CONFIDENTIAL MATERIAL APPEARING IN THIS DOCUMENT HAS BEEN OMITTED AND FILED

SEPARATELY WITH THE SECURITIES AND EXCHANGE COMMISSION IN ACCORDANCE WITH

THE SECURITIES ACT OF 1933, AS AMENDED, AND RULE 24B-2 PROMULGATED THEREUNDER.

OMITTED INFORMATION HAS BEEN REPLACED WITH ASTERISKS.

Exhibit 10.5

Supplemental Agreement No. 59

to

Purchase Agreement No. 1951

(the Agreement)

Between

The Boeing Company

and

Continental Airlines, Inc.

Relating to Boeing Model 737 Aircraft

THIS SUPPLEMENTAL AGREEMENT, is entered into as of July 12, 2012 by and between
THE BOEING COMPANY (Boeing) and CONTINENTAL AIRLINES, INC. (Customer);

WHEREAS, Boeing and Customer agree to *** applicable for the Model 737-924ER
Aircraft ***;

WHEREAS, Customer and Boeing agree to revise the Model 737-924ER performance
guarantees for those aircraft *** to reflect the current configuration and ***;

WHEREAS, Customer and Boeing agree to revise the terms of Customer’s agreement
concerning ***;

WHEREAS, Boeing and Customer agree to implement a *** for Model 737 Aircraft
delivering from ***;

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

 

P.A. 1951

CAL

   SA 59–1   

--------------------------------------------------------------------------------

Supplemental Agreement No. 59 to

Purchase Agreement No. 1951

 

  1. Table of Contents, Articles, Tables, Exhibits, and Letter Agreements:

1.1 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. 59

1.2 Remove and replace, in its entirety, Letter Agreement 6-1162-GOC-131R11,
“Special Matters”, with the revised Letter Agreement 6-1162-GOC-131R12, attached
hereto.

1.3 Remove and replace, in its entirety, Letter Agreement 6-1162-MMF-311R7, ***
with the revised Letter Agreement 6-1162-MMF-311R8, attached hereto.

1.4 Add Letter Agreement CAL-PA-1951-LA-1209037, ***.

1.5 Add Letter Agreement CAL-PA-1951-LA-1208066, “Aircraft Performance
Guarantees – Model 737-924ER Aircraft ***”.

1.6 Add Letter Agreement CAL-PA-1951-LA-1209110, “Privileged and Confidential
Matters”.

The Agreement will be deemed to be supplemented to the extent herein provided as
of the date hereof and as so supplemented will continue in full force and
effect.

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

 

THE BOEING COMPANY     CONTINENTAL AIRLINES, INC. By:   /s/ ***     By:   /s/
Gerald Laderman Its:   Attorney-in-Fact     Its:   Senior Vice President –
Finance and Treasurer

 

P.A. 1951

CAL

   SA 59–2   

--------------------------------------------------------------------------------

TABLE OF CONTENTS

 

          Page
Number      SA
Number  

ARTICLES

     

1.

   Subject Matter of Sale      1-1         SA 39   

2.

   Delivery, Title and Risk of Loss      2-1      

3.

   Price of Aircraft      3-1         SA 39   

4.

   Taxes      4-1      

5.

   Payment      5-1      

6.

   Excusable Delay      6-1      

7.

   Changes to the Detail Specification      7-1         SA 39   

8.

   Federal Aviation Requirements and Certificates and Export License      8-1   
     SA 39   

9.

   Representatives, Inspection, Flights and Test Data      9-1      

10.

   Assignment, Resale or Lease      10-1      

11.

   Termination for Certain Events      11-1      

12.

   Product Assurance; Disclaimer and Release; Exclusion of Liabilities; Customer
Support; Indemnification and Insurance      12-1      

13.

   Buyer Furnished Equipment and Spare Parts      13-1      

14.

   Contractual Notices and Requests      14-1         SA 39   

15.

   Miscellaneous      15-1      

 

P.A. 1951

N/CAL

   SA 59

 

i

--------------------------------------------------------------------------------

TABLE OF CONTENTS

 

          Page
Number      SA
Number  

TABLES

     

1.

   Aircraft Deliveries and Descriptions – 737-500      T-1         SA 3      
Aircraft Deliveries and Descriptions – 737-700      T-2         SA 57      
Aircraft Deliveries and Descriptions – 737-800      T-3         SA 55      
Aircraft Deliveries and Descriptions – 737-600      T-4         SA 4      
Aircraft Deliveries and Descriptions – 737-900      T-5         SA 39      
Aircraft Deliveries and Descriptions – 737-900ER      T-6         SA 58   

EXHIBITS

     

A-1

   Aircraft Configuration – Model 737-724 (Aircraft delivering through July
2004)         SA 26   

A-1.1

   Aircraft Configuration – Model 737-724 (Aircraft delivering on or after
August 2004)         SA 46   

A-2

   Aircraft Configuration – Model 737-824 (Aircraft delivering through July
2004)         SA 26   

A-2.1

   Aircraft Configuration – Model 737-824 (Aircraft delivering August 2004
through December 2007)         SA 41   

A-2.2

   Aircraft Configuration – Model 737-824 (Aircraft delivering January 2008
through July 2008)         SA 45   

A-2.3

   Aircraft Configuration – Model 737-824 (Aircraft scheduled to deliver between
August 2008 and October 2010)         SA 50   

A-2.4

   Aircraft Configuration – Model 737-824 (Aircraft scheduled to deliver in or
after November 2010)         SA 50   

 

 

P.A. 1951

N/CAL

 

   SA 59

ii

--------------------------------------------------------------------------------

TABLE OF CONTENTS

 

          SA
Number
 

EXHIBITS (continued)

     

A-3

   Aircraft Configuration – Model 737-624         SA 1   

A-4

   Aircraft Configuration – Model 737-524         SA 3   

A-5

   Aircraft Configuration – Model 737-924 ***         SA 26   

A-6

   Aircraft Configuration – Model 737-924ER ***         SA 45   

A-6.1

   Aircraft Configuration – Model 737-924ER ***         SA 53   

A-6.2

   Aircraft Configuration – Model 737-924ER ***         SA 53   

B

   Product Assurance Document         SA 1   

C

   Customer Support Document – Code Two – Major Model Differences         SA 1
  

C1

   Customer Support Document – Code Three – Minor Model Differences         SA
39   

D

   Aircraft Price Adjustments – New Generation Aircraft (1995 Base Price – ***
        SA 1   

D1

   Airframe and Engine Price Adjustments – Current Generation Aircraft        
SA 1   

D2

   Aircraft Price Adjustments – New Generation Aircraft (1997 Base Price – ***
        SA 5   

D3

   Aircraft Price Adjustments – New Generation Aircraft (July 2003 Base Price –
***         SA 41   

D4

   Escalation Adjustment – Airframe and Optional Features ***         SA 41   

 

P.A. 1951

N/CAL

 

   SA 59

iii

--------------------------------------------------------------------------------

TABLE OF CONTENTS

 

          SA
Number
 

EXHIBITS (continued)

     

E

   Buyer Furnished Equipment Provisions Document         SA 39   

F

   Defined Terms Document         SA 5   

LETTER AGREEMENTS

     

1951-1

   Not Used      

1951-2R4

   Seller Purchased Equipment         SA 39   

1951-3R22

   Option Aircraft – Model 737-824 Aircraft         SA 38   

1951-4R1

   Waiver of Aircraft Demonstration         SA 1   

1951-5R3

   Promotional Support – New Generation Aircraft         SA 48   

1951-6

   Configuration Matters      

1951-7R1

   Spares Initial Provisioning         SA 1   

1951-8R2

   Escalation Sharing – New Generation Aircraft         SA 4   

1951-9R20

   Option Aircraft – Model 737-724 Aircraft         SA 58   

1951-11R1

   Escalation Sharing – Current Generation Aircraft         SA 4   

1951-12R7

   Option Aircraft – Model 737-924 Aircraft         SA 32   

1951-13

   Configuration Matters – Model 737-924         SA 5   

1951-14

   Installation of Cabin Systems Equipment 737-924         SA 22   

1951-15

   Configuration Matters – Model 737-924ER         SA 39   

 

P.A. 1951

N/CAL

 

   SA 59

iv

--------------------------------------------------------------------------------

TABLE OF CONTENTS

 

     SA
Number  

RESTRICTED LETTER AGREEMENTS

  

6-1162-MMF-295

   Performance Guarantees – Model 737-724 Aircraft   

6-1162-MMF-296

   Performance Guarantees – Model 737-824 Aircraft   

6-1162-MMF-308R4

   Disclosure of Confidential Information      SA 39   

6-1162-MMF-309R1

   ***      SA 1   

6-1162-MMF-311R8

   ***      SA 59   

6-1162-MMF-312R1

   Special Purchase Agreement Provisions      SA 1   

6-1162-MMF-319

   Special Provisions Relating to the Rescheduled Aircraft   

6-1162-MMF-378R1

   Performance Guarantees – Model 737-524 Aircraft      SA 3   

6-1162-GOC-015R1

   ***      SA 31   

6-1162-GOC-131R12

   Special Matters      SA 59   

6-1162-DMH-365

   Performance Guarantees – Model 737-924 Aircraft      SA 5   

6-1162-DMH-624

   ***      SA 8   

6-1162-DMH-680

   Delivery Delay Resolution Program      SA 9   

6-1162-DMH-1020

   ***      SA 14   

6-1162-DMH-1035

   ***      SA 15   

6-1162-DMH-1054

   ***      SA 16   

6-1162-CHL-048

   Rescheduled Aircraft Agreement      SA 26   

 

P.A. 1951

N/CAL

 

   SA 59

v

--------------------------------------------------------------------------------

TABLE OF CONTENTS

 

     SA
Number  

RESTRICTED LETTER AGREEMENTS (continued)

  

6-1162-CHL-195

   Restructure Agreement for Model 737NG and 757-300 Aircraft      SA 30   

6-1162-MSA-768

   Performance Guarantees – Model 737-924ER Aircraft ***      SA 57   

6-1162-SEE-0361

   Performance Guarantees – Model 737-924ER Aircraft ***      SA 57   

6-1162-SEE-133

   Model 737-924ER ***      SA 46   

6-1162-SEE-0176R4

   Record Option Proposals      SA 48   

6-1162-SEE-0187

   Passenger Service Unit Resolution      SA 50   

6-1162-SEE-0225R1

   Use of Aircraft – Carbon Brakes *** Testing      SA 50   

6-1162-SEE-0263

   Use of Aircraft – 737NG Performance Improvement Package Testing      SA 50   

6-1162-RCN-1888

   Use of Aircraft – Boeing 747-800 and 787 Flight Test Training      SA 53   

6-1162-RCN-1890

   Use of Aircraft for Testing      SA 57   

6-1162-SEE-0326

   Model 737 – Koito Seat Resolution      SA 56   

CAL-PA-1951-LA-1208066

   Aircraft Performance Guarantees – Model 737-924ER Aircraft ***      SA 59   

CAL-PA-1951-LA-1209037

   ***      SA 59   

CAL-PA-1951-LA-1209110

   Privileged and Confidential Matters      SA 59   

 

