Document:

Exhibit 4.1.4

AMENDMENT No. 6

TO THE

SECOND A320 FAMILY PURCHASE AGREEMENT

BETWEEN

LAN AIRLINES S.A.

AND

AIRBUS S.A.S.

 

  

 

  

 

This amendment No. 6 to the Second A320 Family Purchase Agreement (as defined below) is entered into as of May 2010, by and between

AIRBUS S.A.S., having its principal office at:

1 Rond-Point Maurice Bellonte

31707 BLAGNAC  -  CEDEX

FRANCE

(hereinafter referred to as the "Seller") of the one part

AND

LAN AIRLINES S.A. having its principal office at :

Edificio Huidobro

Avenida Presidente Riesco 5711– 20th Floor

Las Condes

SANTIAGO

CHILE

 (hereinafter referred to as the "Buyer") of the other part.

The Buyer and the Seller being collectively referred to as the "Parties" and individually as a "Party"

 

  

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WHEREAS

	
A

	
The Buyer and the Seller entered into an A320 family purchase agreement dated March 20th, 1998 covering the purchase by the Buyer and the sale by the Seller of twenty (20) A320 family aircraft bearing rank numbers 1 to 20. By an amendment No.1 to such purchase agreement, entered into by the Buyer and the Seller on February 24th, 2000 the number of A320 family aircraft to be purchased by the Buyer pursuant to such purchase agreement was increased to twenty five (25), with the additional five (5) A320 family aircraft bearing rank numbers 21 to 25. Such twenty five (25) A320 family aircraft are hereinafter referred to as the “Original A320 Family Aircraft”, and such purchase agreement, amendment No.1, and all exhibits, appendices and letter agreements thereto are together referred to as the “Original A320 Family Purchase Agreement”.

	
B

	
The Buyer and the Seller entered into a deed of amendment and restatement of the Original A320 Family Purchase Agreement, dated August 2nd, 2000, dividing the Original A320 Family Purchase Agreement into two (2) separate purchase agreements, the first agreement concerning the Original A320 Family Aircraft bearing rank numbers 1 to 20, and the second agreement concerning the Original A320 Family Aircraft bearing rank numbers 21 to 25. The second agreement as supplemented with all exhibits and appendices thereto is hereinafter referred to as the “Second A320 Family Purchase Agreement”.

	
C

	
The Buyer and the Seller entered into an amendment No.1 to the Second A320 Family Purchase Agreement dated November 14th 2003 (the “Amendment No.1”) modifying certain provisions of the Second A320 Family Purchase Agreement.

	
D

	
The Buyer and the Seller entered into an amendment No.2 to the Second A320 Family Purchase Agreement dated October 4th, 2005 (the “Amendment No.2”) covering the purchase by the Buyer and the sale by the Seller of twenty five (25) additional firm A320 family aircraft comprising twenty (20) A318-100, one (1) A319-100 and four (4) A320-200 aircraft type (the ”Additional Aircraft”).

	
E

	
The Buyer and the Seller entered into an amendment No.3 to the Second A320 Family Purchase Agreement dated March 6th, 2007 (the “Amendment No.3”) covering the conversion of fifteen (15) Option Aircraft (as defined in the Amendment No.2) into firmly ordered Converted Aircraft (as defined in Amendment No.3).

	
F

	
The Buyer and the Seller entered into an amendment No. 4 to the Second A320 Family Purchase Agreement dated June 11th, 2008 (the “Amendment No.4”) covering the conversion of five (5) A318-100 Additional Aircraft bearing rank Nos. 26 to 30 as set forth in Amendment No.2 and three (3) A318-100 Converted Aircraft bearing rank Nos. 37, 40 and 43 as set forth in Amendment No.3, into A319 aircraft type.

	
G

	
The Buyer and the Seller entered into an amendment No. 5 to the Second A320 Family Purchase Agreement dated December 23rd, 2009 (the “Amendment No.5”) covering the order of thirty (30) incremental A319-100 and A320-200 aircraft and amending certain provisions of the Second A320 Family Purchase Agreement.

	
H

	
[***]

	
I

	
The Buyer and the Seller wish to enter into this amendment No. 6 to the Second A320 Family Purchase Agreement (the “Amendment No.6”) covering the conversion of the aircraft type of three (3) A319-100 First Batch of Incremental Aircraft (as defined in the Amendment No.5) into firmly ordered A320-200 First Batch Incremental Aircraft and the advancement of the scheduled delivery positions of Two (2) Aircraft from the First Batch of Incremental Aircraft and Eleven (11) Aircraft from the Second Batch of Incremental Aircraft (as defined in the Amendment No.5).

 

  

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NOW IT IS HEREBY AGREED AS FOLLOWS :

	
0.

	
DEFINITIONS

	
0.1

	
The terms "herein", "hereof" and "hereunder" and words of similar import refer to this Amendment N° 6 and capitalized terms used herein and not otherwise defined in this Amendment N° 6 shall have the meanings assigned thereto in the  Purchase Agreement (as defined below).

	
0.2

	
Purchase Agreement:       means the Second A320 Family Purchase Agreement together with Amendments No. 1 to 5 thereto.

	
1.

	
SCOPE

	
1.1

	
The Buyer has requested and the Seller has agreed to hereby convert the aircraft type of three (3) Aircraft from the First Batch of Incremental Aircraft and advance the Scheduled Delivery Quarters of Two (2) Aircraft from the First Batch of Incremental Aircraft and Eleven (11) Aircraft from the Second Batch of Incremental Aircraft upon the terms and conditions contained in this Amendment No.6.

	
1.2

	
The Parties agree to amend certain provisions of the Second A320 Family Purchase Agreement pursuant to the terms and conditions set out in this Amendment No.6.

	
1.3

	
The Parties hereby agree that in the event of any inconsistency between the terms and conditions of the Second A320 Family Purchase Agreement (save for Amendments Nos.1 to 5) and those of the Original A320 Family Purchase Agreement, then the Original A320 Family Purchase Agreement shall prevail to the extent of such inconsistency.

 

  

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2.

	
DELIVERY SCHEDULE

Pursuant to the Buyer’s request, the Scheduled Delivery Quarters of two (2) Aircraft from the First Batch of Incremental Aircraft and eleven (11) Aircraft from the Second Batch of Incremental Aircraft shall be amended as set forth in the table here below :

	
Rank

number

	 	
 

 

Aircraft

Type

	 	
Original Scheduled Delivery Quarters

	 	
Revised

Scheduled

Delivery Months /

Quarters

	 	
Aircraft batch

	
54

	 	
A319-100

	 	
2nd Quarter [***]

	 	
[***]

	 	
First Batch of Incremental Aircraft

	
55

	 	
A320-200

	 	
4th Quarter [***]

	 	
[***]

	 	
First Batch of Incremental Aircraft

	
65

	 	
A320-200

	 	
4th Quarter [***]

	 	
3rd Quarter 2012

	 	
Second Batch of Incremental Aircraft

	
66

	 	
A319-100

	 	
1st Quarter [***]

	 	
[***]

	 	
Second Batch of Incremental Aircraft

	
67

	 	
A320-200

	 	
2nd Quarter [***]

	 	
3rd Quarter [***]

	 	
Second Batch of Incremental Aircraft

	
68

	 	
A319-100

	 	
3rd Quarter [***]

	 	
4th Quarter [***]

	 	
Second Batch of Incremental Aircraft

	
69

	 	
A320-200

	 	
3rd Quarter [***]

	 	
4th Quarter [***]

	 	
Second Batch of Incremental Aircraft

	
70

	 	
A320-200

	 	
4th Quarter [***]

	 	
4th Quarter [***]

	 	
Second Batch of Incremental Aircraft

	
71

	 	
A320-200

	 	
4th Quarter [***]

	 	
1st Quarter [***]

	 	
Second Batch of Incremental Aircraft

	
72

	 	
A319-100

	 	
1st Quarter [***]

	 	
1st Quarter [***]

	 	
Second Batch of Incremental Aircraft

	
73

	 	
A319-100

	 	
3rd Quarter [***]

	 	
2nd Quarter [***]

	 	
Second Batch of Incremental Aircraft

	
74

	 	
A320-200

	 	
4th Quarter [***]

	 	
3rd Quarter [***]

	 	
Second Batch of Incremental Aircraft

	
75

	 	
A320-200

	 	
4th Quarter [***]

	 	
4th Quarter [***]

	 	
Second Batch of Incremental Aircraft

It is furthermore agreed by the Parties that the provisions and obligations set forth in article 9.1.5 of clause 2.1.1 to the Amendment No 5 shall herewith be considered fulfilled in their entirety and neither Party shall have any further rights and or obligations under the Amendment No 5 toward the other Party with respect thereto.

	
3.

	
AIRCRAFT TYPE CONVERSION

Pursuant to the Buyer’s request to convert the aircraft type of three (3) Aircraft from the First Batch of Incremental Aircraft, the Parties hereby agree that the aircraft type of First Batch of Incremental Aircraft with rank numbers 48, 49 and 50, as set forth in article 9.1.2 of clause 2.1.1 of Amendment No.5 shall hereby be amended as set out in the table here below:

 

  

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Rank

number

	 	
Scheduled

Delivery Months

	 	
Original

Aircraft

type

	 	
Revised

Aircraft

type

	 	
Aircraft batch

	
48

	 	
[***]

	 	
A319-100

	 	
A320-200

	 	
First Batch of Incremental Aircraft

	
49

	 	
[***]

	 	
A319-100

	 	
A320-200

	 	
First Batch of Incremental Aircraft

	
50

	 	
[***]

	 	
A319-100

	 	
A320-200

	 	
First Batch of Incremental Aircraft

 

	
4.

	
INCREMENTAL AIRCRAFT

For the avoidance of doubt the quantity per aircraft type as defined in clause 1.1 of Amendment 5 shall hereby be amended to read:

QUOTE

	
  

	
1.1

	
The Seller shall sell and deliver and the Buyer shall buy and take delivery of ten (10) A319-100 aircraft and twenty (20) A320-200 aircraft (respectively the “A319 Aircraft” and the “A320 Aircraft”) upon the terms and conditions contained in this Amendment No.5 (hereinafter for the purposes of this Amendment N°5 collectively the “Incremental Aircraft”).

UNQUOTE

	
5.

	
PREDELIVERY PAYMENTS

The parties hereby agree, that upon signature of this Amendment N° 6, the Buyer shall with respect to the First Batch of Incremental Aircraft with rank numbers 48, 49 and 50 and Second Batch of Incremental Aircraft with rank numbers 54 and 55 and from 65 to 75, [***] Predelivery Payments due in accordance with the Predelivery Payment schedule set out in Clause 5 of the Second A320 Family Purchase Agreement, as replaced by Letter Agreements No.1A and 1B to Amendment No.5.

	
6.

	
AMENDMENT AND LETTER AGREEMENT STATUS

It is hereby agreed by the Parties that the letters agreements n° 1, 2, 3, 4, 5, 6, 7, 8A, 8B, 8C, 9 and 10 to the Second A320 Family Aircraft Purchase Agreement and the Amendments 1, 2, 3 and 4 to the Second A320 Family Aircraft Purchase Agreement shall not in any way be applicable to the Incremental Aircraft unless expressly stated otherwise in Amendment No. 5 or this Amendment N° 6.

	
7.

	
EFFECT OF THE AMENDMENT

	
7.1

	
This Amendment No. 6 contains the entire agreement between the Parties with respect to the subject matter hereof and supersedes any previous understanding, commitments or representations whatsoever, whether oral or written.

	
7.2

	
The Purchase Agreement shall be deemed amended to the extent provided in this Amendment No. 6 and, except as specifically amended hereby, shall continue in full force and effect in accordance with its original terms.

 

  

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7.3

	
The Parties agree that this Amendment No. 6 shall constitute an integral, non-severable part of the Purchase Agreement and be governed by all of its provisions. For the sake of clarity, Amendment 5 and its Appendices, Letter Agreements and Side Letter No.1 shall continue to apply to the First Batch of Incremental Aircraft with rank numbers 48, 49 and 50 and Second Batch of Incremental Aircraft with rank numbers 54 and 55 and from 65 to 75, unless expressly stated otherwise in this Amendment N° 6.

	
7.4

	
In the event of any inconsistency between the terms and conditions of the Purchase Agreement and those of the present Amendment N°6, the latter shall prevail to the extent of such inconsistency, whereas the part not concerned by such inconsistency shall remain in full force and effect.

	
7.5

	
This Amendment N° 6 will not be modified or varied except by an instrument in writing executed by both Parties.

	
7.6

	
Each of the Parties hereto agree that the provisions of this Amendment No. 6 are personal to it and will not without the prior written consent of the other Parties disclose such information to any other Party. [***]

	
7.7

	
The Parties agree that clause 21 of the Second A320 Family Purchase Agreement shall govern the assignability and transferability of each Party’s rights and obligations under this Amendment No.6.

	
7.8

	
This Amendment N°6 may be signed by the Parties hereto in separate counterparts, each of which when so signed and delivered will be an original, but all such counterparts will together constitute but one and the same instrument.

	
7.9

	
This Amendment N°6 shall be governed by and construed in accordance with the laws of England.

 

  

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 IN WITNESS WHEREOF this Amendment No. 6 to the Second A320 Family Purchase Agreement was duly entered into the day and year first above written.

	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S. A. S.

	  	  
	
Name :

	
Name :

	  	  
	
Title :

	
Title :

LAN AIRLINES S.A.

By           :

Its           :

Date           :

 

  

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AMENDMENT No. 7

 

TO THE

 

SECOND A320 FAMILY PURCHASE AGREEMENT

 

BETWEEN

 

LAN AIRLINES S.A.

 

AND

 

AIRBUS S.A.S.

 

A320F - LAN - AMDT 7 - Second A320 Family PA

Ref. CT1001125.2

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

 

  

9/180

  

 

This amendment No. 7 to the Second A320 Family Purchase Agreement (as defined below) is entered into as of May 2010, by and between

 

AIRBUS S.A.S., having its principal office at:

 

1 Rond-Point Maurice Bellonte

 

31707 BLAGNAC  -  CEDEX

 

FRANCE

 

(hereinafter referred to as the "Seller") of the one part

 

AND

 

LAN AIRLINES S.A. having its principal office at :

 

Edificio Huidobro

 

Avenida Presidente Riesco 5711– 20th Floor

 

Las Condes

 

A320F - LAN - AMDT 7 - Second A320 Family PA

Ref. CT1001125.2

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

 

  

10/180

  

 

SANTIAGO

 

CHILE

 

(hereinafter referred to as the "Buyer") of the other part.

 

The Buyer and the Seller being collectively referred to as the "Parties" and individually as a "Party"

 

A320F - LAN - AMDT 7 - Second A320 Family PA

Ref. CT1001125.2

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

 

  

11/180

  

 

WHEREAS

	
A

	
The Buyer and the Seller entered into an A320 family purchase agreement dated March 20th, 1998 covering the purchase by the Buyer and the sale by the Seller of twenty (20) A320 family aircraft bearing rank numbers 1 to 20. By an amendment No.1 to such purchase agreement, entered into by the Buyer and the Seller on February 24th, 2000 the number of A320 family aircraft to be purchased by the Buyer pursuant to such purchase agreement was increased to twenty five (25), with the additional five (5) A320 family aircraft bearing rank numbers 21 to 25. Such twenty five (25) A320 family aircraft are hereinafter referred to as the “Original A320 Family Aircraft”, and such purchase agreement, amendment No.1, and all exhibits, appendices and letter agreements thereto are together referred to as the “Original A320 Family Purchase Agreement”.

 

	
B

	
The Buyer and the Seller entered into a deed of amendment and restatement of the Original A320 Family Purchase Agreement, dated August 2nd, 2000, dividing the Original A320 Family Purchase Agreement into two (2) separate purchase agreements, the first agreement concerning the Original A320 Family Aircraft bearing rank numbers 1 to 20, and the second agreement concerning the Original A320 Family Aircraft bearing rank numbers 21 to 25. The second agreement as supplemented with all exhibits and appendices thereto is hereinafter referred to as the “Second A320 Family Purchase Agreement”.

 

	
C

	
The Buyer and the Seller entered into an amendment No.1 to the Second A320 Family Purchase Agreement dated November 14th 2003 (the “Amendment No.1”) modifying certain provisions of the Second A320 Family Purchase Agreement.

 

	
D

	
The Buyer and the Seller entered into an amendment No.2 to the Second A320 Family Purchase Agreement dated October 4th, 2005 (the “Amendment No.2”) covering the purchase by the Buyer and the sale by the Seller of twenty five (25) additional firm A320 family aircraft comprising twenty (20) A318-100, one (1) A319-100 and four (4) A320-200 aircraft type (the ”Additional Aircraft”).

 

	
E

	
The Buyer and the Seller entered into an amendment No.3 to the Second A320 Family Purchase Agreement dated March 6th, 2007 (the “Amendment No.3”) covering the conversion of fifteen (15) Option Aircraft (as defined in the Amendment No.2) into firmly ordered Converted Aircraft (as defined in Amendment No.3).

 

	
F

	
The Buyer and the Seller entered into an amendment No. 4 to the Second A320 Family Purchase Agreement dated June 11th, 2008 (the “Amendment No.4”) covering the conversion of five (5) A318-100 Additional Aircraft bearing rank Nos. 26 to 30 as set forth in Amendment No.2 and three (3) A318-100 Converted Aircraft bearing rank Nos. 37, 40 and 43 as set forth in Amendment No.3, into A319 aircraft type.

 

A320F - LAN - AMDT 7 - Second A320 Family PA

Ref. CT1001125.2

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

 

  

12/180

  

	
G

	
The Buyer and the Seller entered into an amendment No. 5 to the Second A320 Family Purchase Agreement dated December 23rd, 2009 (the “Amendment No.5”) covering the order of thirty (30) incremental A319-100 and A320-200 aircraft and amending certain provisions of the Second A320 Family Purchase Agreement.

 

	
H

	
[***]

 

	
I

	
The Buyer and the Seller entered into an amendment No. 6 to the Second A320 Family Purchase Agreement (the “Amendment No.6”) covering the conversion of the aircraft type of three (3) A319-100 First Batch of Incremental Aircraft (as defined in the Amendment No.5) into firmly ordered A320-200 First Batch Incremental Aircraft and the advancement of the scheduled delivery positions of Two (2) Aircraft from the First Batch of Incremental Aircraft and Eleven (11) Aircraft from the Second Batch of Incremental Aircraft (as defined in the Amendment No.5).

 

	
J

	
The Buyer and the Seller wish to enter into an amendment No. 7 to the Second A320 Family Purchase Agreement (the “Amendment No.7”) covering the advancement of the scheduled delivery positions of Three (3) Converted Aircraft.

 

NOW IT IS HEREBY AGREED AS FOLLOWS :

 

A320F - LAN - AMDT 7 - Second A320 Family PA

Ref. CT1001125.2

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

 

  

13/180

  

 

	
0.

	
DEFINITIONS

	
0.1

	
The terms "herein", "hereof" and "hereunder" and words of similar import refer to this Amendment N° 7 and capitalized terms used herein and not otherwise defined in this Amendment N° 7 shall have the meanings assigned thereto in the  Purchase Agreement (as defined below).

 

	
0.2

	
Purchase Agreement:     means the Second A320 Family Purchase Agreement together with Amendments No. 1 to 6 thereto.

	
1.

	
SCOPE

 

	
1.4

	
The Buyer has requested and the Seller has agreed to hereby advance the Scheduled Delivery Months of Three (3) Converted Aircraft upon the terms and conditions contained in this Amendment No.7.

 

	
1.5

	
The Parties agree to amend certain provisions of the Second A320 Family Purchase Agreement pursuant to the terms and conditions set out in this Amendment No.7.

 

	
1.6

	
The Parties hereby agree that in the event of any inconsistency between the provisions of the Second A320 Family Purchase Agreement which have not been amended by Amendments Nos. 1 to 6 and those of the Original A320 Family Purchase Agreement, then the Original A320 Family Purchase Agreement shall prevail to the extent of such inconsistency.

 

A320F - LAN - AMDT 7 - Second A320 Family PA

Ref. CT1001125.2

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

 

  

14/180

  

 

	
2.

	
DELIVERY SCHEDULE

 

Pursuant to the Buyer’s request, the Scheduled Delivery Months of three (3) Converted Aircraft shall be amended as set forth in the table here below :

	
Rank

number

	  	
Aircraft

Type

	  	
Original Scheduled

Delivery Months

	  	
Revised

Scheduled

Delivery Months

	  	
Aircraft Batch

	
42

	  	
A319-100

	  	
[***]

	  	
[***]

	  	
Converted Aircraft

	
44

	  	
A320-200

	  	
[***]

	  	
[***]

	  	
Converted Aircraft

	
45

	
  

	
A320-200

	
  

	
[***]

	
  

	
[***]

	
  

	
Converted Aircraft

	
3.

