PURCHASE AGREEMENT NUMBER 2126
between
THE BOEING COMPANY
and
Lan Chile S.A.
Relating to Boeing Model 767-316ER, Model 767-38EF, and Model 767-316F Aircraft
- --------------------------------------------------------------------------------
CONFIDENTIAL TREATMENT REQUESTED
P.A. No. 2126 SA 14
TABLE OF CONTENTS
ARTICLES
- --------
1. Quantity, Model and Description SA 5
2. Delivery Schedule SA 5
3. Price SA 5
4. Payment SA 5
5. Miscellaneous SA 5
TABLE
- -----
1. Aircraft Information Table SA 1
2. Aircraft Information Table SA 1
3. Aircraft Information Table SA 8
4. Aircraft Information Table SA 11
5. Aircraft Information Table SA 14
EXHIBIT
- -------
A. Aircraft Configuration
A-1 Aircraft Configuration SA 1
A-2 Aircraft Configuration SA 5
A-3 Aircraft Configuration SA 10
B. Aircraft Delivery Requirements and Responsibilities SA 1
SUPPLEMENTAL EXHIBITS
- ---------------------
BFE1. BFE Variables SA 1
CS1. Customer Support Variables SA 1
EE1. Engine Escalation/Engine Warranty and Patent Indemnity SA 1
EE1-1. Engine Escalation/Engine Warranty and Patent Indemnity SA 5
BE1-2. Engine Escalation/Engine Warranty and Patent Indemnity SA 13
SLP 1. Service Life Policy Components
P.A. No. 2126 1 SA 14
LETTER AGREEMENTS
- -----------------
2126-1 Seller Purchased Equipment
2126-2 Cabin Systems Equipment
2126-3R4 Option Aircraft SA 13
RESTRICTED LETTER AGREEMENTS
- ----------------------------
6-1162-DMH-350 Performance Guarantees
6-1162-DMH-351 Promotion Support
6-1162-DMH-472 Performance Guarantees SA 1
6-1l62-DMH-475 Configuration Matters SA I
6-1l62-DMH-1031R2 Special Provisions for SA 9
Advance Payments
6-1162-LAJ-311 Special Matters Relating to the SA 11
July 2001 and September 2001
Aircraft
6-1162-LAJ-0895 Business Considerations SA 14
P.A. No. 2126 2 SA 14
Purchase Agreement No. 2126
between
The Boeing Company
and
LanChile S.A.
-------------------
This Purchase Agreement No. 2126 dated as of January 30, 1998
between The Boeing Company (Boeing) and Lan Chile S.A. (Customer) relating to
the purchase and sale of Model 767-316ER, Model 767-38EF, and Model 767-316F
aircraft incorporates the terms and conditions of the Aircraft General Terms
Agreement dated as of May 9, 1997 between the parties, identified as AGTA-LAN
(AGTA).
Article 1. Quantity, Model and Description.
The aircraft to be delivered to Customer will be designated as
Model 767-316ER, Model 767-38EF, and Model 767-316F aircraft (the Aircraft).
Boeing will manufacture and sell to Customer 767-316ER, 767-38EF, and 767-316F
Aircraft to conform to the configurations described in Exhibits A, A-1, A-2, and
A-3, which are part of this Purchase Agreement.
Article 2. Delivery.
The scheduled months of delivery of the Aircraft are listed in
the attached Table 1, Table 2, Table 3, and Table 4, which are part of this
Purchase Agreement. Boeing's and Customer's obligation with respect to delivery
of the Aircraft are contained in Exhibit B to the Purchase Agreement. Boeing and
Customer agree to use reasonable endeavors to comply with the time periods
contained in such Exhibit B.
Article 3. Price.
3.1 Aircraft Basic Price. The Aircraft Basic Price in subject
to escalation dollars is listed in Table 1, Table 2, Table 3, and Table 4.
3.2 Advance Payment Base Prices. The Advance Payment Base
Prices listed in Table 1, Table 2, Table 3 and Table 4 were calculated utilizing
the latest escalation factors available to Boeing on the date of this Purchase
Agreement projected to the month of scheduled delivery.
P.A. No 2126 1 SA 11
3.3 The components of the Aircraft Basic Price and the
calculation of the Advance Payment Base Prices for the Aircraft are listed in
Table 1, Table 2, Table 3, and Table 4.
Article 4. Payment.
4.1 The standard advance payment schedule for the Model 767
aircraft requires the purchaser to make certain advance payments, expressed in a
percentage of the Advance Payment Base Price of each aircraft beginning with a
payment of 1%, less the Deposit, on the effective date of the purchase agreement
for the aircraft. Additional advance payments for each aircraft are due on the
first business day of the months listed in the attached Table 1, Table 2, Table
3, and Table 4.
4.2 Customer will upon signing the Purchase Agreement pay to
Boeing the total amount of deposits required pursuant to the advance payment
schedule in Table 1, Table 2, Table 3, and Table 4. Customer will make
additional advance payments for the Aircraft in accordance with such schedule.
4.3 Customer will pay the balance of the Aircraft Price of
each Aircraft at delivery.
Article 5. Miscellaneous.
5.1 Aircraft Information Table. Table 1, Table 2, Table 3, and
Table 4 consolidates information contained in Articles 1, 2, 3 and 4 with
respect to (i) quantity of Aircraft, (ii) applicable Detail Specification, (iii)
month and year of scheduled deliveries, (iv) Aircraft Basic Price, (v)
applicable escalation factors and (vi) Advance Payment Base Prices and advance
payments and their schedules.
5.2 Buyer Furnished Equipment Variables. Supplemental Exhibit
BFE1 contains vendor selection dates, on dock dates and other variables
applicable to the Model 767-316ER Aircraft only.
5.3 Customer Support Variables. Supplemental Exhibit CS1
contains the variable information applicable to information, training services
and other things furnished by Boeing in support of the Aircraft.
5.4 Engine Escalation Variables. Supplemental Exhibit EE1
contains the applicable engine escalation formula, the engine warranty and the
engine patent indemnity for the Aircraft delivering through December 1999.
5.5 Engine Escalation Variables. Supplemental Exhibit EE1-1
contains the applicable engine escalation formula, the engine warranty and the
engine patent indemnity for the Aircraft delivering after December 1999.
P.A. No 2126 2 SA 11
5.6 Service Life Policy Component Variables. Supplemental
Exhibit SLP1 lists the airframe and landing gear components covered by the
Service Life Policy for the Aircraft.
5.7 Negotiated Agreement; Entire Agreement. This Purchase
Agreement, including the provisions of Article 8.2 of the AGTA relating to
insurance, and Article 11 of Part 2 of Exhibit C of the AGTA relating to
DISCLAIMER AND RELEASE and EXCLUSION OF CONSEQUENTIAL AND OTHER DAMAGES, has
been the subject of discussion and negotiation and is understood by the parties;
the Aircraft Price and other agreements of the parties stated in this Purchase
Agreement were arrived at in consideration of such provisions. This Purchase
Agreement, including the AGTA, contains the entire agreement between the parties
and supersedes all previous proposals, understandings, commitments or
representations whatsoever, oral or written, and may be changed only in writing
signed by authorized representatives of the parties.
******************
DATED AS OF 15 - September 2000
LAN CHILE S.A. THE BOEING COMPANY
By \s\ Carlos Prado C. By \s\ Lyn A. Johnson
------------------------------------------------ -------------------
Its Senior Vice President Corporate Investments Its Attorney-In-Fact
------------------------------------------- --------------------
P.A. No 2126 3 SA 11
Supplemental Agreement No. 14
to
Purchase Agreement No. 2126
between
THE BOEING COMPANY
and
LAN CHILE S.A.
Relating to Boeing Model 767-316ER, Model 767-38EF, and Model
767-316F Aircraft
THIS SUPPLEMENTAL AGREEMENT, entered into as of the 20th day
of April 2004, by and between THE BOEING COMPANY, a Delaware corporation
(hereinafter called Boeing), and Lan Chile S.A, a Chile corporation (hereinafter
called Customer);
W I T N E S S E T H:
- - - - - - - - - -
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, as amended and supplemented,
together with all exhibits, specifications and letter agreements related or
attached thereto, is hereinafter called the "Purchase Agreement;" and
WHEREAS, Customer has decided to purchase two (2) additional 767-316F
aircraft with delivery in July and October of 2005,
WHEREAS, Boeing and Customer have agreed to amend the Purchase
Agreement to incorporate the above change;
NOW THEREFORE, in consideration of the mutual covenants herein
contained, the parties hereto agree to amend the Purchase Agreement as follows:
P.A. No 2126 Page 1 SA 14
1. Purchase of Two (2) Additional 767-316F Aircraft. This Supplemental
Agreement amends the Purchase Agreement to reflect the purchase by Customer
of two (2) additional 767-316F Aircraft (Jul-05 and Oct-05).
1.1. Table of Contents. Remove and replace in its entirety the
Table of Contents, with the Table of Contents attached hereto,
to reflect the changes made by this Supplemental Agreement No.
14.
1.2. Aircraft Description. Boeing will manufacturer and sell to
Customer, and Customer will purchase from Boeing, the Aircraft
described in the attached Aircraft Information Table No. 5.
1.3. Aircraft Delivery Schedule. The scheduled delivery month of
each of the additional Aircraft is set forth in the attached
Aircraft Information Table No. 5.
1.4. Price. The Aircraft Basic Price and each component thereof and
the Advance Payment Base Price for each of the additional
Aircraft set forth in the attached Aircraft Information Table
No. 5.
1.5. Payment.
1.5.1. Boeing acknowledges that Customer has paid deposit payments to
Boeing on March 25, 2004 in the amount of $140,000 for each of
the additional Aircraft.
1.5.2. Customer will make Advance Payments to Boeing in the amount of
30% of the Advance Payment Base Price for each of the
Aircraft. These payments will begin with a payment of 1%, less
any deposit previously paid to Boeing. Additional payments for
the Aircraft are due on the first business day of the months
and in the amounts set forth in the attached Aircraft
Information Table No.5.