P.A. 1951

N/CAL

 

   SA 59

vi

--------------------------------------------------------------------------------

TABLE OF CONTENTS

 

 

SUPPLEMENTAL AGREEMENTS

  

DATED AS OF:

Supplemental Agreement No. 1

   October 10, 1996

Supplemental Agreement No. 2

   March 5, 1997

Supplemental Agreement No. 3

   July 17, 1997

Supplemental Agreement No. 4

   October 10, 1997

Supplemental Agreement No. 5

   May 21, 1998

Supplemental Agreement No. 6

   July 30, 1998

Supplemental Agreement No. 7

   November 12, 1998

Supplemental Agreement No. 8

   December 7, 1998

Supplemental Agreement No. 9

   February 18, 1999

Supplemental Agreement No. 10

   March 19, 1999

Supplemental Agreement No. 11

   May 14, 1999

Supplemental Agreement No. 12

   July 2, 1999

Supplemental Agreement No. 13

   October 13, 1999

Supplemental Agreement No. 14

   December 13, 1999

Supplemental Agreement No. 15

   January 13, 2000

Supplemental Agreement No. 16

   March 17, 2000

Supplemental Agreement No. 17

   May 16, 2000

Supplemental Agreement No. 18

   September 11, 2000

Supplemental Agreement No. 19

   October 31, 2000

Supplemental Agreement No. 20

   December 21, 2000

Supplemental Agreement No. 21

   March 30, 2001

 

P.A. 1951

N/CAL

   SA 59

vii

--------------------------------------------------------------------------------

TABLE OF CONTENTS

 

SUPPLEMENTAL AGREEMENTS

  

DATED AS OF:

Supplemental Agreement No. 22

   May 23, 2001

Supplemental Agreement No. 23

   June 29, 2001

Supplemental Agreement No. 24

   August 31, 2001

Supplemental Agreement No. 25

   December 31, 2001

Supplemental Agreement No. 26

   March 29, 2002

Supplemental Agreement No. 27

   November 6, 2002

Supplemental Agreement No. 28

   April 1, 2003

Supplemental Agreement No. 29

   August 19, 2003

Supplemental Agreement No. 30

   November 4, 2003

Supplemental Agreement No. 31

   August 20, 2004

Supplemental Agreement No. 32

   December 29, 2004

Supplemental Agreement No. 33

   December 29, 2004

Supplemental Agreement No. 34

   June 22, 2005

Supplemental Agreement No. 35

   June 30, 2005

Supplemental Agreement No. 36

   July 21, 2005

Supplemental Agreement No. 37

   March 30, 2006

Supplemental Agreement No. 38

   June 6, 2006

Supplemental Agreement No. 39

   August 3, 2006

Supplemental Agreement No. 40

   December 5, 2006

Supplemental Agreement No. 41

   June 1, 2007

Supplemental Agreement No. 42

   June 13, 2007

 

P.A. 1951

N/CAL

   SA 59

viii

--------------------------------------------------------------------------------

Supplemental Agreement No. 43

   July 18, 2007

Supplemental Agreement No. 44

   December 7, 2007

Supplemental Agreement No. 45

   February 20, 2008

Supplemental Agreement No. 46

   June 25, 2008

Supplemental Agreement No. 47

   October 30, 2008

Supplemental Agreement No. 48

   January 29, 2009

Supplemental Agreement No. 49

   May 1, 2009

Supplemental Agreement No. 50

   July 23, 2009

Supplemental Agreement No. 51

   August 5, 2009

Supplemental Agreement No. 52

   August 31, 2009

Supplemental Agreement No. 53

   December 23, 2009

Supplemental Agreement No. 54

   March 1, 2010

Supplemental Agreement No. 55

   March 31, 2010

Supplemental Agreement No. 56

   August 12, 2010

Supplemental Agreement No. 57

   March 2, 2011

Supplemental Agreement No. 58

   January 6, 2012

Supplemental Agreement No. 59

   July     , 2012

 

P.A. 1951

N/CAL

   SA 59

ix

--------------------------------------------------------------------------------

6-1162-MMF-311R8

July 12, 2012

Continental Airlines, Inc.

1600 Smith Street

Houston, TX 77002

 

Subject:   Letter Agreement No. 6-1162-MMF-311R8 to Purchase Agreement No. 1951
– ***

Ladies and Gentlemen:

This Letter Agreement amends Purchase Agreement No. 1951 dated July 23, 1996
(the Agreement) between The Boeing Company (Boeing) and Continental Airlines,
Inc. (Buyer) relating to Model 737 aircraft (the Aircraft). This Letter
Agreement supersedes and replaces in its entirety Letter Agreement
6-1162-MMF-311R7 dated March 2, 2011.

All terms used herein and in the Agreement, and not defined herein, will have
the same meaning as in the Agreement.

***

 

1. ***.

 

2. ***.

 

3. ***.

 

  3.1 ***.

 

  3.2 ***.

 

  3.3 ***.

 

P.A. No. 1951    SA 59

Boeing / Continental Airlines, Inc. Proprietary

--------------------------------------------------------------------------------

Continental Airlines, Inc.

6-1162-MMF-311R8 Page 2

 

  3.4 ***.

 

  3.5 ***.

 

4. ***.

 

  4.1 ***.

 

  4.2 ***.

 

5. Confidential Treatment.

Buyer and Boeing understand that certain commercial and financial information
contained in this Letter Agreement are considered by Boeing and Buyer as
confidential and are subject to the terms and conditions set forth in Letter
Agreement No. CAL-PA-1951-LA-1209110.

If this Letter Agreement correctly states your understanding of the matters
treated herein, please so indicate by signature below.

Very truly yours,

THE BOEING COMPANY

 

P.A. No. 1951    SA 59

Boeing / Continental Airlines, Inc. Proprietary

--------------------------------------------------------------------------------

Continental Airlines, Inc.

6-1162-MMF-311R8 Page 3

 

By   /s/ *** Its   Attorney-in-Fact ACCEPTED AND AGREED TO this Date: July 12,
2012 CONTINENTAL AIRLINES, INC. By  

/s/ Gerald Laderman

Its   Senior Vice President – Finance and Treasurer

 

P.A. No. 1951    SA 59

Boeing / Continental Airlines, Inc. Proprietary

--------------------------------------------------------------------------------

Attachment A to

Letter Agreement 6-1162-MMF-311R8

 

Date:    

Continental Airlines, Inc.

1600 Smith Street

Houston, TX 77002

 

Attention:    Technical Department Reference:    Letter Agreement
6-1162-MMF-311R8 to Boeing/CAL Purchase Agreement 1951 Transmitted by
Facsimile:      TBD

***

Very truly yours,

THE BOEING COMPANY

 

By:     Its:    

 

P.A. No. 1951    SA 59

Boeing / Continental Airlines, Inc. Proprietary

--------------------------------------------------------------------------------

Attachment B to

Letter Agreement 6-1162-MMF-311R8

***

 

P.A. No. 1951    SA 59

Boeing / Continental Airlines, Inc. Proprietary

--------------------------------------------------------------------------------

The Boeing Company

P.O. Box 3707

Seattle, WA 98124-2207

July 12, 2012

6-1162-GOC-131R12

Continental Airlines, Inc.

1600 Smith Street

Houston, Texas 77002

 

LOGO [g408868g66d28.jpg]   Subject:   

Letter Agreement No. 6-1162-GOC-131R11 to Purchase

Agreement No. 1951 – Special Matters

Ladies and Gentlemen:

This Letter Agreement amends Purchase Agreement No. 1951 dated as of July 23,
1996 (the Agreement) between The Boeing Company (Boeing) and Continental
Airlines, Inc. (Buyer) relating to Model 737 aircraft (the Aircraft). This
Letter Agreement supersedes and replaces in its entirety Letter Agreement
6-1162-GOC-131R11 dated March 2, 2011.

All terms used herein and in the Agreement, and not defined herein, will have
the same meaning as in the Agreement.

 

  1. ***.

1.1 Model 737-724 Aircraft. In consideration of Buyer’s purchase of Model
737-724 Aircraft, *** at the time of delivery of each such Aircraft ***.

1.2 Model 737-824 Aircraft. In consideration of Buyer’s purchase of Model
737-824 Aircraft, *** at the time of delivery of each such ***.

1.3 Model 737-624 Aircraft. In consideration of Buyer’s purchase of Model
737-624 Aircraft, *** at the time of delivery of each such Aircraft ***.

1.4 Model 737-524 Aircraft. In consideration of Buyer’s purchase of Model
737-524 Aircraft, *** at the time of delivery of each such ***.

1.5 Model 737-324 Aircraft. ***.

1.6 Model 737-924 Aircraft. In consideration of Buyer’s purchase of Model
737-924 Aircraft, *** at the time of delivery of each such Aircraft ***.

 

P.A. No. 1951    SA 59

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Continental Airlines, Inc.

6-1162-GOC-131R12 Page 2

 

1.7 737-924ER Aircraft ***.

Boeing has introduced the 737-900 extended range aircraft (the 737-924ER
Aircraft). In consideration of Buyer’s purchase of Model 737-924ER Aircraft,
***.

1.8 ***.

***     

LOGO [g408868g66d28.jpg]

1.9 ***

***

1.10 ***.

For Buyer’s 737NG fleet, as well as any 737NG Aircraft delivering to Buyer ***.

 

P.A. No. 1951    SA 59

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Continental Airlines, Inc.

6-1162-GOC-131R12 Page 3

 

  2. *** Advance Payment Schedule.

 

  2.1 Firm Aircraft. ***

LOGO [g408868g66d28.jpg]

 

P.A. No. 1951    SA 59

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Continental Airlines, Inc.

6-1162-GOC-131R12 Page 4

 

2.2 Option Aircraft and follow-on Firm Aircraft. ***

3.   ***.

3.1   ***

3.2   ***

3.3   ***

3.4   ***

LOGO [g408868g66d28.jpg]

4.   ***.

4.1   ***

4.2   ***

4.2   ***

4.3   ***

4.4   ***

4.5   ***

4.6   ***

4.7   ***

5.   Option Aircraft.

5.1   ***

5.2   ***

6.   ***.

6.1   ***

6.2   ***

6.3   ***

 

P.A. No. 1951    SA 59

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Continental Airlines, Inc.

6-1162-GOC-131R12 Page 5

 

  6.4 ***

 

  6.6 ***

 

  6.7 ***

 

  6.8 ***

 

  6.9 ***

 

LOGO [g408868g66d28.jpg]

 

  7. Assignment of Credits.

Buyer may not assign the credit memoranda described in this Letter Agreement
without Boeing’s prior written consent ***

 

  8. Confidential Treatment.

 

P.A. No. 1951    SA 59

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Continental Airlines, Inc.

6-1162-GOC-131R12 Page 6

 

Buyer and Boeing understand that certain commercial and financial information
contained in this Letter Agreement are considered by Boeing and Buyer as
confidential and are subject to the terms and conditions set forth in Letter
Agreement No. CAL-PA-1951-LA-1209110.