	
PREDELIVERY PAYMENTS

 

The Parties hereby agree that, in [***], the Buyer shall with respect to the Converted Aircraft with rank number 45 [***] of the Predelivery Payments due in accordance with the Predelivery Payment schedule set out in Clause 5 of the Second A320 Family Purchase Agreement, as amended by Amendment No.2.

 

	
4.

	
EFFECT OF THE AMENDMENT

 

	
4.1

	
This Amendment No. 7 contains the entire agreement between the Parties with respect to the subject matter hereof and supersedes any previous understanding, commitments or representations whatsoever, whether oral or written.

 

	
4.2

	
The Purchase Agreement shall be deemed amended to the extent provided in this Amendment No. 7 and, except as specifically amended hereby, shall continue in full force and effect in accordance with its original terms.

 

	
4.3

	
The Parties agree that this Amendment No. 7 shall constitute an integral, non-severable part of the Purchase Agreement and be governed by all of its provisions.

 

A320F - LAN - AMDT 7 - Second A320 Family PA

Ref. CT1001125.2

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

 

  

15/180

  

 

	
4.4

	
In the event of any inconsistency between the terms and conditions of the Purchase Agreement and those of the present Amendment N°7, the latter shall prevail to the extent of such inconsistency, whereas the part not concerned by such inconsistency shall remain in full force and effect.

 

	
4.5

	
This Amendment N° 7 will not be modified or varied except by an instrument in writing executed by both Parties.

 

A320F - LAN - AMDT 7 - Second A320 Family PA

Ref. CT1001125.2

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

 

  

16/180

  

 

	
4.6

	
Each of the Parties hereto agree that the provisions of this Amendment No. 7 are personal to it and will not without the prior written consent of the other Parties disclose such information to any other Party. [***]

 

	
4.7

	
The Parties agree that clause 21 of the Second A320 Family Purchase Agreement shall govern the assignability and transferability of each Party’s rights and obligations under this Amendment No.7.

	
4.8

	
This Amendment N°7 may be signed by the Parties hereto in separate counterparts, each of which when so signed and delivered will be an original, but all such counterparts will together constitute but one and the same instrument.

 

	
4.9

	
This Amendment N°7 shall be governed by and construed in accordance with the laws of England.

 

A320F - LAN - AMDT 7 - Second A320 Family PA

Ref. CT1001125.2

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

 

  

17/180

  

 

IN WITNESS WHEREOF this Amendment No. 7 to the Second A320 Family Purchase Agreement was duly entered into the day and year first above written.

	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S. A. S.

	  	  
	
Name :

	
Name :

	  	  
	
Title :

	
Title :

 

LAN AIRLINES S.A.

By           :

Its           :

Date           :

A320F - LAN - AMDT 7 - Second A320 Family PA

Ref. CT1001125.2

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

 

  

18/180

  

 

AMENDMENT No. 8

 

TO THE

 

SECOND A320 FAMILY PURCHASE AGREEMENT

 

BETWEEN

 

LAN AIRLINES S.A.

 

AND

 

AIRBUS S.A.S.

 

A320F - LAN - AMDT 8 - Second A320 Family PA

Ref. CT1003497

***This information is subject to confidential treatment and has been omitted and filed separately with the commission

 

 

19/180

 

  

This amendment No. 8 to the Second A320 Family Purchase Agreement (as defined below) is entered into as of          September 2010, by and between

 

AIRBUS S.A.S., having its principal office at:

1 Rond-Point Maurice Bellonte

31707 BLAGNAC  -  CEDEX

FRANCE

 

(hereinafter referred to as the "Seller") of the one part

 

AND

 

LAN AIRLINES S.A. having its principal office at :

Edificio Huidobro

Avenida Presidente Riesco 5711– 20th Floor

Las Condes

SANTIAGO

CHILE

 

(hereinafter referred to as the "Buyer") of the other part.

 

The Buyer and the Seller being collectively referred to as the "Parties" and individually as a "Party"

 

A320F - LAN - AMDT 8 - Second A320 Family PA

Ref. CT1003497

***This information is subject to confidential treatment and has been omitted and filed separately with the commission

 

  

20/180

  

 

WHEREAS

 

	
A

	
The Buyer and the Seller entered into an A320 family purchase agreement dated March 20th, 1998 covering the purchase by the Buyer and the sale by the Seller of twenty (20) A320 family aircraft bearing rank numbers 1 to 20. By an amendment No.1 to such purchase agreement, entered into by the Buyer and the Seller on February 24th, 2000 the number of A320 family aircraft to be purchased by the Buyer pursuant to such purchase agreement was increased to twenty five (25), with the additional five (5) A320 family aircraft bearing rank numbers 21 to 25. Such twenty five (25) A320 family aircraft are hereinafter referred to as the “Original A320 Family Aircraft”, and such purchase agreement, amendment No.1, and all exhibits, appendices and letter agreements thereto are together referred to as the “Original A320 Family Purchase Agreement”.

 

	
B

	
The Buyer and the Seller entered into a deed of amendment and restatement of the Original A320 Family Purchase Agreement, dated August 2nd, 2000, dividing the Original A320 Family Purchase Agreement into two (2) separate purchase agreements, the first agreement concerning the Original A320 Family Aircraft bearing rank numbers 1 to 20, and the second agreement concerning the Original A320 Family Aircraft bearing rank numbers 21 to 25. The second agreement as supplemented with all exhibits and appendices thereto is hereinafter referred to as the “Second A320 Family Purchase Agreement”.

 

	
C

	
The Buyer and the Seller entered into an amendment No.1 to the Second A320 Family Purchase Agreement dated November 14th 2003 (the “Amendment No.1”) modifying certain provisions of the Second A320 Family Purchase Agreement.

 

	
D

	
The Buyer and the Seller entered into an amendment No.2 to the Second A320 Family Purchase Agreement dated October 4th, 2005 (the “Amendment No.2”) covering the purchase by the Buyer and the sale by the Seller of twenty five (25) additional firm A320 family aircraft comprising twenty (20) A318-100, one (1) A319-100 and four (4) A320-200 aircraft type (the ”Additional Aircraft”).

 

	
E

	
The Buyer and the Seller entered into an amendment No.3 to the Second A320 Family Purchase Agreement dated March 6th, 2007 (the “Amendment No.3”) covering the conversion of fifteen (15) Option Aircraft (as defined in the Amendment No.2) into firmly ordered Converted Aircraft (as defined in Amendment No.3).

 

	
F

	
The Buyer and the Seller entered into an amendment No. 4 to the Second A320 Family Purchase Agreement dated June 11th, 2008 (the “Amendment No.4”) covering the conversion of five (5) A318-100 Additional Aircraft bearing rank Nos. 26 to 30 as set forth in Amendment No.2 and three (3) A318-100 Converted Aircraft bearing rank Nos. 37, 40 and 43 as set forth in Amendment No.3, into A319 aircraft type.

 

	
G

	
The Buyer and the Seller entered into an amendment No. 5 to the Second A320 Family Purchase Agreement dated December 23rd, 2009 (the “Amendment No.5”) covering the order of thirty (30) incremental A319-100 and A320-200 aircraft and amending certain provisions of the Second A320 Family Purchase Agreement.

 

A320F - LAN - AMDT 8 - Second A320 Family PA

Ref. CT1003497

***This information is subject to confidential treatment and has been omitted and filed separately with the commission

 

  

21/180

  

 

	
H

	
[***]

 

	
I

	
The Buyer and the Seller entered into an amendment No. 6 to the Second A320 Family Purchase Agreement dated May 10th, 2010 (the “Amendment No.6”) covering the conversion of the aircraft type of three (3) A319-100 First Batch of Incremental Aircraft (as defined in the Amendment No.5) into firmly ordered A320-200 First Batch of Incremental Aircraft and the advancement of the scheduled delivery positions of Two (2) Aircraft from the First Batch of Incremental Aircraft and Eleven (11) Aircraft from the Second Batch of Incremental Aircraft (as defined in the Amendment No.5).

 

	
J

	
The Buyer and the Seller entered into an amendment No. 7 to the Second A320 Family Purchase Agreement dated May 19th, 2010 (the “Amendment No.7”) covering the advancement of the scheduled delivery positions of Three (3) Converted Aircraft.

 

	
K

	
The Buyer and the Seller wish to enter into an amendment No. 8 to the Second A320 Family Purchase Agreement (the “Amendment No.8”) covering (i) the advancement of the scheduled delivery positions of Two (2) Aircraft from the First Batch of Incremental Aircraft and Two (2) Aircraft from the Second Batch of Incremental Aircraft and (ii) the conversion of the aircraft type of one (1) A319-100 from the Second Batch of Incremental into firmly ordered A320-200 from the Second Batch of Incremental Aircraft.

 

NOW IT IS HEREBY AGREED AS FOLLOWS :

 

A320F - LAN - AMDT 8 - Second A320 Family PA

Ref. CT1003497

***This information is subject to confidential treatment and has been omitted and filed separately with the commission

 

  

22/180

  

 

	
0.

	
DEFINITIONS

	
0.1

	
The terms "herein", "hereof" and "hereunder" and words of similar import refer to this Amendment N° 8 and capitalized terms used herein and not otherwise defined in this Amendment N° 8 shall have the meanings assigned thereto in the  Purchase Agreement (as defined below).

 

	
0.2

	
Purchase Agreement:     means the Second A320 Family Purchase Agreement together with Amendments No. 1 to 7 thereto.

	
1.

	
SCOPE

 

	
1.7

	
The Buyer has requested and the Seller has agreed to hereby (i) advance the Scheduled Delivery Months of Two (2) Aircraft from the First Batch of Incremental Aircraft and Two (2) Aircraft from the Second Batch of Incremental Aircraft and (ii) convert the aircraft type of one (1) A319-100 from the Second Batch of Incremental Aircraft into firmly ordered A320-200 from the Second Batch Incremental Aircraft.

 

	
1.8

	
[***]

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2.

	
DELIVERY SCHEDULE

 

The Scheduled Delivery Months of Two (2) Aircraft from the First Batch of Incremental Aircraft and Two (2) Aircraft from the Second Batch of Incremental Aircraft shall be amended as set forth in the table here below :

 

	
Rank

number

	  	
Aircraft

Type

	  	  	  	
Original Scheduled

Delivery Months

	  	
Revised Scheduled

Delivery Months

	  	
Aircraft Batch

	  	  	  	  	  	  	  	  	  	  	  
	
53

	  	
A320-200

	  	  	  	
[***]

	  	
[***]

	  	
First Batch of Incremental Aircraft

	
55

	  	
A320-200

	  	  	  	
[***]

	  	
[***]

	  	
First Batch of Incremental Aircraft

	
62

	  	
A320-200

	  	  	  	
[***]

	  	
[***]

	  	
Second Batch of Incremental Aircraft

	
64

	
  

	
A320-200

	
  

	  	
  

	
[***]

	
  

	
[***]

	
  

	
Second Batch of Incremental Aircraft

	
3.

	
AIRCRAFT TYPE CONVERSION

Pursuant to the Buyer’s request to convert the aircraft type of one (1) Aircraft from the Second Batch of Incremental Aircraft, the Parties hereby agree that the aircraft type of Second Batch of Incremental Aircraft with rank number 66 shall hereby be amended as set out in the table here below:

	
Rank

number

	  	
Scheduled

Delivery Months

	  	
Original

Aircraft

type

	  	
Revised

Aircraft

type

	  	
Aircraft batch

	
66

	
  

	
[***]

	
  

	
A319-100

	
  

	
A320-200

	
  

	
Second Batch of Incremental Aircraft

It is furthermore agreed by the Parties that the provisions and obligations set forth in letter agreement No.5B to the Amendment No 5 in relation to the Second Batch of Incremental Aircraft shall herewith be considered fulfilled in their entirety with regard to the Aircraft with rank number 66 and neither Party shall have any further rights and or obligations under the Amendment No 5 toward the other Party with respect thereto.

	
4.

	
INCREMENTAL AIRCRAFT

The Parties agree to delete in its entirety clause 1.1 of Amendment No. 5, amended pursuant to clause 4 of Amendment No. 6, and replace it as follows

QUOTE

	
  

	
1.1

	
The Seller shall sell and deliver and the Buyer shall buy and take delivery of nine (9) A319-100 aircraft and twenty one (21) A320-200 aircraft (respectively the “A319 Aircraft” and the “A320 Aircraft”) upon the terms and conditions contained in this Amendment No.5 (hereinafter for the purposes of this Amendment N°5 collectively the “Incremental Aircraft”).

 

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UNQUOTE

	
5.

	
PREDELIVERY PAYMENTS

 

The Parties hereby agree, that upon signature of this Amendment N° 8, the Buyer shall with respect to the Aircraft from the First Batch of Incremental Aircraft with rank numbers 53 and 55 and the Aircraft from the Second Batch of Incremental Aircraft with rank numbers 62, 64 and 66, [***] Predelivery Payments due in accordance with the Predelivery Payment schedule set out in Clause 5 of the Second A320 Family Purchase Agreement, as amended by Amendment No.2.

 

	
6.

	
PROPULSION SYSTEMS

With reference to the Aircraft bearing rank numbers 46 to 75 the Parties hereby agree to delete in its entirety clause 1.3.2 of the Second A320 Family Purchase Agreement, amended by clause 3.1 of Amendment No.2 and by clause 2.2.3 of Amendment No.5, and replace it with the following quoted text:

 

	
  

	
1.3.2

	
[***]

 

	
7.

	
EFFECT OF THE AMENDMENT

 

	
7.1

	
This Amendment No. 8 contains the entire agreement between the Parties with respect to the subject matter hereof and supersedes any previous understanding, commitments or representations whatsoever, whether oral or written.

 

	
7.2

	
The Purchase Agreement shall be deemed amended to the extent provided in this Amendment No. 8 and, except as specifically amended hereby, shall continue in full force and effect in accordance with its original terms.

 

	
7.3

	
The Parties agree that this Amendment No. 8 shall constitute an integral, non-severable part of the Purchase Agreement and be governed by all of its provisions.

 

	
7.4

	
In the event of any inconsistency between the terms and conditions of the Purchase Agreement and those of the present Amendment No. 8, the latter shall prevail to the extent of such inconsistency, whereas the part not concerned by such inconsistency shall remain in full force and effect.

 

	
7.5

	
This Amendment N° 8 will not be modified or varied except by an instrument in writing executed by both Parties.

 

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7.6

	
Each of the Parties hereto agree that the provisions of this Amendment No. 8 are personal to it and will not without the prior written consent of the other Parties disclose such information to any other Party.  [***]

 

	
7.7

	
The Parties agree that clause 21 of the Second A320 Family Purchase Agreement shall govern the assignability and transferability of each Party’s rights and obligations under this Amendment No. 8.

	
7.8

	
This Amendment No. 8 may be signed by the Parties hereto in separate counterparts, each of which when so signed and delivered will be an original, but all such counterparts will together constitute but one and the same instrument.

 

	
7.9

	
This Amendment No. 8 shall be governed by and construed in accordance with the laws of England.

 

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IN WITNESS WHEREOF this Amendment No. 8 to the Second A320 Family Purchase Agreement was duly entered into the day and year first above written.

	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S. A. S.

	  	  
	
Name :

	
Name :

	  	  
	
Title :

	
Title :

 

LAN AIRLINES S.A.

By           :

Its           :

Date           :

 

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AMENDMENT No. 9

TO THE

SECOND A320 FAMILY PURCHASE AGREEMENT

BETWEEN

LAN AIRLINES S.A.

AND

AIRBUS S.A.S.

 

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This amendment No. 9 to the Second A320 Family Purchase Agreement (as defined below) is entered into as of December 2010, by and between

 

AIRBUS S.A.S., having its principal office at:

1 Rond-Point Maurice Bellonte

31707 BLAGNAC  -  CEDEX

FRANCE

(hereinafter referred to as the "Seller") of the one part

AND

LAN AIRLINES S.A. having its principal office at :

Edificio Huidobro

Avenida Presidente Riesco 5711– 20th Floor

Las Condes

SANTIAGO

CHILE

(hereinafter referred to as the "Buyer") of the other part.

The Buyer and the Seller being collectively referred to as the "Parties" and individually as a "Party"

 

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WHEREAS

	
A

	
The Buyer and the Seller entered into an A320 family purchase agreement dated March 20th, 1998 covering the purchase by the Buyer and the sale by the Seller of twenty (20) A320 family aircraft bearing rank numbers 1 to 20. By an amendment No.1 to such purchase agreement, entered into by the Buyer and the Seller on February 24th, 2000 the number of A320 family aircraft to be purchased by the Buyer pursuant to such purchase agreement was increased to twenty five (25), with the additional five (5) A320 family aircraft bearing rank numbers 21 to 25. Such twenty five (25) A320 family aircraft are hereinafter referred to as the “Original A320 Family Aircraft”, and such purchase agreement, amendment No.1, and all exhibits, appendices and letter agreements thereto are together referred to as the “Original A320 Family Purchase Agreement”.

	
B

	
The Buyer and the Seller entered into a deed of amendment and restatement of the Original A320 Family Purchase Agreement, dated August 2nd, 2000, dividing the Original A320 Family Purchase Agreement into two (2) separate purchase agreements, the first agreement concerning the Original A320 Family Aircraft bearing rank numbers 1 to 20, and the second agreement concerning the Original A320 Family Aircraft bearing rank numbers 21 to 25. The second agreement as supplemented with all exhibits and appendices thereto is hereinafter referred to as the “Second A320 Family Purchase Agreement”.

	
C

	
The Buyer and the Seller entered into an amendment No.1 to the Second A320 Family Purchase Agreement dated November 14th 2003 (the “Amendment No.1”) modifying certain provisions of the Second A320 Family Purchase Agreement.

	
D

	
The Buyer and the Seller entered into an amendment No.2 to the Second A320 Family Purchase Agreement dated October 4th, 2005 (the “Amendment No.2”) covering the purchase by the Buyer and the sale by the Seller of twenty five (25) additional firm A320 family aircraft comprising twenty (20) A318-100, one (1) A319-100 and four (4) A320-200 aircraft type (the ”Additional Aircraft”).

	
E

	
The Buyer and the Seller entered into an amendment No.3 to the Second A320 Family Purchase Agreement dated March 6th, 2007 (the “Amendment No.3”) covering the conversion of fifteen (15) Option Aircraft (as defined in the Amendment No.2) into firmly ordered Converted Aircraft (as defined in Amendment No.3).

	
F

	
The Buyer and the Seller entered into an amendment No. 4 to the Second A320 Family Purchase Agreement dated June 11th, 2008 (the “Amendment No.4”) covering the conversion of five (5) A318-100 Additional Aircraft bearing rank Nos. 26 to 30 as set forth in Amendment No.2 and three (3) A318-100 Converted Aircraft bearing rank Nos. 37, 40 and 43 as set forth in Amendment No.3, into A319 aircraft type.

	
G

	
The Buyer and the Seller entered into an amendment No. 5 to the Second A320 Family Purchase Agreement dated December 23rd, 2009 (the “Amendment No.5”) covering the order of thirty (30) incremental A319-100 and A320-200 aircraft (the ”Incremental  Aircraft”) and amending certain provisions of the Second A320 Family Purchase Agreement.

	
H

	
[***]

	
I

	
The Buyer and the Seller entered into an amendment No. 6 to the Second A320 Family Purchase Agreement dated May 10th, 2010 (the “Amendment No.6”) covering the conversion of the aircraft type of three (3) A319-100 First Batch of Incremental Aircraft (as defined in the Amendment No.5) into firmly ordered A320-200 First Batch Incremental Aircraft and the advancement of the scheduled delivery positions of Two (2) Aircraft from the First Batch of Incremental Aircraft and Eleven (11) Aircraft from the Second Batch of Incremental Aircraft (as defined in the Amendment No.5).

	
J

	
The Buyer and the Seller entered into an amendment No. 7 to the Second A320 Family Purchase Agreement dated May 19th, 2010 (the “Amendment No.7”) covering the advancement of the scheduled delivery positions of Three (3) Converted Aircraft.

 

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K

	
The Buyer and the Seller entered into an amendment No. 8 to the Second A320 Family Purchase Agreement dated September 23rd, 2010 (the “Amendment No.8”) covering (i) the advancement of the scheduled delivery positions of Two (2) Aircraft from the First Batch of Incremental Aircraft and Two (2) Aircraft from the Second Batch of Incremental Aircraft and (ii) the conversion of the aircraft type of one (1) A319-100 from the Second Batch of Incremental into firmly ordered A320-200 from the Second Batch Incremental Aircraft.