1.5.3. The total amount of Advance Payments due upon the date of this
agreement will include all Advance Payments that are or were
due on or before such date in accordance with the Advance
Payment Schedule set forth in the attached Aircraft
Information Table No. 5.
P.A. No 2126 Page 2 SA 14
1.5.4. Any payments due to Boeing shall be made via wire transfer to
the Boeing bank account as identified below.
Bank: JPMorgan Chase
Account Name: The Boeing Company
ABA No. 021000021
Account No. 910-1-012764
Attention: Marla Chavez
2. Engine Escalation Variables. Supplemental Exhibit EE1-2 contains the
applicable engine escalation formula, the engine warranty and the engine
patent indemnity for the additional Aircraft identified in this
Supplemental Agreement.
3. Letter Agreements. Remove and replace, in its entirety, Letter Agreement
Letter Agreement 6-l162-LAJ-310Rl, Business Considerations, with Letter
Agreement 6-1l62-LAJ-0895, Business Considerations, attached hereto to
reflect the current business offer.
4. Confidentiality.
Customer understands that the information contained in this Letter
Agreement is considered confidential. Customer agrees to treat this Letter
Agreement as confidential and will not, without the prior written consent of
Boeing, disclose this Letter Agreement or any information contained herein to
any third parties.
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 CHILE S.A.
By \s\ Lyn A. Johnson By \s\ Carlos Prado C.
------------------------------------ ----------------------------------
Its Attorney-In-Fact Its Senior VP Corporate Investments
------------------------------------ ----------------------------------
P.A. No 2126 Page 3 SA 14
Supplemental Agreement No. 15
to
Purchase Agreement No. 2126
between
THE BOEING COMPANY
and
LANCHILE S.A.
Relating to Boeing Model 767-316ER, Model 767-38EF, and Model 767-316F Aircraft
THIS SUPPLEMENTAL AGREEMENT, entered into as of the 31st day of May
2004, by and between THE BOEING COMPANY, a Delaware corporation (hereinafter
called Boeing), and Lan Chile S.A., a Chile corporation (hereinafter called
Customer);
W I T N E S S E T H:
- - - - - - - - - -
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, as amended and supplemented,
together with all exhibits, specifications and letter agreements related or
attached thereto, is hereinafter called the "Purchase Agreement;" and
WHEREAS, Customer and Boeing have come to agreement on the basic
configuration of upcoming Customer 767-316F aircraft with delivery in July and
October 2005,
WHEREAS, Boeing and Customer have agreed to amend the Purchase
Agreement to incorporate the above change;
NOW THEREFORE, in consideration of the mutual covenants herein
contained, the parties hereto agree to amend the Purchase Agreement as follows:
P.A. No 2126 Page 1 SA 15
1. Configuration of Two (2) 767-316F Aircraft. This Supplemental Agreement
amends the Purchase Agreement to reflect the Define and Control Aircraft
Configuration (DCAC) of Customers two (2) 767-316F Aircraft (Jul-05 and
Oct-05) which were added to the Purchase Agreement via Supplemental
Agreement No. 14.
1.1. Table of Contents. Remove and replace in its entirety the Table of
Contents, with the Table of Contents attached hereto, to reflect the
changes made by this Supplemental Agreement No. 15.
1.2. Aircraft Description. Boeing will manufacturer and sell to Customer,
and Customer will purchase from Boeing, the Aircraft described in the
attached Aircraft Information Table No. 5. This attached Aircraft
Information Table No. 5 includes the updated detail specification
number of Customer's Aircraft and will replace the prior Table No. 5.
Such Aircraft are further described in the attached Exhibit A-4
entitled Aircraft Configuration.
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 CHILE S.A.
By Lyn A. Johnson By Carlos Prado C.
------------------------------------ ----------------------------------
Its Attorney-In-Fact Its Senior VP Corporate Investments
------------------------------------ ----------------------------------
P.A. No 2126 Page 2 SA 15
PURCHASE AGREEMENT NUMBER 2126
between
THE BOEING COMPANY
and
Lan Chile S.A.
Relating to Boeing Model 767-316ER, Model 767-38EF, and Model 767-316F Aircraft
P.A. No 2126 SA 15
TABLE OF CONTENTS
ARTICLES
- --------
1. Quantity, Model and Description SA 5
2. Delivery Schedule SA 5
3. Price SA 5
4. Payment SA 5
5. Miscellaneous SA 5
TABLE
- -----
1. Aircraft Information Table SA 1
2. Aircraft Information Table SA 1
3. Aircraft Information Table SA 8
4. Aircraft Information Table SA 11
5. Aircraft Information Table SA 15
EXHIBIT
- -------
A. Aircraft Configuration
A-1 Aircraft Configuration SA 1
A-2 Aircraft Configuration SA 5
A-3 Aircraft Configuration SA 10
A-4 Aircraft Configuration SA 15
B. Aircraft Delivery Requirements and Responsibilities SA 1
SUPPLEMENTAL EXHIBITS
- ---------------------
BFE1. BFE Variables SA 1
CS1. Customer Support Variables SA 1
EE1. Engine Escalation/Engine Warranty and Patent Indemnity SA 1
EE1-1. Engine Escalation/Engine Warranty and Patent Indemnity SA 5
EE1-2. Engine Escalation/Engine Warranty and Patent Indemnity SA 13
SLP1. Service Life Policy Components
P.A. No 2126 1 SA 15
LETTER AGREEMENTS
2126-1 Seller Purchased Equipment
2126-2 Cabin Systems Equipment
2126-3R4 Option Aircraft SA 13
RESTRICTED LETTER AGREEMENTS
6-1162-DMH-350 Performance Guarantees
6-1162-DMH-351 Promotion Support
6-1162-DMH-472 Performance Guarantees SA 1
6-1162-DMH-475 Configuration Matters SA 1
6-1162-DMH-1031R2 Special Provisions for SA 9
Advance Payments
6-1162-LAJ-311 Special Matters Relating to the July SA 11
2001 and September 2001 Aircraft
6-1162-LAJ-0895 Business Considerations SA 14
P.A. No 2126 2 SA 15
Aircraft Information Table No. 5
to Purchase Agreement No. 2126
Aircraft Delivery, Description, Price and Advance Payments
Airframe Model/MTGW: 767-300F 412,000 Detail Specification: DO19T002LAN63F-1 (4/2004)
Engine Model: CF6-80C2B6F Airframe Price Base Year: Jul-03
Airframe Price: $109,022,000 Engine Price Base Year: Jul-03
Optional Features: $1,410,200
------------
Sub-Total of Airframe
and Features: $110,432,200 Airframe Escalation Data:
------------------------
Engine Price (Per Aircraft): $18,424,006 Base Year Index (ECI): 165.00
Aircraft Basic Price
(Excluding BFE/SPE): $128,856,206 Base Year Index (ICI): 136.80
------------
Buyer Furnished Equipment
(BFE) Estimate: $0 Engine Escalation Data:
----------------------
Seller Purchased Equipment
(SPE) Estimate: $1,400,000 Base Year Index (CPI): 151.980
Refundable Deposit per Aircraft $140,000
at Proposal Acceptance:
====================================================================================================================================
Escalation Escalation Escalation Estimate
Delivery Number of Factor Factor Manufacturer Adv Payment Base
Advance Payment Per Aircraft (Amts. Due/Mos. Prior to
Date Aircraft (Airframe) (Engine) Serial Number Price Per A/P Delivery):
- -----------------------------------------------------------------------------------------------------------------------------------
At Signing 24 Mos. 21/18/12/9/6 Mos Total
1% 4% 5% 30%
- -----------------------------------------------------------------------------------------------------------------------------------
Jul-2005 1 1.0607 1.069 34245 $138,381,000 $1,243,810 $5,535,240 $6,919,050 $41,514,300
- -----------------------------------------------------------------------------------------------------------------------------------
Oct-2005 1 1.0689 1.076 34246 $139,415,000 $1,254,150 $5,576,600 $6,970,750 $41,824,500
- -----------------------------------------------------------------------------------------------------------------------------------
LAN PA2126 SA No.15 Page 1
AIRCRAFT CONFIGURATION
between
THE BOEING COMPANY
and
LANCHILE S.A.
Exhibit A to Purchase Agreement Number 2126
P.A. No. 2126 A
AIRCRAFT CONFIGURATION
Relating to
BOEING MODEL 767-316F AIRCRAFT
THE LANCHILE AIRCRAFT
The Detail Specification for the Aircraft is Boeing Customer Detail
Specification D019T002LAN63F-1 dated April 20, 2004. Such Detail Specification
will be comprised of Boeing Configuration Specification D019T002, Revision E
dated August 28, 2003, as amended to incorporate the applicable specification
language to reflect the effect of the Optional Features attached hereto and any
other accepted changes, including the effects of such changes on Manufacturer's
Empty Weight (MEW) and Operating Empty Weight (OEW). As soon as practicable,
Boeing will furnish to Buyer copies of the Detail Specification, which copies
will reflect the effect of such Optional Features and any other accepted
changes. The Aircraft Basic Price reflects and includes all effects of such
Optional Features attached hereto, except such Aircraft Basic Price does not
include the price effects of any Buyer Furnished Equipment or Seller Purchased
Equipment.
This Aircraft Configuration has taken the last Customer configuration, described
in Detail Specification D6T10340LAN-l, Revision E, and re-defined that
configuration into new Define and Control Airplane Configuration (DCAC)
specification D019T002LAN63F-1.