Very truly yours,

THE BOEING COMPANY

 

LOGO [g408868g66d28.jpg]

 

  By   /s/ ***   Its   Attorney-in-Fact   ACCEPTED AND AGREED TO this   Date:  
July 12, 2012   CONTINENTAL AIRLINES, INC.   By  

/s/ Gerald Laderman

  Its   Senior Vice President – Finance and Treasurer

 

P.A. No. 1951    SA 59

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

LOGO [g408868g13d55.jpg]    The Boeing Company

P.O. Box 3707

Seattle, WA 98124-2207

CAL-PA-1951-LA-1208066

Continental Airlines, Inc.

1600 Smith Street

Houston, Texas 77002

 

Subject: Aircraft Performance Guarantees – Model 737-900ER Aircraft ***

 

Reference: Purchase Agreement No. 1951 (Purchase Agreement) between The Boeing
Company (Boeing) and Continental Airlines, Inc. (Customer) relating to
Model 737-924ER aircraft (Aircraft)

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

1. Aircraft Performance Guarantees.

Boeing agrees to provide Customer with the performance guarantees in the
Attachment. ***. Such guarantees are exclusive and will expire upon delivery of
the Aircraft to Customer.

2. Aircraft Configuration.

The performance guarantees as described in the Attachment for the Aircraft are
based on Detail Specification ***. Such performance guarantees as described in
the Attachment, may be revised as defined in Letter Agreement No. 1951-15.

3. Assignment.

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

4. Confidential Treatment.

Customer and Boeing understand that certain commercial and financial information
contained in this Letter Agreement are considered by Boeing and Customer as
confidential and are subject to the terms and conditions set forth in Letter
Agreement No. CAL-PA-1951-LA-1209110.

 

CAL-PA-1951-LA-1208066

  P.A. No. 1951

Performance Guarantees

  Page 1

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

 

LOGO [g408868g13d55.jpg]

Very truly yours,

 

THE BOEING COMPANY

By

  /s/ ***

Its

  Attorney-in-Fact

ACCEPTED AND AGREED TO this

Date:

  July 12, 2012

Continental Airlines, Inc.

By

  /s/ Gerald Laderman

Its

  Senior Vice President – Finance and Treasurer

 

CAL-PA-1951-LA-1208066

Performance Guarantees

  

P.A. No. 1951

Page 2

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 1

 

MODEL 737-900ER *** PERFORMANCE GUARANTEES

FOR CONTINENTAL AIRLINES, INC.

 

SECTION

  CONTENTS   

1

  AIRCRAFT MODEL APPLICABILITY   

2

  FLIGHT PERFORMANCE   

3

  MANUFACTURER’S EMPTY WEIGHT   

4

  AIRCRAFT CONFIGURATION   

5

  GUARANTEE CONDITIONS   

6

  GUARANTEE COMPLIANCE   

7

  EXCLUSIVE GUARANTEES   

 

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 1

 

1 AIRCRAFT MODEL APPLICABILITY

The guarantees contained in this Attachment (the “Performance Guarantees”) are
applicable to the 737-900ER Aircraft *** and a maximum takeoff weight of ***
pounds, a maximum landing weight of *** pounds, and a maximum zero fuel weight
of ***, and equipped with Boeing furnished *** engines.

 

2 FLIGHT PERFORMANCE

 

2.1 Takeoff

 

2.1.1 The FAA approved takeoff field length at a gross weight at the start of
the ground roll of *** pounds, at a temperature of ***°F, at a sea level
altitude, with an alternate forward center of gravity limit of *** percent of
the mean aerodynamic chord, and using maximum takeoff thrust, shall not be more
than the following guarantee value:

 

GUARANTEE:

   *** Feet

 

2.1.2 The FAA approved takeoff gross weight at the start of ground roll, at a
temperature of ***F, at an altitude of *** feet, from a *** foot runway, with an
alternate forward center of gravity limit of *** percent of the mean aerodynamic
chord, and using maximum takeoff thrust, shall not be less than the following
guarantee value:

 

GUARANTEE:

   *** Pounds

 

2.2 Landing

 

2.2.1 The FAA approved landing field length at a gross weight of *** pounds and
at a *** altitude, shall not be more than the following guarantee value:

 

GUARANTEE:

   *** Feet

 

2.2.2 The FAA approved landing field length at a gross weight of *** pounds and
at an altitude of *** feet, shall not be more than the following guarantee
value:

 

GUARANTEE:

   *** Feet

 

2.3 Speed

The level flight speed at a gross weight of *** pounds, on an ISA+10°C day, at
an altitude of *** feet and using not more than maximum cruise thrust, shall not
be less than the following guarantee value:

 

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 2

 

NOMINAL:

  *** KTAS

TOLERANCE:

  *** KTAS

GUARANTEE:

  *** KTAS

 

2.4 Altitude Capability – All Engines Operating

The altitude capability at a gross weight of *** pounds, on an ISA+10°C day, at
*** Mach number, and satisfying the conditions defined below, shall not be less
than the following guarantee value:

 

GUARANTEE:

  *** Feet

Conditions:

 

  1) The Aircraft shall be capable of maintaining level cruising flight using
not more than maximum cruise thrust.

 

  2) The Aircraft shall be capable of maintaining a rate of climb of *** feet
per minute using not more than maximum climb thrust.

 

  3) The Aircraft shall be capable of at least a *** g maneuver load factor at
buffet onset.

 

2.5 Enroute One-Engine-Inoperative Altitude

The FAA approved enroute one-engine-inoperative altitude at which the available
gross climb gradient equals *** percent at a gross weight of *** pounds on an
ISA+10°C day using not more than maximum continuous thrust, shall not be less
than the following guarantee value:

 

GUARANTEE:

  *** Feet

 

2.6 Cruise Range

The still air range at an initial cruise altitude of *** feet on a standard day
at *** Mach number, starting at a gross weight of *** pounds and consuming ***
pounds of fuel, and using not more than maximum cruise thrust (except maximum
climb thrust may be used during a step climb) and using the conditions and
operating rules defined below, shall not be less than the following guarantee
value:

 

NOMINAL:

  *** Nautical Miles

TOLERANCE:

  *** Nautical Miles

GUARANTEE:

  *** Nautical Miles

 

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 3

 

Conditions and operating rules:

A step climb or multiple step climbs of *** feet altitude may be used when
beneficial to minimize fuel burn.

 

2.7 Mission

 

2.7.1 Mission Payload

The payload for a stage length of *** nautical miles in still air (equivalent to
a distance of *** nautical miles with a *** knot headwind, representative of a
*** to *** route) using the conditions and operating rules defined below, shall
not be less than the following guarantee value:

 

NOMINAL:

  *** Pounds

TOLERANCE:

  *** Pounds

GUARANTEE:

  *** Pounds

Conditions and operating rules:

 

 

Stage Length:

  The stage length is defined as the sum of the distances for climb, cruise, and
descent.

Takeoff:

  The airport altitude is *** feet.   The airport temperature is ***°F.   The
runway length is *** feet.   The following obstacle definition is based on a
straight out departure where obstacle height and distance are specified with
reference to the liftoff end of the runway:  

         Distance               Height

 

1.        *** feet            *** feet

 

2.        *** feet            *** feet

 

3.        *** feet            *** feet

 

4.        *** feet            *** feet

 

5.        *** feet            *** feet

 

6.        *** feet            *** feet

  Takeoff performance is based on an alternate forward center of gravity limit
of *** percent of the mean aerodynamic chord.

 

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 4

 

   Maximum takeoff thrust is used for the takeoff.    The takeoff gross weight
shall conform to FAA Regulations.

Climbout Maneuver:

   Following the takeoff to *** feet, the Aircraft accelerates to *** KCAS while
climbing to *** feet above the departure airport altitude and retracting flaps
and landing gear.

Climb:

   The Aircraft climbs from *** feet above the departure airport altitude to ***
feet altitude at *** KCAS.    The Aircraft then accelerates at a rate of climb
of *** feet per minute to the recommended climb speed for minimum block fuel.   
The climb continues at the recommended climb speed for minimum block fuel until
*** Mach number is reached.    The climb continues at *** Mach number to the
initial cruise altitude.    The temperature is standard day during climb.   
Maximum climb thrust is used during climb.

Cruise:

   The Aircraft cruises at *** Mach number.    The initial cruise altitude is
*** feet.    A step climb or multiple step climbs of *** feet altitude may be
used when beneficial to minimize fuel burn.    The temperature is standard day
during cruise.    The cruise thrust is not to exceed maximum cruise thrust
except during a step climb when maximum climb thrust may be used.

Descent:

   The Aircraft descends from the final cruise altitude at *** KCAS to an
altitude of *** feet above the destination airport altitude.

 

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 5

 

  Throughout the descent, the cabin pressure will be controlled to a maximum
rate of descent equivalent to *** feet per minute at sea level.   The
temperature is standard day during descent.

Approach and Landing Maneuver:

  The Aircraft decelerates to the final approach speed while extending landing
gear and flaps, then descends and lands.   The destination airport altitude is
*** feet.

Fixed Allowances:

  For the purpose of this guarantee and for the purpose of establishing
compliance with this guarantee, the following shall be used as fixed quantities
and allowances:   Taxi-Out:  

Fuel            *** Pounds

  Takeoff and Climbout Maneuver:  

Fuel            *** Pounds

  Approach and Landing Maneuver:  

Fuel            *** Pounds

  Taxi-In (shall be consumed from the reserve fuel):  

Fuel            *** Pounds

  Usable reserve fuel remaining upon completion of the approach and landing
maneuver: *** Pounds   For information purposes, the reserve fuel is based on a
standard day temperature and a contingency fuel allowance equivalent to ***
minutes of continued cruise starting at the end of the mission cruise and at ***
Mach number.

 

2.7.2 Mission Payload

The payload for a stage length of *** nautical miles in still air (equivalent to
a distance of *** nautical miles with a *** knot headwind, representative of a
*** to *** route) using the conditions and operating rules defined below, shall
not be less than the following guarantee value:

 

NOMINAL:

  *** Pounds

TOLERANCE:

  *** Pounds

GUARANTEE:

  *** Pounds

 

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 6

 

Conditions and operating rules:

 

Stage Length:

  The stage length is defined as the sum of the distances for climb, cruise, and
descent.

Takeoff:

  The airport altitude is *** feet.   The takeoff gross weight is not limited by
the airport conditions.   Maximum takeoff thrust is used for the takeoff.   The
takeoff gross weight shall conform to FAA Regulations.

Climbout Maneuver:

  Following the takeoff to *** feet, the Aircraft accelerates to *** KCAS while
climbing to *** feet above the departure airport altitude and retracting flaps
and landing gear.

Climb:

  The Aircraft climbs from *** feet above the departure airport altitude to ***
feet altitude at *** KCAS.   The Aircraft then accelerates at a rate of climb of
*** feet per minute to the recommended climb speed for minimum block fuel.   The
climb continues at the recommended climb speed for minimum block fuel until ***
Mach number is reached.   The climb continues at the recommended climb speed for
minimum block fuel until the initial cruise altitude is reached.   The
temperature is ISA+5°C during climb.   Maximum climb thrust is used during
climb.

