AISLE EXIT SIGNS - PASSENGER CABIN                                                                                                               | [***] |
| 3324B657K03 | MP - INFORMATION SIGNS - REPLACEMENT - STANDARD OVER AISLE EXIT SIGNS - PASSENGER CABIN                                                               | [***] |
| 3342-000009 | TAXI LIGHTS  -  NOSE GEAR MOUNTED  -  SPACE PROVISIONS                                                        | [***] |
| 3350A704A30 | EMERGENCY ESCAPE PATH LIGHTING - SEAT/MONUMENT MOUNTED                                                                                                | [***] |
| 3350B657K04 | MP - EMERGENCY ESCAPE PATH LIGLHTLING - REVISION - FLOOR MOUNTED INLIEU OF SEAT/MONUMENT MOUNTED - PASSENGER CABIN                                    | [***] |
| 3413-000027 | MACH/AIRSPEED INDICATOR - TWO KNOT GRADUATIONS BELOW 250 KNOTS                                                                                        | [***] |
| 3421-000042 | FAA MACH/AIRSPEED LIMITS AND OVERSPEED ALERTING                                                                                                       | [***] |
| 3423-000006 | STANDBY MAGNETIC COMPASS COMPENSATION FOR ELECTRICAL CIRCUITS (+/- 5 DEGREES)                                                                         | [***] |
| 3430-000187 | ILS/GPS MULTI-MODE RECEIVER (MMR) - ROCKWELL - P/N 822-1152-002 - BFE/SPE                                                                             | [***] |
| 3433-000032 | RADIO ALTIMETER (RA)  -  ROCKWELL INTERNATIONAL CORP  -  P/N 822-0334-002  -  BFE/SPE     | [***] |
| 3443-000050 | DUAL WEATHER RADAR CONTROL PANEL - ROCKWELL P/N 622-5130-114 - BFE/SPE                                                                                | [***] |
| 3443A065A34 | DUAL WEATHER RADAR SYSTEM - WITH PREDICTIVE WINDSHEAR - ROCKWELL TRANSCEIVER P/N 622-5132-633 - BFE/SPE                                               | [***] |
| 3445A065A86 | TCAS SYSTEM - ROCKWELL COLLINS TCAS COMPUTER P/N 822-1293-002 - TCAS CHANGE 7 COMPLIANT - BFE/SPE                                                     | [***] |
| 3446-000045 | STANDARD VOLUME FOR ALTITUDE CALLOUTS                                                                                                                 | [***] |
| 3446-000048 | ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) - BANK ANGLE CALLOUT ENABLE                                                                          | [***] |
| 3446-000049 | 500 SMART CALLOUT INHIBITED                                                                                                                           | [***] |
| 3446A065A49 | EGPWS - PEAKS AND OBSTACLES FEATURES                                                                                                                  | [***] |
| 3446B800D17 | GROUND PROXIMITY WARNING SYSTEM - MODE 6 ALTITUDE CALLOUTS - 2500, 1000, 500, 400, 300, 200, 100, 50, 40, 30, 20, 10, MINIMUMS                        | [***] |
| 3451-000022 | VOR/MARKER BEACON - ROCKWELL RECEIVER P/N 822-0297-001 - BFE/SPE                                                                                      | [***] |
| 3453B866A16 | ATC SYSTEM - ROCKWELL COLLINS ATC TRANSPONDER P/N 822-1338-003 - ELS/EHS/ES AND TCAS CHANGE 7 COMPLIANT - GABLES CONTROL PANEL P/N G6992-12 - BFE/SPE | [***] |
| 3455-000019 | DISTANCE MEASURING EQUIPMENT (DME) - ROCKWELL INTERROGATOR P/N 822-0329-001 - BFE/SPE                                                                 | [***] |
| 3457-000219 | AUTOMATIC DIRECTION FINDER (ADF) - DUAL SYSTEM - ROCKWELL ADF-900/700 SERIES - ADF RECEIVER P/N 822-0299-001 - ADF ANTENNA P/N 622-5404-003 - BFE/SPE | [***] |