P.A. No. 2126 A-4 SA 15
- --------------------------------------------------------------------------------------------------------------------------------
2003 $'S
Price
Change Request Title Per A/C
- --------------------------------------------------------------------------------------------------------------------------------
0110-000035 MAJOR MODEL 767 AIRPLANE INCL
- --------------------------------------------------------------------------------------------------------------------------------
0110-000038 MINOR MODEL 767-300F FREIGHTER AIRPLANE INCL
- --------------------------------------------------------------------------------------------------------------------------------
0110-000094 MODEL 767-300 GENERAL MARKET FREIGHTER AIRPLANE INCL
- --------------------------------------------------------------------------------------------------------------------------------
0220-000040 FAA TYPE CERTIFICATION INCL
- --------------------------------------------------------------------------------------------------------------------------------
0220-000136 15 KNOT MAXIMUM TAKEOFF AND LANDING TAILWIND COMPONENT CERTIFICATION INCL
- --------------------------------------------------------------------------------------------------------------------------------
0221-000002 DISPATCH WITH GEAR EXTENDED FOR REVENUE FLIGHT INCL
- --------------------------------------------------------------------------------------------------------------------------------
0221A251A19 ENGINE INOPERATIVE TEN-MINUTE TAKEOFF THRUST OPERATION - CF6-80C2B6F THRUST RATING INCL
- --------------------------------------------------------------------------------------------------------------------------------
0228-000032 OPERATIONS MANUAL IN FAA FORMAT INCL
- --------------------------------------------------------------------------------------------------------------------------------
0229A141A41 PERFORMANCE - CERTIFICATION FOR OPERATION AT AIRPORT ALTITUDES OF 9500 FEET AND BELOW INCL
- --------------------------------------------------------------------------------------------------------------------------------
0252-000014 ENVIRONMENTAL CONTROL SYSTEM - TEMPERATURE INDICATIONS IN DEGREES CELSIUS INCL
- --------------------------------------------------------------------------------------------------------------------------------
0252-000017 INSTRUMENTATION WITH METRIC UNITS - MODEL 767 INCL
- --------------------------------------------------------------------------------------------------------------------------------
0315C262A22 CERTIFIED OPERATIONAL AND STRUCTURAL DESIGN WEIGHTS, 767-300F INCL
- --------------------------------------------------------------------------------------------------------------------------------
0351A114C45 TAKEOFF PERFORMANCE IMPROVEMENT - ALTERNATE FORWARD CENTER OF GRAVITY LIMITS INCL
- --------------------------------------------------------------------------------------------------------------------------------
0360B604F64 MISCELLANEOUS WEIGHT COLLECTOR INCL
- --------------------------------------------------------------------------------------------------------------------------------
1110C262A21 EXTERIOR COLOR SCHEME AND MARKINGS - LAN 767-316F INCL
- --------------------------------------------------------------------------------------------------------------------------------
1130-000344 BOEING STANDARD MARKINGS - MAIN DECK CARGO COMPARTMENT INCL
- --------------------------------------------------------------------------------------------------------------------------------
130A931A06 IATA STANDARD MARKINGS - LOWER LOBE CARGO COMPARTMENT INCL
- --------------------------------------------------------------------------------------------------------------------------------
2145-000004 BULK CARGO AREA HEATING AND VENTILATING FOR ANIMAL CARRIAGE INCL
- --------------------------------------------------------------------------------------------------------------------------------
2210-000030 AUTOFLIGHT - THREE DIGIT MACH NUMBER ON MODE CONTROL PANEL INCL
- --------------------------------------------------------------------------------------------------------------------------------
2210-000031 AUTOFLIGHT - AUTOMATIC AUTOPILOT CHANNEL SELECTION IN APPROACH MODE INCL
- --------------------------------------------------------------------------------------------------------------------------------
2210-000037 AUTOFLIGHT - BANK ANGLE HOLD AT AUTOPILOT COMMAND ENGAGE INCL
- --------------------------------------------------------------------------------------------------------------------------------
2210-000039 AUTOFLIGHT - FULL TIME FLIGHT DIRECTOR INCL
- --------------------------------------------------------------------------------------------------------------------------------
2210-000151 AUTOFLIGHT - ENABLE GLIDE SLOPE CAPTURE PRIOR TO LOCALIZER CAPTURE INCL
- --------------------------------------------------------------------------------------------------------------------------------
2210-000311 AUTOFLIGHT - FLIGHT CONTROL COMPUTER (FCC) WITHOUT ONBOARD SOFTWARE LOADING CAPABILITY INCL
- --------------------------------------------------------------------------------------------------------------------------------
2210A064A02 AUTOFLIGHT - ALTITUDE ALERT - 300/900 FEET INCL
- --------------------------------------------------------------------------------------------------------------------------------
2210B403A07 MODE CONTROL PANEL WITH BACKCOURSE SWITCH INCL
- --------------------------------------------------------------------------------------------------------------------------------
2230-000127 AUTOTHROTTLE - SELECTION OF CLIMB DERATES INCL
- --------------------------------------------------------------------------------------------------------------------------------
2230-000133 AUTOTHROTTLE - FIXED PERCENTAGE DERATE LEVELS OF 10% AND 20% INCL
- --------------------------------------------------------------------------------------------------------------------------------
2230-000135 AUTOTHROTTLE - CLIMB DERATE WASHOUT SCHEDULE - 10,000 TO 12,000 FEET INCL
- --------------------------------------------------------------------------------------------------------------------------------
2311-000122 HF COMMUNICATIONS - DUAL GABLES HF CONTROL PANEL WITH SENSITIVITY CONTROL - P/N INCL
G7401-03 - BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
2311A213A84 HF COMMUNICATIONS - DUAL ROCKWELL HF TRANSCEIVERS - P/N 822-0330-001 AND DIGITAL HF INCL
COUPLERS - P/N 822-0987-003 - BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
2312-000432 VHF COMMUNICATIONS - TRIPLE GABLES VHF TUNING PANELS (DUAL KNOB) - P/N G7400-27 - INCL
BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
2312-000703 VHF COMMUNICATIONS - ACTIVATION OF 8.33 KHZ CHANNEL SPACING INCL
- --------------------------------------------------------------------------------------------------------------------------------
2312-000786 VHF COMMUNICATIONS -TRIPLE ROCKWELL ARINC 716/750 VHF-900B FM IMMUNE TRANSCEIVERS WITH INCL
8.33 KHZ CHANNEL SPACING AND CMC INTERFACE CAPABILITY - P/N 822-1047-003 - BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
2315A213A67 SATCOM - PARTIAL PROVISIONS FOR SATCOM SYSTEM AND TOP MOUNTED HIGH GAIN ANTENNA SYSTEM INCL
- MODEL 767
- --------------------------------------------------------------------------------------------------------------------------------
2315B800C72 SATCOM - HF/SATCOM SELECT PANEL - INSTALLATION - FLIGHT DECK INCL
- --------------------------------------------------------------------------------------------------------------------------------
2321B401A04 SELCAL - AVTECH FIVE CHANNEL DECODER - P/N NA138-714C - BFE/SPE INCL
- --------------------------------------------------------------------------------------------------------------------------------
2322-000250 ACARS - PARTIAL PROVISIONS FOR SINGLE ARINC 724B ACARS INCL
- --------------------------------------------------------------------------------------------------------------------------------
2340B800C73 CREW COMMUNICATION - PILOTS' CALL PANEL - SELCAL AND CARGO LOADING/GROUND CALL - 767 INCL
FREIGHTER
- --------------------------------------------------------------------------------------------------------------------------------
2350B800C71 AUDIO INTEGRATING - AUDIO SELECTOR PANELS - FLIGHT DECK INCL
- --------------------------------------------------------------------------------------------------------------------------------
2351-000042 CONTROL WHEEL PUSH TO TALK (PTT) SWITCH - STANDARD THREE POSITION INCL
- --------------------------------------------------------------------------------------------------------------------------------
2351A138C64 HAND HELD MICROPHONE - CAPTAIN, FIRST OFFICER AND FIRST OBSERVER - TELEPHONICS - P/N INCL
107C800-22 BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
2351A213A33 AUDIO INTEGRATION - INSTALLATION- TWO-PLUG AUDIO JACKS IN THE FLIGHT DECK INCL
- --------------------------------------------------------------------------------------------------------------------------------
P.A. 2126/SA No. 15 BOEING PROPRIETARY Page 1 of 4
- --------------------------------------------------------------------------------------------------------------------------------
2003 $'S
Price
Change Request Title Per A/C
- --------------------------------------------------------------------------------------------------------------------------------
2351A213B77 BOOM MICROPHONE HEADSETS - CAPTAIN AND FIRST OFFICER - TELEX AIRMAN 750 - P/N INCL
64300-200-BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
2351A213B80 HEADPHONE- FIRST OBSERVER -TELEX - P/N 64400-200 - BFE/SPE INCL
- --------------------------------------------------------------------------------------------------------------------------------
2371-000009 NO MONITOR JACK IN THE WHEEL WELL INCL
- --------------------------------------------------------------------------------------------------------------------------------
2371-000017 SOLID STATE VOICE RECORDER ED56A AND SOLID STATE MICROPHONE/MONITOR ED56A - INCL
ALLIEDSIGNAL - 2 HOUR RECORDING TIME - P/N 980-6022-001 AND P/N 980-6116-002 - BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
2433-000021 STANDBY POWER - EXTENDED TIME CAPABILITY - BATTERY PARALLELING INCL
- --------------------------------------------------------------------------------------------------------------------------------
2511-000022 MANUALLY OPERATED SEATS - CAPTAIN AND FIRST OFFICER INCL
- --------------------------------------------------------------------------------------------------------------------------------
2513-000405 SUNVISOR INSTALLATION - NUMBER 1 AND 2 WINDOWS - FLIGHT DECK - SFE INCL
- --------------------------------------------------------------------------------------------------------------------------------
2527-000732 CONVERSION OPTION - GALLEY/ENTRY AND LAVATORY MAT INSTALLATION -TARAFLEX - 767 INCL
FREIGHTER
- --------------------------------------------------------------------------------------------------------------------------------
2530B604F65 GALLEY INSERT PART NUMBERS - BFE/SPE INCL
- --------------------------------------------------------------------------------------------------------------------------------
2550-000157 DELIVERY CONFIGURATION - MAIN DECK - TRANSVERSE TYPE A (88"" X 125"") PALLETS INCL
- --------------------------------------------------------------------------------------------------------------------------------
2550-000162 ALTERNATE CARGO COMPARTMENT ARRANGEMENT - MAIN DECK - SIDE BY SIDE CONTOURED 88"" X INCL
125"" TYPE A PALLETS
- --------------------------------------------------------------------------------------------------------------------------------
2550-000261 CONVERSION OPTION - FIRST PALLET POSITION FOR ACCESS TO LIVE ANIMAL CARRIAGE OR INCL
HAZARDOUS MATERIAL CARRIAGE - 767 FREIGHTER
- --------------------------------------------------------------------------------------------------------------------------------
2550-000263 CONVERSION OPTION - ALTERNATE CARGO COMPARTMENT ARRANGEMENT - MAIN DECK - ADDITIONAL INCL