Cruise:

  The Aircraft cruises at *** Mach number.   The initial cruise altitude is ***
feet.   A step climb or multiple step climbs of *** feet altitude may be used
when beneficial to minimize fuel burn.   The temperature is ISA+5°C during
cruise.

 

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 7

 

  The cruise thrust is not to exceed maximum cruise thrust except during a step
climb when maximum climb thrust may be used.

Descent:

  The Aircraft descends from the final cruise altitude at *** KCAS to an
altitude of *** feet above the destination airport altitude.   Throughout the
descent, the cabin pressure will be controlled to a maximum rate of descent
equivalent to *** feet per minute at sea level.   The temperature is ISA+5°C
during descent.

Approach and Landing Maneuver:

  The Aircraft decelerates to the final approach speed while extending landing
gear and flaps, then descends and lands.   The destination airport altitude is
*** feet.

Fixed Allowances:

  For the purpose of this guarantee and for the purpose of establishing
compliance with this guarantee, the following shall be used as fixed quantities
and allowances:  

Taxi-Out:

Fuel            *** Pounds

 

Takeoff and Climbout Maneuver:

Fuel            *** Pounds

 

Approach and Landing Maneuver:

Fuel            *** Pounds

 

Taxi-In (shall be consumed from the reserve fuel):

Fuel            *** Pounds

  Usable reserve fuel remaining upon completion of the approach and landing
maneuver: *** Pounds   For information purposes, the reserve fuel is based on a
standard day temperature and a contingency fuel allowance equivalent to ***
minutes of continued cruise starting at the end of the mission and at a *** Mach
number.

 

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 8

 

2.7.3 Mission Payload

The payload for a stage length of *** nautical miles in still air (equivalent to
a distance of *** nautical miles with a *** knot tailwind, representative of a
*** to *** route) using the conditions and operating rules defined below, shall
not be less than the following guarantee value:

 

NOMINAL:

  *** Pounds

TOLERANCE:

  *** Pounds

GUARANTEE:

  *** Pounds

Conditions and operating rules:

 

Stage Length:

  The stage length is defined as the sum of the distances for climb, cruise, and
descent.

Takeoff:

  The airport altitude is *** feet.   The airport temperature is ***°F.   The
runway length is *** feet.   The runway slope is *** percent downhill.   Takeoff
performance is based on an alternate forward center of gravity limit of ***
percent of the mean aerodynamic chord.   Maximum takeoff thrust is used for the
takeoff.   The takeoff gross weight shall conform to FAA Regulations.

Climbout

  Following the takeoff to *** feet, the Aircraft accelerates to

Maneuver:

  *** KCAS while climbing to *** feet above the departure airport altitude and
retracting flaps and landing gear.

Climb:

  The Aircraft climbs from *** feet above the departure airport altitude to ***
feet altitude at *** KCAS.   The Aircraft then accelerates at a rate of climb of
*** feet per minute to the recommended climb speed for minimum block fuel.

 

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 9

 

  The climb continues at the recommended climb speed for minimum block fuel
until *** Mach number is reached.   The climb continues at *** Mach number to
the initial cruise altitude.   The temperature is ISA+10°C during climb.  
Maximum climb thrust is used during climb.

Cruise:

  The Aircraft cruises at *** Mach number.   The initial cruise altitude is ***
feet.   A step climb or multiple step climbs of *** feet altitude may be used
when beneficial to minimize fuel burn.   The temperature is ISA+10°C during
cruise.   The cruise thrust is not to exceed maximum cruise thrust except during
a step climb when maximum climb thrust may be used.

Descent:

  The Aircraft descends from the final cruise altitude at *** KCAS to an
altitude of *** feet above the destination airport altitude.   Throughout the
descent, the cabin pressure will be controlled to a maximum rate of descent
equivalent to *** feet per minute at sea level.   The temperature is ISA+10°C
during descent.

Approach and Landing Maneuver:

  The Aircraft decelerates to the final approach speed while extending landing
gear and flaps, then descends and lands.   The destination airport altitude is
*** feet.

Fixed Allowances:

  For the purpose of this guarantee and for the purpose of establishing
compliance with this guarantee, the following shall be used as fixed quantities
and allowances:  

Taxi-Out:

 

        Fuel            *** Pounds

 

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 10

 

  Takeoff and Climbout Maneuver:           Fuel            *** Pounds   Approach
and Landing Maneuver:           Fuel            *** Pounds   Taxi-In (shall be
consumed from the reserve fuel):           Fuel            *** Pounds   Usable
reserve fuel remaining upon completion of the approach and landing maneuver: ***
Pounds   For information purposes, the reserve fuel is based on a standard day
temperature and a contingency fuel allowance equivalent to *** minutes of
continued cruise starting at the end of the mission cruise and at *** Mach
number.

 

2.7.4 Mission Block Fuel

The block fuel for a stage length of *** nautical miles in still air with a ***
pound payload using the conditions and operating rules defined below, shall not
be more than the following guarantee value:

 

    NOMINAL:   *** Pounds     TOLERANCE:   *** Pounds     GUARANTEE:   ***
Pounds

 

Conditions and operating rules:

 

Stage Length:

  The stage length is defined as the sum of the distances for climb, cruise, and
descent.

Block Fuel:

  The block fuel is defined as the sum of the fuel used for taxi-out, takeoff
and climbout maneuver, climb, cruise, descent, approach and landing maneuver,
and taxi-in.

Takeoff:

  The airport altitude is ***   The takeoff gross weight is *** the airport
conditions.   Maximum takeoff thrust is used for the takeoff.   The takeoff
gross weight shall conform to FAA Regulations.

 

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 11

 

Climbout Maneuver:    Following the takeoff to *** feet, the Aircraft
accelerates to *** KCAS while climbing to *** feet above the departure airport
altitude and retracting flaps and landing gear. Climb:    The Aircraft climbs
from *** feet above the departure airport altitude to *** feet altitude at ***
KCAS.    The Aircraft then accelerates at a rate of climb of *** feet per minute
to the recommended climb speed for minimum block fuel.    The climb continues at
the recommended climb speed for minimum block fuel until *** Mach number is
reached.    The climb continues at *** Mach number to the initial cruise
altitude.    The temperature is standard day during climb.    Maximum climb
thrust is used during climb. Cruise:    The Aircraft cruises at *** Mach number.
   The initial cruise altitude is *** feet.    A step climb or multiple step
climbs of *** feet altitude may be used when beneficial to minimize fuel burn.
   The temperature is standard day during cruise.    The cruise thrust is not to
exceed maximum cruise thrust except during a step climb when maximum climb
thrust may be used. Descent:    The Aircraft descends from the final cruise
altitude at *** KCAS to an altitude of *** feet above the destination airport
altitude.    Throughout the descent, the cabin pressure is controlled to a
maximum rate of descent equivalent to *** feet per minute at sea level.    The
temperature is standard day during descent.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 12

 

Approach and

Landing Maneuver:

   The Aircraft decelerates to the final approach speed while extending landing
gear and flaps, then descends and lands.    The destination airport altitude is
a *** airport. Fixed Allowance:    For the purpose of this guarantee and for the
purpose of establishing compliance with this guarantee, the following shall be
used as fixed quantities and allowances:   

Taxi-Out:

 

Fuel        *** Pounds

 

Takeoff and Climbout Maneuver:

 

Fuel        *** Pounds

 

Approach and Landing Maneuver:

 

Fuel        *** Pounds

 

Taxi-In (shall be consumed from the reserve fuel):

 

Fuel        *** Pounds

   Usable reserve fuel remaining upon completion of the approach and landing
maneuver: *** Pounds    For information purposes, the reserve fuel is based on a
standard day temperature and a contingency fuel allowance equivalent to ***
minutes of continued cruise starting at the end of the mission cruise and at ***
Mach number.   

 

2.7.5 Mission Block Fuel

The block fuel for a stage length of *** nautical miles in still air with a ***
pound payload using the conditions and operating rules defined below, shall not
be more than the following guarantee value:

 

  NOMINAL:    *** Pounds      TOLERANCE:    *** Pounds      GUARANTEE:    ***
Pounds   

Conditions and operating rules:

 

Stage Length:    The stage length is defined as the sum of the distances for
climb, cruise, and descent.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 13

 

Block Fuel:    The block fuel is defined as the sum of the fuel used for
taxi-out, takeoff and climbout maneuver, climb, cruise, descent, approach and
landing maneuver, and taxi-in. Takeoff:    The airport altitude is sea level.   
The takeoff gross weight is *** by the airport conditions.    Maximum takeoff
thrust is used for the takeoff.    The takeoff gross weight shall conform to FAA
Regulations. Climbout Maneuver:    Following the takeoff to *** feet, the
Aircraft accelerates to *** KCAS while climbing to *** feet above the departure
airport altitude and retracting flaps and landing gear. Climb:    The Aircraft
climbs from *** feet above the departure airport altitude to *** feet altitude
at *** KCAS.    The Aircraft then accelerates at a rate of climb of *** feet per
minute to the recommended climb speed for minimum block fuel.    The climb
continues at the recommended climb speed for minimum block fuel until *** Mach
number is reached.    The climb continues at *** Mach number to the initial
cruise altitude.    The temperature is standard day during climb.    Maximum
climb thrust is used during climb. Cruise:    The Aircraft cruises at *** Mach
number.    The initial cruise altitude is *** feet.    A step climb or multiple
step climbs of *** feet altitude may be used when beneficial to minimize fuel
burn.    The temperature is standard day during cruise.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 14

 

   The cruise thrust is not to exceed maximum cruise thrust except during a step
climb when maximum climb thrust may be used. Descent:    The Aircraft descends
from the final cruise altitude at *** KCAS to an altitude of *** feet above the
destination airport altitude.    Throughout the descent, the cabin pressure is
controlled to a maximum rate of descent equivalent to *** feet per minute at sea
level.    The temperature is standard day during descent. Approach and
Landing Maneuver:    The Aircraft decelerates to the final approach speed while
extending landing gear and flaps, then descends and lands.    The destination
airport altitude is a sea level airport. Fixed Allowance:    For the purpose of
this guarantee and for the purpose of establishing compliance with this
guarantee, the following shall be used as fixed quantities and allowances:   

Taxi-Out:

 

Fuel        *** Pounds

 

Takeoff and Climbout Maneuver:

 

Fuel        *** Pounds

 

Approach and Landing Maneuver:

 

Fuel        *** Pounds

 

Taxi-In (shall be consumed from the reserve fuel):

 

Fuel        *** Pounds

   Usable reserve fuel remaining upon completion of the approach and landing
maneuver: *** Pounds    For information purposes, the reserve fuel is based on a
standard day temperature and a contingency fuel allowance equivalent to ***
minutes of continued cruise starting at the end of the mission cruise and at ***
Mach number

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 15

 

2.7.6 Mission Block Fuel

The block fuel for a stage length of *** nautical miles in still air (equivalent
to a distance of *** nautical miles with a *** knot headwind, representative of
a *** *** to *** route) with a *** pound payload using the conditions and
operating rules defined below, shall not be more than the following guarantee
value:

 

  NOMINAL:    *** Pounds      TOLERANCE:    *** Pounds      GUARANTEE:    ***
Pounds   