	
L

	
The Buyer and the Seller wish to enter into this amendment No. 9 to the Second A320 Family Purchase Agreement (the “Amendment No.9”) covering the order of fifty (50) incremental A319-100, A320-200 and A321-200 aircraft and amending certain provisions of the Second A320 Family Purchase Agreement.

	
M

	
[***]

NOW IT IS HEREBY AGREED AS FOLLOWS :

 

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2

	
DEFINITIONS

Capitalized terms used herein and not otherwise defined in this Amendment No. 9 will have the meanings assigned to them in the Purchase Agreement (as defined below).

The terms “herein,” “hereof,” and “hereunder” and words of similar import refer to this Amendment No.9.

	 Predelivery Payment	 	means the payment(s) determined in accordance with clause 5.2.1 of the Second A320 Family Purchase Agreement.
	  	  	  
	
Purchase Agreement

	  	
means the Second A320 Family Purchase Agreement together with Amendments N° 1 to 8 thereto.

	  	  	  
	
Specification

	  	
means the Standard Specification as modified by Specification Change Notices (SCN) to be selected after signature of this Amendment No.9 and which shall constitute the Buyer’s detailed Specification.

	  	  	  
	
Standard Specification

	  	
means for the A319 Aircraft, the Standard Specification Document N° [***] with the following design weights: MTOW: [***], MLW: [***], MZFW: [***] tons as set forth in Amendment No.5 and for which a preliminary list of SCNs is attached in Exhibit A of Appendix 1 to Amendment No.9,

	  	  	  
	
 

	  	
means for the A320 Aircraft, the Standard Specification Document N° [***] with the following design weights: MTOW: [***], MLW: [***], MZFW: [***] as set forth in Amendment No.5 and for which a preliminary list of SCNs is attached in Exhibit B of Appendix 1 to Amendment No.9,

	  	  	  
	  	
  

	
means for the A321 Aircraft, the Standard Specification Document N° [***] with the following design weights: MTOW: [***], MLW: [***], MZFW: [***], and for which a preliminary list of SCNs is attached in Exhibit C of Appendix 1 to Amendment No.9.

 

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3

	
SCOPE

	
1.1

	
The Seller shall sell and deliver and the Buyer shall buy and take delivery of six (6) A319-100 aircraft, thirty four (34) A320-200 aircraft and ten (10) A321-200 aircraft (respectively the “2010 A319 Aircraft”, the “2010 A320 Aircraft” and the “2010 A321 Aircraft”) upon the terms and conditions contained in this Amendment No.9 (hereinafter for the purposes of this Amendment N°9 collectively the “2010 Incremental Aircraft

	
1.2

	
The Parties agree to amend certain provisions of the Second A320 Family Purchase Agreement pursuant to the terms and conditions set out in this Amendment No.9.

	
1.3

	
All references to Aircraft in the Purchase Agreement and this Amendment N° 9 shall be deemed to refer to the 2010 Incremental Aircraft unless expressly stipulated otherwise herein.

	
1.4

	
The Parties hereby agree that in the event of any inconsistency between the terms and conditions of the Second A320 Family Purchase Agreement (save for Amendments Nos.1 to 8) and those of the Original A320 Family Purchase Agreement, then the Original A320 Family Purchase Agreement shall prevail to the extent of such inconsistency.

 

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2.

	
2010 INCREMENTAL AIRCRAFT

	
2.1

	
DELIVERY SCHEDULE

	
2.1.1

	
With reference to the Aircraft bearing rank numbers 37 to 125 the Parties hereby agree to delete clause 9.1 of the Second A320 Family Purchase Agreement as substituted by clause 2.1.1 of Amendment No.5, and as subsequently amended by clauses 2 and 3 of Amendment No.6, clause 2 of Amendment No.7 and clauses 2 and 3 of Amendment No.8 in its entirety and replace it with the following quoted text:

QUOTE

	
  

	
9.1

	
Delivery Schedule

	
  

	
9.1.1

	
Swap of Aircraft definition:

The Parties agree to swap the Aircraft definition between Aircraft bearing rank numbers 62 and 54. Therefore, the Aircraft bearing rank number 62 shall be defined as Aircraft from the First Batch of Incremental Aircraft and the Aircraft bearing rank number 54 shall be defined as Aircraft from the Second Batch of Incremental Aircraft as set out in the table here below.

	
  

	
9.1.2

	
Subject to the provisions of Clauses 2, 7, 8, 10 and 18 the Seller shall have the Aircraft ready for Delivery at the Delivery Location in accordance with the following schedule:

	
Scheduled Delivery Months or

Scheduled Delivery Quarters

	  	
Rank

number

	  	
Aircraft

type

	  	
Aircraft defined as

	
[***]

	  	
[***]

	  	  	  	  	  	  
	
[***]

	  	
[***]

	  	  	  	  	  	  
	
[***]

	  	
[***]

	  	
37

	  	
A320-200

	  	
Converted Aircraft

	
[***]

	  	
[***]

	  	
38

	  	
A320-200

	  	
Converted Aircraft

	
[***]

	  	
[***]

	  	
39

	  	
A319-100

	  	
Converted Aircraft

	
[***]

	  	
[***]

	  	
44

	  	
A320-200

	  	
Converted Aircraft

	
[***]

	  	
[***]

	  	
40

	  	
A320-200

	  	
Converted Aircraft

	
[***]

	  	
[***]

	  	
41

	  	
A319-100

	  	
Converted Aircraft

	
[***]

	  	
[***]

	  	
42

	  	
A319-100

	  	
Converted Aircraft

	
[***]

	  	
[***]

	  	
45

	  	
A320-200

	  	
Converted Aircraft

	
[***]

	  	
[***]

	  	
43

	  	
A320-200

	  	
Converted Aircraft

	
[***]

	  	
[***]

	  	
53

	  	
A320-200

	  	
First Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
55

	  	
A320-200

	  	
First Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
46

	  	
A320-200

	  	
First Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
47

	  	
A320-200

	  	
First Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
48

	  	
A320-200

	  	
First Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
49

	  	
A320-200

	  	
First Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
50

	  	
A320-200

	  	
First Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
51

	  	
A319-100

	  	
First Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
52

	  	
A320-200

	  	
First Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
62

	  	
A320-200

	  	
First Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
54

	  	
A319-100

	  	
Second Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
76

	  	
A319-100

	  	
2010 Incremental Aircraft

	
[***]

	  	
[***]

	  	
64

	  	
A320-200

	  	
Second Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
66

	  	
A320-200

	  	
Second Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
77

	  	
A320-200

	  	
2010 Incremental Aircraft

 

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[***]

	  	
[***]

	  	
65

	  	
A320-200

	  	
Second Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
78

	  	
A320-200

	  	
2010 Incremental Aircraft

	
[***]

	  	
[***]

	  	
67

	  	
A320-200

	  	
Second Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
79

	  	
A320-200

	  	
2010 Incremental Aircraft

	
[***]

	  	
[***]

	  	
80

	  	
A319-100

	  	
2010 Incremental Aircraft

	
[***]

	  	
[***]

	  	
68

	  	
A319-100

	  	
Second Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
69

	  	
A320-200

	  	
Second Batch of Incremental Aircraft

	
[***]

	  	
[***]

	  	
70

	  	
A320-200

	  	
Second Batch of Incremental Aircraft

	
2013

	  	
[***]

	  	
81

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
82

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
56

	  	
A320-200

	  	
Second Batch of Incremental Aircraft

	  	  	
[***]

	  	
71

	  	
A320-200

	  	
Second Batch of Incremental Aircraft

	  	  	
[***]

	  	
72

	  	
A319-100

	  	
Second Batch of Incremental Aircraft

	  	  	
[***]

	  	
83

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
84

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
85

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
57

	  	
A320-200

	  	
Second Batch of Incremental Aircraft

	  	  	
[***]

	  	
73

	  	
A319-100

	  	
Second Batch of Incremental Aircraft

	  	  	
[***]

	  	
58

	  	
A319-100

	  	
Second Batch of Incremental Aircraft

	  	  	
[***]

	  	
59

	  	
A319-100

	  	
Second Batch of Incremental Aircraft

	  	  	
[***]

	  	
74

	  	
A320-200

	  	
Second Batch of Incremental Aircraft

	  	  	
[***]

	  	
60

	  	
A320-200

	  	
Second Batch of Incremental Aircraft

	  	  	
[***]

	  	
75

	  	
A320-200

	  	
Second Batch of Incremental Aircraft

	
2014

	  	
[***]

	  	
61

	  	
A319-100

	  	
Second Batch of Incremental Aircraft

	  	  	
[***]

	  	
86

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
87

	  	
A321-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
88

	  	
A321-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
89

	  	
A319-100

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
90

	  	
A321-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
91

	  	
A321-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
63

	  	
A319-100

	  	
Second Batch of Incremental Aircraft

	  	  	
[***]

	  	
92

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
93

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
94

	  	
A321-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
95

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
96

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
97

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
98

	  	
A321-200

	  	
2010 Incremental Aircraft

	
2015

	  	
[***]

	  	
99

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
100

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
101

	  	
A321-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
102

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
103

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
104

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
105

	  	
A321-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
106

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
107

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
108

	  	
A320-200

	  	
2010 Incremental Aircraft

 

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[***]

	  	
109

	  	
A321-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
110

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
111

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
112

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
113

	  	
A321-200

	  	
2010 Incremental Aircraft

	
2016

	  	
[***]

	  	
114

	  	
A319-100

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
115

	  	
A319-100

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
116

	  	
A319-100

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
117

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
118

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
119

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
120

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
121

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
122

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
123

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	  	
[***]

	  	
124

	  	
A320-200

	  	
2010 Incremental Aircraft

	  	
  

	
[***]

	
  

	
125

	
  

	
A320-200

	
  

	
2010 Incremental Aircraft

	
  

	
9.1.2

	
[***]

	
  

	
9.1.3

	
[***]

UNQUOTE

	
2.1.2

	
For the avoidance of doubt the provisions set forth in clause 9.1 of the Second A320 Family Purchase Agreement as amended pursuant to clause 2 of Amendment No.1, clause 3.5 of Amendment No.2, clause 2 of Amendment No.3, clause 3.1 of Amendment No.4 and relevant to the Aircraft with rank numbers 1 to 30 shall hereby remain in full force and effect. Clause 9.1 of the Second A320 Family Purchase Agreement, as substituted by clause 2.1.1 of Amendment No.5, will apply to Aircraft with rank number 31 to 37.

 

	
2.2

	
SPECIFICATION

	
  

	
2.2.1

	
2010 Incremental Aircraft Specification

	
  

	
With respect to the 2010 Incremental Aircraft, the Parties hereby agree to delete clause 1.2.1 of the Second A320 Family Purchase Agreement in its entirety and replace it with the Standard Specification as defined in this Amendment N° 9, as may be modified or varied after the date of this Amendment N° 9 by the Specification Change Notices listed in:

	
  

	
- Exhibit A of Appendix 1 to Amendment No.9 for 2010 A319 Aircraft, and

	
  

	
- Exhibit B of Appendix 1 to Amendment No.9 for 2010 A320 Aircraft, and

	
  

	
- Exhibit C of Appendix 1 to Amendment No.9 for 2010 A321 Aircraft.

	
3.2.2

	
Clauses 1.2.2 and 1.2.3 of the Second A320 Family Purchase Agreement shall apply to the 2010 Incremental Aircraft.

	
3.2.3

	
With respect to the 2010 Incremental Aircraft, the Parties hereby agree to delete clauses 1.3, 1.3.1 and 1.3.2 of the Second A320 Family Purchase Agreement, amended by clause 3.1 of Amendment No.2 in its entirety and replace them with the following quoted text:

 

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QUOTE

	 	
1.3

	
The Airframe shall be equipped with a set of two (2) engines including nacelles and thrust reversers (the “Propulsion Systems”) as follows:

	
  

	
For the A319 Aircraft:

                                            CFM INTERNATIONAL 56-5B6/3                    (23,500 lb)

                                            or

                                            INTERNATIONAL AERO ENGINE V2524-A5 (23,500 lb)

For the A320 Aircraft:

                                           CFM INTERNATIONAL 56-5B4/3                    (27,000 lb)

                                           or

                                           INTERNATIONAL AERO ENGINE V2527E-A5 or V2527-A5         (26,500 lb)

For the A321 Aircraft:

                                            CFM INTERNATIONAL 56-5B3/3                    (33,000 lb)

                                            or

                                            INTERNATIONAL AERO ENGINE V2533                    (33,000 lb)

	
  

	
1.3.1

	
In the event the Buyer has not selected the Propulsion Systems for the Aircraft with rank numbers 76 to 125, as of the date of the Amendment No.9, the Buyer shall notify the Seller of such choice as follows;

	 	
  

	
- [***]

	 	
  

	
- [***]

 

	
  

	
1.3.2

	
Notwithstanding the foregoing the Buyer shall have the right to select the alternate Propulsion Systems Manufacturer, in each case as mentioned in the above Clause 1.3 for all or any of the Aircraft at any time, provided that such selection is notified in writing to the Seller not less than [***] prior to the first (1st) day of Scheduled Delivery Month of the relevant Aircraft and it being understood that it shall be the sole responsibility of the Buyer to inform, negotiate and conclude a settlement with the Propulsion Systems Manufacturer initially selected by the Buyer.

 UNQUOTE

	
3.

	
INCREMENTAL AIRCRAFT BASIC PRICES

It is hereby agreed that clauses 3.1 and 3.2 of the Second A320 Purchase Agreement shall not apply to the 2010 Incremental Aircraft and the Basic Prices of the 2010 Incremental Aircraft and the Final Price of the 2010 Incremental Aircraft are set forth in Appendix 2 to Amendment No.9.

	
4.

	
GENERAL PAYMENT TERMS

	
4.1

	
With respect to the 2010 Incremental Aircraft, the Parties agree to delete sub-clause 5.2.2 of the Second A320 Purchase Agreement in its entirety and replace it as follows:

 

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QUOTE

	
  

	
5.2.2

	
Balance of the Final Aircraft Price

	 	
5.2.2.1

	
The Balance of the Final Aircraft Price payable by the Buyer to the Seller on the Delivery Date shall be the Final Aircraft Price less the amount of Predelivery Payment received by the Seller on or before the Delivery Date.

	 	
5.2.2.2

	
Upon receipt of the Seller’s invoice and immediately prior to Delivery of the Aircraft, the Buyer shall pay to the Seller the Balance of the Final Aircraft Price.

 

	 	
5.2.2.3

	
Any Predelivery Payment received by the Seller shall constitute an instalment in respect of the Final Aircraft Price. The Seller shall be entitled to hold and use any such Predelivery Payment as absolute owner thereof (the “Status of Predelivery Payments”); subject only to the obligation of the Seller to: (i) deduct an amount equal to any such Predelivery Payments from the Final Aircraft Price when calculating the balance of the Final Aircraft Price; or (ii) pay to the Buyer (or to any assignee or transferee of the Buyer permitted by the terms of this Purchase Agreement) an amount equal to any such Predelivery Payments pursuant to any other provision of this Second A320 Family Purchase Agreement.

 

UNQUOTE

	
4.2

	
In conjunction with the transaction of the buy back from the Buyer of fifteen (15) Airbus A318-100 aircraft and with respect to the Incremental Aircraft, the  2010 Incremental Aircraft and the A330 Converted Aircraft, the Parties agree to delete sub-clauses 5.4.5 and 5.4.6 to the Second A320 Purchase Agreement amended by clause 4.2 of the Amendment No.5 and replace it as follows:

QUOTE

	 	
5.4.5

	
[***]

 

	 	
5.4.5.1

	
[***].

 

	 	
5.4.5.2

	
[***]:

 

	
  

	
(i)

	
[***] and unconditionally released to the Buyer upon such cure or waiver);

 

	
  

	
(ii)

	
[***].

 

UNQUOTE

	
  

	
5.

	
[***]

 

	
5.1

	
[***]: 

	
6.

	
Termination for Default

With respect to the Converted Aircraft, the Incremental Aircraft, the 2010 Incremental Aircraft and the A330 Converted Aircraft (if any), the Parties agree to insert sub-clause 20.5 to the Second A320 Purchase Agreement as follows:

 

QUOTE

[***].

 

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UNQUOTE

	
7.

	
AMENDMENT AND LETTER AGREEMENT STATUS

	
  

	
It is hereby agreed by the Parties that the letter agreements inserted or further amended or deleted to the Second A320 Family Aircraft Purchase Agreement and the Amendments 1, 2, 3, 4, 5, 6, 7 and 8 to the Second A320 Family Aircraft Purchase Agreement shall not in any way be applicable to the 2010 Incremental Aircraft as defined herein unless expressly stated otherwise in this Amendment N° 9.

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8.

	
EFFECT OF THE AMENDMENT

	
8.1

	
This Amendment No. 9 contains the entire agreement between the Parties with respect to the subject matter hereof and supersedes any previous understanding, commitments or representations whatsoever, whether oral or written.

	
8.2

	
The Purchase Agreement shall be deemed amended to the extent provided in this Amendment No. 9 and, except as specifically amended hereby, shall continue in full force and effect in accordance with its original terms.

	
8.3

	
The Parties agree that this Amendment No. 9 shall constitute an integral, non-severable part of the Purchase Agreement and be governed by all of its provisions.

	
8.4

	
In the event of any inconsistency between the terms and conditions of the Purchase Agreement and those of the present Amendment N°9, the latter shall prevail to the extent of such inconsistency, whereas the part not concerned by such inconsistency shall remain in full force and effect.

	
8.5

	
This Amendment N° 9 will not be modified or varied except by an instrument in writing executed by both Parties.

	
8.6

	
Each of the Parties hereto agree that the provisions of this Amendment No. 9 are personal to it and will not without the prior written consent of the other Parties disclose such information to any other Party. [***]

	
8.7

	
The Parties agree that clause 21 of the Second A320 Family Purchase Agreement shall govern the assignability and transferability of each Party’s rights and obligations under this Amendment No.9

	
8.8

	
This Amendment N°9 may be signed by the Parties hereto in separate counterparts, each of which when so signed and delivered will be an original, but all such counterparts will together constitute but one and the same instrument.

	
8.9

	
This Amendment N°9 shall be governed by and construed in accordance with the laws of England.

 

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 IN WITNESS WHEREOF this Amendment No. 9 to the Second A320 Family Purchase Agreement was duly entered into the day and year first above written.

	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S. A. S.

	  	  
	
Name :

	
Name :

	  	  
	
Title :

	
Title :

	
LAN AIRLINES S.A.

	  
	  	  
	
By

	
:

	  
	  	  	  
	
Its

	
:

	  
	  	  	  
	
Date

	
:

	  

 

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Appendix 1 - Exhibit A – A319 SCNs List

	
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Appendix 1 - Exhibit A – A319 SCNs List

	
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Appendix 1 - Exhibit A – A319 SCNs List

	
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Appendix 1 - Exhibit A – A319 SCNs List

	
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Appendix 1 - Exhibit A – A319 SCNs List

	
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Appendix 1 - Exhibit A – A319 SCNs List

	
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Appendix 1 - Exhibit A – A319 SCNs List

 

	
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Appendix 1 - Exhibit B– A320 SCNs List

	
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Appendix 1 - Exhibit B– A320 SCNs List

	
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Appendix 1 - Exhibit B– A320 SCNs List

	
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Appendix 1 - Exhibit B– A320 SCNs List

	
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Appendix 1 - Exhibit B– A320 SCNs List

	
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Appendix 1 - Exhibit B– A320 SCNs List

	
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Appendix 1 – Exhibit C – A321 SCNs List

	
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Appendix 1 – Exhibit C – A321 SCNs List

	
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Appendix 1 – Exhibit C – A321 SCNs List

	
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A320F - LAN - AMDT 9 - Second A320 Family PA

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57/180

  

Appendix 1 – Exhibit C – A321 SCNs List

	
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Appendix 2 – to Amendment 9

	
1.

	
With respect to the 2010 Incremental Aircraft, the provisions contained in clauses 3.1 and 3.2 of the Second A320 Family Purchase Agreement are hereby cancelled and replaced by the following quoted provisions:

QUOTE

	
3.1

	
PRICE OF [***]

The base price of each 2010 Incremental Aircraft (the “Aircraft Base Price”) is the sum of:

[***]

and is exclusive of any variation resulting from price revision provisions.

	
3.1.1

	
Airframe Base Price

The base price of the Airframe (the “Airframe Base Price”) is the sum of:

	
  

	
(i)

	
[***]

	
  

	
(ii)

	
[***]

	
3.1.2

	
Propulsion Systems Base Price

The base price of the Propulsion Systems (the “Propulsion Systems Base Price”) shall be, as applicable pursuant to Clauses 3.1.2.1 or 3.1.2.2, the base price of the Propulsion Systems selected by the Buyer.

	
3.1.2.1

	
The base price of a set of two (2) CFM INTERNATIONAL Propulsion Systems

[***]

	
  

	
at economic conditions prevailing for a theoretical delivery in [***].