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| 3457-000289 | DUAL ADF CONTROL PANEL - BOEING - 285T0557-2 - WITHOUT BFO OR TONE SWITCH - SFE                                            | [***] |
|-------------|----------------------------------------------------------------------------------------------------------------------------|-------|
| 3461A425A03 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - OFFPATH DESCENT CIRCLES AND DISTANCE MEASURING EQUIPMENT RANGE RINGS DISPLAYED  | [***] |
| 3461A425A04 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - SCANNING DME OPERATIONS - ENABLE                                                | [***] |
| 3461A425A05 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - RUNWAY DISTANCE AND OFFSET POSITION SHIFT IN UNITS OF FEET                      | [***] |
| 3461A425A10 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - NAVIGATION DATABASE - CUSTOMER SUPPLIED                                         | [***] |
| 3461A425A12 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - TAKEOFF DATA LINK - ENABLE                                                      | [***] |
| 3461A425A13 | FMCS - AIRLINE MODIFIABLE INFORMATION (AMI) - CUSTOMER SUPPLIED                                                            | [***] |
| 3461A425A16 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - AIR TRAFFIC SERVICES DATA LINK (ATS DL) - FANS FEATURE ACTIVATION               | [***] |
| 3461A425A17 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - AIRLINE OPERATIONAL COMMUNICATIONS DATA LINK (AOC DL) - FANS FEATURE ACTIVATION | [***] |
| 3461A425A18 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - PRINTER INTERFACE - FANS FEATURE ACTIVATION                                     | [***] |
| 3511B899B48 | CREW OXYGEN MASKS - AUTOMATIC PRESSURE BREATHING TYPE - CAPTAIN AND FIRST OFFICER - EROS - BFE/SPE                         | [***] |
| 3511B899B49 | CREW OXYGEN MASKS - AUTOMATIC PRESSURE BREATHING TYPE - FIRST OBSERVER - EROS - BFE/SPE                                    | [***] |
| 3511B899B50 | CREW OXYGEN MASKS - AUTOMATIC PRESSURE BREATHING TYPE - SECOND OBSERVER - EROS/SCOTT AVIATION - BFE/SPE                    | [***] |
| 3611-000005 | HAMILTON STANDARD  -  INTERMEDIATE PRESSURE (IP) CHECK VALVES - GE\P&W ENGINES                     | [***] |
| 3811-000022 | POTABLE WATER - SERVICEABLE TO 149 GALLONS                                                                                 | [***] |
| 3831-000008 | WASTE TANK CAPACITY  -  116 GALLONS                                                                    | [***] |
| 3832-000031 | VACUUM WASTE SYSTEM  -  ENVIROVAC TOILET ASSEMBLIES                                                    | [***] |
| 3910B800A77 | CONTROL PANEL ARRANGEMENT - P8 AISLE STAND - FLIGHT DECK - LAN                                                             | [***] |
| 4970-000046 | APU CYCLEMETER   -  AFT ELECTRONIC EQUIPMENT (E/E) COMPARTMENT                                    | [***] |
| 4970-000047 | APU HOURMETER  -  AFT ELECTRONIC EQUIPMENT (E/E) COMPARTMENT                                           | [***] |
| 5210-000024 | TYPE A  - III - III - A DOOR ARRANGEMENT                                                                         | [***] |
| 5300B657K48 | MP - INSTALLATION OF SEAT TRACKS - BL 45.5 LEFT AND RIGHT - STA 389 TO STA 721.805                                         | [***] |
| 7200-000382 | STANDARD FAN SPINNER - GE ENGINES                                                                                          | [***] |
| 7200-000412 | GE PROPULSION SYSTEM                                                                                                       | [***] |