96"" X 196"" PALLETS - FREIGHTER
- --------------------------------------------------------------------------------------------------------------------------------
2553-000044 HARDWARE FOR CARRIAGE OF 88 X 125 AND 96 X 125 INCH PALLETS AND STANDARD CONTAINERS IN INCL
THE FORWARD CARGO COMPARTMENT
- --------------------------------------------------------------------------------------------------------------------------------
2555-000053 CONVERSION OPTION - INSTALLATION OF ADDITIONAL NET AFT OF THE AFT CARGO DOOR INCL
- --------------------------------------------------------------------------------------------------------------------------------
2560-000177 HALON FIRE EXTINGUISHER - FLIGHT DECK - WALTER KIDDE INCL
- --------------------------------------------------------------------------------------------------------------------------------
2560A141A86 CREW LIFE VESTS - FLIGHT DECK - SWITLIK- P/N S-31850-6300-AAR001 - BFE/SPE INCL
- --------------------------------------------------------------------------------------------------------------------------------
2560B599A35 PROTECTIVE BREATHING EQUIPMENT - FLIGHT DECK - B/E AEROSPACE - BFE/SPE INCL
- --------------------------------------------------------------------------------------------------------------------------------
2562A115D57 EMERGENCY LOCATOR TRANSMITTER (RESCU 406) - INSTALLATION - BFE/SPE INCL
- --------------------------------------------------------------------------------------------------------------------------------
2564-000215 CONVERSION OPTION - FIRST AID KIT - UPS - BFE/SPE INCL
- --------------------------------------------------------------------------------------------------------------------------------
2610-000025 KIDDE FIRE DETECTION SYSTEM - GE CF6-80C2 ENGINES AND APU INCL
- --------------------------------------------------------------------------------------------------------------------------------
2618-000009 SINGLE LOOP DUCT LEAK DETECTION SYSTEM - 3 ZONE INCL
- --------------------------------------------------------------------------------------------------------------------------------
2622-000002 FIRE BOTTLE COMMONALITY - CF6-80C2 ENGINES AND APU INCL
- --------------------------------------------------------------------------------------------------------------------------------
2732-000001 STALL WARNING COMPUTER SPEED TAPE ACTIVATION - INHIBIT DISPLAY OF MINIMUM MANEUVER INCL
SPEED ON TAKEOFF
- --------------------------------------------------------------------------------------------------------------------------------
2844-000005 FUEL MEASURING STICKS IN KILOGRAMS WITH CONVERSION TABLES IN KILOGRAMS INCL
- --------------------------------------------------------------------------------------------------------------------------------
2911-000003 AC MOTOR-DRIVEN HYDRAULIC PUMPS - VICKERS (P/N S270T201-7) INCL
- --------------------------------------------------------------------------------------------------------------------------------
2911-000038 ENGINE-DRIVEN HYDRAULIC PUMPS - VICKERS INC. (60B00200-12) INCL
- --------------------------------------------------------------------------------------------------------------------------------
3042-000003 WINDSHIELD WIPERS - TWO SPEED - SINGLE SWITCH INCL
- --------------------------------------------------------------------------------------------------------------------------------
3080-000006 MANUAL ANTI-ICING SYSTEM - NO ICE DETECTION INCL
- --------------------------------------------------------------------------------------------------------------------------------
3120-000011 ELECTRONIC CLOCKS - WITHOUT TENTHS OF MINUTE DISPLAY - MAIN INSTRUMENT PANEL INCL
- --------------------------------------------------------------------------------------------------------------------------------
3131-000143 ACCELEROMETER - Honeywell P/N 971-4193-001 - BFE/SPE INCL
- --------------------------------------------------------------------------------------------------------------------------------
3131-000187 DIGITAL FLIGHT DATA RECORDER- ALLIEDSIGNAL - 256 WORDS PER SECOND MAXIMUM DATA RATE - INCL
P/N 980-4700-042 BFE/SPE
- -------------------------------------------------------------------------------------------------------------------------------
3131-000435 INTEGRATED DISPLAY UNIT (IDU) INSTALLATION - BFE/SPE - TELEDYNE P/N 2229346-7 INCL
- --------------------------------------------------------------------------------------------------------------------------------
3131A218A57 DIGITAL FLIGHT DATA ACQUISITION UNIT (DFDAU) WITH ACMS CAPABILITY AND ZNTERGRATED INCL
PCMCIA MEDIA INTERFACE-TELEDYNE CONTROLS - P/N 2233000-816-1 - BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
3131B800C90 DIGITAL FLIGHT DATA ACQUISITION UNIT (DFDAU) WITH ACMS CAPABILITY AND INTERGRATED INCL
PCMCIA MEDIA INTERFACE-TELEDYNE CONTROLS - P/N 2233000-816-1 - BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
3132-000105 PORTABLE DATA LOADER/RECORDER CONNECTOR IN FLIGHT DECK - ARINC 615 - SFE INCL
- --------------------------------------------------------------------------------------------------------------------------------
3132-000117 DATA LOADER SELECTOR SWITCH MODULE - 20 POSITION 3 WAY - SFE INCL
- --------------------------------------------------------------------------------------------------------------------------------
3133-000057 FULL FORMAT PRINTER - MILTOPE - ARINC 744 - P/N 706300-212 - BFE/SPE INCL
- --------------------------------------------------------------------------------------------------------------------------------
3133-000126 ARINC 744 PRINTER PROVISIONS IN ANAISLESTAND EXTENSION IN THE FLIGHT DECK INCL
- --------------------------------------------------------------------------------------------------------------------------------
3151-000042 FIREBELL AURAL WARNING - 1 SECOND ON, 9 SECONDS OFF INCL
- --------------------------------------------------------------------------------------------------------------------------------
P.A. 2126/SA No. 15 BOEING PROPRIETARY Page 2 of 4
- --------------------------------------------------------------------------------------------------------------------------------
2003 $'S
Price
Change Request Title Per A/C
- --------------------------------------------------------------------------------------------------------------------------------
3151-000046 AUTOPILOT DISCONNECT - AURAL WARNING SIREN - AURAL WARNING AND MASTER WARNING LIGHT INCL
INHIBITED WHEN AUTOPILOT DISCONNECT SWITCH IS DOUBLE PRESSED QUICKLY
- --------------------------------------------------------------------------------------------------------------------------------
3151A065A47 RESETTABLE OVERSPEED AURAL WARNING - SIREN INCL
- --------------------------------------------------------------------------------------------------------------------------------
3161-000135 HYDRAULIC PRESSURE ON EICAS STATUS PAGES INCL
- --------------------------------------------------------------------------------------------------------------------------------
3161-000137 APU RPM ON PICAS STATUS PAGES INCL
- --------------------------------------------------------------------------------------------------------------------------------
3161-000139 APU OIL QUANTITY LEVEL ON EICAS INCL
- --------------------------------------------------------------------------------------------------------------------------------
3161-000141 ADDITIONAL ENVIRONMENTAL CONTROL SYSTEM (ECS) PARAMETERS - DISPLAY ON EICAS INCL
MAINTENANCE PAGE
- --------------------------------------------------------------------------------------------------------------------------------
3161-000144 GENERATOR OFF AND ENGINE OIL PRESSURE - EICAS ADVISORY LEVEL MESSAGES INCL
- --------------------------------------------------------------------------------------------------------------------------------
3161-000147 ECS PRECOOLER OUTLET TEMPERATURE - (PW AND GE ENGINES) - DISPLAY ON EICAS INCL
- --------------------------------------------------------------------------------------------------------------------------------
3161-000152 BULK CARGO COMPARTMENT TEMPERATURE - DISPLAY ON EICAS INCL
- --------------------------------------------------------------------------------------------------------------------------------
3161-000154 RAM AIR OUTLET DOOR POSITION - DISPLAY ON EICAS INCL
- --------------------------------------------------------------------------------------------------------------------------------
3161-000189 ENGINE FUEL FLOW - FULL TIME DISPLAY - LOWER EICAS DISPLAY INCL
- --------------------------------------------------------------------------------------------------------------------------------
3162-000016 FLIGHT MODE ANNUNCIATION AT TOP OF ADI INCL
- --------------------------------------------------------------------------------------------------------------------------------
3162-000021 AIRSPEED TAPE - ROLLING DIGITS AND TREND VECTOR - ADI INCL
- --------------------------------------------------------------------------------------------------------------------------------
3162-000022 FLIGHT DIRECTOR COMMAND DISPLAY- SPLIT AXIS - ADI INCL
- --------------------------------------------------------------------------------------------------------------------------------
3162-000026 DISPLAY OF ROUND DIAL AND DIGITAL RADIO ALTITUDE - ADI INCL
- --------------------------------------------------------------------------------------------------------------------------------
3162-000030 RISING RUNWAY - DISPLAYED ON THE ADI INCL
- --------------------------------------------------------------------------------------------------------------------------------
3162-000034 RADIO ALTITUDE HEIGHT ALERT DISPLAY - 2500 FEET - ADI INCL
- --------------------------------------------------------------------------------------------------------------------------------
3162-000054 ILS DEVIATION WARNING - ADI INCL
- --------------------------------------------------------------------------------------------------------------------------------
3162-000059 MAP MODE ORIENTATION - TRACK UP - NAVIGATION DISPLAY INCL
- --------------------------------------------------------------------------------------------------------------------------------
3162-000066 TRUE AIRSPEED AND GROUND SPEED - NAVIGATION DISPLAY INCL
- --------------------------------------------------------------------------------------------------------------------------------
3162-000070 WIND BEARING DIGITAL DISPLAY - NAVIGATION DISPLAY INCL
- --------------------------------------------------------------------------------------------------------------------------------
3221-000011 TORQUE ARM QUICK DISCONNECT - NOSE LANDING GEAR INCL
- --------------------------------------------------------------------------------------------------------------------------------
3242A114B69 ANTISKID/AUTOBRAKE CONTROL UNIT (AACU) P/N 42-767-2 (S283T001-27) - INSTALLATION INCL
- --------------------------------------------------------------------------------------------------------------------------------
3244-000022 PARKING BRAKE REPEATER LIGHT - SINGLE LIGHT - NOSE LANDING GEAR AREA -LIGHT VISIBLE INCL
TO GROUND CREW
- --------------------------------------------------------------------------------------------------------------------------------
3245-000230 WHEELS AND TIRES - NOSE LANDING GEAR - WHEELS - ALLIEDSIGNAL - INSTALLATION WITH SFE INCL
24 PR, 235 MPH TIRES
- --------------------------------------------------------------------------------------------------------------------------------
3245A298A12 BRAKES - CARBON - MESSIER-BUGAITI INCL
- --------------------------------------------------------------------------------------------------------------------------------
3245A438A27 OPERATIONAL TIRE SPEED LIMITS - 235MPH INCL
- --------------------------------------------------------------------------------------------------------------------------------
3245A438A28 WHEELS AND TIRES - MAIN LANDING GEAR - HIGH GROSS WEIGHT WHEELS - MESSIER-BUGAVFI - INCL
INSTALLATION WITH SFE 32 PR, 235 MPH TIRES.