Such base prices have been computed from the propulsion systems’ reference prices (the “Propulsion Systems Reference Price”) as defined in Exhibit B of Appendix 3 to Amendment No 9.

[***]

The CFM INTERNATIONAL Propulsion Systems Reference Prices have been established in accordance with the delivery conditions prevailing in January 2002 at Reference Composite Price Index of 148.84 and shall be subject to revision up to the Delivery Date of each 2010 Incremental Aircraft in accordance with the CFM INTERNATIONAL Price Revision Formula set out in Exhibit B of Appendix 3 of Amendment No.9.

	
3.1.2.2

	
The base price for a set of two (2) IAE Propulsion Systems is:

[***]

at economic conditions prevailing for a theoretical delivery in [***].

Such base prices have been computed from the Reference Prices of propulsion systems’ reference prices (the “Propulsion Systems Reference Price”) as defined in Exhibit C of Appendix 3 to Amendment No 9. :

[***]

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Appendix 2 – to Amendment 9

The INTERNATIONAL AERO ENGINES Propulsion Systems Reference Prices are expressed at theoretical delivery conditions prevailing in January 2006 and shall be subject to revision up to the Delivery Date of each 2010 Incremental Aircraft Delivery Date in accordance with the INTERNATIONAL AERO ENGINES Price Revision Formula set out in Exhibit C of Appendix 3 to Amendment No.9.

	
3.1.2.3

	
Seller confirms that the above-mentioned quotations as well as Propulsion Systems Manufacturer Price Revision Formulae (as set out in Clauses 4.2 and 4.3, as inserted by Exhibits B and C of Appendix 3 to Amendment No.9) are based upon information received from the respective Propulsion Systems Manufacturer and remain subject to any modification that might be imposed by the Propulsion Systems Manufacturer on the Seller. [***].

	
3.2

	
Final Aircraft Price

The final price of each [***] (the “Final Aircraft Price”) at Delivery shall be the sum of:

	
  

	
(i)

	
[***]

	
  

	
(ii)

	
[***];

	
  

	
(iii)

	
[***]

	
  

	
(iv)

	
[***].

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Appendix 3 Exhibit A – to Amendment 9

UNQUOTE

With respect to the 2010 Incremental Aircraft, the provisions contained in Clause 4.1 of the Second A320 Family Purchase Agreement are hereby cancelled and replaced by the following quoted provisions:

[***]

	
4.1.

	
[***]

	
4.1.1

	
[***]

[***].

	
4.1.2

	
[***]

[***].

	
4.1.3

	
[***]

[***]

	
4.1.4

	
[***]

[***]

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4.1.5

	
[***]

	
4.1.5.1

	
[***]

	
  

	
[***]

	
4.1.5.2

	
[***]

 

	 	
(i)

	
[***]

 

	
  

	
(ii)

	
[***]

 

	
  

	
(iii)

	
[***];

	
4.1.5.3

	
[***]

[***]

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Appendix 3 Exhibit B– to Amendment 9

With respect to [***], the provisions contained in Clause 4.2 of the Second A320 Family Purchase Agreement are hereby cancelled and replaced by the following quoted provisions:

QUOTE

	
4.2.

	
[***]

	
4.2.1

	
[***]

	
4.2.2

	
[***].

	
4.2.3

	
[***].

	
4.2.4

	
[***]

 

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Appendix 3 Exhibit B– to Amendment 9

	
4.2.5

	
[***]

	
4.2.5.1

	
[***]

	
4.2.5.2

	
[***]

	
4.2.5.3

	
[***].

	
4.2.5.4

	
[***]

	
4.2.5.5

	
[***].

[***]

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Appendix 3 Exhibit C– to Amendment 9

With respect to the [***], the provisions contained in Clause 4.3 of the Second A320 Family Purchase Agreement are hereby cancelled and replaced by the following quoted provisions:

[***]

	
4.3.

	
[***]

	
4.3.1

	
[***]

	
4.3.2

	
[***]

	
4.3.3

	
[***].

	
4.3.4

	
[***]

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Appendix 3 Exhibit C– to Amendment 9

	
4.3.5

	
[***]

	
4.3.5.1

	
[***].

	
4.3.5.2

	
[***]

	
4.3.5.3

	
[***].

	
4.3.5.4

	
[***].

	
4.3.5.5

	
[***].

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 1

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

Subject  : PREDELIVERY PAYMENTS OF THE [***]

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the Incremental Aircraft described therein.

Capitalized terms used herein and not otherwise defined in this letter agreement N°1 to Amendment N°9 (the “Letter Agreement N°1”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

Both Parties agree that this Letter Agreement N°1, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°1.

A320F - LAN - AMDT 9 - Second A320 Family PA

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67/180

  

Letter Agreement No. 1

	
1.

	
With respect to the [***], the provisions contained in clause 5.1 and 5.2 of the Second A320 Family Purchase Agreement are hereby cancelled in their entirety and replaced by the following quoted provisions:

QUOTE

	
5.1

	
Seller's Account

The Buyer shall pay the Predelivery Payments, the Balance of Final Aircraft Price and/or any other amount due by the Buyer to the Seller, to the Seller's account:

[***]

	
  

	
or to such other account as may be designated by the Seller in such other jurisdiction where the Buyer shall not be required to withhold or make other deductions on account of taxes in relation to such payment.

	
5.2

	
Predelivery Payments

	
5.2.0

	
[***].

	
5.2.1

	
The Buyer shall pay Predelivery Payments to the Seller calculated on the predelivery payment reference price of each [***]. The predelivery payment reference price is determined by the following formula:

A = Pb (1 + 0.03N)

Where

	
  

	
A

	
:

	
The predelivery payment reference price for Aircraft of the [***] to be delivered in year T;

	
  

	
T

	
:

	
the year of Delivery of the relevant [***];

	
  

	
Pb

	
:

	
the Aircraft Base Price;

	
  

	
N

	
:

	
[***]

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5.2.2

	
Such Predelivery Payments shall be made in accordance with the following schedule:

	
DUE DATE OF PAYMENTS

	  	
PERCENTAGE OF PREDELIVERY

PAYMENT REFERENCE PRICE

	
Upon signature of this Amendment No.9

	  	
[***]

	  	  	  
	
On the first day of each of the following months prior to the Scheduled Delivery Month

	  	  
	
[***] months

	  	
[***]

	  	  	  
	
[***] months

	  	
[***]

	  	  	  
	
[***]months

	  	
[***]

	  	  	  
	
___________________________

	
  

	
[***]

	
Total Payment prior to Delivery

	  	  

In the event of the above schedule resulting in any Predelivery Payment falling due prior to the date of signature of the Amendment No.9, such Predelivery Payments shall be made upon signature of this Amendment No.9.

UNQUOTE

	
2.

	
Assignment

	
  

	
The Parties agree that clause 21 of the Second A320 Family Purchase Agreement shall govern the assignability and transferability of each Party’s rights and obligations under this Letter Agreement N°1.

	
3.

	
Confidentiality

Each of the Parties hereto agree that the provisions of this Letter Agreement N°1 are personal to it and will not without the prior written consent of the other Parties disclose such information to any other Party. [***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 1

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°1 to the Seller.

	
Agreed and Accepted

	  	
Agreed and Accepted

	  	  	  	  	  	  	  
	
For and on behalf of

	  	
For and on behalf of

	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  	
AIRBUS S.A.S.

	  	  	  	  	  	  	  
	
By

	
:

	  	  	
By

	
:

	  
	  	  	  	  	  	  	  
	
Its

	
:

	  	  	
Its

	
:

	  
	  	  	  	  	  	  	  
	
Date

	
:

	  	  	
Date

	
:

	  
	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  	  	  	  
	  	  	  	  	  	  	  
	
By

	
:

	  	  	  	  	  
	  	  	  	  	  	  	  
	
Its

	
:

	  	  	  	  	  
	  	  	  	  	  	  	  
	
Date

	
:

	  	  	  	  	  

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 2

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

Subject: [***]

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the Incremental Aircraft described therein.

Capitalized terms used herein and not otherwise defined in this letter agreement N°2 to Amendment N°9 (the “Letter Agreement N°2”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

Both Parties agree that this Letter Agreement N°2, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°2.

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 2

	
1.

	
This Letter Agreement No.2 shall be applicable to the [***].

	
2.

	
[***]

	
2.1

	
[***]

	
2.2

	
[***].

	
2.3

	
[***].

	
2.4

	
[***].

	
2.5

	
[***].

	
3.

	
Assignment

	
  

	
The Parties agree that clause 21 of the Second A320 Family Purchase Agreement shall govern the assignability and transferability of each Party’s rights and obligations under this Letter Agreement N°2.

	
4.

	
Confidentiality

	
  

	
Each of the Parties hereto agree that the provisions of this Letter Agreement N°2 are personal to it and will not without the prior written consent of the other Parties disclose such information to any other Party. [***]

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Letter Agreement No. 2

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°2 to the Seller.

	
Agreed and Accepted

	  	
Agreed and Accepted

	  	  	  	  	  	  	  
	
For and on behalf of

	  	
For and on behalf of

	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  	
AIRBUS S.A.S.

	  	  	  	  	  	  	  
	
By

	
:

	  	  	
By

	
:

	  
	  	  	  	  	  	  	  
	
Its

	
:

	  	  	
Its

	
:

	  
	  	  	  	  	  	  	  
	
Date

	
:

	  	  	
Date

	
:

	  
	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  	  	  	  
	  	  	  	  	  	  	  
	
By

	
:

	  	  	  	  	  
	  	  	  	  	  	  	  
	
Its

	
:

	  	  	  	  	  
	  	  	  	  	  	  	  
	
Date

	
:

	  	  	  	  	  

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 3

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

Subject  : [***]

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the Incremental Aircraft described therein.

Capitalized terms used herein and not otherwise defined in this letter agreement N°3 to Amendment N°9 (the “Letter Agreement N°3”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

Both Parties agree that this Letter Agreement N°3, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°3.

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 3

	
1.

	
This Letter Agreement No.3 shall be applicable to the [***].

	
2

	
[***]

	
3.

	
Assignment

	
  

	
The Parties agree that clause 21 of the Second A320 Family Purchase Agreement shall govern the assignability and transferability of each Party’s rights and obligations under this Letter Agreement N°3.

	
4.

	
Confidentiality

	
  

	
Each of the Parties hereto agree that the provisions of this Letter Agreement N°3 are personal to it and will not without the prior written consent of the other Parties disclose such information to any other Party. [***]

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 3

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°3 to the Seller.

	
Agreed and Accepted

	  	
Agreed and Accepted

	  	  	  	  	  	  	  
	
For and on behalf of

	  	
For and on behalf of

	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  	
AIRBUS S.A.S.

	  	  	  	  	  	  	  
	
By

	
:

	  	  	
By

	
:

	  
	  	  	  	  	  	  	  
	
Its

	
:

	  	  	
Its

	
:

	  
	  	  	  	  	  	  	  
	
Date

	
:

	  	  	
Date

	
:

	  
	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  	  	  	  
	  	  	  	  	  	  	  
	
By

	
:

	  	  	  	  	  
	  	  	  	  	  	  	  
	
Its

	
:

	  	  	  	  	  
	  	  	  	  	  	  	  
	
Date

	
:

	  	  	  	  	  

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 4

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

Subject  : [***]

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the 2010 Incremental Aircraft described therein.

Capitalized terms used herein and not otherwise defined in this letter agreement N°04 to Amendment N°9 (the “Letter Agreement N°04”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

Reference in this Letter Agreement N°04 to “Facility” shall mean any ECA supported financing facility to be provided in respect of any or all of the 2010 Incremental Aircraft.

Both Parties agree that this Letter Agreement N°04, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°04.

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 4

GENERAL TERMS AND CONDITIONS

[***]:

	
1

	
[***].

	
2

	
[***].

	
3

	
[***]

	
4

	
[***].

	
5

	
[***].

	
6

	
[***].

	
7

	
[***].

	
8

	
[***].

	
9

	
[***]

	
9.1

	
[***].

	
9.2

	
[***]

	
10

	
[***]

	
10.1.

	
[***].

	
10.2.

	
[***].

	
11.

	
Assignment

The Parties agree that clause 21 of the Second A320 Family Purchase Agreement shall govern the assignability and transferability of each Party’s rights and obligations under this Letter Agreement N°04.

	
12.

	
Confidentiality

Each of the Parties hereto agree that the provisions of this Letter Agreement N°04 are personal to it and will not without the prior written consent of the other Parties disclose such information to any other Party. [***]

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 4

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement No.4 to the Seller.

	
Agreed and Accepted

	  	
Agreed and Accepted

	  	  	  	  	  	  	  
	
For and on behalf of

	  	
For and on behalf of

	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  	
AIRBUS S.A.S.

	  	  	  	  	  	  	  
	
By

	
:

	  	  	
By

	
:

	  
	  	  	  	  	  	  	  
	
Its

	
:

	  	  	
Its

	
:

	  
	  	  	  	  	  	  	  
	
Date

	
:

	  	  	
Date

	
:

	  
	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  	  	  	  
	  	  	  	  	  	  	  
	
By

	
:

	  	  	  	  	  
	  	  	  	  	  	  	  
	
Its

	
:

	  	  	  	  	  
	  	  	  	  	  	  	  
	
Date

	
:

	  	  	  	  	  

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 4

Table 1

[***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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80/180

  

Letter Agreement No. 4

[***]

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 5

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

Subject  : [***]

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the Incremental Aircraft described therein.

Capitalized terms used herein and not otherwise defined in this letter agreement N°5 to Amendment N°9 (the “Letter Agreement N°5”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

Both Parties agree that this Letter Agreement N° 5, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°5.

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 5

	
1.

	
This Letter Agreement No.5 shall be applicable to the [***].

	
2.

	
[***]

	
3.

	
[***]

	
4.

	
Assignment

	
  

	
The Parties agree that clause 21 of the Second A320 Family Purchase Agreement shall govern the assignability and transferability of each Party’s rights and obligations under this Letter Agreement N° 5.

	
5.

	
Confidentiality

	
  

	
Each of the Parties hereto agree that the provisions of this Letter Agreement N° 5 are personal to it and will not without the prior written consent of the other Parties disclose such information to any other Party. [***]

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 5

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°5 to the Seller.

	
Agreed and Accepted

	  	
Agreed and Accepted

	  	  	  	  	  	  	  
	
For and on behalf of

	  	
For and on behalf of

	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  	
AIRBUS S.A.S.

	  	  	  	  	  	  	  
	
By

	
:

	  	  	
By

	
:

	  
	  	  	  	  	  	  	  
	
Its

	
:

	  	  	
Its

	
:

	  
	  	  	  	  	  	  	  
	
Date

	
:

	  	  	
Date

	
:

	  
	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  	  	  	  
	  	  	  	  	  	  	  
	
By

	
:

	  	  	  	  	  
	  	  	  	  	  	  	  
	
Its

	
:

	  	  	  	  	  
	  	  	  	  	  	  	  
	
Date

	
:

	  	  	  	  	  

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 6

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

Subject : PRODUCT SUPPPORT FOR 2010 INCREMENTAL AIRCRAFT

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the 2010 Incremental Aircraft described therein.

Capitalized terms used herein and not otherwise defined in this letter agreement N°6 to Amendment N°9 (the “Letter Agreement N°6”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

Both Parties agree that this Letter Agreement N°6, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°6.

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 6

	
1.

	
GENERAL

	
1.1

	
For the avoidance of doubt, all quantities indicated below are the total quantities granted for the [***] firmly ordered 2010 Incremental Aircraft unless otherwise specified.

Should the Buyer decide to cancel any of the [***] 2010 Incremental Aircraft, the Seller reserves the right to modify the quantities as defined herein.

	
1.2

	
The Buyer and the Seller mutually agree that the contractual training allocations provided by the Seller under clauses 14.4.1, 15.1.1, 16.3 and 16.4.2 of the Second A320 Purchase Agreement, shall not be applicable to the 2010 Incremental Aircraft.

In substitution, the Seller shall provide the Buyer with the training allocations defined in this Letter Agreement N°6.

	
1.3

	
The contractual training courses defined in Clause 2 here below shall be provided up to [***] 2010 Incremental Aircraft delivered under Amendment N°9.

	
2

	
TRAINING SUPPORT AND SERVICES

	
2.1

	
With respect to the 2010 Incremental Aircraft, the provisions contained in clause 16.3.1 of the Second A320 Family Purchase Agreement, are hereby cancelled in their entirety and replaced by the following quoted provisions:

	
2.1.1

	
Notwithstanding the above Clause 1.3, the flight operations training courses as defined in this Clause 2 shall be granted to and may be utilised by the Buyer on the basis of [***] during the [***] 2010 Incremental Aircraft.

	
2.1.2

	
Such flight operations training courses shall be granted on a cumulative basis.

	
2.1.3

	
Furthermore in the event the Buyer has any remaining flight operations training courses upon Delivery of the last 2010 Incremental Aircraft the Buyer may utilise such remaining flight operations training courses [***].

QUOTE

	
16.3.1

	
Flight Crew Training Course

	
16.3.1.1

	
The Seller shall perform a flight crew training course program (standard transition course or a cross crew qualification program as applicable) for a total of [***] of the Buyer's flight crews, each of which shall consist of [***]. The training manual used shall be the Seller’s Flight Crew Operating Manual (FCOM), except for base Flight training, for which the Buyer’s customized FCOM shall be used.

	
16.3.1.2

	
If a [***] is required, the Buyer shall use its delivered Aircraft, or any other aircraft operated by the Buyer, for any base flight training, which shall not exceed [***], according to the related Airbus training course definition. In the event of it being necessary to ferry the Buyer’s delivered Aircraft to the location where the base flight training shall take place, the additional flight time required for the ferry flight to and/or from the base training field shall not be deducted from the base flight training allowance.

	
  

	
However, if the base flight training is performed outside of the zone where the Seller usually performs such training, the ferry flight to the location where the base flight training shall take place shall be performed by a crew composed of the Seller’s and/or the Buyer’s qualified pilots, in accordance with the Aviation Authorities’ regulations related to the place of performance of the base flight training.

A320F - LAN - AMDT 9 - Second A320 Family PA

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Letter Agreement No. 6

 

	
16.3.1.3

	
[***]

The Seller shall provide free [***] for a total of [***] of the Buyer's flight crews having followed Flight Crew Training as per Clause 16.3.1.1 above.

UNQUOTE

	
2.2

	
With respect to the 2010 Incremental Aircraft, clause 16.3.3 is hereby inserted in the Second A320 Family Purchase Agreement with the following quoted provisions:

QUOTE

	
16.3.3

	
Maintenance Training

The Seller shall provide to the Buyer [***] of maintenance training [***] for the Buyer's personnel.

The available courses are listed in the Seller's applicable Training Courses Catalog.

The above trainee days shall be used solely for the Maintenance training courses as defined in the Seller’s applicable Training Courses Catalog.

Within the above trainee days allowance, the number of Engine Run-up courses shall be limited to [***] 2010 Incremental Aircraft and to a [***] in total.

The Buyer shall provide the Seller with an attendance list of trainees at the latest [***] start of the training course.

The practical training provided in the frame of maintenance training is performed exclusively on the training devices in use in the Seller’s Training Centers or Affiliated Training Center.

In the event of practical training on aircraft being requested by the Buyer, such practical training can be organized with the assistance of the Seller, in accordance with Clause 16.3.3

UNQUOTE

	
2.3

	
With respect to the 2010 Incremental Aircraft, the provisions contained in clause 16.3.7 of the Second A320 Family Purchase Agreement are hereby cancelled in their entirety and replaced by the following quoted provisions:

QUOTE

	
16.3.7

	
Trainee days accounting

	
16.3.7.1

	
Definitions

Seller’s Training Centers: Seller’s training center in Blagnac, France, and/or in Hamburg, Germany.

Affiliated Training Center: Seller’s affiliated training center in Miami, U.S.A.

	
16.3.7.2

	
Trainee days are counted as follows:

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For instruction at the Seller's Training Centers or Affiliated Training Center: [***] of instruction for [***] trainee equals [***] trainee day. The number of trainees originally registered at the beginning of the course shall be counted as the number of trainees to have taken the course.

For instruction outside of the Seller's Training Centers or Affiliated Training Center: [***] of instruction by [***] Seller Instructor equals the actual number of trainees attending the course or a minimum of [***] trainee days, except for structure maintenance training course(s).

For structure maintenance training courses outside the Seller’s Training Center(s) or Affiliated Training Center, [***] day of instruction by [***] Seller Instructor equals the actual number of trainees attending the course or the minimum number of trainees as indicated in the Seller’s Customer Services Catalog.

For practical training, whether on training devices or on aircraft, [***] day of instruction by [***] Seller Instructor equals the actual number of trainees attending the course or a minimum of [***] trainee days.