Conditions and operating rules:

Stage Length:    The stage length is defined as the sum of the distances for
climb, cruise, and descent. Block Fuel:    The block fuel is defined as the sum
of the fuel used for taxi-out, takeoff and climbout maneuver, climb, cruise,
descent, approach and landing maneuver, and taxi-in. Takeoff:    The airport
altitude is *** feet.    The takeoff gross weight is *** the airport conditions.
   Maximum takeoff thrust is used for the takeoff.    The takeoff gross weight
shall conform to FAA Regulations. Climbout Maneuver:    Following the takeoff to
*** feet, the Aircraft accelerates to *** KCAS while climbing to *** feet above
the departure airport altitude and retracting flaps and landing gear. Climb:   
The Aircraft climbs from *** feet above the departure airport altitude to ***
feet altitude at *** KCAS.    The Aircraft then accelerates at a rate of climb
of *** feet per minute to the recommended climb speed for minimum block fuel.   
The climb continues at the recommended climb speed for minimum block fuel until
*** Mach number is reached.    The climb continues at *** Mach number to the
initial cruise altitude.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 16

 

   The temperature is standard day during climb. Maximum climb thrust is used
during climb. Cruise:    The Aircraft cruises at *** Mach number.    The initial
cruise altitude is *** feet.    A step climb or multiple step climbs of *** feet
altitude may be used when beneficial to minimize fuel burn.    The temperature
is standard day during cruise.    The cruise thrust is not to exceed maximum
cruise thrust except during a step climb when maximum climb thrust may be used.
Descent:    The Aircraft descends from the final cruise altitude at *** KCAS to
an altitude of *** feet above the destination airport altitude.    Throughout
the descent, the cabin pressure is controlled to a maximum rate of descent
equivalent to *** feet per minute at sea level.    The temperature is standard
day during descent. Approach and
Landing Maneuver:    The Aircraft decelerates to the final approach speed while
extending landing gear and flaps, then descends and lands.    The destination
airport altitude is *** feet. Fixed Allowance:    For the purpose of this
guarantee and for the purpose of establishing compliance with this guarantee,
the following shall be used as fixed quantities and allowances:   

Taxi-Out:

 

Fuel        *** Pounds

 

Takeoff and Climbout Maneuver:

 

Fuel        *** Pounds

 

Approach and Landing Maneuver:

 

Fuel        *** Pounds

 

Taxi-In (shall be consumed from the reserve fuel):

 

Fuel        *** Pounds

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 17

 

   Usable reserve fuel remaining upon completion of the approach and landing
maneuver: *** Pounds    For information purposes, the reserve fuel is based on a
standard day temperature and a contingency fuel allowance equivalent to ***
minutes of continued cruise starting at the end of the mission cruise and at ***
Mach number

 

2.7.7 Operational Empty Weight Basis

The Operational Empty Weight (OEW) derived in Paragraph 2.7.8 is the basis for
the mission guarantees of Paragraphs 2.7.1, 2.7.2, 2.7.3, 2.7.4, 2.7.5, and
2.7.6.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 18

 

2.7.8 737-900ER Weight Summary—United Air Lines

 

     Pounds  

Standard Model Specification MEW

     * ** 

Configuration Specification D019A001, Rev. M, Dated January 30, 2009

  

*** Tourist Class Passengers

  

CFM56-7 Engines

  

*** lb (*** kg) Maximum Taxi Weight

  

*** U.S. Gallons (*** liters) Fuel Capacity

 

  

Changes for United Air Lines

  

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

United Air Lines Manufacturer’s Empty Weight (MEW)

     ***   

Standard and Operational Items Allowance (Paragraph 2.7.9)

     ***    United Air Lines Operational Empty Weight (OEW)      ***   

***

     ***   

United Air Lines Post-Delivery Operational Empty Weight (OEW)

     ***   

 

     Quantity      Pounds      Pounds  

* Seat Weight Included:

           ***   

***

     ***         ***      

***

     ***         ***      

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 19

 

***

   ***      * ** 

 

2.7.9 Standard and Operational Items Allowance

 

     ***      ***      ***      ***  

Standard Items Allowance

              ***   

Unusable Fuel

           ***      

Oil

           ***      

Oxygen Equipment

           ***      

Passenger Portable

     ***         ***         

Crew Masks

     ***         ***         

Miscellaneous Equipment

           ***      

Crash Axe

     ***         ***         

Megaphones

     ***         ***         

Flashlights

     ***         ***         

Smoke Hoods

     ***         ***         

Galley Structure & Fixed Inserts

           ***      

Operational Items Allowance

              ***   

Crew and Crew Baggage

           ***      

Flight Crew

     ***         ***         

Cabin Crew

     ***         ***         

Baggage

     ***         ***         

Catering Allowance & Removable Inserts

           ***      

First Class

     ***         ***         

Business Class

     ***         ***         

Economy Class

     ***         ***         

Passenger Service Equipment

     ***            ***      

Potable Water—60 USG

           ***      

Waste Tank Disinfectant

           ***      

Emergency Equipment

           ***      

Escape Slides—Forward

     ***         ***         

Escape Slides—Aft

     ***         ***         

Life Vests—Crew and Passengers

     ***         ***         

Life Rafts

     ***         ***         

Auto Radio Beacon (ELT)

     ***         ***         

Total Standard and Operational Items Allowance

              ***   

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 20

 

3 MANUFACTURER’S EMPTY WEIGHT

 

     The Manufacturer’s Empty Weight (MEW) is guaranteed not to exceed the value
in Section 03-60-00 of Detail Specification ***, Revision *** including assumed
changes to a new United Airlines configuration, plus one percent.

 

4 AIRCRAFT CONFIGURATION

 

4.1 The guarantees contained in this Attachment are based on the Aircraft
configuration as defined in Revision B of the Detail Specification ***
(hereinafter referred to as the Detail Specification) including assumed changes
to a new United Airlines configuration. Appropriate adjustment shall be made for
changes in such Detail Specification approved by the Customer and Boeing or
otherwise allowed by the Purchase Agreement which cause changes to the flight
performance and/or weight and balance of the Aircraft. Such adjustment shall be
accounted for by Boeing in its evidence of compliance with the guarantees.

 

4.2 The guarantee payloads of Paragraph 2.7.1, 2.7.2, and 2.7.3 and the
specified payloads of Paragraph 2.7.4, 2.7.5, and 2.7.6 block fuel guarantees
will be adjusted by Boeing for the effect of the following on OEW and the
Manufacturer’s Empty Weight guarantee of Section 3 will be adjusted by Boeing
for the following in its evidence of compliance with the guarantees:

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

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

 

5 GUARANTEE CONDITIONS

 

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

 

5.2 The Federal Aviation Administration (FAA) regulations referred to in this
Attachment are, unless otherwise specified, the 737-900ER Certification Basis
regulations specified in the Type Certificate Data Sheet A16WE, Revision 40,
dated April 27, 2007.

 

5.3

In the event a change is made to any law, governmental regulation or
requirement, or in the interpretation of any such law, governmental regulation
or requirement

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 21

 

that affects the certification basis for the Aircraft as described in Paragraph
5.2, and as a result thereof, a change is made to the configuration and/or the
performance of the Aircraft in order to obtain certification, the guarantees set
forth in this Attachment shall be appropriately modified to reflect any such
change.

 

5.4 The takeoff and landing guarantees, and the takeoff portion of the mission
guarantees are based on hard surface, level and dry runways with no wind or
obstacles, no clearway or stopway, *** mph tires, with Category P brakes and
anti-skid operative, and with the Aircraft center of gravity at the most forward
limit unless otherwise specified. The takeoff performance is based on no engine
bleed for air conditioning or thermal anti-icing and the ***. Unbalanced field
length calculations and the improved climb performance procedure will be used
for takeoff as required. The landing performance is based on the use of
automatic spoilers.

 

5.5 The enroute one-engine-inoperative altitude guarantee is based on engine
bleed for air conditioning with one pack operating. No engine bleed for thermal
anti-icing is provided unless otherwise specified. The APU is turned off unless
otherwise specified.

 

5.6 The speed, altitude capability, and cruise range guarantees, and the climb,
cruise and descent portions of the mission guarantees include allowances for
normal power extraction and engine bleed for normal operation of the air
conditioning system. Normal electrical power extraction shall be defined as not
less than a *** kilowatts total electrical load. Normal operation of the air
conditioning system shall be defined as pack switches in the “Auto” position,
the temperature control switches in the “Auto” position that results in a
nominal cabin temperature of ***°F, and all air conditioning systems operating
normally. This operation allows a maximum cabin pressure differential of ***
pounds per square inch at higher altitudes, with a nominal Aircraft cabin
ventilation rate of *** cubic feet per minute including passenger cabin
recirculation (nominal recirculation is *** percent). ***.

 

5.7 The speed, altitude capability, and cruise range guarantees, and the climb,
cruise and descent portions of the mission guarantees are based on an Aircraft
center of gravity location of *** percent of the mean aerodynamic chord.

 

5.8 Performance, where applicable, is based on a fuel Lower Heating Value
(LHV) of *** BTU per pound and a fuel density of *** pounds per U.S. gallon.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 22

 

6 GUARANTEE COMPLIANCE

 

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

 

6.2 Compliance with the takeoff, landing, and enroute one-engine- inoperative
altitude guarantees, the buffet onset portion of the altitude capability
guarantee, and the takeoff portion of the mission guarantee shall be based on
the FAA approved Airplane Flight Manual for the Model 737-900ER.

 

6.3 Compliance with the speed, altitude capability, and cruise range guarantees,
and the climb, cruise and descent portions of the mission guarantees shall be
established by calculations based on flight test data obtained from an aircraft
in a configuration similar to that defined by the Detail Specification.

 

6.4 The OEW used for compliance with the mission guarantees shall be the actual
MEW plus the Standard and Operational Items Allowance in Paragraph 03-60-00 of
the Detail Specification.

 

6.5 Compliance with the Manufacturer’s Empty Weight guarantee shall be based on
information in the “Weight and Balance Control and Loading Manual—Aircraft
Report.”

 

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

 

6.7 Compliance shall be based on the performance of the airframe and engines in
combination, and shall not be contingent on the engine meeting its
manufacturer’s performance specification.

 

7 EXCLUSIVE GUARANTEES

 

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

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 1

 

MODEL 737-900ER *** PERFORMANCE GUARANTEES

FOR CONTINENTAL AIRLINES, INC.

 

SECTION                       CONTENTS     

1

  AIRCRAFT MODEL APPLICABILITY   

2

  FLIGHT PERFORMANCE   

3

  MANUFACTURER’S EMPTY WEIGHT   

4

  AIRCRAFT CONFIGURATION   

5

  GUARANTEE CONDITIONS   

6

  GUARANTEE COMPLIANCE   

7

  EXCLUSIVE GUARANTEES   

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 2

 

1. AIRCRAFT MODEL APPLICABILITY

 

     The guarantees contained in this Attachment (the “Performance Guarantees”)
are applicable to the 737-900ER Aircraft with winglets and a maximum takeoff
weight of *** pounds, a maximum landing weight of *** pounds, and a maximum zero
fuel weight of *** pounds, and equipped with Boeing furnished CFM56- 7B27E/F
engines.