- --------------------------------------------------------------------------------------------------------------------------------
3246-000005 BRAKE TEMPERATURE MONITORING SYSTEM INCL
- --------------------------------------------------------------------------------------------------------------------------------
3342-000009 TAXI LIGHTS - NOSE GEAR MOUNTED - SPACE PROVISIONS INCL
- --------------------------------------------------------------------------------------------------------------------------------
3413-000027 MACH/AIRSPEED INDICATOR - TWO KNOT GRADUATIONS BELOW 250 KNOTS INCL
- --------------------------------------------------------------------------------------------------------------------------------
3421-000042 FAA MACH/AIRSPEED LIMITS AND OVERSPEED ALERTING INCL
- --------------------------------------------------------------------------------------------------------------------------------
3423-000006 STANDBY MAGNETIC COMPASS COMPENSATION FOR ELECTRICAL CIRCUITS (+/- 5 DEGREES) INCL
- --------------------------------------------------------------------------------------------------------------------------------
3430-000187 ILS/GPS MULTI-MODE RECEIVER (MMR) - ROCKWELL - P/N 822-1152-002 - BFE/SPE INCL
- --------------------------------------------------------------------------------------------------------------------------------
3433-000032 RADIO ALTIMETER (RA) - ROCKWELL INTERNATIONAL CORP - P/N 822 -0334-002 - BFE/SPE INCL
- --------------------------------------------------------------------------------------------------------------------------------
3443-000050 DUAL WEATHER RADAR CONTROL PANEL - ROCKWELL P/N 622-5130-114 - BFE/SPE INCL
- --------------------------------------------------------------------------------------------------------------------------------
3443A065A34 DUAL WEATHER RADAR SYSTEM - WITH PREDICTIVE WINDSHEAR - ROCKWELL TRANSCEIVER P/N INCL
622-5132-633 - BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
3443A141A90 WEATHER RADAR INDICATOR ON FORWARD ELECTRONICS PANEL - ROCKWELL COLLINS - BFE/SPE INCL
- --------------------------------------------------------------------------------------------------------------------------------
3445A065A86 TCAS SYSTEM - ROCKWELL COLLINS TCAS COMPUTER P/N 822-1293-002- TCAS CHANGE 7 INCL
COMPLIANT- BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
3446-000045 STANDARD VOLUME FOR ALTITUDE CALLOUTS INCL
- --------------------------------------------------------------------------------------------------------------------------------
3446-000048 ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) - BANK ANGLE CALLOUT ENABLE INCL
- --------------------------------------------------------------------------------------------------------------------------------
3446-000050 500 SMART CALLOUT INCL
- --------------------------------------------------------------------------------------------------------------------------------
3446-000088 GROUND PROXIMITY WARNING SYSTEM ALTITUDE CALLOUT5 - 2500, 1000, 50, 40, 30, 20, 10, INCL
APPROACHING DECISION HEIGHT, MINIMUMS
- --------------------------------------------------------------------------------------------------------------------------------
P.A. 2126/SA No. 15 BOEING PROPRIETARY Page 3 of 4
- --------------------------------------------------------------------------------------------------------------------------------
2003 $'S
Price
Change Request Title Per A/C
- --------------------------------------------------------------------------------------------------------------------------------
3451-000022 VOR/MARKER BEACON - ROCKWELL RECEIVER P/N 822-0297-001 - BFE/SPE INCL
- --------------------------------------------------------------------------------------------------------------------------------
3453B866A16 ATC SYSTEM - ROCKWELL COLLINS ATC TRANSPONDER P/N 822-1338-003 - ELS/EHS/ES AND TCAS INCL
CHANGE 7 COMPLIANT - GABLES CONTROL PANEL P/N G6992-12 - BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
3455-000019 DISTANCE MEASURING EQUIPMENT (DME) - ROCKWELL INTERROGATOR PIN 822-0329-001 - BFE/SPE INCL
- --------------------------------------------------------------------------------------------------------------------------------
3457-000212 AUTOMATIC DIRECTION FINDER (ADF) - DUAL SYSTEM - ROCKWELL ADF-900 SERIES - ADF INCL
RECEIVER P/N 822-0299-001; ADF ANTENNA P/N 822-5404-001 - BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
3457-000219 AUTOMATIC DIRECTION FINDER (ADF) - DUAL SYSTEM - ROCKWELL ADF-900/700 SERIES - ADF INCL
RECEIVER P/N 822-0299-001 - ADF ANTENNA P/N 622-5404-003 - BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
3457-000289 DUAL ADF CONTROL PANEL - BOEING - 285T0557-2 - WITHOUT BFO OR TONE SWITCH - SFE INCL
- --------------------------------------------------------------------------------------------------------------------------------
3461A425A03 FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - OFFPATH DESCENT CIRCLES AND DISTANCE INCL
MEASURING EQUIPMENT RANGE RINGS DISPLAYED
- --------------------------------------------------------------------------------------------------------------------------------
3461A425A04 FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - SCANNING DME OPERATIONS - ENABLE INCL
- --------------------------------------------------------------------------------------------------------------------------------
3461A425A06 FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - RUNWAY DISTANCE AND OFFSET POSITION SHIFT INCL
IN UNITS OF METERS
- --------------------------------------------------------------------------------------------------------------------------------
3461A425A10 FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - NAVIGATION DATABASE - CUSTOMER SUPPLIED INCL
- --------------------------------------------------------------------------------------------------------------------------------
3511B899B43 CREW OXYGEN MASKS - DILUTER DEMAND REGULATORS WITH SEPARATE SMOKE GOGGLES - CAPTAIN INCL
AND FIRST OFFICER - EROS - BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
3511B899B44 CREW OXYGEN MASKS - DILUTER DEMAND TYPE REGULATORS WITH SEPARATE SMOKE GOGGLES - INCL
FIRST OBSERVER - EROS - BFE/SPE
- --------------------------------------------------------------------------------------------------------------------------------
3611-000006 ALLIEDSIGNAL INC. - INTERMEDIATE PRESSURE (IP) CHECK VALVES - GE\P&W ENGINES INCL
- --------------------------------------------------------------------------------------------------------------------------------
4970-000045 APU HOURMETER - RIGHT DECK INCL
- --------------------------------------------------------------------------------------------------------------------------------
7200-000382 STANDARD FAN SPINNER - GE ENGINES INCL
- --------------------------------------------------------------------------------------------------------------------------------
7200-000412 GE PROPULSION SYSTEM INCL
- --------------------------------------------------------------------------------------------------------------------------------
7200-000459 GENERAL ELECTRIC ENGINES - CF6-80C2-B6F - B6F RATING - WITH FADEC INCL
- --------------------------------------------------------------------------------------------------------------------------------
7830-000012 MANUAL OPENING OF THRUST REVERSER ASSEMBLIES - GE CF6-80C2 ENGINES INCL
- --------------------------------------------------------------------------------------------------------------------------------
7900-000117 LUBRICATING OIL - BP TURBO OIL 2380 INCL
- --------------------------------------------------------------------------------------------------------------------------------
8011-000006 HAMILTON STANDARD STARTERS AND STARTER VALVES - GE ENGINES INCL
- --------------------------------------------------------------------------------------------------------------------------------
MISC FO FOLLOW ON EXH A VR259 $1,410,200
- --------------------------------------------------------------------------------------------------------------------------------
OPTIONS: 147 TOTALS: $1,410,200
- --------------------------------------------------------------------------------------------------------------------------------
P.A. 2126/SA No. 15 BOEING PROPRIETARY Page 4 of 4
AIRCRAFT DELIVERY REQUIREMENTS AND RESPONSIBILITIES
between
THE BOEING COMPANY
and
Lan Chile S.A.
Exhibit B to Purchase Agreement Number 2126
P.A. No. 2126 B
Exhibit B to
Purchase Agreement No. 2126
Page 1
AIRCRAFT DELIVERY REQUIREMENTS AND RESPONSIBILITIES
relating to
BOEING MODEL 767-316ER MODEL 767-38EF AIRCRAFT
Both Boeing and Customer have certain documentation and approval
responsibilities at various times during the construction cycle of Customer's
Aircraft that are critical to making the delivery of each Aircraft a positive
experience for both parties. This Exhibit B documents those responsibilities and
indicates recommended completion deadlines for the actions to be accomplished.
P.A. No. 2126 B-1 SA 1
Exhibit B to
Purchase Agreement No. 2126
Page 2
1. GOVERNMENT DOCUMENTATION REQUIREMENTS.
Certain actions are required to be taken by Customer in advance of the scheduled
delivery month of each Aircraft with respect to obtaining certain government
issued documentation.