UNQUOTE

	
3

	
SELLER REPRESENTATIVE SERVICES

	
3.1

	
The Parties agree that the Seller’s representative allocations provided to the Buyer under clause 15.1.1 of the Second A320 Purchase Agreement shall not be applicable to the 2010 Incremental Aircraft. In substitution, the Seller shall provide the Buyer with the Seller Representative allocation for the 2010 Incremental Aircraft as defined hereunder.

QUOTE

	
15.1

	
The Seller shall provide to the Buyer, Seller Representative services at the Buyer's main base or at other locations to be mutually agreed for a total of [***].

For the sake of clarification, such Seller Representatives’ services shall include initial Aircraft Entry Into Service (EIS) assistance and sustaining support services.

The number of the Seller Representatives assigned to the Buyer at any one time shall be mutually agreed, but shall at no time exceed [***] Seller Representatives.

UNQUOTE

	
4

	
TECHNICAL DATA AND SOFTWARE REVISION SERVICE

	
4.1

	
The Parties agree that the terms and conditions of the Technical Publications Revision Service (now called Technical Data and Software Revision Service) provided to the Seller under clause 14.4.1 of the Second A320 Purchase Agreement shall not be applicable to the 2010 Incremental Aircraft. In substitution, the Seller shall provide the Buyer with the Technical Data and Software Revision Service for the 2010 Incremental Aircraft as defined hereunder.

QUOTE

A320F - LAN - AMDT 9 - Second A320 Family PA

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14.4.1

	
General

For each firmly ordered 2010 Incremental Aircraft covered under the Amendment No 9, the Technical Data and Software Revision Service shall be provided [***] 2010 Incremental Aircraft.

Thereafter the Revision Service shall be provided in accordance with the terms and conditions set forth in the Seller’s then current Customer Services Catalog.

Mandatory changes (including Aviation Authority Airworthiness Directives) and Alert Service Bulletins shall be incorporated into the Technical Publications at no charge [***].

UNQUOTE

	
5

	
LOAD AND TRIM SHEET SOFTWARE

	
5.1

	
Description

The “Load and Trim Sheet Software” (LTS) is a ground software which allows the Buyer to produce, for a given aircraft configuration, a cabin configuration combination, a paper trim sheet with the standard Airbus layout and its associated AHM 560 document.

	
5.2

	
Commercial Conditions

LTS shall be provided to the Buyer [***] for each firmly ordered 2010 Incremental Aircraft for the [***] of the applicable 2010 Incremental Aircraft [***].

After said period, the LTS shall be [***] to the Buyer at standard [***] as set forth in the Seller's then current Customer Services Catalog.

	
5.3

	
Delivery

Delivery of LTS shall be mutually scheduled and agreed upon between the parties.

	
5.4

	
Installation

Prerequisites to the functioning of LTS and conditions of site preparation shall be indicated by the Seller to the Buyer.

[***].

	
5.5

	
Support

Support, assistance and training shall be provided upon the Buyer’s request on a chargeable basis at the rates defined in the Seller’s Customer Services Catalog.

	
5.6

	
Licence

The use of LTS by the Buyer is subject to the signature of the applicable LTS License Agreement by the Buyer.

	
6.

	
ASSIGNMENT

	
  

	
The Parties agree that clause 21 of the Second A320 Family Purchase Agreement shall govern the assignability and transferability of each Party’s rights and obligations under this Letter Agreement N°6.

A320F - LAN - AMDT 9 - Second A320 Family PA

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89/180

  

Letter Agreement No. 6

	
7.

	
CONFIDENTIALITY

	
  

	
Each of the Parties hereto agree that the provisions of this Letter Agreement N°6 are personal to it and will not without the prior written consent of the other Parties disclose such information to any other Party. [***]

A320F - LAN - AMDT 9 - Second A320 Family PA

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90/180

  

 

Letter Agreement No. 6

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°6 to the Seller.

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  
	
By

	
:

	  	  	
By

	
:

	  	  
	  	  	  	  	  	  	  	  
	
Its

	
:

	  	  	
Its

	
:

	  	  
	  	  	  	  	  	  	  	  
	
Date

	
:

	  	  	
Date

	
:

	  	  
	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  
	  	  	  	  
	
By

	
:

	  	  	  
	  	  	  	  	  
	
Its

	
:

	  	  	  
	  	  	  	  	  
	
Date

	
:

	  	  	  

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

91/180

  

Letter Agreement No. 7A

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

Subject  : [***]

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the 2010 Incremental Aircraft described therein.

Capitalized terms used herein and not otherwise defined in this letter agreement N°7A to Amendment N°9 (the “Letter Agreement N°7A”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

Both Parties agree that this Letter Agreement N° 7A, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°7A.

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

92/180

  

Letter Agreement No. 7A

This Letter Agreement No.7A shall be applicable to the 2010 A319 Aircraft.

1           [***].

2           [***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

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93/180

  

Letter Agreement No. 7A

3           [***]

4           [***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

94/180

  

Letter Agreement No. 7A

5           [***]

6           [***].

7           [***].

8           [***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

95/180

  

Letter Agreement No. 7A

9           [***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

96/180

  

Letter Agreement No. 7A

	
10.

	
[***].

	
11.

	
[***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

97/180

  

Letter Agreement No. 7A

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°7A to the Seller.

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  
	
By

	
:

	  	  	
By

	
:

	  	  
	  	  	  	  	  	  	  	  
	
Its

	
:

	  	  	
Its

	
:

	  	  
	  	  	  	  	  	  	  	  
	
Date

	
:

	  	  	
Date

	
:

	  	  
	  	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  	  	  	  
	  	  	  	  	  	  	  	  
	
By

	
:

	  	  	  	  	  	  
	  	  	  	  	  	  	  	  
	
Its

	
:

	  	  	  	  	  	  
	  	  	  	  	  	  	  	  
	
Date

	
:

	  	  	  	  	  	  

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

98/180

  

Letter Agreement No. 7A

APPENDIX No.1 to LETTER AGREEMENT No.7A

[***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

99/180

  

 

LETTER AGREEMENT N°7B

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

Subject  : [***]

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the 2010 Incremental Aircraft described therein.

Capitalized terms used herein and not otherwise defined in this letter agreement N°7B to Amendment N°9 (the “Letter Agreement N°7B”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

Both Parties agree that this Letter Agreement N°7B, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°7B.

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

100/180

  

LETTER AGREEMENT N°7B

This Letter Agreement No.7B shall be applicable to the [***].

1           [***]

2           [***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

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101/180

  

LETTER AGREEMENT N°7B

3           [***]

4           [***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

102/180

  

LETTER AGREEMENT N°7B

	
5

	
[***]

	
5.1

	
[***].

	
5.2

	
[***].

	
5.2.1

	
[***].

	
5.2.2

	
[***]

	
5.3

	
[***].

	
5.4

	
[***].

	
5.5

	
[***].

	
6

	
[***]

	
6.1

	
[***].

	
6.2

	
[***].

	
6.3

	
[***].

	
6.4

	
[***].

	
6.5

	
[***].

	
6.6

	
[***].

	
6.7

	
[***].

	
6.8

	
[***].

	
7

	
[***]

	
7.1

	
[***].

	
7.2

	
[***].

	
8

	
[***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

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103/180

  

LETTER AGREEMENT N°7B

9           [***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

104/180

  

LETTER AGREEMENT N°7B

	
10.

	
[***].

	
11.

	
[***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

105/180

  

LETTER AGREEMENT N°7B

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°7B to the Seller.

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  
	
By

	
:

	  	  	
By

	
:

	  	  
	  	  	  	  	  	  	  	  
	
Its

	
:

	  	  	
Its

	
:

	  	  
	  	  	  	  	  	  	  	  
	
Date

	
:

	  	  	
Date

	
:

	  	  
	  	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  
	  	  	  	  	  	  	  	  
	
By

	
:

	  	  	  	  	  	  
	  	  	  	  	  	  	  	  
	
Its

	
:

	  	  	  	  	  	  
	  	  	  	  	  	  	  	  
	
Date

	
:

	  	  	  	  	  	  

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

106/180

  

LETTER AGREEMENT N°7B

APPENDIX No.1 to LETTER AGREEMENT No.7B

[***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

107/180

  

LETTER AGREEMENT N°7C

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

Subject  : [***]

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the 2010 Incremental Aircraft described therein.

Capitalized terms used herein and not otherwise defined in this letter agreement N°7C to Amendment N°9 (the “Letter Agreement N°7C”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

Both Parties agree that this Letter Agreement N° 7C, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°7C.

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

108/180

  

LETTER AGREEMENT N°7C

This Letter Agreement No.7C shall be applicable to the [***].

1           [***].

2           [***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

109/180

  

LETTER AGREEMENT N°7C

	
3

	
[***]

 

	
4

	
[***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

110/180

  

LETTER AGREEMENT N°7C

	
5

	
[***]

	
5.1

	
[***].

	
5.2

	
[***]

	
5.2.1

	
[***]

	
5.2.2

	
[***]

	
5.3

	
[***]

	
5.4

	
[***].

	
5.5

	
[***]

	
6

	
[***]

	
6.1

	
[***].

	
6.2

	
[***]

	
6.3

	
[***]

	
6.4

	
[***]

	
6.5

	
[***]

	
6.6

	
[***]

	
6.7

	
[***]

	
6.8

	
[***]

	
7

	
[***]

	
7.1

	
[***]

	
7.2

	
[***]:

	 	
a) 

	
[***]

	 	
b) 

	
[***]

	 	
c)

	
[***]

	
8

	
[***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

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111/180

  

LETTER AGREEMENT N°7C

	
9

	
[***]

	
9.1

	
[***]:

	
9.1.1

	
[***].

	
9.1.2

	
[***].

	
9.1.3

	
[***].

	
9.2

	
[***].

	
9.3

	
[***].

	
9.4

	
[***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

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112/180

  

LETTER AGREEMENT N°7C

	
10.

	
[***].

	
11.

	
[***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

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113/180

  

LETTER AGREEMENT N°7C

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°7C to the Seller.

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  
	
By

	
:

	  	  	
By

	
:

	  	  
	  	  	  	  	  	  	  	  
	
Its

	
:

	  	  	
Its

	
:

	  	  
	  	  	  	  	  	  	  	  
	
Date

	
:

	  	  	
Date

	
:

	  	  
	  	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  	  	  	  
	  	  	  	  	  	  	  	  
	
By

	
:

	  	  	  	  	  	  
	  	  	  	  	  	  	  	  
	
Its

	
:

	  	  	  	  	  	  
	  	  	  	  	  	  	  	  
	
Date

	
:

	  	  	  	  	  	  

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

114/180

  

LETTER AGREEMENT N°7C

APPENDIX No.1 to LETTER AGREEMENT No.7C

[***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

115/180

  

 

LETTER AGREEMENT N°7D

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

Subject  : [***]

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the 2010 Incremental Aircraft described therein.

Capitalized terms used herein and not otherwise defined in this letter agreement N°7D to Amendment N°9 (the “Letter Agreement N°7D”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

Both Parties agree that this Letter Agreement N° 7D, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°7D.

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

116/180

  

LETTER AGREEMENT N°7D

This Letter Agreement No.7D shall be applicable to the [***]

1           [***]

2           [***].

3           [***]

4           [***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

117/180

  

LETTER AGREEMENT N°7D

 

	
5

	
[***]

	
5.1

	
[***].

	
5.2

	
[***]

	
5.2.1

	
[***]

	
5.2.2

	
[***]

	
5.3

	
[***]

	
5.4

	
[***]

	
5.5

	
[***].

	
6

	
[***]

	
6.1

	
[***].

	
6.2

	
[***].

	
6.3

	
[***].

	
6.4

	
[***]

	
6.5

	
[***].

	
6.6

	
[***].

	
6.7

	
[***].

	
6.8

	
[***].

	
7

	
[***]

	
7.1

	
[***]

	
7.2

	
[***]t.

	
8

	
[***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

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118/180

  

LETTER AGREEMENT N°7D

	
9

	
[***].

	
9.1

	
[***]:

	
9.1.1

	
[***]

	
9.1.2

	
[***]

	
9.1.3

	
[***]

	
9.2

	
[***].

	
9.3

	
[***].

	
9.4

	
[***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

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119/180

  

LETTER AGREEMENT N°7D

	
10.

	
[***].

	
11.

	
[***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

120/180

  

LETTER AGREEMENT N°7D

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°7D to the Seller.

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  	  	  	  	  
	
By

	
:

	  	  	
By

	
:

	  	  
	  	  	  	  	  	  	  	  
	
Its

	
:

	  	  	
Its

	
:

	  	  
	  	  	  	  	  	  	  	  
	
Date

	
:

	  	  	
Date

	
:

	  	  
	  	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  	  	  	  
	  	  	  	  	  	  	  	  
	
By

	
:

	  	  	  	  	  	  
	  	  	  	  	  	  	  	  
	
Its

	
:

	  	  	  	  	  	  
	  	  	  	  	  	  	  	  
	
Date

	
:

	  	  	  	  	  	  

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

121/180

  

 

LETTER AGREEMENT N°7D

APPENDIX No.1 to LETTER AGREEMENT No.7D

[***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

122/180

  

LETTER AGREEMENT N°7E

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

Subject  : [***].

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the 2010 Incremental Aircraft described therein.

Capitalized terms used herein and not otherwise defined in this letter agreement N°7E to Amendment N°9 (the “Letter Agreement N°7E”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

Both Parties agree that this Letter Agreement N° 7E, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°7E.

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

123/180

  

LETTER AGREEMENT N°7E

This Letter Agreement No.7E shall be applicable to the [***]

1           [***].

2           [***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

124/180

  

LETTER AGREEMENT N°7E

3           [***]

4           [***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

125/180

  

LETTER AGREEMENT N°7E

	
5

	
[***]

	
5.1

	
[***].

	
5.2

	
[***].

	
5.2.1

	
[***].

	
5.2.2

	
[***]

 

	
5.3

	
[***]

	
5.4

	
[***].

	
5.5

	
[***]

	
6

	
[***]

	
6.1

	
[***].

	
6.2

	
[***].

	
6.3

	
[***].

	
6.4

	
[***].

	
6.5

	
[***].

	
6.6

	
[***].

	
6.7

	
[***].

	
6.8

	
[***].

	
7

	
[***]

	
7.1

	
[***].

	
7.2

	
[***].

	
8

	
[***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

126/180

  

LETTER AGREEMENT N°7E

	
9

	
[***].

	
9.1

	
[***]:

	
9.1.1

	
[***].

	
9.1.2

	
[***].

	
9.1.3

	
[***].

	
9.2

	
[***].

	
9.3

	
[***].

	
9.4

	
[***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

127/180

  

LETTER AGREEMENT N°7E

	
10.

	
[***].

	
11.

	
[***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

128/180

  

LETTER AGREEMENT N°7E

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°7E to the Seller.

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  	  	  	  	  	  	  
	
By

	
:

	  	  	
By

	
:

	  	  
	  	  	  	  	  	  	  	  
	
Its

	
:

	  	  	
Its

	
:

	  	  
	  	  	  	  	  	  	  	  
	
Date

	
:

	  	  	
Date

	
:

	  	  
	  	  	  	  	  	  	  	  
	
LAN AIRLINES S.A.

	  	  	  	  
	  	  	  	  	  	  	  	  
	
By

	
:

	  	  	  	  	  	  
	  	  	  	  	  	  	  	  
	
Its

	
:

	  	  	  	  	  	  
	  	  	  	  	  	  	  	  
	
Date

	
:

	  	  	  	  	  	  

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

129/180

  

  

LETTER AGREEMENT N°7E

APPENDIX No.1 to LETTER AGREEMENT No.7E

[***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

130/180

  

  

LETTER AGREEMENT N°7F

 

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

Subject  : [***].

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the 2010 Incremental Aircraft described therein.

Capitalized terms used herein and not otherwise defined in this letter agreement N°7F to Amendment N°9 (the “Letter Agreement N°7F”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

Both Parties agree that this Letter Agreement N° 7F, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°7F.

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

131/180

  

  

LETTER AGREEMENT N°7F 

 

This Letter Agreement No.7f shall be applicable to the [***]

1           [***]

2           [***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

132/180

  

   

LETTER AGREEMENT N°7F

 

3           [***]

4           [***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

133/180

  

    

LETTER AGREEMENT N°7F

 

5           [***].

6           [***]

7           [***].

8           [***].

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

134/180

  

  

LETTER AGREEMENT N°7F

 

9           [***]

  

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

135/180

  

 

LETTER AGREEMENT N°7F

 

	
10.

	
[***].

 

	
11.

	
[***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

136/180

  

LETTER AGREEMENT N°7F

 

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°7F to the Seller.

 

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  	  	  	  	  
	
By

	
:

	
____________________

	
By

	
:

	
____________________

	  	  	  	  	  	  
	
Its

	
:

	
____________________

	
Its

	
:

	
____________________

	  	  	  	  	  	  
	
Date

	
:

	
____________________

	
Date

	
:

	
____________________

 

	
LAN AIRLINES S.A.

	 
	  	 
	
By

	
:

	
___________________

	 
	  	  	  	 
	
Its

	
:

	
___________________

	 
	  	  	  	 
	
Date

	
:

	
___________________

	 

 

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LETTER AGREEMENT N°7F

 

APPENDIX No.1 to LETTER AGREEMENT No.7F

 

[***]

 

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LETTER AGREEMENT N°7G

 

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

 

Subject  : [***]

 

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the 2010 Incremental Aircraft described therein.

 

Capitalized terms used herein and not otherwise defined in this letter agreement N°7G to Amendment N°9 (the “Letter Agreement N°7G”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

 

Both Parties agree that this Letter Agreement N° 7G, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°7G.

 

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139/180

  

LETTER AGREEMENT N°7G

 

This Letter Agreement No.7G shall be applicable to the [***]

 

1           [***]

 

2           [***].

 

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LETTER AGREEMENT N°7G

 

3           [***]

 

4           [***].

 

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141/180

  

LETTER AGREEMENT N°7G

 

5           [***].

 

6           [***].

 

7           [***].

 

8           [***].

 

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LETTER AGREEMENT N°7G

 

9           [***].

 

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143/180

  

LETTER AGREEMENT N°7G

 

	
10.

	
[***].

 

	
11.

	
[***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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144/180

  

LETTER AGREEMENT N°7G

 

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°7G to the Seller.

 

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  	  	  	  	  
	
By

	
:

	
____________________

	
By

	
:

	
____________________

	  	  	  	  	  	  
	
Its

	
:

	
____________________

	
Its

	
:

	
____________________

	  	  	  	  	  	  
	
Date

	
:

	
____________________

	
Date

	
:

	
____________________

 

	
LAN AIRLINES S.A.

	 
	  	 
	
By

	
:

	
___________________

	 
	  	  	  	 
	
Its

	
:

	
___________________

	 
	  	  	  	 
	
Date

	
:

	
___________________

	 

A320F - LAN - AMDT 9 - Second A320 Family PA

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145/180

  

LETTER AGREEMENT N°7G

 

APPENDIX No.1 to LETTER AGREEMENT No.7G

 

[***]

 

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LETTER AGREEMENT N°7H

 

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

 

Subject  : [***]

 

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the 2010 Incremental Aircraft described therein.

 

Capitalized terms used herein and not otherwise defined in this letter agreement N°7H to Amendment N°9 (the “Letter Agreement N°7H”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

 

Both Parties agree that this Letter Agreement N° 7H, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°7H.

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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147/180

  

LETTER AGREEMENT N°7H

 

This Letter Agreement No.7H shall be applicable to the [***]

 

	
1

	
[***].

 

	
2

	
[***]

 

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LETTER AGREEMENT N°7H

 

	
3

	
[***]

 

	
4

	
[***]

 

	
5

	
[***]

 

	
6

	
[***]

 

	
7

	
[***]

 

	
8

	
[***]

 

	
9

	
[***]

 

	
10.

	
[***]

 

	
11.

	
[***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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149/180

  

LETTER AGREEMENT N°7H

 

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°7H to the Seller.

 

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  	  	  	  	  
	
By

	
:

	
____________________

	
By

	
:

	
____________________

	  	  	  	  	  	  
	
Its

	
:

	
____________________

	
Its

	
:

	
____________________

	  	  	  	  	  	  
	
Date

	
:

	
____________________

	
Date

	
:

	
____________________

 

	
LAN AIRLINES S.A.

	 
	  	 
	
By

	
:

	
___________________

	 
	  	  	  	 
	
Its

	
:

	
___________________

	 
	  	  	  	 
	
Date

	
:

	
___________________

	 

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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150/180

  

LETTER AGREEMENT N°7H

 

APPENDIX No.1 to LETTER AGREEMENT No.7H

 

[***]

 

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151/180

  

LETTER AGREEMENT N°7I

 

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

 

Subject: [***]

 

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the 2010 Incremental Aircraft described therein.