 

2. FLIGHT PERFORMANCE

 

2.1 Takeoff

 

2.1.1 The FAA approved takeoff field length at a gross weight at the start of
the ground roll of *** pounds, at a temperature of ***, at a *** altitude, with
an alternate forward center of gravity limit of *** percent of the mean
aerodynamic chord, and using maximum takeoff thrust, shall not be more than the
following guarantee value:

 

GUARANTEE:

  *** Feet

 

2.1.2 The FAA approved takeoff gross weight at the start of ground roll, at a
temperature of ***°F, at an altitude of *** feet, from a *** foot runway, with
an alternate forward center of gravity limit of *** percent of the mean
aerodynamic chord, and using maximum takeoff thrust, shall not be less than the
following guarantee value:

 

GUARANTEE:

  *** Pounds

 

2.2 Landing

 

2.2.1 The FAA approved landing field length at a gross weight of *** pounds and
at a *** altitude, shall not be more than the following guarantee value:

 

GUARANTEE:

  *** Feet

 

2.2.2 The FAA approved landing field length at a gross weight of *** pounds and
at an altitude of *** feet, shall not be more than the following guarantee
value:

 

GUARANTEE:

  *** Feet

 

2.3 Speed

 

     The level flight speed at a gross weight of *** pounds, on an ISA+10°C day,
at an altitude of *** feet and using not more than maximum cruise thrust, shall
not be less than the following guarantee value:

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 3

 

NOMINAL:

  *** KTAS

TOLERANCE:

  *** KTAS

GUARANTEE:

  *** KTAS

 

2.4 Altitude Capability—All Engines Operating

The altitude capability at a gross weight of *** pounds, on an ISA+10°C day, at
*** Mach number, and satisfying the conditions defined below, shall not be less
than the following guarantee value:

 

GUARANTEE:

  *** Feet

Conditions:

1) The Aircraft shall be capable of maintaining level cruising flight using not
more than maximum cruise thrust.

2) The Aircraft shall be capable of maintaining a rate of climb of *** feet per
minute using not more than maximum climb thrust.

3) The Aircraft shall be capable of at least a *** g maneuver load factor at
buffet onset.

 

2.5 Enroute One-Engine-Inoperative Altitude

The FAA approved enroute one-engine-inoperative altitude at which the available
gross climb gradient equals *** percent at a gross weight of *** pounds on an
ISA+10°C day using not more than maximum continuous thrust, shall not be less
than the following guarantee value:

 

GUARANTEE:

  *** Feet

 

2.6 Cruise Range

The still air range at an initial cruise altitude of *** feet on a standard day
at *** Mach number, starting at a gross weight of *** pounds and consuming ***
pounds of fuel, and using not more than maximum cruise thrust (except maximum
climb thrust may be used during a step climb) and using the conditions and
operating rules defined below, shall not be less than the following guarantee
value:

 

NOMINAL:

  *** Nautical Miles

TOLERANCE:

  *** Nautical Miles

GUARANTEE:

  *** Nautical Miles

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 4

 

Conditions and operating rules:

A step climb or multiple step climbs of *** feet altitude may be used when
beneficial to minimize fuel burn.

 

2.7 Mission

 

2.7.1 Mission Payload

The payload for a stage length of *** nautical miles in still air (equivalent to
a distance of *** nautical miles with a *** knot headwind, representative of a
*** *** to *** route) using the conditions and operating rules defined below,
shall not be less than the following guarantee value:

 

   NOMINAL:    *** Pounds       TOLERANCE:    *** Pounds       GUARANTEE:    ***
Pounds   

Conditions and operating rules:

Stage Length:    The stage length is defined as the sum of the distances for
climb, cruise, and descent. Takeoff:    The airport altitude is *** feet.    The
airport temperature is ***°F.    The runway length is *** feet.    The following
obstacle definition is based on a straight out departure where obstacle height
and distance are specified with reference to the liftoff end of the runway:     
     Distance    Height   

1.

   ***    *** feet   

2.

   ***    *** feet   

3.

   ***    *** feet   

4.

   ***    *** feet   

5.

   ***    *** feet   

6.

   ***    *** feet    Takeoff performance is based on an alternate forward
center of gravity limit of *** percent of the mean aerodynamic chord.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 5

 

   Maximum takeoff thrust is used for the takeoff.    The takeoff gross weight
shall conform to FAA Regulations. Climbout Maneuver:    Following the takeoff to
*** feet, the Aircraft accelerates to *** KCAS while climbing to *** feet above
the departure airport altitude and retracting flaps and landing gear. Climb   
The Aircraft climbs from *** feet above the departure airport altitude to ***
feet altitude at *** KCAS.    The Aircraft then accelerates at a rate of climb
of *** feet per minute to the recommended climb speed for minimum block fuel.   
The climb continues at the recommended climb speed for minimum block fuel until
*** Mach number is reached.    The climb continues at *** Mach number to the
initial cruise altitude.    The temperature is standard day during climb.   
Maximum climb thrust is used during climb. Cruise:    The Aircraft cruises at
*** Mach number.    The initial cruise altitude is *** feet.    A step climb or
multiple step climbs of *** feet altitude may be used when beneficial to
minimize fuel burn.    The temperature is standard day during cruise.    The
cruise thrust is not to exceed maximum cruise thrust except during a step climb
when maximum climb thrust may be used. Descent:    The Aircraft descends from
the final cruise altitude at *** KCAS to an altitude of *** feet above the
destination airport altitude.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 6

 

   Throughout the descent, the cabin pressure will be controlled to a maximum
rate of descent equivalent to *** feet per minute at sea level.    The
temperature is standard day during descent. Approach and
Landing Maneuver:    The Aircraft decelerates to the final approach speed while
extending landing gear and flaps, then descends and lands.    The destination
airport altitude is *** feet. Fixed Allowances:    For the purpose of this
guarantee and for the purpose of establishing compliance with this guarantee,
the following shall be used as fixed quantities and allowances:   

Taxi-Out:

 

Fuel        *** Pounds

 

Takeoff and Climbout Maneuver:

 

Fuel        *** Pounds

 

Approach and Landing Maneuver:

 

Fuel        *** Pounds

 

Taxi-In (shall be consumed from the reserve fuel):

 

Fuel        *** Pounds

   Usable reserve fuel remaining upon completion of the approach and landing
maneuver: *** Pounds    For information purposes, the reserve fuel is based on a
standard day temperature and a contingency fuel allowance equivalent to ***
minutes of continued cruise starting at the end of the mission cruise and at ***
Mach number.

 

2.7.2 Mission Payload

The payload for a stage length of *** nautical miles in still air (equivalent to
a distance of *** nautical miles with a *** knot headwind, representative of a
*** to *** route) using the conditions and operating rules defined below, shall
not be less than the following guarantee value:

 

   NOMINAL:    *** Pounds       TOLERANCE:    *** Pounds       GUARANTEE:    ***
Pounds   

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 7

 

Conditions and operating rules:

Stage Length:    The stage length is defined as the sum of the distances for
climb, cruise, and descent. Takeoff:    The airport altitude is *** feet.    The
takeoff gross weight is *** the airport conditions.    Maximum takeoff thrust is
used for the takeoff.    The takeoff gross weight shall conform to FAA
Regulations. Climbout Maneuver:    Following the takeoff to *** feet, the
Aircraft accelerates to *** KCAS while climbing to *** feet above the departure
airport altitude and retracting flaps and landing gear. Climb:    The Aircraft
climbs from *** feet above the departure airport altitude to *** feet altitude
at *** KCAS.    The Aircraft then accelerates at a rate of climb of *** feet per
minute to the recommended climb speed for minimum block fuel.    The climb
continues at the recommended climb speed for minimum block fuel until *** Mach
number is reached.    The climb continues at the recommended climb speed for
minimum block fuel until the initial cruise altitude is reached.    The
temperature is ISA+5°C during climb.    Maximum climb thrust is used during
climb. Cruise:    The Aircraft cruises at *** Mach number.    The initial cruise
altitude is *** feet.    A step climb or multiple step climbs of *** feet
altitude may be used when beneficial to minimize fuel burn.    The temperature
is ISA+5°C during cruise.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 8

 

   The cruise thrust is not to exceed maximum cruise thrust except during a step
climb when maximum climb thrust may be used. Descent:    The Aircraft descends
from the final cruise altitude at *** KCAS to an altitude of *** feet above the
destination airport altitude.    Throughout the descent, the cabin pressure will
be controlled to a maximum rate of descent equivalent to *** feet per minute at
sea level.    The temperature is ISA+5°C during descent. Approach and
Landing Maneuver:    The Aircraft decelerates to the final approach speed while
extending landing gear and flaps, then descends and lands.    The destination
airport altitude is *** feet. Fixed Allowance:    For the purpose of this
guarantee and for the purpose of establishing compliance with this guarantee,
the following shall be used as fixed quantities and allowances:   

Taxi-Out:

 

Fuel        *** Pounds

 

Takeoff and Climbout Maneuver:

 

Fuel        *** Pounds

 

Approach and Landing Maneuver:

 

Fuel        *** Pounds

 

Taxi-In (shall be consumed from the reserve fuel):

 

Fuel        *** Pounds

   Usable reserve fuel remaining upon completion of the approach and landing
maneuver: *** Pounds    For information purposes, the reserve fuel is based on a
standard day temperature and a contingency fuel allowance equivalent to ***
minutes of continued cruise starting at the end of the mission and at a *** Mach
number.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 9

 

2.7.3 Mission Payload

The payload for a stage length of *** nautical miles in still air (equivalent to
a distance of *** nautical miles with a *** knot tailwind, representative of a
*** to *** route) using the conditions and operating rules defined below, shall
not be less than the following guarantee value:

 

   NOMINAL:    *** Pounds       TOLERANCE:    *** Pounds       GUARANTEE:    ***
Pounds   

Conditions and operating rules:

Stage Length:    The stage length is defined as the sum of the distances for
climb, cruise, and descent. Takeoff:    The airport altitude is *** feet.   

The airport temperature is ***°F.

 

The runway length is *** feet.

