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
Exhibit 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:
|
|||
|
Xxxxxx X. Xxxxxx
|
Xx. Xxxxxxx Xxxx
|
|||
|
Its
|
Attorney-In-Fact
|
Its:
|
Sr. Vice President Strategic Planning & Corporate Development
|
|
|
By:
|
||||
|
Xx. Xxxxxxxxx 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
|
||
|
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.
Xxxxxxx Xxxxxxxxxx Xxxxxx 0000
Xxxx 00
Xxx Xxxxxx
Xxxxxxxx, Xxxxx
|
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:
|
||
|
Xxxxxx X. Xxxxxx
|
||
|
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:
|
||
|
Xx. Xxxxxxx Xxxx
|
||
|
Its:
|
Sr. Vice President Strategic Planning
|
|
|
& Corporate Development
|
|
|
|
By:
|
||
|
Xx. Xxxxxxxxx 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 XXXXXXXX XX TRANSCEIVERS - P/N 000-0000-000 AND DIGITAL HF COUPLERS - P/N 000-0000-000 - 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 XXXXXXXX XX TRANSCEIVERS AND COUPLERS - 000-0000-000 AND 000-0000-000 IN LIEU OF 000-0000-000 AND 000-0000-000 - 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 000-0000-000 - 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 - 000-0000-000 IN LIEU OF 000-0000-000 - 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 XXXXXXX 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 XXXX IN THE WHEEL WELL
|
[***]
|
||
|
2371-000017
|
SOLID STATE VOICE RECORDER ED56A AND SOLID STATE MICROPHONE/MONITOR ED56A - ALLIEDSIGNAL - 2 HOUR RECORDING TIME - P/N 000-0000-000 AND P/N 000-0000-000 - 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 - XXXXXX XXXXX
|
[***]
|
||
|
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 - XXXXXX 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 - XXXXXXX (P/N S270T201-7)
|
[***]
|
||
|
2911-000038
|
ENGINE-DRIVEN HYDRAULIC PUMPS - XXXXXXX 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 000-0000-000 - BFE/SPE
|
[***]
|
||
|
3131-000187
|
DIGITAL FLIGHT DATA RECORDER - ALLIEDSIGNAL - 256 WORDS PER SECOND MAXIMUM DATA RATE - P/N 000-0000-000 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 - XXXXXXX-BUGATTI
|
[***]
|
||
|
3245A438A27
|
OPERATIONAL TIRE SPEED LIMITS - 235MPH
|
[***]
|
||
|
3245A438A28
|
WHEELS AND TIRES - MAIN LANDING GEAR - HIGH GROSS WEIGHT WHEELS - XXXXXXX-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 000-0000-000 - BFE/SPE
|
[***]
|
|
3433-000032
|
RADIO ALTIMETER (RA) - ROCKWELL INTERNATIONAL CORP - P/N 000-0000-000 - BFE/SPE
|
[***]
|
||
|
3443-000050
|
DUAL WEATHER RADAR CONTROL PANEL - ROCKWELL P/N 000-0000-000 - BFE/SPE
|
[***]
|
||
|
3443A065A34
|
DUAL WEATHER RADAR SYSTEM - WITH PREDICTIVE WINDSHEAR - ROCKWELL TRANSCEIVER P/N 000-0000-000 - BFE/SPE
|
[***]
|
||
|
3443A141A90
|
WEATHER RADAR INDICATOR ON FORWARD ELECTRONICS PANEL - ROCKWELL XXXXXXX - BFE/SPE
|
[***]
|
||
|
3445A065A86
|
TCAS SYSTEM - ROCKWELL XXXXXXX TCAS COMPUTER P/N 000-0000-000 - 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 000-0000-000 - BFE/SPE
|
[***]
|
||
|
3453B866A16
|
ATC SYSTEM - ROCKWELL XXXXXXX ATC TRANSPONDER P/N 000-0000-000 - 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 000-0000-000 - BFE/SPE
|
[***]
|
||
|
3457-000212
|
AUTOMATIC DIRECTION FINDER (ADF) - DUAL SYSTEM - ROCKWELL ADF-900 SERIES - ADF RECEIVER P/N 000-0000-000; ADF ANTENNA P/N 000-0000-000 - BFE/SPE
|
[***]
|
||
|
3457-000219
|
AUTOMATIC DIRECTION FINDER (ADF) - DUAL SYSTEM - ROCKWELL ADF-900/700 SERIES - ADF RECEIVER P/N 000-0000-000 - ADF ANTENNA P/N 000-0000-000 - 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
|
XXXXXXXX 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 XXXXXXXX XX TRANSCEIVERS - P/N 000-0000-000 AND DIGITAL HF COUPLERS - P/N 000-0000-000 - 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 XXXXXXXX XX TRANSCEIVERS AND COUPLERS - 000-0000-000 AND 000-0000-000 IN LIEU OF 000-0000-000 AND 000-0000-000 - 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 000-0000-000 - 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 - 000-0000-000 IN LIEU OF 000-0000-000 - 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 XXXXXXX 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 XXXX IN THE WHEEL WELL
|
[***]
|
|
2371-000017
|
SOLID STATE VOICE RECORDER ED56A AND SOLID STATE MICROPHONE/MONITOR ED56A - ALLIEDSIGNAL - 2 HOUR RECORDING TIME - P/N 000-0000-000 AND P/N 000-0000-000 - 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 - XXXXXX XXXXX
|
[***]
|
||
|
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 - XXXXXX 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 - XXXXXXX (P/N S270T201-7)
|
[***]
|
||
|
2911-000038
|
ENGINE-DRIVEN HYDRAULIC PUMPS - XXXXXXX 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 000-0000-000 - BFE/SPE
|
[***]
|
||
|
3131-000187
|
DIGITAL FLIGHT DATA RECORDER - ALLIEDSIGNAL - 256 WORDS PER SECOND MAXIMUM DATA RATE - P/N 000-0000-000 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 - XXXXXXX-BUGATTI