 

Capitalized terms used herein and not otherwise defined in this letter agreement N°7I to Amendment N°9 (the “Letter Agreement N°7I”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

 

Both Parties agree that this Letter Agreement N° 7I, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°7I.

 

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152/180

  

LETTER AGREEMENT N°7I

 

This Letter Agreement No.7I shall be applicable to the [***]..

 

	
1

	
[***].

 

	
2

	
[***]

 

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153/180

  

LETTER AGREEMENT N°7I

 

	
3

	
[***]

 

	
4

	
[***]

 

	
5

	
[***]

 

	
6

	
[***]

 

	
7

	
[***]

 

	
8

	
[***]

 

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LETTER AGREEMENT N°7I

 

	
9

	
[***]

 

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155/180

  

LETTER AGREEMENT N°7I

 

	
10.

	
[***]

 

	
11.

	
[***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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156/180

  

LETTER AGREEMENT N°7I

 

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°7I to the Seller.

 

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  	  	  	  	  
	
By

	
:

	
____________________

	
By

	
:

	
____________________

	  	  	  	  	  	  
	
Its

	
:

	
____________________

	
Its

	
:

	
____________________

	  	  	  	  	  	  
	
Date

	
:

	
____________________

	
Date

	
:

	
____________________

 

	
LAN AIRLINES S.A.

	 
	  	 
	
By

	
:

	
___________________

	 
	  	  	  	 
	
Its

	
:

	
___________________

	 
	  	  	  	 
	
Date

	
:

	
___________________

	 

A320F - LAN - AMDT 9 - Second A320 Family PA

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157/180

  

LETTER AGREEMENT N°7I

 

APPENDIX No.1 to LETTER AGREEMENT No.7I

 

[***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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158/180

  

LETTER AGREEMENT N°7J

 

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

 

Subject: [***]

 

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the 2010 Incremental Aircraft described therein.

 

Capitalized terms used herein and not otherwise defined in this letter agreement N°7J to Amendment N°9 (the “Letter Agreement N°7J”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

 

Both Parties agree that this Letter Agreement N° 7J, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°7J.

 

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LETTER AGREEMENT N°7J

 

This Letter Agreement No.7J shall be applicable to the [***]

 

	
1

	
[***]

 

	
2

	
[***]

 

	
3

	
[***]

 

	
4

	
[***].

 

	
5

	
[***].

 

	
6

	
[***]

 

	
7

	
[***].

 

	
8

	
[***]

 

	
9

	
[***].

 

	
10.

	
[***].

 

	
11.

	
[***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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160/180

  

LETTER AGREEMENT N°7J

 

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°7J to the Seller.

 

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  	  	  	  	  
	
By

	
:

	
____________________

	
By

	
:

	
____________________

	  	  	  	  	  	  
	
Its

	
:

	
____________________

	
Its

	
:

	
____________________

	  	  	  	  	  	  
	
Date

	
:

	
____________________

	
Date

	
:

	
____________________

 

	
LAN AIRLINES S.A.

	 
	  	 
	
By

	
:

	
___________________

	 
	  	  	  	 
	
Its

	
:

	
___________________

	 
	  	  	  	 
	
Date

	
:

	
___________________

	 

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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161/180

  

LETTER AGREEMENT N°7J

 

APPENDIX No.1 to LETTER AGREEMENT No.7J

 

[***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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162/180

  

LETTER AGREEMENT N°7K

 

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

 

Subject: [***].

 

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the 2010 Incremental Aircraft described therein.

 

Capitalized terms used herein and not otherwise defined in this letter agreement N°7K to Amendment N°9 (the “Letter Agreement N°7K”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

 

Both Parties agree that this Letter Agreement N° 7K, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°7K.

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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LETTER AGREEMENT N°7K

 

This Letter Agreement No.7K shall be applicable to the [***]

 

	
1

	
[***]

 

	
2

	
[***]

 

	
3

	
[***]

 

	
4

	
[***]

 

	
5

	
[***]

 

	
6

	
[***]

 

	
7

	
[***]

 

	
8

	
[***]

 

	
9

	
[***]

 

	
10.

	
[***]

 

	
11.

	
[***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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164/180

  

LETTER AGREEMENT N°7K

 

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°7K to the Seller.

 

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  	  	  	  	  
	
By

	
:

	
____________________

	
By

	
:

	
____________________

	  	  	  	  	  	  
	
Its

	
:

	
____________________

	
Its

	
:

	
____________________

	  	  	  	  	  	  
	
Date

	
:

	
____________________

	
Date

	
:

	
____________________

 

	
LAN AIRLINES S.A.

	 
	  	 
	
By

	
:

	
___________________

	 
	  	  	  	 
	
Its

	
:

	
___________________

	 
	  	  	  	 
	
Date

	
:

	
___________________

	 

A320F - LAN - AMDT 9 - Second A320 Family PA

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165/180

  

LETTER AGREEMENT N°7K

 

APPENDIX No.1 to LETTER AGREEMENT No.7K

 

[***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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LETTER AGREEMENT N°7L

 

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

 

Subject: [***]

 

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the 2010 Incremental Aircraft described therein.

 

Capitalized terms used herein and not otherwise defined in this letter agreement N°7L to Amendment N°9 (the “Letter Agreement N°7L”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

 

Both Parties agree that this Letter Agreement N° 7L, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°7L.

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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167/180

  

LETTER AGREEMENT N°7L

 

This Letter Agreement No.7L shall be applicable to the [***]

 

	
1

	
[***].

 

	
2

	
[***].

 

	
3

	
[***]

 

	
4

	
[***].

 

	
5

	
[***].

 

	
6

	
[***].

 

	
7

	
[***].

 

	
8

	
[***].

 

	
9

	
[***].

 

	
10.

	
[***].

 

	
11.

	
[***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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168/180

  

LETTER AGREEMENT N°7L

 

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°7L to the Seller.

 

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  	  	  	  	  
	
By

	
:

	
____________________

	
By

	
:

	
____________________

	  	  	  	  	  	  
	
Its

	
:

	
____________________

	
Its

	
:

	
____________________

	  	  	  	  	  	  
	
Date

	
:

	
____________________

	
Date

	
:

	
____________________

 

	
LAN AIRLINES S.A.

	 
	  	 
	
By

	
:

	
___________________

	 
	  	  	  	 
	
Its

	
:

	
___________________

	 
	  	  	  	 
	
Date

	
:

	
___________________

	 

A320F - LAN - AMDT 9 - Second A320 Family PA

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169/180

  

LETTER AGREEMENT N°7L

 

APPENDIX No.1 to LETTER AGREEMENT No.7L

 

[***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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170/180

  

Letter Agreement No. 8

 

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

 

Subject  : [***]

 

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the Incremental Aircraft described therein.

 

Capitalized terms used herein and not otherwise defined in this letter agreement N°8 to Amendment N°9 (the “Letter Agreement N°8”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

 

Both Parties agree that this Letter Agreement N° 8, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°8.

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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171/180

  

Letter Agreement No. 8

 

	
0.

	
[***].

 

	
1.

	
T[***]

 

	
2.

	
[***]

 

	
3.

	
Assignment

 

	
  

	
The Parties agree that clause 21 of the Second A320 Family Purchase Agreement shall govern the assignability and transferability of each Party’s rights and obligations under this Letter Agreement N° 8.

 

	
4.

	
Confidentiality

 

	
  

	
Each of the Parties hereto agree that the provisions of this Letter Agreement N° 8 are personal to it and will not without the prior written consent of the other Parties disclose such information to any other Party. [***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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172/180

  

Letter Agreement No. 8

 

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°8 to the Seller.

 

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  	  	  	  	  
	
By

	
:

	
____________________

	
By

	
:

	
____________________

	  	  	  	  	  	  
	
Its

	
:

	
____________________

	
Its

	
:

	
____________________

	  	  	  	  	  	  
	
Date

	
:

	
____________________

	
Date

	
:

	
____________________

 

	
LAN AIRLINES S.A.

	 
	  	 
	
By

	
:

	
___________________

	 
	  	  	  	 
	
Its

	
:

	
___________________

	 
	  	  	  	 
	
Date

	
:

	
___________________

	 

A320F - LAN - AMDT 9 - Second A320 Family PA

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173/180

  

Letter Agreement No. 9

 

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

 

Subject: [***]

 

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the Incremental Aircraft described therein.

 

Capitalized terms used herein and not otherwise defined in this letter agreement N°9 to Amendment N°9 (the “Letter Agreement N°9”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

 

Both Parties agree that this Letter Agreement N°9, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Letter Agreement N°9.

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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174/180

  

Letter Agreement No. 9

 

	
1.

	
[***].

 

	
2.

	
[***].

 

	
3.

	
Assignment

 

	
  

	
The Parties agree that clause 21 of the Second A320 Family Purchase Agreement shall govern the assignability and transferability of each Party’s rights and obligations under this Letter Agreement N°9.

 

	
4.

	
Confidentiality

 

	
  

	
Each of the Parties hereto agree that the provisions of this Letter Agreement N°9 are personal to it and will not without the prior written consent of the other Parties disclose such information to any other Party. [***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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175/180

  

Letter Agreement No. 9

 

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Letter Agreement N°9 to the Seller.

 

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  	  	  	  	  
	
By

	
:

	
____________________

	
By

	
:

	
____________________

	  	  	  	  	  	  
	
Its

	
:

	
____________________

	
Its

	
:

	
____________________

	  	  	  	  	  	  
	
Date

	
:

	
____________________

	
Date

	
:

	
____________________

 

	
LAN AIRLINES S.A.

	 
	  	 
	
By

	
:

	
___________________

	 
	  	  	  	 
	
Its

	
:

	
___________________

	 
	  	  	  	 
	
Date

	
:

	
___________________

	 

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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176/180

  

Letter Agreement No. 9

 

Appendix 1

 

[***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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177/180

  

Side Letter No. 1

 

LAN AIRLINES S.A.

Edificio Huidobro

Avenida Presidente Riesco 5711

Las Condes

Santiago - Chile

 

Subject  : [***]

 

LAN Airlines S.A (the “Buyer") and Airbus S.A.S. (the “Seller") have entered into an amendment N°9 to the Second A320 Purchase Agreement (as defined therein) dated of even date herewith (“Amendment N°9”), and which covers the manufacture and the sale by the Seller and the purchase by the Buyer of the Incremental Aircraft described therein.

 

Capitalized terms used herein and not otherwise defined in this side letter N°1 to Amendment N°9 (the “Side Letter N°1”) shall have the meanings assigned thereto in the Second A320 Family Purchase Agreement and/or Amendment N°9 as the case may be.

 

Both Parties agree that this Side Letter N°1, upon execution thereof, shall constitute an integral, non-severable part of said Amendment N°9 and shall be governed by all its provisions, as such provisions have been specifically amended pursuant to this Side Letter N°1.

 

A320F - LAN - AMDT 9 - Second A320 Family PA

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178/180

  

Side Letter No. 1

 

	
1.

	
[***]

 

	
2.

	
[***]

 

	
3.

	
Assignment

 

	
  

	
This Side Letter N°1 and the rights and obligations of the Buyer herein shall not be assigned or transferred in any manner without the prior written consent of the Seller, and any attempted assignment or transfer in contravention of the provisions of this Side Letter N°1  shall be void and of no force or effect.

 

	
4.

	
Confidentiality

 

	
  

	
Each of the Parties hereto agree that the provisions of this Side Letter N°1 are personal to it and will not without the prior written consent of the other Parties disclose such information to any other Party. [***]

 

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

179/180

  

Side Letter No. 1

 

If the foregoing correctly sets forth our understanding, please execute two (2) originals in the space provided below and return one (1) original of this Side Letter N°1 to the Seller.

 

	
Agreed and Accepted

	
Agreed and Accepted

	  	  
	
For and on behalf of

	
For and on behalf of

	  	  
	
LAN AIRLINES S.A.

	
AIRBUS S.A.S.

	  	  	  	  	  	  
	
By

	
:

	
____________________

	
By

	
:

	
____________________

	  	  	  	  	  	  
	
Its

	
:

	
____________________

	
Its

	
:

	
____________________

	  	  	  	  	  	  
	
Date

	
:

	
____________________

	
Date

	
:

	
____________________

 

	
LAN AIRLINES S.A.

	 
	  	 
	
By

	
:

	
___________________

	 
	  	  	  	 
	
Its

	
:

	
___________________

	 
	  	  	  	 
	
Date

	
:

	
___________________

	 

 

A320F - LAN - AMDT 9 - Second A320 Family PA

Ref. CT1003496

  

180/180Exhibit 4.2.4

 

Supplemental Agreement No. 28 (“SA-28”)

to

Purchase Agreement No. 2126

between

THE BOEING COMPANY

and

LAN AIRLINES S.A.

 

Relating to Boeing Model 767-316ER, Model 767-38EF, and Model 767-316F Aircraft

 

THIS SUPPLEMENTAL AGREEMENT, entered into as of the 22 day of  March of 2010, by and between THE BOEING COMPANY, a Delaware corporation (hereinafter called “Boeing”), and LAN Airlines S.A., a Chilean corporation (hereinafter called “Customer”);

 

WITNESSETH:

 

WHEREAS, the parties entered into that certain Purchase Agreement No. 2126, dated as of January 30, 1998 relating to the purchase and sale of Boeing Model 767-316ER, Model 767-38EF, and Model 767-316F aircraft (hereinafter referred to as "Aircraft") which agreement, including all tables, exhibits, supplemental exhibits and specifications thereto, together with all letter agreements then or thereafter entered into that by their terms constitute part of such purchase agreement and as such purchase agreement may be amended or supplemented from time to time, is hereinafter called the "Purchase Agreement;"

 

WHEREAS, the parties have agreed to accelerate the delivery of ten (10) Model 787-8 aircraft, substitute four (4) aircraft from 787-916 to 787-816 and substitute three (3) 767-316ER to 767-316F freighter aircraft, and

 

WHEREAS, the parties have agreed upon the three (3) Boeing Model 767-316ER Aircraft being substituted to 767-316F Aircraft and have agreed to a deferral in the delivery of such Aircraft.

 

WHEREAS, Boeing and Customer have agreed to amend the Purchase Agreement to incorporate the above changes;

 

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

 

1.           Substitute 767 Freighter Aircraft.  In accordance with Letter Agreement 6-1162-ILK-0383R1, paragraph 3 the two (2) 767-316ER 2012 Deferral Aircraft are substituted to 767-316F Aircraft leaving no 2012 Deferral Aircraft and in accordance with Letter Agreement 6-1162-KSW-6424, paragraph 3 one (1) 767-316ER Incremental Aircraft is substituted to a 767-316F Aircraft leaving one Incremental Aircraft remaining.  Letter Agreement 6-1162-KSW-6424, paragraphs 4 and 5 no longer apply to the Incremental Aircraft converted to a 767-316F aircraft.  The three (3) Aircraft substituted from 767-316ER Aircraft to 767-316F Aircraft are shown in the chart below (hereinafter the “Substitute 767 Freighter Aircraft”).

  

 

  

	
Manufacturer’s

Serial Number

	  	
Previous Aircraft

Minor Model

	  	
Revised Aircraft

Minor Model

	  	
Original

Contract

Delivery

	  	
Revised Contract

Delivery

	  	  	  	  	  	  	  	  	  
	
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

 

2.           Boeing will notify Customer of the delivery month of each Substitute 767 Freighter Aircraft eighteen (18) months prior to the scheduled delivery month and a supplemental agreement will be executed within thirty (30) days making the changes to the Purchase Agreement reflecting the delivery month, the corresponding price (the current price escalated in accordance with the escalation factor) and the BFE on dock dates.  Boeing and Customer will work diligently and in good faith to sign the supplemental agreement in 30 days.

3.           Table of Contents.  The Table of Contents to the Purchase Agreement is revised and a revised Table of Contents dated January 2010 is attached hereto.

 

4.           Tables.

 

4.1           Aircraft Information Table 11, Aircraft Delivery, Description, Price and Advance Payments is revised to delete the Aircraft delivering in September 2012, October 2012 and November 2012.  The revised Table 11 dated January 2010 is attached hereto.

 

4.2           Aircraft Information Table 12, Aircraft Delivery, Description, Price and Advance Payments for the Substitute 767 Freighter Aircraft, attached hereto, is added to the Purchase Agreement.

 

5.           Exhibits.

 

Exhibit A-10, Aircraft Configuration relating to the Substitute 767 Freighter Aircraft, attached hereto, is added to the Purchase Agreement.

 

6.           Letter Agreements.

 

6.1           Letter Agreement 6-1162-ILK-0381R1 entitled “Special Matters Letter Applicable to the 2011 Accelerated Aircraft and the 2012 Deferral Aircraft is deleted and replaced by Letter Agreement 6-1162-ILK-0381R2 entitled “Special Matters Letter Applicable to the 2011 Accelerated Aircraft and the Substitute 767 Freighter Aircraft,” attached hereto.

 

6.2           Letter Agreement 6-1162-ILK-0384R2 entitled “16G Seats Requirements” does not apply to the Substitute 767 Freighter Aircraft.

 

6.3           Letter Agreement 6-1162-ILK-0388 entitled “Option Aircraft” is deleted.

 

6.4           Letter Agreement 6-1162-KSW-6456 entitled “Performance Guarantees Relating to the Substitute 767 Freighter Aircraft, attached hereto, is added to the Purchase Agreement.

  

 

  

 

7.           Amount Due at Signing.  [***].

 

8.           Confidentiality.

 

Boeing and Customer understand that the commercial and financial information contained in this Supplemental Agreement is considered by the parties as confidential (Confidential Information) and both agree not to disclose such Confidential Information except as provided herein.  In addition to the parties’ respective officers, directors and employees who need to know the Confidential Information and who understand the obligation to keep it confidential, the parties may disclose Confidential Information (1) to the extent required by law and (2) to its agents, auditors and advisors who need to know the Confidential Information for purposes of enabling each party to understand, perform its obligations under, or receive the benefits of, this Supplemental Agreement and who have agreed not to use or disclose the Confidential Information for any other purpose without the other party’s prior written consent.  In the event that a party concludes that disclosure of Confidential Information contained in this Supplemental Agreement is required by applicable law, the party will so advise the other party promptly in writing and endeavor to protect the confidentiality of such Confidential Information to the widest extent possible.  In the event of a legal dispute with Boeing, nothing herein will preclude Customer from sharing with its legal counsel information necessary for purposes of enabling counsel to advise or represent Customer provided that so long as Customer causes its legal counsel to maintain the confidentiality of information that is the subject of this Article.  Except as provided in the assignment provisions of Article 7 of the Special Matters Applicable to the Incremental Aircraft; 6-1162-KSW-6423; Article 21 of Letter Agreement 6-1162-LAJ-0895R6 entitled “Business Considerations”; Article 8 of Letter Agreement 6-1162-ILK-0381R2 entitled “Special Matters Letter Applicable to the 2011 Accelerated Aircraft and the Substitute 767 Freighter Aircraft”; and Article 9 of Letter Agreement 6-1162-ILK-0412 entitled “Special Matters Relating to Three Aircraft Originally Scheduled to Deliver in 2009”, Customer will not disclose this Supplemental Agreement for purposes of financing payments without the prior written consent of Boeing, which consent will be provided once the financier enters into a Non Disclosure Agreement with Boeing in form and substance reasonably satisfactory to Boeing, which will include agreeing not to disclose or use Confidential Information except for the purpose set forth herein. This provision shall not apply to any Confidential Information that is in the public domain except that a party will be liable to the other for breach of its obligations under this provision if the Confidential Information entered the public domain as a consequence of a wrongful act or omission on its part.

  

 

  

The Purchase Agreement shall be deemed amended to the extent herein provided and as amended shall continue in full force and effect.

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

	
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

  

 

  

PURCHASE AGREEMENT NUMBER 2126

between

THE BOEING COMPANY

and

LAN Airlines  S.A.

 

Relating to Boeing Model 767-316ER, Model 767-38EF, and Model 767-316F Aircraft

  

 

  

TABLE OF CONTENTS

	  	 	  	 	
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

  

 

  

 

RESTRICTED LETTER AGREEMENTS

 

	
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

	
  

	  	
  

	  	
  

	  	
  

	  	
  

	  	
  

	  	
  

	  	
  

	  

	
[***]     

	
[***]

	  	
[***]

	  	
[***]

  

 

  

 

6-1162-ILK-0381R2

 

LAN Airlines S.A.

Avenida Presidente Riesco 5711

Piso 19

Las Condes

Santiago, Chile

 

	
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")

 

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

 

	
  

	
1.

	
 Definitions.