   The runway slope is *** percent downhill.    Takeoff performance is based on
an alternate forward center of gravity limit of *** percent of the mean
aerodynamic chord.    Maximum takeoff thrust is used for the takeoff.    The
takeoff gross weight shall conform to FAA Regulations. Climbout Maneuver:   
Following the takeoff to *** feet, the Aircraft accelerates to *** KCAS while
climbing to *** feet above the departure airport altitude and retracting flaps
and landing gear. Climb:    The Aircraft climbs from *** feet above the
departure airport altitude to *** feet altitude at *** KCAS.    The Aircraft
then accelerates at a rate of climb of *** feet per minute to the recommended
climb speed for minimum block fuel.    The climb continues at the recommended
climb speed for minimum block fuel until *** Mach number is reached.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 10

 

   The climb continues at *** Mach number to the initial cruise altitude.    The
temperature is ISA+10°C during climb.    Maximum climb thrust is used during
climb. Cruise:    The Aircraft cruises at *** Mach number.    The initial cruise
altitude is *** feet.    A step climb or multiple step climbs of *** feet
altitude may be used when beneficial to minimize fuel burn.    The temperature
is ISA+10°C during cruise.    The cruise thrust is not to exceed maximum cruise
thrust except during a step climb when maximum climb thrust may be used.
Descent:    The Aircraft descends from the final cruise altitude at *** KCAS to
an altitude of *** feet above the destination airport altitude.    Throughout
the descent, the cabin pressure will be controlled to a maximum rate of descent
equivalent to *** feet per minute at sea level.    The temperature is ISA+10°C
during descent. Approach and
Landing Maneuver:    The Aircraft decelerates to the final approach speed while
extending landing gear and flaps, then descends and lands.    The destination
airport altitude is *** feet. Fixed Allowances:    For the purpose of this
guarantee and for the purpose of establishing compliance with this guarantee,
the following shall be used as fixed quantities and allowances:   

Taxi-Out:

 

Fuel        *** Pounds

 

Takeoff and Climbout Maneuver:

 

Fuel        *** Pounds

 

Approach and Landing Maneuver:

 

Fuel        *** Pounds

 

Taxi-In (shall be consumed from the reserve fuel):

 

Fuel        *** Pounds

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 11

 

   Usable reserve fuel remaining upon completion of the approach and landing
maneuver: *** Pounds    For information purposes, the reserve fuel is based on a
standard day temperature and a contingency fuel allowance equivalent to ***
minutes of continued cruise starting at the end of the mission cruise and at ***
Mach number.

 

2.7.4 Mission Block Fuel

The block fuel for a stage length of *** nautical miles in still air with a ***
pound payload using the conditions and operating rules defined below, shall not
be more than the following guarantee value:

 

  NOMINAL:    *** Pounds   TOLERANCE:    *** Pounds   GUARANTEE:    *** Pounds

Conditions and operating rules:

 

Stage Length:    The stage length is defined as the sum of the distances for
climb, cruise, and descent. Block Fuel:    The block fuel is defined as the sum
of the fuel used for taxi-out, takeoff and climbout maneuver, climb, cruise,
descent, approach and landing maneuver, and taxi-in. Takeoff:    The airport
altitude is ***.    The takeoff gross weight is *** the airport conditions.   
Maximum takeoff thrust is used for the takeoff.    The takeoff gross weight
shall conform to FAA Regulations. Climbout
Maneuver:    Following the takeoff to *** feet, the Aircraft accelerates to ***
KCAS while climbing to *** feet above the departure airport altitude and
retracting flaps and landing gear.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 12

 

Climb:    The Aircraft climbs from *** feet above the departure airport altitude
to *** feet altitude at *** KCAS.    The Aircraft then accelerates at a rate of
climb of *** feet per minute to the recommended climb speed for minimum block
fuel.    The climb continues at the recommended climb speed for minimum block
fuel until *** Mach number is reached.    The climb continues at *** Mach number
to the initial cruise altitude.    The temperature is standard day during climb.
   Maximum climb thrust is used during climb. Cruise:    The Aircraft cruises at
*** Mach number.    The initial cruise altitude is *** feet.    A step climb or
multiple step climbs of *** feet altitude may be used when beneficial to
minimize fuel burn.    The temperature is standard day during cruise.    The
cruise thrust is not to exceed maximum cruise thrust except during a step climb
when maximum climb thrust may be used. Descent:    The Aircraft descends from
the final cruise altitude at *** KCAS to an altitude of *** feet above the
destination airport altitude.    Throughout the descent, the cabin pressure is
controlled to a maximum rate of descent equivalent to *** feet per minute at sea
level.    The temperature is standard day during descent. Approach and
Landing Maneuver:    The Aircraft decelerates to the final approach speed while
extending landing gear and flaps, then descends and lands.    The destination
airport altitude is a *** airport. Fixed Allowances:    For the purpose of this
guarantee and for the purpose of establishing compliance with this guarantee,
the following shall be used as fixed quantities and allowances:

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 13

 

  Taxi-Out:              Fuel    *** Pounds   Takeoff and Climbout Maneuver:  
        Fuel    *** Pounds   Approach and Landing Maneuver:           Fuel   
*** Pounds   Taxi-In (shall be consumed from the reserve fuel):           Fuel
   *** Pounds

 

  Usable reserve fuel remaining upon completion of the approach and landing
maneuver: *** Pounds   For information purposes, the reserve fuel is based on a
standard day temperature and a contingency fuel allowance equivalent to ***
minutes of continued cruise starting at the end of the mission cruise and at ***
Mach number

 

2.7.5 Mission Block Fuel

The block fuel for a stage length of *** nautical miles in still air with a ***
pound payload using the conditions and operating rules defined below, shall not
be more than the following guarantee value:

 

  NOMINAL:    *** Pounds  

TOLERANCE:

   *** Pounds  

GUARANTEE:

   *** Pounds

Conditions and operating rules:

Stage Length:    The stage length is defined as the sum of the distances for
climb, cruise, and descent. Block Fuel:    The block fuel is defined as the sum
of the fuel used for taxi-out, takeoff and climbout maneuver, climb, cruise,
descent, approach and landing maneuver, and taxi-in.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 14

 

Takeoff:    The airport altitude is ***.    The takeoff gross weight is *** the
airport conditions.    Maximum takeoff thrust is used for the takeoff.    The
takeoff gross weight shall conform to FAA Regulations. Climbout
Maneuver:    Following the takeoff to *** feet, the Aircraft accelerates to ***
KCAS while climbing to *** feet above the departure airport altitude and
retracting flaps and landing gear. Climb:    The Aircraft climbs from *** feet
above the departure airport altitude to *** feet altitude at *** KCAS.    The
Aircraft then accelerates at a rate of climb of *** feet per minute to the
recommended climb speed for minimum block fuel.    The climb continues at the
recommended climb speed for minimum block fuel until *** Mach number is reached.
   The climb continues at *** Mach number to the initial cruise altitude.    The
temperature is standard day during climb.    Maximum climb thrust is used during
climb. Cruise:    The Aircraft cruises at *** Mach number.    The initial cruise
altitude is *** feet.    A step climb or multiple step climbs of *** feet
altitude may be used when beneficial to minimize fuel burn.    The temperature
is standard day during cruise.    The cruise thrust is not to exceed maximum
cruise thrust except during a step climb when maximum climb thrust may be used.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 15

 

Descent:    The Aircraft descends from the final cruise altitude at *** KCAS to
an altitude of *** feet above the destination airport altitude.    Throughout
the descent, the cabin pressure is controlled to a maximum rate of descent
equivalent to *** feet per minute at sea level.    The temperature is standard
day during descent. Approach and
Landing Maneuver:    The Aircraft decelerates to the final approach speed while
extending landing gear and flaps, then descends and lands.    The destination
airport altitude is a *** airport. Fixed Allowances:    For the purpose of this
guarantee and for the purpose of establishing compliance with this guarantee,
the following shall be used as fixed quantities and allowances:   

Taxi-Out:

 

Fuel        *** Pounds

 

Takeoff and Climbout Maneuver:

 

Fuel        *** Pounds

 

Approach and Landing Maneuver:

 

Fuel        *** Pounds

 

Taxi-In (shall be consumed from the reserve fuel):

 

Fuel        *** Pounds

   Usable reserve fuel remaining upon completion of the approach and landing
maneuver: *** Pounds    For information purposes, the reserve fuel is based on a
standard day temperature and a contingency fuel allowance equivalent to ***
minutes of continued cruise starting at the end of the mission cruise and at ***
Mach number

 

2.7.6 Mission Block Fuel

The block fuel for a stage length of *** nautical miles in still air (equivalent
to a distance of *** nautical miles with a *** knot headwind, representative of
a *** to *** route) with a *** pound payload using the conditions and operating
rules defined below, shall not be more than the following guarantee value:

 

   NOMINAL:    *** Pounds       TOLERANCE:    *** Pounds       GUARANTEE:    ***
Pounds   

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 16

 

Conditions and operating rules:

Stage Length:    The stage length is defined as the sum of the distances for
climb, cruise, and descent. Block Fuel:    The block fuel is defined as the sum
of the fuel used for taxi-out, takeoff and climbout maneuver, climb, cruise,
descent, approach and landing maneuver, and taxi-in. Takeoff:    The airport
altitude is *** feet.    The takeoff gross weight is *** the airport conditions.
   Maximum takeoff thrust is used for the takeoff.    The takeoff gross weight
shall conform to FAA Regulations. Climbout Maneuver:    Following the takeoff to
*** feet, the Aircraft accelerates to *** KCAS while climbing to *** feet above
the departure airport altitude and retracting flaps and landing gear. Climb:   
The Aircraft climbs from *** feet above the departure airport altitude to ***
feet altitude at *** KCAS.    The Aircraft then accelerates at a rate of climb
of *** feet per minute to the recommended climb speed for minimum block fuel.   
The climb continues at the recommended climb speed for minimum block fuel until
*** Mach number is reached.    The climb continues at *** Mach number to the
initial cruise altitude.    The temperature is standard day during climb.
Maximum climb thrust is used during climb. Cruise:    The Aircraft cruises at
*** Mach number.    The initial cruise altitude is *** feet.    A step climb or
multiple step climbs of *** feet altitude may be used when beneficial to
minimize fuel burn.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 17

 

   The temperature is standard day during cruise.    The cruise thrust is not to
exceed maximum cruise thrust except during a step climb when maximum climb
thrust may be used. Descent:    The Aircraft descends from the final cruise
altitude at *** KCAS to an altitude of *** feet above the destination airport
altitude.    Throughout the descent, the cabin pressure is controlled to a
maximum rate of descent equivalent to *** feet per minute at sea level.    The
temperature is standard day during descent. Approach and
Landing Maneuver:    The Aircraft decelerates to the final approach speed while
extending landing gear and flaps, then descends and lands.    The destination
airport altitude is a *** airport. Fixed Allowances:    For the purpose of this
guarantee and for the purpose of establishing compliance with this guarantee,
the following shall be used as fixed quantities and allowances:   

Taxi-Out:

 

Fuel        *** Pounds

 

Takeoff and Climbout Maneuver:

 

Fuel        *** Pounds

 

Approach and Landing Maneuver:

 

Fuel        *** Pounds

 

Taxi-In (shall be consumed from the reserve fuel):

 

Fuel        *** Pounds

   Usable reserve fuel remaining upon completion of the approach and landing
maneuver: *** Pounds    For information purposes, the reserve fuel is based on a
standard day temperature and a contingency fuel allowance equivalent to ***
minutes of continued cruise starting at the end of the mission cruise and at ***
Mach number

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 18

 

2.7.7 Operational Empty Weight Basis

The Operational Empty Weight (OEW) derived in Paragraph 2.7.8 is the basis for
the mission guarantees of Paragraphs 2.7.1, 2.7.2, 2.7.3, 2.7.4, 2.7.5, and
2.7.6.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 19

 

2.7.8 737-900ER Weight Summary—United Air Lines

 

     Pounds  

Standard Model Specification MEW

     ***   

Configuration Specification D019A001, Rev. M, Dated January 30, 2009

  