1.1 Airworthiness and Registration Documents.
Not later than 6 months prior to delivery of each
Aircraft, Customer will notify Boeing of the registration number to be painted
on the side of the Aircraft. In addition, and not later than 3 months prior to
delivery of each Aircraft, Customer will if and to the extent required under
applicable law, by letter to the regulatory authority having jurisdiction,
authorize the temporary use of such registration numbers by Boeing during the
pre-delivery testing of the Aircraft.
Customer is responsible for furnishing any Temporary or Permanent Registration
Certificates required by any governmental authority having jurisdiction to be
displayed aboard the Aircraft after delivery.
1.2 Certificate of Sanitary Construction.
1.2.1 U.S. Registered Aircraft. Boeing will obtain
from the United States Public Health Service, a United States Certificate of
Sanitary Construction to be displayed aboard each Aircraft after delivery to
Customer.
1.2.2 Non-U.S. Registered Aircraft. Unless Customer
notifies Boeing that the Certificate of Sanitary Construction is not required,
Boeing will obtain such Certificate and provide it at delivery.
1.3 Customs Documentation.
1.3.1 Import Documentation. If the Aircraft is
intended to be exported from the United States, Customer must notify Boeing not
later than 3 months prior to delivery of each Aircraft of any documentation
required by the customs authorities or by any other agency of the country of
import.
1.3.2 General Declaration - U.S. If the Aircraft is
intended to be exported from the United States, Boeing will prepare Customs Form
7507, General Declaration, for execution by U.S. Customs immediately prior to
the ferry flight of the Aircraft. For this purpose, Customer will furnish to
Boeing not later than 20 days prior to delivery a complete crew and passenger
list and a complete ferry flight itinerary, including point of exit from the
United States for the Aircraft.
If Customer intends, during the ferry flight of an Aircraft, to land at a U.S.
airport after clearing Customs at delivery, Customer must notify Boeing not
later than 20 days priorto delivery of such intention. If Boeing receives such
P.A. No. 2126 B-2 SA 1
Exhibit B to
Purchase Agreement No. 2126
Page 3
notification, Boeing will provide to Customer the documents constituting a
Customs permit to proceed, allowing such Aircraft to depart after any such
landing. Sufficient copies of completed Form 7507, along with passenger
manifest, will be furnished Customer to cover U.S. stops scheduled for the ferry
flight.
1.3.3 Export Declaration - U.S. If the Aircraft is
intended to be exported from the United States, Boeing will prepare Form 7525V
and, immediately prior to the ferry flight, will submit such Form to U.S.
Customs in Seattle in order to obtain clearance for the departure of the
Aircraft, including any cargo, from the United States. U.S. Customs will deliver
the Export Declaration to the U.S. Department of Commerce after export.
2. INSURANCE CERTIFICATES.
Unless provided earlier, Customer will provide to Boeing not
later than 30 days prior to delivery of the first Aircraft, a copy of the
requisite annual insurance certificate in accordance with the requirements of
Article 8 of the AGTA.
3. NOTICE OF FLYAWAY CONFIGURATION.
Not later than 20 days prior to delivery of the Aircraft,
Customer will provide to Boeing a configuration letter, stating the requested
"flyaway configuration" of the Aircraft for its ferry flight. This configuration
letter should include:
(i) the name of the company which is to furnish fuel for the
ferry flight and any scheduled post-delivery flight training, the
method of payment for such fuel, and fuel load for the ferry flight;
(ii) the cargo to be loaded and where it is to be stowed on
board the Aircraft and address where cargo is to be shipped after
flyaway;
(iii) any BFE equipment to be removed prior to flyaway and
returned to Boeing BFE stores for installation on Customer's subsequent
Aircraft;
(iv) a complete list of names and citizenship of each crew
member and non-revenue passenger who will be aboard the ferry flight;
and
(v) a complete ferry flight itinerary.
P.A. No. 2126 B-3 SA 1
4. DELIVERY ACTIONS BY BOEING.
4.1 Schedule of Inspections. All FAA, Boeing, Customer
and, if required, U.S. Customs Bureau inspections will be scheduled by Boeing
for completion prior to delivery or departure of the Aircraft. Boeing will
provide Customer with reasonable notice of such inspections.
4.2 Schedule of Demonstration Flights. All FAA and
Customer demonstration flights will be scheduled by Boeing for completion prior
to delivery of the Aircraft. Boeing will provide Customer with reasonable notice
of such flights.
4.3 Schedule for Customer's Flight Crew. Boeing will
provide Customer with reasonable notice of the date that a flight crew is
required for acceptance routines associated with delivery of the Aircraft.
4.4 Fuel Provided by Boeing. Boeing will provide to
Customer, without charge, the amount of fuel shown in U.S. gallons in the table
below for the model of Aircraft being delivered and full capacity of engine oil
at the time of delivery or prior to the ferry flight of the Aircraft.
Aircraft Model Fuel Provided
-------------- -------------
737 1,000
747 4,000
757 1,600
767 2,000
777 3,000
4.5 Flight Crew and Passenger Consumables. Boeing will
provide food, coat hangers, towels, toilet tissue, drinking cups and soap for
the first segment of the ferry flight for the Aircraft.
4.6 Delivery Papers, Documents and Data. Boeing will
have available at the time of delivery of the Aircraft certain delivery papers,
documents and data for execution and delivery. If title for the Aircraft will be
transferred to Customer through a Boeing sales subsidiary and if the Aircraft
will be registered with the FAA, Boeing will pre-position in Oklahoma City,
Oklahoma, for filing with the FAA at the time of delivery of the Aircraft an
executed original Form 8050-2, Aircraft Bill of Sale, indicating transfer of
title to the Aircraft from Boeing's sales subsidiary to Customer.
4.7 Delegation of Authority. If specifically requested
in advance by Customer, Boeing will present a certified copy of a Resolution of
Boeing's Board of Directors, designating and authorizing certain persons to act
on its behalf in connection with delivery of the Aircraft.
P.A. No. 2126 B-4 SA 1
5. DELIVERY ACTIONS BY CUSTOMER.
5.1 Aircraft Radio Station License. At delivery Customer
will provide its Aircraft Radio Station License to be placed on board the
Aircraft following delivery.
5.2 Aircraft Flight Log. At delivery Customer will
provide the Aircraft Flight Log for the Aircraft.
5.3 Delegation of Authority. Customer will present to
Boeing at delivery of the Aircraft an original or certified copy of Customer's
Delegation of Authority designating and authorizing certain persons to act on
its behalf in connection with delivery of the specified Aircraft.
P.A. No. 2126 B-5 SA 1
BUYER FURNISHED EQUIPMENT VARIABLES
between
THE BOEING COMPANY
and
LanChile S.A.
Supplemental Exhibit BFE1 to Purchase Agreement Number 2126
P.A. No. 2126 BFE1
P.A. No. 2126 BFE-1
BUYER FURNISHED EQUIPMENT VARIABLES
relating to
BOEING MODEL 767-316ER AIRCRAFT
This Supplemental Exhibit BFE1 contains vendor selection dates, on-dock dates
and other variables applicable to the Aircraft.
1. Supplier Selection.
Customer will:
1.1 Select and notify Boeing of the suppliers of the following
BFE items by the following dates:
Galley System May 21, 1998
------------
Seats (passenger) May 29, 1998
------------
P.A. No. 2126 BFE1-1
2. On-dock Dates
On or before September 1, 1998, Boeing will provide to Customer a BFE
Requirements On-Dock/Inventory Document (BFE Document) or an electronically
transmitted BFE Report which may be periodically revised, setting forth the
items, quantities, on-dock dates and shipping instructions relating to the
in-sequence installation of BFE. For planning purposes, a preliminary BFE
on-dock schedule is set forth below:
Item Preliminary On-Dock Dates
- ---- -------------------------
June 1999 Aircraft November 1999 Aircraft
------------------ ----------------------
Seats March 17, 1999 July 30, 1999
Galleys March 4, 1999 July 19, 1999
Electronics January 15, 1999 May 28, 1999
Furnishings March 26, 1999 August 10, 1998
P.A. No. 2126 BFE1-2
CUSTOMER SUPPORT VARIABLES
between
THE BOEING COMPANY
and
Lan Chile S.A.
Supplemental Exhibit CS1 to Purchase Agreement Number 2126
P.A. No. 2126 CS1 SA 1
CUSTOMER SUPPORT VARIABLES
relating to
BOEING MODEL 767-316ER AND MODEL 767-38EF AIRCRAFT
Customer and Boeing will conduct planning conferences approximately 12 months
prior to delivery of the first Aircraft, or as mutually agreed, in order to
develop and schedule a customized Customer Support Program to be furnished by
Boeing in support of the Aircraft.
The customized Customer Services Program will be based upon and equivalent to
the entitlements summarized below.
1. Maintenance Training.
1.1 Maintenance Training Minor Model Differences Course, if
required, covering operational, structural or systems
differences between Customer's newly-purchased Aircraft and an
aircraft of the same model currently operated by Customer; 1
class of 15 students;
1.2 Training materials, if applicable, will be provided to each
student. In addition, one set of training materials as used in
Boeing's training program, including visual aids, text and
graphics will be provided for use in Customers own training
program.
2. Flight Training.
Boeing will provide, if required, one classroom course to acquaint up
to 15 students with operational, systems and performance differences
between Customer's newly-purchased Aircraft and an aircraft of the
same model currently operated by Customer.
Training materials, if applicable, will be provided to each student.
In addition, one set of training materials as used in Boeing's
training program, including visual aids, text and graphics will be
provided for use in Customer's own training program.
3. Planning Assistance.
3.1 Maintenance and Ground Operations.
Upon request, Boeing will provide planning assistance
regarding Minor Model Differences requirements for facilities,
tools and equipment.
P.A. No. 2126 CS1-1 SA 1
3.2 Spares.
Boeing will revise, as applicable, the customized Recommended
Spares Parts List (RSPL) and Illustrated Parts Catalog (IPC).