 

1.1      “STE” when used specifically in relation to any credit memorandum contained in this letter agreement shall mean that the relevant credit memorandum shall be escalated to the month of delivery in the same manner as the Airframe Price in accordance with the escalation formula reflected in Supplemental Exhibit AE1 2008$ to the Purchase Agreement entitled “Escalation adjustment - airframe and optional features”.

 

1.2      “Limitations on Use” when used in relation to any credit memorandum contained in this letter agreement shall mean that the applicable credit memorandum may be used for the purchase of Boeing goods and services or applied to the final delivery payment for the Aircraft for which the credit was issued, but that the relevant credit memorandum shall be prohibited from use for satisfaction of any Advance Payment obligation.

 

1.3      “2011 Accelerated Aircraft” shall mean either or both, as the case may be, of the two new Boeing Model 767-316ER Aircraft originally scheduled for delivery during the months of February and March of 2012, which contingent upon satisfaction of the terms of this letter agreement, are now scheduled for delivery in October and November of 2011, respectively.

 

1.4      “2012 Deferral Aircraft” shall mean the two (2) 767-300ER Aircraft scheduled for delivery in October and November 2012 that were substituted to 767-316F Aircraft.

 

1.5      [***].

 

1.6      “Incremental Aircraft” shall mean either or both, as the case may be, of the two new Boeing Model 767-316ER Aircraft scheduled for delivery during the months of September 2011 and September of 2012 to be purchased by Customer.  Supplemental Agreement 28 converts the September 2012 Incremental Aircraft into a Substitute 767 Freighter Aircraft.

 

1.7      [***].

 

1.8       “Table 11” shall mean the table entitled “Aircraft Information Table 11 to the Purchase Agreement”.

 

1.9      “Table 12” shall mean the table entitled “Aircraft Information Table 12 for the Substitute 767 Aircraft to the Purchase Agreement”.

  

 

  

  

 

  

 

1.10    “Substitute 767 Freighter Aircraft” shall mean the three (3) Boeing Model 767-316F Aircraft bearing serial numbers 40799, 40592, and 40593 now scheduled for delivery in 2nd Quarter 2013, 4th Quarter 2013, and 1st Quarter 2014, respectively.  Prior to substitution, these Aircraft were the two (2) 2012 Deferral Aircraft and one (1) Incremental Aircraft.

 

	
  

	
2.

	
Export License.

 

Customer understands and confirms that it is Customer’s responsibility to obtain any required Export License from the relevant U.S. authority.  Without accepting any liability for any failure to do so, Boeing will use reasonable endeavors to alert Customer to any regulatory changes of which Boeing becomes aware and which require Customer to obtain such Export License.

 

	
  

	
3.

	
Warranty Modification.

 

Notwithstanding paragraph 3.2 of Part 2 of Exhibit C to the AGTA, Boeing agrees that the warranty period for a Corrected Boeing Product resulting from a defect in material or workmanship is 6 months or the remainder of the initial warranty period, whichever is longer.

 

	
  

	
4.

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

 

Subject to Customer’s adherence to the Limitations on Use, Boeing will provide the Customer with a credit memorandum concurrently with the delivery of each Aircraft, in description and amount which is identified in the credit memoranda table 4.1 for each of the 2011 Accelerated Aircraft and in credit memoranda table 4.2 for each of the Substitute 767 Freighter Aircraft:

 

Table 4.1 Credit Memoranda Table Exclusive to the 2011 Accelerated Aircraft

 

	
[***]

	
[***]

	  	  
	
[***]

	
[***]

	  	  
	
[***]

	
[***]

	  	  
	
[***]

	
[***]

 

Table 4.2 Credit Memoranda Table Exclusive to the Substitute 767 Freighter Aircraft

 

	
[***]

	
[***]

	  	  
	
[***]

	
[***]

	  	  
	
[***]

	
[***]

	  	  
	
[***]

	
[***]

  

 

  

 

4.2.3                 [***].

 

[***].

 

	
  

	
5.

	
[***].

 

5.1            [***]:

 

	 	
[***].

	
[***]

	
[***]

	 	 
	
[***]

	
[***]

	 	 
	
[***]

	
[***]

	
[***]

	
[***]

	
[***]

	
[***]

	
[***]

	
[***]

	
[***]

	
[***]

	
[***]

	
[***]

	
[***]

	
[***]

	
[***]

	
[***]

 

* - [***].

 

ü - [***].

 

# [***].

 

5.2            [***]. [***]                      

 

5.3            [***]:

 

(i)  [***]

 

(ii) [***].

 

5.4            [***].

 

	
  

	
6.

	
Special Considerations for the Substitute Aircraft.

 

6.1            If Customer elects to change the configuration of any 2011 Accelerated Aircraft from a 767-316ER Passenger Aircraft to a 767-316F Freighter Aircraft in accordance with the terms of Letter Agreement 6-1162-ILK-0383R1 entitled “Aircraft Model Substitution Relating to the 2011 Accelerated Aircraft (such Customer election creating a Substitute Aircraft), then the following provisions shall apply:

 

6.2            Aircraft Purchase Price.  The Airframe Base Price, Optional Features Prices, Engine Price and Aircraft Basic Price of a Substitute Aircraft shall be as set forth in Exhibit A to this Letter Agreement for the applicable Substitute Aircraft.

  

 

  

 

6.3            Economic Considerations. The credit memoranda applicable to any Substitute Aircraft will be revised as set forth in Exhibit B to this Letter Agreement.

 

6.4            Optional Features.  The Aircraft Basic Price for any Substitute Aircraft incorporates the selected Optional Features Prices set forth in Exhibit C to this Letter Agreement.

 

6.5            Advance Payments.  Customer may apply the terms of the following to its payment obligations arising from Customer’s purchase of any Substitute Aircraft:

 

	
  

	
6.5.1

	
Article 5 of this Letter Agreement; and

 

	
  

	
6.5.2

	
[***].

 

	
  

	
7.

	
Intentionally Deleted.

 

	
  

	
8.

	
Assignment.

 

Any assignment by Customer of any benefits, entitlements, or services described in this Letter Agreement requires Boeing's prior written consent.  Further, Customer will not reveal to any third party the amount of the credit memoranda provided to Customer by Boeing without Boeing’s prior written consent and subject to such circumstances as Boeing may reasonably require.

 

Boeing will not unreasonably withhold consent to Customer’s request to assign, as security, rights in the Purchase Agreement if done for purposes of obtaining financing or for such other purpose consistent with fulfilling its obligations under the Purchase Agreement.  Boeing’s consent will be conditioned on all parties accepting Boeing’s customary conditions for consenting to an assignment, including, but not limited to, the following: assignor and assignee indemnification of Boeing for any actions taken by an assignee under any assignment agreement; Boeing’s right to exercise the manufacturer’s option to assume Customer’s rights under the Purchase Agreement in the event of a default under an assignment agreement; and confidentiality.  A Party that is

 

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

 

shall be deemed a “Financing Party”.

 

Without Boeing’s consent, Customer may represent to any Financing Party that Boeing will provide to that Financing Party, concurrently with the delivery of each of the Aircraft to that Financing Party, a financier credit memorandum equal to

 

(a)  [***]

 

(b)  [***]

 

escalated to the month of delivery in the same manner as the Airframe Price as described in Supplemental Exhibit AE-1 and in conformance with terms and conditions of this Letter Agreement.  Insofar as such Financing Party is concerned, this Financier Credit Memorandum shall be in lieu of any other provision in the Letter Agreement. When the Customer identifies a Financing Party and the preliminary terms of an assignment under which pre-delivery payment financing or aircraft purchase financing could be provided, at Customer’s request, Boeing agrees to enter into discussions with the Customer to consider whether an additional credit memorandum can be assigned, with the goal of helping Customer obtain third-party financing.

  

 

  

 

Boeing will consent to any reasonable request by Customer to assign the Purchase Agreement to an affiliate provided that Boeing is provided with an adequate  guarantee of performance of all obligations under this Purchase Agreement and in a form reasonably satisfactory to Boeing.

 

Customer understands that Boeing is not required under any circumstances to consent to an assignment that would constitute a novation.

 

The foregoing provisions are intended to supplement, and not to supersede, the assignment provisions of the AGTA, which address delivery date and post-delivery assignments, merger-type assignments, and other matters.

 

	
  

	
9.

	
16G Seat Requirement Credit Memorandum.

 

In the event that Customer notifies Boeing of a selection of record option 2525C826G85 (for Boeing certification of the business class, economy class and attendant seats to Federal Aviation Administration (FAA) Regulation Information Number 2120-AC84 entitled “Improved Seats in Air Carrier Transport Category Airplanes” (the 16G Requirement) in lieu of existing 9G capability) (such record option, including successor record options which supersede the identified record option, are herein referred to as the 16G Record Option), [***]:

	
[***]

	
[***]

	
[***]

	
[***]

	
[***]

	
[***]

 

Boeing acknowledges that Customer has provided a waiver for the 2011 Aircraft and does not have to comply with the 16G requirement for said Aircraft.

 

	
  

	
10.

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

 

	
  

	
11.

	
[***].

 

	
  

	
12.

	
Confidentiality.

 

Boeing and Customer understand that the commercial and financial information contained in this Letter Agreement is considered by the parties as confidential (Confidential Information) and both agree not to disclose such Confidential Information except as provided herein.  In addition to the parties’ respective officers, directors and employees who need to know the Confidential Information and who understand the obligation to keep it confidential, the parties may disclose Confidential Information (1) to the extent required by law and (2) to its agents, auditors and advisors who need to know the Confidential Information for purposes of enabling each party to understand, perform its obligations under, or receive the benefits of, this Letter Agreement and who have agreed not to use or disclose the Confidential Information for any other purpose without the other party’s prior written consent.  In the event that a party concludes that disclosure of Confidential Information contained in this Letter Agreement is required by applicable law, the party will so advise the other party promptly in writing and endeavor to protect the confidentiality of such Confidential Information to the widest extent possible.  In the event of a legal dispute with Boeing, nothing herein will preclude Customer from sharing with its legal counsel information necessary for purposes of enabling counsel to advise or represent Customer provided that so long as Customer causes its legal counsel to maintain the confidentiality of information that is the subject of this Article.  Except as provided in the assignment provisions of Article 7 of Letter Agreement 6-1162-KSW-6423, Special Matters Applicable to the Incremental Aircraft; Article 21 of Letter Agreement 6-1162-LAJ-0895, as amended, entitled “Business Considerations”; Article 8 herein and Article 9 of Letter Agreement 6-1162-ILK-0412 entitled “Special Matters Relating to Three Aircraft Originally Scheduled to Deliver in 2009”, Customer will not disclose this Letter Agreement for purposes of financing payments without the prior written consent of Boeing, which consent will be provided once the financier enters into a Non Disclosure Agreement with Boeing in form and substance reasonably satisfactory to Boeing, which will include agreeing not to disclose or use Confidential Information except for the purpose set forth herein. This provision shall not apply to any Confidential Information that is in the public domain except that a party will be liable to the other for breach of its obligations under this provision if the Confidential Information entered the public domain as a consequence of a wrongful act or omission on its part.

  

 

  

The Purchase Agreement shall be deemed amended to the extent herein provided and as amended shall continue in full force and effect.

 

Very truly yours,

	
THE BOEING COMPANY

	  	 	  
	
By:

	 	  
	  	
Kathie S. Weibel

	 
	 	 	 
	
Its:

	Attorney-In-Fact	 

 

  

 

  

 

If the foregoing correctly sets forth your understanding of our agreement with respect to the matters treated herein, please indicate your acceptance, agreement and approval.

	
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:

	
  

	
[***]

  

 

  

AIRCRAFT CONFIGURATION

between

THE BOEING COMPANY

and

LAN AIRLINES S.A.

Exhibit A-10 to Purchase Agreement Number 2126

  

 

  

AIRCRAFT CONFIGURATION

relating to

BOEING MODEL 767-316F AIRCRAFT

THE LAN AIRCRAFT

The Detail Specification will be D019-T002LAN63F-2 which will be comprised of Boeing Configuration Specification D019T002, Revision I dated December 12, 2008 revised to incorporate the Options listed below, including the effects on Manufacturer's Empty Weight (MEW) and Operating Empty Weight (OEW).  These Options are the same Options listed in Letter Agreement 6-1162-KSW-6423 Exhibit C.  As soon as practicable, Boeing will furnish to Customer copies of the Detail Specification, which copies will reflect such Options.  The Aircraft Basic Price reflects and includes all effects of such Options, except such Aircraft Basic Price does not include the price effects of any Buyer Furnished Equipment or Seller Purchased Equipment.

  

 

  

	
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:

	
  

	
[***]

  

 

  

 

Exhibit A to Letter Agrement 6-1162-ILK-0381R2

Article 6.2

Substitute Aircraft Delivery, Description, Price and Advance Payments

 

	
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

	
  

	  	
  

	  	
  

	  	
  

	  	
  

	  	
  

	  	
  

	  	
  

	  

 

EXHIBIT 2: ARTICLE 6.2, SUBSTITUTE AIRCRAFT

 

SA-28

	
P. A. No. 2126

	
Boeing Proprietary

	  
	
Attachment A

	  	
Page 1

 

  

 

  

6-1162-KSW-6456

 

LAN Airlines S.A.

Avenida Presidente Riesco 5711

Piso 19

Las Condes

Santiago, Chile

Subject:           Aircraft Performance Guarantees

Reference:       Purchase Agreement No. 2126 (Purchase Agreement) between The Boeing Company (Boeing) and LAN Airlines S.A. (Customer) relating to three Model 767-316F aircraft (Substitute 767 Freighter Aircraft)

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

Boeing agrees to provide Customer with the performance guarantees in the Attachment.  [***].

Notwithstanding any other provisions of the Purchase Agreement, the rights and obligations described in this Letter Agreement are provided to Customer in consideration of Customer becoming the operator of the Aircraft and cannot be assigned, in whole or in part.

The information contained herein represents confidential business information and has value precisely because it is not available generally or to other parties.  Customer will limit the disclosure of its contents to employees of Customer with a need to know the contents for purposes of helping Customer perform its obligations under the Purchase Agreement and who understand they are not to disclose its contents to any other person or entity without the prior written consent of Boeing.

  

 

  

	
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

  

 

  

 

MODEL 767-316F FREIGHTER PERFORMANCE GUARANTEES

 

FOR LAN AIRLINES S.A.

 

	
SECTION

	 	
CONTENTS

	  	 	  
	
1

	 	
AIRCRAFT MODEL APPLICABILITY

	  	 	  
	
2

	 	
FLIGHT PERFORMANCE

	  	 	  
	
3

	 	
MANUFACTURER'S EMPTY WEIGHT

	  	 	  
	
4

	 	
AIRCRAFT CONFIGURATION

	  	 	  
	
5

	 	
GUARANTEE CONDITIONS

	  	 	  
	
6

	 	
GUARANTEE COMPLIANCE

	  	 	  
	
7

	 	
EXCLUSIVE GUARANTEES

  

 

  

	
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:

 

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

 

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

 

	
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

 

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

 

  

 

  

Supplemental Agreement No. 29 (“SA-29”)

 

to

 

Purchase Agreement No. 2126

 

between

 

THE BOEING COMPANY

 

and

 

LAN AIRLINES S.A.

 

Relating to Boeing Model 767-316ER, Model 767-38EF, and Model 767-316F Aircraft

 

THIS SUPPLEMENTAL AGREEMENT, entered into as of the ___ day of November of 2010, by and between THE BOEING COMPANY, a Delaware corporation (hereinafter called “Boeing”), and LAN Airlines S.A., a Chilean corporation (hereinafter called “Customer”);

 

WITNESSETH:

 

WHEREAS, the parties entered into that certain Purchase Agreement No. 2126, dated as of January 30, 1998 relating to the purchase and sale of Boeing Model 767-316ER, Model 767-38EF, and Model 767-316F aircraft (hereinafter referred to as "Aircraft") which agreement, including all tables, exhibits, supplemental exhibits and specifications thereto, together with all letter agreements then or thereafter entered into that by their terms constitute part of such purchase agreement and as such purchase agreement may be amended or supplemented from time to time, is hereinafter called the "Purchase Agreement;"

 

WHEREAS, the parties have mutually agreed to (i) accelerate the delivery of three Aircraft and (ii) substitute the three Aircraft from 767-316F to 767-316ER (each and collectively “2012 Accelerated Aircraft”); and

 

WHEREAS, Boeing and Customer have agreed to amend the Purchase Agreement to incorporate the above changes;

 

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

 

	
1.

	
Table of Contents, Articles, Tables, Exhibits and Supplemental Exhibits:

 

1.1.          Table of Contents. The “Table of Contents” to the Purchase Agreement is deleted in its entirety and the new “Table of Contents” attached hereto is substituted in lieu thereof to reflect the changes made by this SA-29.

 

1.2.          Deletion of Table 12.  The “Aircraft Information Table 12 to Purchase Agreement No. 2126, Aircraft Delivery, Description, Price and Advance Payments” is deleted in its entirety since it is no longer applicable.

 

1.3.          Addition of Table 13.  “Aircraft Information Table 13 to Purchase Agreement No. 2126, Aircraft Delivery, Description, Price and Advance Payments” attached hereto is added to the Purchase Agreement to reflect, among other things, the scheduled delivery month, price and Advance Payments applicable to the 2012 Accelerated Aircraft.

  

 

  

 

1.4.          Deletion of Exhibit A-10.  “Aircraft Configuration 767-316F Aircraft-2008$ to Purchase Agreement No. 2126”, Aircraft Delivery, Description, Price and Advance Payments” is deleted in its entirety since it is no longer applicable.

 

1.5.          Addition of Exhibit A-11.  “Aircraft Configuration 767-316ER Aircraft-2010$ to Purchase Agreement No. 2126” attached hereto is added to the Purchase Agreement to reflect, among other things, the price of Customer selected Optional Features applicable to the 2012 Accelerated Aircraft.

 

1.6.          Addition of Supplemental Exhibit EE1-2010$.  Supplemental Exhibit EE1-2010$ entitled “Engine Escalation, Engine Warranty & Patent Indemnity” attached hereto is added to the Purchase Agreement to provide the 2010 base year escalation formula applicable to the prices of engines selected by the Customer for the 2012 Accelerated Aircraft.

 

1.7.          Addition of Supplemental Exhibit AE1-2010$.  Supplemental Exhibit AE1-2010$ entitled “Escalation adjustment-airframe and optional features” attached hereto is added to the Purchase Agreement to provide the 2010 base year escalation formula applicable to the 2012 Accelerated Aircraft.

 

	
2.

	
Restricted Letter Agreements.

 

2.1.          Addition of Special Matters Letter Applicable to the 2012 Accelerated Aircraft.  Letter Agreement 6-1162-ILK-0450 entitled “Special Matters Letter Applicable to the 2012 Accelerated Aircraft” (Special Matters Letter Applicable to the 2012 Accelerated Aircraft), a copy of which is attached hereto, is added to the Agreement to provide the terms and conditions, including the economic considerations, applicable to each 2012 Accelerated Aircraft.

 

2.2.          Revision of Special Matters Letter Applicable to the 2011 Accelerated Aircraft and the Substitute 767 Freighter Aircraft.  The parties mutually agree that Letter Agreement 6-1162-ILK-0381R2 entitled “Special Matters Letter Applicable to the 2011 Accelerated Aircraft and the Substitute 767 Freighter Aircraft” is no longer applicable.

 

2.3.          Deletion of Performance Guarantees Relating to the Substitute 767 Freighter Aircraft.  Letter Agreement 6-1162-KSW-6456 entitled “Performance Guarantees Relating to the Substitute 767 Freighter Aircraft” is deleted from the Purchase Agreement since it is no longer applicable.

 

2.4.          Applicability of 16G Seats Letter to each 2012 Accelerated Aircraft.  Letter Agreement 6-1162-ILK-0384R1 entitled “16G Seats” applies to each 2012 Accelerated Aircraft.

 

	
3.

	
Payment Due at Effective Date of this Supplemental Agreement.

 

To effect the implementation of this SA-29, payments to Boeing are due by Customer as follows:

 

	
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.