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| 7200A114C89  | GENERAL ELECTRIC ENGINES - CF6-80C2-B6F - B6F RATING - WITH FADEC                | [***]  |
|--------------|----------------------------------------------------------------------------------|--------|
| 7830-000012  | MANUAL OPENING OF THRUST REVERSER ASSEMBLIES - GE CF6-80C2 ENGINES               | [***]  |
| 7900-000117  | LUBRICATING OIL - BP TURBO OIL 2380                                              | [***]  |
| 8011-000006  | HAMILTON STANDARD STARTERS AND STARTER VALVES  -  GE ENGINES | [***]  |
| MISC         | INTERIOR ALLOWANCE                                                               | [***]  |
| MISC/FAA5    | FIRE PENETRATION - BURNTHROUGH, FAR 25.865 (b)                                   | [***]  |
|         |                                                                             |   |
| OPTIONS: 299 | [***]                                                                            | [***]  |

----

|   | Pb  = |  Engine Price (per Aircraft), as set forth in Table 13 of the Purchase Agreement. |
|--------|-----------------|----------------------------------------------------------------------------------------|

|   | F= |  0.005 x (N/12) x Pbwhere N is the number of calendar months which have elapsed from the Engine Price base year and month up to and including the month of delivery, both as shown in Table 13 of the Purchase Agreement. |
|--------|----|--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

|   | L  = | A value determined using the U.S. Department of Labor, Bureau of Labor Statistics "Employment Cost Index Wages and Salaries for Aircraft Manufacturing (BLS series ID ciu2023211000000i)”, base 100 = December 2005, calculated as a 3-month arithmetic average of the released values (expressed as a decimal and rounded to the nearest tenth) using the values for the 12th, 13th, and 14th months prior to the month of scheduled Aircraft delivery, then multiplied by sixty-five percent (65%) (rounded to the nearest thousandth). |
|--------|----------------|-------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

|   | ICI  = | A value determined using the U.S. Department of Labor, Bureau of Labor Statistics "Producer Prices and Price Index - Industrial Commodities Index (BLS series ID wpu03thru15)", base 100 = Calendar year 1982, calculated as a 3 month arithmetic average of the released monthly values (expressed as a decimal and rounded to the nearest hundredth) using the values for the 12th, 13th and 14th months prior to the month of scheduled Aircraft delivery, then multiplied by thirty-five percent (35%) (rounded to the nearest thousandth). |
|--------|------------------|-------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

----

| NOTE: | The factor (CPI divided by the base year index) by which the Engine Price is to be multiplied will be expressed as a decimal and rounded to the nearest thousandth.  Any rounding of a number, as required under this Supplemental Exhibit EE1 with respect to escalation of the Engine Price, will be accomplished as follows:  if the first digit of the portion to be dropped from the number to be rounded is five or greater, the preceding digit will be raised to the next higher number. |
|-------|----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

----

----

----

|   |   P = | Airframe Price plus the price of the Optional Features (as set forth in Table 13 of this Purchase Agreement). |
|--------|-----------------|---------------------------------------------------------------------------------------------------------------|

----

| Note: | i. | In determining the values of L and M, all calculations and resulting values will be expressed as a decimal rounded to the nearest ten-thousandth. |
|-------|----|---------------------------------------------------------------------------------------------------------------------------------------------------|

|   | ii. | .65 is the numeric ratio attributed to labor in the Airframe Price Adjustment formula. |
|--------|-----|----------------------------------------------------------------------------------------|

|   | iii. | .35 is the numeric ratio attributed to materials in the Airframe Price Adjustment formula. |
|--------|------|--------------------------------------------------------------------------------------------|

|   | iv. | The denominators (base year indices) are the actual average values reported by the U.S. Department of Labor, Bureau of Labor Statistics.  The actual average values are calculated as a 3-month arithmetic average of the released monthly values (expressed as a decimal and rounded to the nearest tenth) using the values for the [***].  The applicable base year and corresponding denominator is provided by Boeing in Table 13 of this Purchase Agreement. |
|--------|-----|---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

|   | v. | The final value of Pa will be rounded to the nearest dollar. |
|--------|----|--------------------------------------------------------------|

|   | vi. | The Airframe Price Adjustment will not be made if it will result in a decrease in the Aircraft Basic Price. |
|--------|-----|-------------------------------------------------------------------------------------------------------------|