4. Technical Data and Documents
4.1. Flight Operations.
Airplane Flight Manual
Operations Manual
Quick Reference Handbook
Weight and Balance Manual
Dispatch Deviation Procedures Guide
Flight Crew Training Manual
Baggage/Cargo Loading Manual
Performance Engineer's Manual
Jet Transport Performance Methods
FMC Supplemental Data Document
Operational Performance Software
4.2. Maintenance.
Aircraft Maintenance Manual
Wiring Diagram Manual
Systems Schematics Manual
Connector Part Number Options Document
Structural Repair Manual
Overhaul/Component Maintenance Manual
Standard Overhaul Practices Manual
Standard Wiring Practices Manual
Non-Destructive Test Manual
Service Bulletins and Index
Corrosion Prevention Manual
Fault Isolation Manual
Fuel Measuring Stick Calibration Document
Power Plant Buildup Manual
Built-In Test Equipment (BITE) Manual
Central Maintenance Computer System Reporting Table
In Service Activity Report
All Operator Letters
Service Letters
Structural Item Interim Advisory
Maintenance Tips
Combined Index
P.A. No. 2126 CS1-2 SA 1
4.3. Maintenance Planning.
Maintenance Planning Data Document
Maintenance Planning Data Tasks Masterfile
Maintenance Task Cards and Index
Maintenance Inspection Intervals Report
4.4. Spares.
Illustrated Parts Catalog
Standards Books
4.5. Facilities and Equipment Planning.
Facilities and Equipment Planning Document
Special Tool and Ground Handling Equipment Drawings and Index
Supplementary Tooling Documentation
System Test Equipment Document
Illustrated Tool and Equipment List/Manual
Aircraft Recovery Document
Airplane Characteristics for Airport Planning Document
Airplane Rescue and Fire Fighting Document
Engine Handling Document
4.6. Computer Software Index.
4.7. Supplier Technical Data.
Service Bulletins
Ground Support Equipment Data
Provisioning Information
Component Maintenance/Overhaul Manuals and Index
Publications Index
Product Support Supplier Directory
P.A. No. 2126 CS1-3 SA 1
ENGINE ESCALATION,
ENGINE WARRANTY AND PATENT INDEMNITY
between
THE BOEING COMPANY
and
Lan Chile S.A.
Supplemental Exhibit EE1-2 to Purchase Agreement Number 2126
P.A. No. 2126 SA13 EE1-2
ENGINE ESCALATION,
ENGINE WARRANTY AND PATENT INDEMNITY
relating to
BOEING MODEL 767-316F AIRCRAFT
1. ENGINE ESCALATION.
(a) The Aircraft Basic Price of each Aircraft set forth in Table 1 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 CPLb is the Engine Escalation Base Year Index as set forth in Table 1 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 1
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 1 of the Purchase
Agreement.
CPI = L + ICI (rounded to the nearest hundredth)
0 = A value determined using the U.S. Department of
Labor, Bureau of Labor Statistics "Employment Cost
Index Wages and Salaries for Aircraft Manufacturing
(SIC 3721)", 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 65% and
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" calculated
PA. No. 2126 SA13 EE1-2 Page 1
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
delivery of the Aircraft, then multiplied by 35% and
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 (SIC 3721) and
Producer Prices and Price Index - Industrial Commodities Index used will be
those published as of a date 30 days prior to the first day of the scheduled
Aircraft delivery month to Customer. As the Employment Cost Index Wages and
Salaries for Aircraft Manufacturing (SIC 3721) values are only released on a
quarterly basis, the value released for the month of March will be used for the
months of January and February; the value for June used for April and May; the
value for September used for July and August; and the value for December used
for October and November. 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 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
PA. No. 2126 SA13 EE1-2 Page 2
reflect any substitute values. However, if within 24 months from delivery of the
Aircraft, the U.S. Department of Labor, Bureau of Labor Statistics should resume
releasing values for the months needed to determine the Engine Price Adjustment,
such values will be used to determine the increase or decrease in the Engine
Price Adjustment determined at the time of delivery of such Aircraft.
NOTE: The factor (CPI divided by the base year index) by which the
Engine Price is to be multiplied will be expressed as a decimal
and rounded to the nearest thousandth. Any rounding of a number,
as required under this Supplemental Exhibit 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.
PA. No. 2126 SA13 EE1-2 Page 3
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.
PA. No. 2126 SA13 EE1-2 Page 4
SERVICE LIFE POLICY COMPONENTS
between
THE BOEING COMPANY
and
LanChile S.A.
Supplemental Exhibit SLP1 to Purchase Agreement Number 2126
PA. No. 2126 SLP1
COVERED SERVICE LIFE COMPONENTS
relating to
BOEING MODEL 767 AIRCRAFT
This is the listing of Covered Components for the Aircraft which relate to Part
3, Boeing Service Life Policy of Exhibit C, Product Assurance Document to the
AGTA and is a part of Purchase Agreement No. 2126.
1. Wing.
(a) Upper and lower wing skins and stiffeners between the forward
and rear wing spars.
(b) Wing spar webs, chords and stiffeners.
(c) Inspar wing ribs.
(d) Inspar splice plates and fittings.
(e) Main landing gear support structure.
(f) Wing center section lower beams, spanwise beams and floor
beams, but not the seat tracks attached to the beams.
(g) Wing-to-body structural attachments.
(h) Engine strut support fittings attached directly to wing
primary structure.
(i) Support structure in the wing for spoilers and spoiler
actuators; for aileron hinges and reaction links; and for
leading edge devices and trailing edge flaps.
(j) Leading edge device and trailing edge flap support system.
(k) Aileron, leading edge device and trailing edge flap internal,
fixed attachment and actuator support structure.
2. Body.
(a) External surface skins and doublers, longitudinal stiffeners,
longerons and circumferential rings and frames between the
PA. No. 2126 SLP1-1
forward pressure bulkhead and the vertical stabilizer rear
spar bulkhead, and structural support and enclosure for the
APU but excluding all system components and related
installation and connecting devices, insulation, lining, and
decorative panels and related installation and connecting
devices.
(b) Window and windshield structure but excluding the windows and
windshields.
(c) Fixed attachment structure of the passenger doors, cargo doors
and emergency exits excluding door mechanisms and movable
hinge components. Sills and frames around the body openings
for the passenger doors, cargo doors and emergency exits,
excluding scuff plates and pressure seals.
(d) Nose wheel well structure, including the wheel well walls,
pressure deck, forward and aft bulkheads, and the gear support
structure.
(e) Main gear wheel well structure including pressure deck,
bulkheads and landing gear beam support structure.
(f) Floor beams and support posts in the control cab and passenger
cabin area, but excluding seat tracks.
(g) Forward and aft pressure bulkheads.
(h) Keel structure between the wing front spar bulkhead and the
main gear wheel well aft bulkhead, including splices.
(i) Wing front and rear spar support bulkheads, and vertical and
horizontal stabilizer front and rear spar support bulkheads
including terminal fittings but excluding all system
components and related installation and connecting devices,
insulation, lining, and decorative panels and related
installation and connecting devices.
(j) Support structure in the body for the stabilizer pivot and
stabilizer screw.
3. Vertical Stabilizer.
(a) External skins between front and rear spars including splices.
(b) Front, rear and auxiliary spar chords, webs and stiffeners,
and attachment fittings between vertical stabilizer and body.
PA. No. 2126 SLP1-2
(c) Inspar ribs.
(d) Support structure in the vertical stabilizer for rudder
hinges, reaction links and actuators.
(e) Rudder internal, fixed attachment and actuator support
structure.
(f) Rudder hinges and supporting ribs, excluding bearings.
4. Horizontal Stabilizer.
(a) External skins between front and rear spars.
(b) Front, rear and auxiliary spar chords, webs and stiffeners.
(c) Inspar ribs.
(d) Stabilizer center section and fittings splicing to outboard
stabilizer including pivot and screw support structure.
(e) Support structure in the horizontal stabilizer for the
elevator hinges, reaction links and actuators.
(f) Elevator internal, fixed attachment and actuator support
structure.
5. Engine Strut.
(a) Strut external surface skin and doublers and stiffeners.
(b) Internal strut chords, frames and bulkheads.
(c) Strut to wing fittings and diagonal brace.
(d) Engine mount support fittings attached directly to strut
structure.
(e) For Aircraft equipped with General Electric or Pratt & Whitney
engines only, the engine mounted support fittings.
6. Main Landing Gear.
(a) Outer cylinder.
(b) Inner cylinder.
(c) Upper and lower side strut, including spindles and universals.
(d) Upper and lower drag strut, including spindles and universals.
PA. No. 2126 SLP1-3
(e) Orifice support tube.
(f) Downlock links, including spindles and universals
(g) Torsion links.
(h) Bogie beam.
(i) Axles.
7. Nose Landing Gear.
(a) Outer cylinder.
(b) Inner cylinder, including axles.
(c) Orifice support tube.
(d) Upper and lower drag strut, including lock links.
(e) Steering plates and steering collar.
(f) Torsion links.
(g) Actuator support beam and hanger.
NOTE: The Service Life Policy does not cover any bearings, bolts, bushings,
clamps, brackets, actuating mechanisms or latching mechanisms used in
or on the Covered Components.
PA. No. 2126 SLP1-4
Boeing Commercial Airplane Group
P.O. Box 3707
Seattle. WA 98124-2207
2126-1
LanChile S.A.
Estado l0
Casilla 147D
Santiago, Chile
Subject: Seller Purchased Equipment
Reference: Purchase Agreement No. 2126 (the Purchase Agreement) between
The Boeing Company (Boeing) and LanChile S.A. (Customer)
relating to Model 767-316ER aircraft (the Aircraft)
This 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.
Definition of Terms:
Seller Purchased Equipment (SPE): Buyer Furnished Equipment (BFE) that Boeing
purchases for Customer.
Developmental Buyer Furnished Equipment (DBFE): BFE not previously certified for
installation on the same model aircraft.
Developmental Avionics: Developmental avionics are avionics that have not been
previously certified for installation on the same model aircraft. This Letter
Agreement does not include developmental avionics.