|
[***]
|
||
|
3245A438A27
|
OPERATIONAL TIRE SPEED LIMITS - 235MPH
|
[***]
|
||
|
3245A438A28
|
WHEELS AND TIRES - MAIN LANDING GEAR - HIGH GROSS WEIGHT WHEELS - XXXXXXX-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 000-0000-000 - BFE/SPE
|
[***]
|
||
|
3433-000032
|
RADIO ALTIMETER (RA) - ROCKWELL INTERNATIONAL CORP - P/N 000-0000-000 - BFE/SPE
|
[***]
|
||
|
3443-000050
|
DUAL WEATHER RADAR CONTROL PANEL - ROCKWELL P/N 000-0000-000 - BFE/SPE
|
[***]
|
||
|
3443A065A34
|
DUAL WEATHER RADAR SYSTEM - WITH PREDICTIVE WINDSHEAR - ROCKWELL TRANSCEIVER P/N 000-0000-000 - BFE/SPE
|
[***]
|
||
|
3443A141A90
|
WEATHER RADAR INDICATOR ON FORWARD ELECTRONICS PANEL - ROCKWELL XXXXXXX - BFE/SPE
|
[***]
|
||
|
3445A065A86
|
TCAS SYSTEM - ROCKWELL XXXXXXX TCAS COMPUTER P/N 000-0000-000 - 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 000-0000-000 - BFE/SPE
|
[***]
|
||
|
3453B866A16
|
ATC SYSTEM - ROCKWELL XXXXXXX ATC TRANSPONDER P/N 000-0000-000 - 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 000-0000-000 - BFE/SPE
|
[***]
|
||
|
3457-000212
|
AUTOMATIC DIRECTION FINDER (ADF) - DUAL SYSTEM - ROCKWELL ADF-900 SERIES - ADF RECEIVER P/N 000-0000-000; ADF ANTENNA P/N 000-0000-000 - BFE/SPE
|
[***]
|
||
|
3457-000219
|
AUTOMATIC DIRECTION FINDER (ADF) - DUAL SYSTEM - ROCKWELL ADF-900/700 SERIES - ADF RECEIVER P/N 000-0000-000 - ADF ANTENNA P/N 000-0000-000 - 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
|
XXXXXXXX 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.
Xxxxxxx Xxxxxxxxxx Xxxxxx 0000
Xxxx 00
Xxx Xxxxxx
Xxxxxxxx, Xxxxx
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
|
|
|
Xx. Xxxxxxx Xxxx
|
|
|
Its
|
Sr. Vice President Strategic
|
|
Planning & Corporate Planning
|
|
|
By
|
|
|
Xx. Xxxxxxxxx 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:
|
|||
|
Xx. Xxxx X. Xxxxxxx
|
Xx. Xxxxxxx Xxxx
|
|||
|
Its
|
Attorney-In-Fact
|
Its:
|
Sr. Vice President Strategic Planning &
|
|
| Corporate Development | ||||
|
By:
|
||
|
Xx. Xxxxxxxxx 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 XXXXX - XXXXX 000
|
[***]
|
|
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 XXXXXXXX XX VOICE/DATA TRANSCEIVERS - P/N 000-0000-000 AND DIGITAL HF COUPLERS - P/N 000-0000-000 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 000-0000-000 - 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 XXXXXXX ARINC 758 LEVEL AOA CMU - P/N 000-0000-000 - BFE / SPE
|
[***]
|
|
2322B800A68
|
AIRCRAFT COMMUNICATIONS ADDRESSING AND REPORTING SYSTEM (ACARS) - LARGE FORMAT MULTIPURPOSE INTERACTIVE DISPLAY UNIT (MIDU) - ROCKWELL - P/N 000-0000-000 - 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 XXXXXXX
|
[***]
|
|
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 XXXX IN THE WHEEL WELL
|
[***]
|
|
2371-000017
|
SOLID STATE VOICE RECORDER ED56A AND SOLID STATE MICROPHONE/MONITOR ED56A - ALLIEDSIGNAL - 2 HOUR RECORDING TIME - P/N 000-0000-000 AND P/N 000-0000-000 - 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 - XXXXXXXXX - 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 - XXXXXX XXXXX
|
[***]
|
|
2560-000200
|
PROTECTIVE BREATHING EQUIPMENT - FLIGHT DECK - XXXXX 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 - XXXXX (XXXXXXX) S270T201-7
|
[***]
|
|
2911-000038
|
ENGINE-DRIVEN HYDRAULIC PUMPS - XXXXXXX 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 000-0000-000 - BFE/SPE
|
[***]
|
|
3131-000187
|
DIGITAL FLIGHT DATA RECORDER - ALLIEDSIGNAL - 256 WORDS PER SECOND MAXIMUM DATA RATE - P/N 000-0000-000 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 - 000-0000-000 - 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 - XXXXXXX-BUGATTI
|
[***]
|
|
3245A438A27
|
OPERATIONAL TIRE SPEED LIMITS - 235MPH
|
[***]
|
|
3245A438A28
|
WHEELS AND TIRES - MAIN LANDING GEAR - HIGH GROSS WEIGHT WHEELS - XXXXXXX-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 - XX/XX XXX 000 - XXX 000-00
|
[***]
|
|
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 000-0000-000 - BFE/SPE
|
[***]
|
|
3433-000032
|
RADIO ALTIMETER (RA) - ROCKWELL INTERNATIONAL CORP - P/N 000-0000-000 - BFE/SPE
|
[***]
|
|
3443-000050
|
DUAL WEATHER RADAR CONTROL PANEL - ROCKWELL P/N 000-0000-000 - BFE/SPE
|
[***]
|
|
3443A065A34
|
DUAL WEATHER RADAR SYSTEM - WITH PREDICTIVE WINDSHEAR - ROCKWELL TRANSCEIVER P/N 000-0000-000 - BFE/SPE
|
[***]
|
|
3445A065A86
|
TCAS SYSTEM - ROCKWELL XXXXXXX TCAS COMPUTER P/N 000-0000-000 - 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 000-0000-000 - BFE/SPE
|
[***]
|
|
3453B866A16
|
ATC SYSTEM - ROCKWELL XXXXXXX ATC TRANSPONDER P/N 000-0000-000 - 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 000-0000-000 - BFE/SPE
|
[***]
|
|
3457-000219
|
AUTOMATIC DIRECTION FINDER (ADF) - DUAL SYSTEM - ROCKWELL ADF-900/700 SERIES - ADF RECEIVER P/N 000-0000-000 - ADF ANTENNA P/N 000-0000-000 - 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/XXXXX AVIATION - BFE/SPE