 

Boeing and Customer understand that the commercial and financial information contained in this Supplemental Agreement is considered by the parties as confidential (Confidential Information) and both agree not to disclose such Confidential Information except as provided herein.  In addition to the parties’ respective officers, directors and employees who need to know the Confidential Information and who understand the obligation to keep it confidential, the parties may disclose Confidential Information (1) to the extent required by law and (2) to its agents, auditors and advisors who need to know the Confidential Information for purposes of enabling each party to understand, perform its obligations under, or receive the benefits of, this Supplemental Agreement and who have agreed not to use or disclose the Confidential Information for any other purpose without the other party’s prior written consent.  In the event that a party concludes that disclosure of Confidential Information contained in this Supplemental Agreement is required by applicable law, the party will so advise the other party promptly in writing and endeavor to protect the confidentiality of such Confidential Information to the widest extent possible.  In the event of a legal dispute with Boeing, nothing herein will preclude Customer from sharing with its legal counsel information necessary for purposes of enabling counsel to advise or represent Customer provided that so long as Customer causes its legal counsel to maintain the confidentiality of information that is the subject of this Article.  Except as provided in the assignment provisions of Article 7 of Letter Agreement 6-1162-KSW-6423 entitled “Special Matters Applicable to the Incremental Aircraft”; Article 21 of Letter Agreement 6-1162-LAJ-0895R6 entitled “Business Considerations”; Article 8 of Letter Agreement 6-1162-ILK-0381R2 entitled “Special Matters Letter Applicable to the 2011 Accelerated Aircraft and the Substitute 767 Freighter Aircraft”; Article 9 of Letter Agreement 6-1162-ILK-0412 entitled “Special Matters Relating to Three Aircraft Originally Scheduled to Deliver in 2009” and Article 6 of Letter Agreement 6-1162-ILK-0450 entitled “Special Matters Relating to 2012 Accelerated Aircraft”, Customer will not disclose this Supplemental Agreement for purposes of financing payments without the prior written consent of Boeing, which consent will be provided once the financier enters into a Non Disclosure Agreement with Boeing in form and substance reasonably satisfactory to Boeing, which will include agreeing not to disclose or use Confidential Information except for the purpose set forth herein. This provision shall not apply to any Confidential Information that is in the public domain except that a party will be liable to the other for breach of its obligations under this provision if the Confidential Information entered the public domain as a consequence of a wrongful act or omission on its part.

  

 

  

 

The Purchase Agreement shall be deemed amended to the extent herein provided and as amended shall continue in full force and effect.

 

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

	
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

  

 

  

PURCHASE AGREEMENT NUMBER 2126

between

THE BOEING COMPANY

and

LAN Airlines  S.A.

Relating to Boeing Model 767-316ER, Model 767-38EF, and Model 767-316F Aircraft

  

 

  

TABLE OF CONTENTS

	  	  	 	
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

	
29

DELETED

	
          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

  

 

  

 

THIS TABLE IS NO LONGER APPLICABLE.

 

  

 

  

	
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

	
  

	 	
 

	 	
  

	 	
  

	  	
  

	  	
  

	  	
  

	  	
  

	 

 

  

 

  

AIRCRAFT CONFIGURATION

between

THE BOEING COMPANY

and

LAN AIRLINES S.A.

Exhibit A-11 to Purchase Agreement Number 2126

  

 

  

AIRCRAFT CONFIGURATION

relating to

BOEING MODEL 767-300ER AIRCRAFT

THE LAN AIRCRAFT

For the 2012 Accelerated Aircraft, the detail specification is Boeing Detail Specification D019T001, Revision L dated as of February 10, 2010.  Such Detail Specification will be comprised of Boeing Configuration Specification D019T001, Revision K dated December 1, 2008 to incorporate the Options listed below, including the effects on Manufacturer's Empty Weight (MEW) and Operating Empty Weight (OEW).  As soon as practicable, Boeing will furnish to Customer copies of the Detail Specification, which copies will reflect such Options.  The Aircraft Basic Price reflects and includes all effects of such Options, except such Aircraft Basic Price does not include the price effects of any Buyer Furnished Equipment or Seller Purchased Equipment.

  

 

  

	
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

	
[***]

  

 

  

	
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

	
[***]

  

 

  

	
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

	
[***]

	
[***]

ENGINE ESCALATION,

ENGINE WARRANTY AND PATENT INDEMNITY

between

THE BOEING COMPANY

and

LAN AIRLINES S.A

Supplemental Exhibit EE1 to Purchase Agreement Number 2126

  

 

  

ENGINE ESCALATION,

ENGINE WARRANTY AND PATENT INDEMNITY

relating to

BOEING MODEL 767-316ER and BOEING MODEL 767-316F AIRCRAFT

1.            [***] ENGINE ESCALATION.

(a)           The Aircraft Basic Price of each Aircraft set forth in Table 13 of the Purchase Agreement includes an aggregate price for engines and all accessories, equipment and parts provided by General Electric Aircraft Engines (GE).  The adjustment in Engine Price applicable to each Aircraft (Engine Price Adjustment) will be determined at the time of Aircraft delivery in accordance with the following formula:

 Pe = [(Pb + F)  x ( CPI / CPIb )] - Pb

where CPIb is the engine escalation base year index of 133.190 as set forth in Table 13 of the Purchase Agreement .

(b)   The following definitions will apply herein:

 Pe =           Engine Price Adjustment

	 	
Pb  =

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

	 	
F=

	
 0.005 x (N/12) x Pb where 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.

 CPI =        L + ICI  (rounded to the nearest hundredth)

	
  

	
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).

The Engine Price Adjustment will not be made if it would result in a decrease in the Engine Price.

(c)           The values of the Employment Cost Index Wages & Salaries and Producer Prices and Price Index - Industrial Commodities Index used will be those published as of a date thirty (30) days prior to the first day of the scheduled Aircraft delivery month to Customer.  As the Employment Cost Index values are only released on a quarterly basis, the value released for the first quarter will be used for the months of January, February and March; the value released for the second quarter will be used for the months of April, May and June; the value released for the third quarter will be used for the months of July, August and September; the value released for the fourth quarter will be used for the months of October, November and December.  Such values will be considered final and no Engine Price Adjustment will be made after Aircraft delivery for any subsequent changes in published index values.  If no values have been released for an applicable month, the provisions set forth in paragraph 1(e), below, will apply.  If prior to delivery of an Aircraft, the U.S. Department of Labor, Bureau of Labor Statistics changes the base year for determination of the L or ICI values as defined above, such rebase values will be incorporated in the Engine Price Adjustment calculation.

  

 

  

(d)           If at the time of delivery of an Aircraft, Boeing is unable to determine the Engine Price Adjustment because the applicable values to be used to determine L and ICI have not been released by the U.S. Department of Labor, Bureau of Labor Statistics; then, in the event the Engine Price escalation provisions are made non enforceable or otherwise rendered null and void by any agency of the United States Government, GE agrees to meet jointly with Boeing and Customer (to the extent such parties may lawfully do so) to adjust equitably  the Aircraft Basic Price of any affected Aircraft to reflect an allowance for increase or decrease in labor compensation and material costs occurring since February of the base price year which is consistent with the application provisions of this Supplemental Exhibit EE1.

(e)           If prior to delivery of an Aircraft, the U.S. Department of Labor, Bureau of Labor Statistics substantially revises the methodology used for the determination of the values to be used to determine the L and ICI values (in contrast to benchmark adjustments or other corrections of previously released values), Customer, Boeing and GE will, prior to delivery of such Aircraft, select a substitute for such values from data published by the U.S. Department of Labor, Bureau of Labor Statistics or other similar data reported by non-governmental United States organizations, such substitute to lead in application to the same adjustment result insofar as possible, as would have been achieved by continuing the use of the original values as they may have fluctuated during the applicable time period.  Appropriate revisions of the formula will be made as required to reflect any substitute values.  However, if within twenty-four (24) months from delivery of the Aircraft, the U.S. Department of Labor, Bureau of Labor Statistics should resume releasing values for the months needed to determine the Engine Price Adjustment, such values will be used to determine the increase or decrease in the Engine Price Adjustment determined at the time of delivery of such Aircraft.

	
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.

  

 

  

2.           ENGINE WARRANTY AND PRODUCT SUPPORT PLAN.

Boeing has obtained from GE the right to extend to Customer the provisions of GE's warranty and product support plan (Warranty and Product Support Plan); subject, however, to Customer's acceptance of the conditions set forth herein and in such Warranty and Product Support Plan.  Accordingly, Boeing hereby extends to Customer and Customer hereby accepts the provisions of GE's Warranty and Product Support Plan, and such Warranty and Product Support Plan shall apply to all CF6 turbofan engines including all Modules and Parts thereof, as these terms are defined in the Warranty and Product Support Plan, (Engines) installed in the Aircraft at the time of delivery or purchased from Boeing by Customer for support of the Aircraft except that, if Customer and GE have executed a general terms agreement (Engine GTA), then the terms of the Engine GTA shall be substituted for and supersede the below-stated provisions and such provisions shall be of no force or effect and neither Boeing nor GE shall have any obligation arising therefrom.  In consideration for Boeing's extension of the GE Warranty and Product Support Plan to Customer, Customer hereby releases and discharges Boeing from any and all claims, obligations and liabilities whatsoever arising out of the purchase or use of the Engines and Customer hereby waives, releases and renounces all its rights in all such claims, obligations and liabilities.

The Warranty and Product Support Plan is set forth in Exhibit C to the applicable purchase contract between GE and Boeing.  Copies of the Warranty and Product Support Plan shall be provided to Customer by Boeing upon request.

  

 

  

ESCALATION ADJUSTMENT

AIRFRAME AND OPTIONAL FEATURES

between

THE BOEING COMPANY

and

LAN AIRLINES S.A

Supplemental Exhibit AE1 [***] to Purchase Agreement Number 2126

 

  

 

  

1.           [***].

Airframe and Optional Features price adjustments (Airframe Price Adjustment) are used to allow prices to be stated in current year dollars at the signing of this Purchase Agreement and to adjust the amount to be paid by Customer at delivery for the effects of economic fluctuation.  The Airframe Price Adjustment will be determined at the time of Aircraft delivery in accordance with the following formula:

Pa = (P) (L + M) - P

Where:

Pa =   Airframe Price Adjustment.

	
  

	
  P =

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

L =           .65 x (ECI

            ECIb)

Where:

ECIb is the base year airframe escalation index (computed as the three month arithmetic average value of 106.8 for June, July and August [***] as set forth in Table 13 of this Purchase Agreement);

ECI is a value determined using the U.S. Department of Labor, Bureau of Labor Statistics, Employment Cost Index for NAICS Manufacturing – Total Compensation (BLS Series ID CIU2013000000000I), calculated by establishing a three-month arithmetic average value (expressed as a decimal and rounded to the nearest tenth) using the values for the 11th, 12th, and 13th months prior to the month of scheduled delivery of the applicable Aircraft.  As the Employment Cost Index values are only released on a quarterly basis, the value released for the first quarter will be used for the months of January, February, and March; the value released for the second quarter will be used for the months of April, May, and June; the value released for the third quarter will be used for the months of July, August, and September; the value released for the fourth quarter will be used for the months of October, November, and December.

M =           .35 x (CPI 

             CPIb )

Where:

CPIb is the base year airframe escalation index (computed as the three month arithmetic average value of 215.6 for June, July and August of 2009 as set forth in Table 13 of this Purchase Agreement); and

CPI is a value determined using the U.S. Department of Labor, Bureau of Labor Statistics, Consumer Price Index – All Urban Consumers (BLS Series ID CUUR0000SA0), calculated as a three (3) month arithmetic average of the released monthly values (expressed as a decimal and rounded to the nearest tenth) using the values for the 11th, 12th, and 13th months prior to the month of scheduled delivery of the applicable Aircraft.

  

 

  

As an example, for an Aircraft scheduled to be delivered in the month of July, the months of June, July, and August of the preceding year will be utilized in determining the value of ECI and CPI.

	
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.

2.           Values to be Utilized in the Event of Unavailability.

2.1           If the Bureau of Labor Statistics substantially revises the methodology used for the determination of the values to be used to determine the ECI and CPI values (in contrast to benchmark adjustments or other corrections of previously released values), or for any reason has not released values needed to determine the applicable Airframe Price Adjustment, the parties will, prior to the delivery of any such Aircraft, select a substitute from other Bureau of Labor Statistics data or similar data reported by non-governmental organizations.  Such substitute will result in the same adjustment, insofar as possible, as would have been calculated utilizing the original values adjusted for fluctuation during the applicable time period.  However, if within 24 months after delivery of the Aircraft, the Bureau of Labor Statistics should resume releasing values for the months needed to determine the Airframe Price Adjustment, such values will be used to determine any increase or decrease in the Airframe Price Adjustment for the Aircraft from that determined at the time of delivery of the Aircraft.

2.2           Notwithstanding Article 2.1 above, if prior to the scheduled delivery month of an Aircraft the Bureau of Labor Statistics changes the base year for determination of the ECI and CPI values as defined above, such re-based values will be incorporated in the Airframe Price Adjustment calculation.

2.3           In the event escalation provisions are made non-enforceable or otherwise rendered void by any agency of the United States Government, the parties agree, to the extent they may lawfully do so, to equitably adjust the Aircraft Price of any affected Aircraft to reflect an allowance for increases or decreases consistent with the applicable provisions of paragraph 1 of this Supplemental Exhibit AE1 in labor compensation and material costs occurring since August of the year prior to the price base year shown in the Purchase Agreement.

2.4           If within twelve (12) months of Aircraft delivery, the published index values are revised due to an acknowledged error by the Bureau of Labor Statistics, the Airframe Price Adjustment will be re-calculated using the revised index values (this does not include those values noted as preliminary by the Bureau of Labor Statistics).  A credit memorandum or supplemental invoice will be issued for the Airframe Price Adjustment difference. Interest charges will not apply for the period of original invoice to issuance of credit memorandum or supplemental invoice.

  

 

  

	
  

	
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.

  

 

  

6-1162-ILK-0450

 

LAN Airlines S.A.

Avenida Presidente Riesco 5711

Piso 19

Las Condes

Santiago, Chile

 

	
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")

 

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

 

	
13.

	
Definitions.

 

1.11           “STE” when used specifically in relation to any credit memorandum contained in this letter agreement shall mean that the relevant credit memorandum shall be escalated to the month of delivery in the same manner as the Airframe Price in accordance with the escalation formula reflected in Supplemental Exhibit AE1 2010$ to the Purchase Agreement entitled “Escalation adjustment - airframe and optional features”.

 

1.12           “Limitations on Use” when used in relation to any credit memorandum contained in this letter agreement shall mean that the applicable credit memorandum may be used for the purchase of Boeing goods and services or applied to the final delivery payment for the Aircraft for which the credit was issued, but that the relevant credit memorandum shall be prohibited from use for satisfaction of any Advance Payment obligation.

 

1.13           “2012 Accelerated Aircraft” shall mean each or all three, as the case may be, of the three Substitute 767 Freighter Aircraft (as previously defined in Article 1 of Supplemental Agreement No. 28 to the Purchase Agreement) scheduled for delivery during the second and fourth quarters of 2013 and the first quarter of 2014, which contingent upon satisfaction of the terms of this letter agreement, are substituted to Boeing Model 767-316ER Aircraft scheduled for delivery in June, July and October of 2012, respectively.

 

1.14           “Initial Payment” [***].

 

1.15           “Table 13” shall mean the table entitled “Aircraft Information Table 767-316ER Aircraft [***]”.

 

	
14.

	
Export License.

 

Customer understands and confirms that it is Customer’s responsibility to obtain any required Export License from the relevant U.S. authority.  Without accepting any liability for any failure to do so, Boeing will use reasonable endeavors to alert Customer to any regulatory changes of which Boeing becomes aware and which require Customer to obtain such Export License.

 

	
15.

	
Warranty Modification.

 

[***]

  

 

  

 

	
16. 

	
Credit Memoranda for the 2012 Accelerated Aircraft.

 

Subject to Customer’s adherence to the Limitations on Use, Boeing will provide the Customer with a credit memorandum concurrently with the delivery of each Aircraft, in description and amount which is identified in the credit memoranda table 4.1 for each of the 2012 Accelerated Aircraft:

 

Table 4.1 Credit Memoranda Table Exclusive to the 2012 Accelerated Aircraft

 

	
[***]

	
[***]

	  	  
	
[***]

	
[***]

	  	  
	
[***]

	
[***]

	  	  
	
[***]

	
[***]

 

	
17.

	
[***]

 

	
18.

	
Assignment.

 

Any assignment by Customer of any benefits, entitlements, or services described in this Letter Agreement requires Boeing's prior written consent.  Further, Customer will not reveal to any third party the amount of the credit memoranda provided to Customer by Boeing without Boeing’s prior written consent and subject to such circumstances as Boeing may reasonably require.

 

Boeing will not unreasonably withhold consent to Customer’s request to assign, as security, rights in the Purchase Agreement if done for purposes of obtaining financing or for such other purpose consistent with fulfilling its obligations under the Purchase Agreement.  Boeing’s consent will be conditioned on all parties accepting Boeing’s customary conditions for consenting to an assignment, including, but not limited to, the following: assignor and assignee indemnification of Boeing for any actions taken by an assignee under any assignment agreement; Boeing’s right to exercise the manufacturer’s option to assume Customer’s rights under the Purchase Agreement in the event of a default under an assignment agreement; and confidentiality.  A Party that is

 

	 	
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

 

[***]

 

Boeing will consent to any reasonable request by Customer to assign the Purchase Agreement to an affiliate provided that Boeing is provided with an adequate  guarantee of performance of all obligations under this Purchase Agreement and in a form reasonably satisfactory to Boeing.

 

Customer understands that Boeing is not required under any circumstances to consent to an assignment that would constitute a novation.

 

The foregoing provisions are intended to supplement, and not to supersede, the assignment provisions of the AGTA, which address delivery date and post-delivery assignments, merger-type assignments, and other matters.

  

 

  

 

	
19. 

	
16G Seat Requirement Credit Memorandum.

 

In the event that Customer notifies Boeing of a selection of record option 2525C826G85 (for Boeing certification of the business class, economy class and attendant seats to Federal Aviation Administration (FAA) Regulation Information Number 2120-AC84 entitled “Improved Seats in Air Carrier Transport Category Airplanes” (the 16G Requirement) in lieu of existing 9G capability) (such record option, including successor record options which supersede the identified record option, are herein referred to as the 16G Record Option), then Boeing will provide the Customer, concurrently with the delivery of each Aircraft, a credit memorandum equal to the cost of the 16G Record Option.  The parties shall document the effect of Customer’s notification that it has selected the 16G Record Option through appropriate Purchase Agreement documentation. The parties agree that Customer’s selection of the 16G Record Option is due by the dates identified below:

 

	
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.

 

Boeing and Customer understand that the commercial and financial information contained in this Letter Agreement is considered by the parties as confidential (Confidential Information) and both agree not to disclose such Confidential Information except as provided herein.  In addition to the parties’ respective officers, directors and employees who need to know the Confidential Information and who understand the obligation to keep it confidential, the parties may disclose Confidential Information (1) to the extent required by law and (2) to its agents, auditors and advisors who need to know the Confidential Information for purposes of enabling each party to understand, perform its obligations under, or receive the benefits of, this Letter Agreement and who have agreed not to use or disclose the Confidential Information for any other purpose without the other party’s prior written consent.  In the event that a party concludes that disclosure of Confidential Information contained in this Letter Agreement is required by applicable law, the party will so advise the other party promptly in writing and endeavor to protect the confidentiality of such Confidential Information to the widest extent possible.  In the event of a legal dispute with Boeing, nothing herein will preclude Customer from sharing with its legal counsel information necessary for purposes of enabling counsel to advise or represent Customer provided that so long as Customer causes its legal counsel to maintain the confidentiality of information that is the subject of this Article.  Except as provided in the assignment provisions of Article 7 of Letter Agreement 6-1162-KSW-6423 entitled “Special Matters Applicable to the Incremental Aircraft”; Article 21 of Letter Agreement 6-1162-LAJ-0895R6 entitled “Business Considerations”; Article 8 of Letter Agreement 6-1162-ILK-0381R3 entitled “Special Matters Letter Applicable to the 2011 Accelerated Aircraft”; Article 9 of Letter Agreement 6-1162-ILK-0412 entitled “Special Matters Relating to Three Aircraft Originally Scheduled to Deliver in 2009” and Article 6 herein, Customer will not disclose this Letter Agreement for purposes of financing payments without the prior written consent of Boeing, which consent will be provided once the financier enters into a Non Disclosure Agreement with Boeing in form and substance reasonably satisfactory to Boeing, which will include agreeing not to disclose or use Confidential Information except for the purpose set forth herein. This provision shall not apply to any Confidential Information that is in the public domain except that a party will be liable to the other for breach of its obligations under this provision if the Confidential Information entered the public domain as a consequence of a wrongful act or omission on its part.

 

The Purchase Agreement shall be deemed amended to the extent herein provided and as amended shall continue in full force and effect.

  

 

  

 

	
Very truly yours,

	  	  
	  	  	  
	
THE BOEING COMPANY

	  	  
	 	 	 
	
By:

	  	  	  
	
Irma L. Krueger

	  	  
	  	  	  
	
Its:

	
Attorney-In-Fact

	  	  

  

 

  

 

If the foregoing correctly sets forth your understanding of our agreement with respect to the matters treated herein, please indicate your acceptance, agreement and approval.

 

ACCEPTED AND AGREED TO this  day of November of 2010.

 

	
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

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