1. Price.
Advance Payments. An estimated SPE price will be included in the
Advance Payment Base Price for the purpose of establishing the advance payments
for the Aircraft. The estimated price of this SPE for the Aircraft is $***
expressed in July 1995 dollars.
Aircraft Price. The Aircraft Price will be adjusted to reflect (i) the
actual costs charged Boeing by the SPE suppliers, (ii) a handling fee of 10% of
such costs and (iii) reasonable transportation charges. If all DBFE, except for
Developmental Avionics, is converted to SPE, Boeing will waive the handling fee
for all SPE.
PA. No. 2126
2. Responsibilities.
2.1 Customer is responsible for
(i) selecting the supplier on or before:
May 21, 1998 for galleys
-------------
May 29, 1998 for seats
-------------
(ii) selecting a FAA certifiable part; and
(iii) providing to Boeing the SPE part
specification/Customer requirements.
2.2. Boeing is responsible for:
(i) placing and managing the purchase order with the
supplier;
(ii) coordinating with the suppliers on technical issues;
(iii) ensuring that the delivered SPE complies with the
part specification;
(iv) obtaining certification of the Aircraft with the SPE
installed; and
(v) obtaining for Customer the supplier's standard
warranty for the SPE. SPE is deemed to be BFE for
purposes of Part 2 of Exhibit C, the Product
Assurance Document.
3. Supplier Selection For SPE Galleys and Seats.
In addition to those responsibilities described above, for SPE galleys
and seats the following provisions apply with respect to Customer's selection of
suppliers:
Galley Requirements. Customer will provide Boeing the definitive galley
configuration requirements not later than TBD.
Bidder's List. For information purposes, Boeing will submit to Customer
a bidder's list of existing suppliers of seats and galleys within 120 days of
the supplier selection date shown above.
PA. No. 2126
Request for Quotation (REQ). Approximately 90 days prior to the
supplier selection date, Boeing will issue its REQ inviting potential bidders to
submit bids for the galleys and seats within 30 days of the selection date.
Recommended Bidders. Not later than 15 days prior to the supplier
selection date, Boeing will submit to Customer a list of recommended bidders
from which to choose a supplier for the galleys and seats. The recommendation is
based on an evaluation of the bids submitted using price, weight, warranty and
schedule as the criteria.
Supplier Selection. If Customer selects a seat or galley supplier that
is not on the Boeing recommended list, such seat or galley will become BFE and
the provisions of Exhibit A, Buyer Furnished Equipment Provisions Document, of
the AGTA will apply.
4. Changes.
After this Letter Agreement is signed, changes to SPE may only be made
by and between Boeing and the suppliers. Customer's contacts with SPE suppliers
relating to design (including selection of materials and colors), weights,
prices or schedules are for informational purposes only. If Customer wants any
changes made, requests must be made directly to Boeing for coordination with the
supplier.
5. Proprietary Rights.
Boeing's obligation to purchase SPE will not impose upon Boeing any
obligation to compensate Customer or any supplier for any proprietary rights
Customer may have in the design of the SPE.
6. Remedies.
If Customer does not comply with the obligations above, Boeing may:
(i) delay delivery of the Aircraft;
(ii) deliver the Aircraft without installing the SPE;
(iii) substitute a comparable part and invoice Customer for the cost;
(iv) increase the Aircraft Price by the amount of Boeing's additional
reasonable costs directly attributable to such noncompliance.
PA. No. 2126
7. Customer's Indemnification of Boeing.
Customer will indemnify and hold harmless Boeing from and against all
claims and liabilities, including costs and expenses (including attorneys' fees)
incident thereto or incident to successfully establishing the right to
indemnification, for injury to or death of any person or persons, including
employees of Customer but not employees of Boeing, or for loss of or damage to
any property, including Aircraft, arising out of or in any way connected with
any nonconformance or defect in any SPE and whether or not arising in tort or
occasioned in whole or in part by the negligence of Boeing. This indemnity will
not apply with respect to any nonconformance or defect caused solely by Boeing's
installation of the SPE.
Very truly yours,
THE BOEING COMPANY
By /s/ [Illegible Signature]
--------------------------
Its Attorney-In-Fact
--------------------------
ACCEPTED AND AGREED TO this
Date January 30, 1998
--------------------------
LANCHILE S.A.
By /s/ Carlos Prado C.
--------------------------
Its S.V.P. Technical
--------------------------
PA. No. 2126
Boeing Commercial Airplanes
P.O. Box 3707
Seattle. WA 98124-2207
6-1162-LAJ-0895
Lan Chile S.A.
Santiago, Chile
Subject: Business Considerations
Reference: Purchase Agreement No. 2126 (The Purchase Agreement)
between The Boeing Company (Boeing) and Lan Chile S.A.
(Customer) relating to Model 767-316F aircraft (the Aircraft)
This letter agreement (Letter Agreement) amends the Purchase Agreement. All
terms used but not defined in this Letter Agreement shall have the same meaning
as in the Purchase Agreement. This Letter Agreement supersedes and replaces in
its entirety Letter Agreement 6-1162-LAJ-310R1 dated July 17, 2002.
1. Credit Memorandum.
Boeing will provide concurrent with the delivery of each Model 767-316F
Aircraft contained on the Aircraft Information Table No. 5 of the Purchase
Agreement a credit memorandum equal to ***% of the escalated Airframe Price.
This credit memorandum may be used for the purchase of any Boeing goods and
services including aircraft but the credit memorandum may not be used for
advance payments.
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 Buyer 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.
6-1162-LAJ-0895
Page 2
4. 2005 Special Credit Memorandum for Firm Aircraft.
In consideration of Customer purchasing the Jul-05 and Oct-05 delivery
positions identified in the Aircraft Information Table No. 5 of the Purchase
Agreement, Boeing will provide concurrent with the delivery the Jul-05 and
Oct-05 delivery positions a special 2005 credit memorandum equal to ***% of the
escalated Airframe Price. This credit memorandum may be used for the purchase of
any Boeing goods and services including aircraft but the credit memorandum may
not be used for advance payments.
5. Engine Thrust Reverser Credit Memo.
In consideration of Customer purchasing the purchasing the Jul-05 and
Oct-05 delivery positions identified in the Aircraft Information Table No. 5 of
the Purchase Agreement, Boeing will provide concurrent with the delivery the
Jul-05 and Oct-05 delivery positions a credit memorandum equal to *** dollars
(US $***). This credit memorandum may be used for the purchase of any Boeing
goods and services including aircraft but the credit memorandum may not be used
for advance payments.
6. Special Credit Memo for Purchasing Two (2) Aircraft.
In consideration of Customer purchasing the purchasing the Jul-05 and
Oct-05 delivery positions identified in the Aircraft Information Table No.
5 of the Purchase Agreement, Boeing will provide concurrent with the
delivery the Jul-05 and Oct-05 delivery positions a credit memorandum equal
to *** dollars (US $***). This credit memorandum may be used for the
purchase of any Boeing goods and services including aircraft but the credit
memorandum may not be used for advance payments.
7. Payment Due at Signing of Supplemental Agreement No. 14.
Notwithstanding payment requirements described in Supplemental
Agreement No. 14, Customer may defer the payment(s) that would otherwise be
required at signing to any date on or before ***.
6-1162-LAJ-0895
Page 3
8. Deferred Advance Payment Schedule.
Notwithstanding the Advance Payment Schedule in the Airplane
Information Table No. 5 of the Purchase Agreement, Customer may elect to utilize
the following Deferred Advance Payment Schedule.
Due Date of Payment Amount Due per Aircraft
- ------------------- -----------------------
(Percentage times Advance Payment Base Price)
Signing of Definitive Agreement ***% (less the Deposit)
*** months prior to the first day of the scheduled ***%
delivery month of the Aircraft
*** months prior to the first day of the scheduled ***%
delivery month of the Aircraft
*** months prior to the first day of the scheduled ***%
delivery month of the Aircraft _____
Total ***%
9. Interest Rate for Deferred Advance Payments on Firm Aircraft.
For the period from May 6, 2004 through June 30, 2004 Customer will pay
interest on all amounts that are deferred pursuant to the above schedule at a
fluctuating rate per annum equal to the sixty day (60 day) London Interbank
Offered Rate (LIBOR), as published in The Wall Street Journal on April 1, 2004,
plus ***%. For the remaining period from July 1, 2004 until delivery of each of
the Firm Aircraft, Customer will pay interest on all amounts that are deferred
pursuant to the above schedule at a fluctuating rate per annum equal to the
ninety day (90 day) London Interbank Offered Rate (LIBOR), as published in The
Wall Street Journal effective for the first business day of each calendar
quarter (usually published on the business day just prior to such calendar
quarter), plus ***%. Such interest shall accrue from and including the date on
which such payments would have been due if there were no deferral up to the but
excluding the date on which such amounts are paid in full. Interest shall be due
and payable quarterly with any remaining unpaid amount due at delivery of each
Firm Aircraft (Note: the interest rate as determined above for the period of
July 1, 2004 until delivery of each of the Firm Aircraft will be used for the
entire calendar quarter; e.g., the interest rate determined based on the LIBOR
interest rate for July 1, 2004, would be used for all interest calculations in
July, August and September of 2004.)
6-1162-LAJ-0895
Page 4
10. Confidentiality.
Customer understands that the information contained in this Letter
Agreement is considered confidential. Customer agrees to treat this Letter
Agreement as confidential and will not, without the prior written consent of
Boeing, disclose this Letter Agreement or any information contained herein to
any third parties.
If the foregoing correctly sets forth your understanding of our agreement with
respect to the matters treated above, please indicate your acceptance and
approval below.
Very truly yours,
THE BOEING COMPANY
By /s/ Lyn A. Johnson
--------------------------------
Its Attorney-In-Fact
--------------------------------
ACCEPTED AND AGREED TO this
Date 20th, April, 2004
--------------------------------
LAN CHILE S.A.
By /s/ Carlos Prado C.
--------------------------------
Its Senior VP Corporate Investments
--------------------------------