|
[***]
|
|
3611-000005
|
XXXXXXXX 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
|
XXXXXXXX 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 Xxxxxxx XX0 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.
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Note:
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i.
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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.
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|
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ii.
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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.
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6-1162-ILK-0450
LAN Airlines S.A.
Xxxxxxx Xxxxxxxxxx Xxxxxx 0000
Xxxx 00
Xxx Xxxxxx
Xxxxxxxx, Xxxxx
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Subject:
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Special Matters Letter Applicable to the 2012 Accelerated Aircraft
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Reference:
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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")
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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.
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13.
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Definitions.
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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 [***]”.
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14.
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Export License.
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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.
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15.
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Warranty Modification.
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16.
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Credit Memoranda for the 2012 Accelerated Aircraft.
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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
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[***]
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[***]
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[***]
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[***]
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[***]
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[***]
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[***]
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[***]
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17.
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[***]
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18.
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Assignment.
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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
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i.
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bound by a customary confidentiality agreement;
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ii.
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neither an airplane manufacturer nor an airline; and
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iii.
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responding to a Customer request for proposals to provide financing of Aircraft pursuant to the Purchase Agreement, including pre-delivery payment financing
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[***]
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.
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19.
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16G Seat Requirement Credit Memorandum.
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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
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Due Date for Customer Notification of 16G Record Option
|
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June 2012
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1st of November of 2010
|
|
|
July 2012
|
1st of November of 2011
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|
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October 2012
|
1st of February of 2011
|
|
20.
|
[***]
|
|
21.
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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.
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Very truly yours,
|
|||
|
THE BOEING COMPANY
|
|||
|
By:
|
|||
|
Xxxx X. Xxxxxxx
|
|||
|
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:
|
|||
|
Xx. Xxxxxxx Xxxx
|
|||
|
Its:
|
Sr. Vice President Strategic Planning
|
||
|
& Corporate Development
|
|||
|
By:
|
|||
|
Xx. Xxxxxxxxx de la Fuente Goic
|
|||
|
Its:
|
Chief Financial Officer
|
||