----

|   | Note: | i. | The values released by the Bureau of Labor Statistics and available to Boeing 30 days prior to the first day of the scheduled delivery month of an Aircraft will be used to determine the ECI and CPI values for the applicable months (including those noted as preliminary by the Bureau of Labor Statistics) to calculate the Airframe Price Adjustment for the Aircraft invoice at the time of delivery.  The values will be considered final and no Airframe Price Adjustments will be made after Aircraft delivery for any subsequent changes in published Index values, subject always to Paragraph 2.4 above. |
|--------|-------|----|--------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

|   | ii. | The maximum number of digits to the right of the decimal after rounding utilized in any part of the Airframe Price Adjustment equation will be 4, where rounding of the fourth digit will be increased to the next highest digit when the 5th digit is equal to 5 or greater. |
|--------|-----|-------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

----

| Subject: | Special Matters Letter Applicable to the 2012 Accelerated Aircraft |
|----------|--------------------------------------------------------------------|

| Reference: | Purchase Agreement No. 2126 (the Purchase Agreement) between The Boeing Company (Boeing) and LAN Airlines S.A. (Customer) relating to Model 767-316F, Model 767-38EF and Model 767-316ER aircraft (hereinafter referred to as "Aircraft") |
|------------|----------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------|

| 13. | Definitions. |
|-----|--------------|

| 14. | Export License. |
|-----|-----------------|

| 15. | Warranty Modification. |
|-----|------------------------|

----

| 16.  | Credit Memoranda for the 2012 Accelerated Aircraft. |
|-----------|-----------------------------------------------------|

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

| 17. | [***] |
|-----|-------|

| 18. | Assignment. |
|-----|-------------|

|   | i.  | bound by a customary confidentiality agreement; |
|--------|----------|-------------------------------------------------|

|   | ii.  | neither an airplane manufacturer nor an airline;  and |
|--------|-----------|------------------------------------------------------------|

|   | iii. | responding to a Customer request for proposals to provide financing of Aircraft pursuant to the Purchase Agreement, including pre-delivery payment financing |
|--------|------|--------------------------------------------------------------------------------------------------------------------------------------------------------------|

----

| 19.  | 16G Seat Requirement Credit Memorandum. |
|-----------|-----------------------------------------|

| Scheduled Delivery Month |   | Due Date for Customer Notification of 16G Record Option |
|------------------------------------|--------|-------------------------------------------------------------------------------------------------|
| June 2012                          |   | 1st of November of 2010                                                                         |
| July 2012                          |   | 1st of November of 2011                                                                         |
| October  2012            |   | 1st of February of 2011                                                                         |

| 20. | [***] |
|-----|-------|

| 21. | Confidentiality. |
|-----|------------------|

----

| Very truly yours,  |             |   |
|--------------------|------------------|--------|
|               |             |   |
| THE BOEING COMPANY |             |   |
|               |             |   |
| By:                |             |   |   |
| Irma L. Krueger    |             |   |
|               |             |   |
| Its:               | Attorney-In-Fact |   |   |

----

| LAN AIRLINES S.A.               |                                  |   |
|---------------------------------|---------------------------------------|--------|
|                            |                                  |   |
| By:                             |                                  |   |   |
| Mr. Roberto Alvo                |                                  |   |
|                            |                                  |   |
| Its:                            | Sr. Vice President Strategic Planning |   |   |
|                            | & Corporate Development           |   |   |
|                            |                                  |   |
| By:                             |                                  |   |   |
| Mr. Alejandro de la Fuente Goic |                                  |   |
|                            |                                  |   |
| Its:                            | Chief Financial Officer               |   |   |

----