*** Tourist Class Passengers

  

CFM56-7 Engines

  

*** lb (*** kg) Maximum Taxi Weight

  

*** U.S. Gallons (*** liters) Fuel Capacity

 

  

Changes for United Air Lines

  

***

     ***   

***

  

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

***

     ***   

United Air Lines Manufacturer’s Empty Weight (MEW)

     ***   

Standard and Operational Items Allowance (Paragraph 2.7.9)

     ***   

United Air Lines Operational Empty Weight (OEW)

     ***   

***

     ***   

United Air Lines Post-Delivery Operational Empty Weight (OEW)

     ***   

 

     Quantity      Pounds      Pounds  

* Seat Weight Included:

           ***   

First Class Doubles

     ***         ***      

Premium Economy Class Triples

     ***         ***      

Economy Class Triples

     ***         ***      

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 20

 

2.7.9 Standard and Operational Items Allowance

 

     ***      ***      ***      ***  

Standard Items Allowance

              ***   

Unusable Fuel

           ***      

Oil

           ***      

Oxygen Equipment

           ***      

Passenger Portable

     ***         ***         

Crew Masks

     ***         ***         

Miscellaneous Equipment

           ***      

Crash Axe

     ***         ***         

Megaphones

     ***         ***         

Flashlights

     ***         ***         

Smoke Hoods

     ***         ***         

Galley Structure & Fixed Inserts

           ***      

Operational Items Allowance

              ***   

Crew and Crew Baggage

           ***      

Flight Crew

     ***         ***         

Cabin Crew

     ***         ***         

Baggage

     ***         ***         

Catering Allowance & Removable Inserts

           ***      

First Class

     ***         ***         

Business Class

     ***         ***         

Economy Class

     ***         ***         

Passenger Service Equipment

     ***            ***      

Potable Water—60 USG

           ***      

Waste Tank Disinfectant

           ***      

Emergency Equipment

           ***      

Escape Slides—Forward

     ***         ***         

Escape Slides—Aft

     ***         ***         

Life Vests—Crew and Passengers

     ***         ***         

Life Rafts

     ***         ***         

Auto Radio Beacon (ELT)

     ***         ***         

Total Standard and Operational Items Allowance

              ***   

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 21

 

3. MANUFACTURER’S EMPTY WEIGHT

The Manufacturer’s Empty Weight (MEW) is guaranteed not to exceed the value in
Section 03-60-00 of Detail Specification ***, Revision *** including assumed
changes to a new United Airlines configuration, plus one percent.

 

4. AIRCRAFT CONFIGURATION

 

4.1 The guarantees contained in this Attachment are based on the Aircraft
configuration as defined in Revision B of the Detail Specification ***
(hereinafter referred to as the Detail Specification) including assumed changes
to a new United Airlines configuration. Appropriate adjustment shall be made for
changes in such Detail Specification approved by the Customer and Boeing or
otherwise allowed by the Purchase Agreement which cause changes to the flight
performance and/or weight and balance of the Aircraft. Such adjustment shall be
accounted for by Boeing in its evidence of compliance with the guarantees.

 

4.2 The guarantee payloads of Paragraph 2.7.1, 2.7.2, and 2.7.3 and the
specified payloads of Paragraph 2.7.4, 2.7.5, and 2.7.6 block fuel guarantees
will be adjusted by Boeing for the effect of the following on OEW and the
Manufacturer’s Empty Weight guarantee of Section 3 will be adjusted by Boeing
for the following in its evidence of compliance with the guarantees:

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

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

 

5. GUARANTEE CONDITIONS

 

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

 

5.2 The Federal Aviation Administration (FAA) regulations referred to in this
Attachment are, unless otherwise specified, the 737-900ER Certification Basis
regulations specified in the Type Certificate Data Sheet A16WE, Revision 41,
dated July 31, 2007.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 22

 

5.3 In the event a change is made to any law, governmental regulation or
requirement, or in the interpretation of any such law, governmental regulation
or requirement that affects the certification basis for the Aircraft as
described in Paragraph 5.2, and as a result thereof, a change is made to the
configuration and/or the performance of the Aircraft in order to obtain
certification, the guarantees set forth in this Attachment shall be
appropriately modified to reflect any such change.

 

5.4 The takeoff and landing guarantees, and the takeoff portion of the mission
guarantees are based on hard surface, level and dry runways with no wind or
obstacles, no clearway or stopway, *** mph tires, with Category P brakes and
anti-skid operative, and with the Aircraft center of gravity at the most forward
limit unless otherwise specified. The takeoff performance is based on no engine
bleed for air conditioning or thermal anti-icing and the ***. Unbalanced field
length calculations and the improved climb performance procedure will be used
for takeoff as required. The landing performance is based on the use of
automatic spoilers.

 

5.5 The enroute one-engine-inoperative altitude guarantee is based on engine
bleed for air conditioning with one pack operating. No engine bleed for thermal
anti-icing is provided unless otherwise specified. The APU is turned off unless
otherwise specified.

 

5.6 The speed, altitude capability, and cruise range guarantees, and the climb,
cruise and descent portions of the mission guarantees include allowances for
normal power extraction and engine bleed for normal operation of the air
conditioning system. Normal electrical power extraction shall be defined as not
less than a *** kilowatts total electrical load. Normal operation of the air
conditioning system shall be defined as pack switches in the “Auto” position,
the temperature control switches in the “Auto” position that results in a
nominal cabin temperature of ***°F, and all air conditioning systems operating
normally. This operation allows a maximum cabin pressure differential of ***
pounds per square inch at higher altitudes, with a nominal Aircraft cabin
ventilation rate of *** cubic feet per minute including passenger cabin
recirculation (nominal recirculation is *** percent). ***.

 

5.7 The speed, altitude capability, and cruise range guarantees, and the climb,
cruise and descent portions of the mission guarantees are based on an Aircraft
center of gravity location of *** percent of the mean aerodynamic chord.

 

5.8 Performance, where applicable, is based on a fuel Lower Heating Value
(LHV) of *** BTU per pound and a fuel density of *** pounds per U.S. gallon.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

Attachment to Letter Agreement

No. CAL-PA-1951-LA-1208066

***

Page 23

 

6. GUARANTEE COMPLIANCE

 

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

 

6.2 Compliance with the takeoff, landing, and enroute one-engine- inoperative
altitude guarantees, the buffet onset portion of the altitude capability
guarantee, and the takeoff portion of the mission guarantee shall be based on
the FAA approved Airplane Flight Manual for the Model 737-900ER.

 

6.3 Compliance with the speed, altitude capability, and cruise range guarantees,
and the climb, cruise and descent portions of the mission guarantees shall be
established by calculations based on flight test data obtained from an aircraft
in a configuration similar to that defined by the Detail Specification.

 

6.4 The OEW used for compliance with the mission guarantees shall be the actual
MEW plus the Standard and Operational Items Allowance in Paragraph 03-60-00 of
the Detail Specification.

 

6.5 Compliance with the Manufacturer’s Empty Weight guarantee shall be based on
information in the “Weight and Balance Control and Loading Manual—Aircraft
Report.”

 

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

 

6.7 Compliance shall be based on the performance of the airframe and engines in
combination, and shall not be contingent on the engine meeting its
manufacturer’s performance specification.

 

7. EXCLUSIVE GUARANTEES

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

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

P.A. No. PA-1951

AERO-B-BBA4-M12-0362C

  SS12-0153

--------------------------------------------------------------------------------

LOGO [g408868g13d55.jpg]

 

CAL-PA-1951-LA-1209037

Continental Airlines, Inc.

1600 Smith Street

Houston, Texas 77002

Subject:    ***

 

Reference: Purchase Agreement No. PA-1951 (Purchase Agreement) between The
Boeing Company (Boeing) and Continental Airlines, Inc. (Customer) relating to
Model 737-924ER aircraft (Aircraft)

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

 

1. Definitions.

*** Notice means the written communication provided by Boeing to Customer in
accordance with the requirements of Article 4.1, below.

***

Program Aircraft means each Aircraft specified in Table 1 of the Purchase
Agreement with scheduled deliveries in July 2013 and after as of the date of
this Letter Agreement ***

 

2. Applicability.

Notwithstanding any other provision of the Purchase Agreement to the contrary,
the parties agree that the *** for the Airframe Price and Optional Features
Prices for each Program Aircraft shall be determined in accordance with this
Letter Agreement.

 

3. *** Forecast.

Boeing will release an *** forecast in *** of each year based on Boeing’s then
current standard ***. Only one *** forecast shall be used to conduct the ***
analysis performed in accordance with Article 4.1, below, for a given Program
Aircraft. The *** forecast applicable to a given Program Aircraft is set forth
in Attachment A.

 

4. ***.

 

  4.1 ***

 

  4.1.1 ***

 

  4.1.2 ***

 

  4.1.3 ***

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

CAL-PA-1951-LA-1209037

***

  Page 1

--------------------------------------------------------------------------------

LOGO [g408868g13d55.jpg]

 

  4.1.4 ***

 

  4.2 ***

 

  4.2.1 ***

 

  4.2.2 ***

 

  4.3 ***

 

5. ***

 

  5.1 ***

 

  5.2 ***

 

6. ***

 

     ***

 

  6.1 ***

 

  6.2 ***

 

7. ***

 

     ***

 

8. Assignment.

*** this Letter Agreement is provided as an accommodation to Customer in
consideration of Customer becoming the operator of the Aircraft and cannot be
assigned in whole or in part.

 

9. Confidential Treatment.

Customer and Boeing understand that certain commercial and financial information
contained in this Letter Agreement are considered by Boeing and Customer as
confidential and are subject to the terms and conditions set forth in Letter
Agreement No. CAL-PA-1951-LA-1209110.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

CAL-PA-1951-LA-1209037

***

  Page 2

--------------------------------------------------------------------------------

LOGO [g408868g13d55.jpg]

 

THE BOEING COMPANY By   /s/ *** Its   Attorney-in-Fact ACCEPTED AND AGREED TO
this Date:   July 12, 2012 Continental Airlines, Inc. By   /s/ Gerald Laderman
Its   Senior Vice President – Finance and Treasurer

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

CAL-PA-1951-LA-1209037

***

  Page 3

--------------------------------------------------------------------------------

LOGO [g408868g13d55.jpg]

 

ATTACHMENT A

*** Forecast & *** Notice Date

 

***

Forecast

  

Applicable to Program Aircraft

Delivering in Time Period

       

***

Notice
Date

***           

***

     

***

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

CAL-PA-1951-LA-1209037

***

  Page 4

--------------------------------------------------------------------------------

LOGO [g408868g13d55.jpg]

 

ATTACHMENT B

*** Factors—July 2005 Base Year

 

***

  

***

   ***    ***

***

   ***    ***    ***

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

CAL-PA-1951-LA-1209037

***

  Page 5

--------------------------------------------------------------------------------

LOGO [g408868g13d55.jpg]     

The Boeing Company

P.O. Box 3707

Seattle, WA 98124-2207

 

CAL-PA-1951-LA-1209110

Continental Airlines, Inc.

1600 Smith Street

Houston, Texas 77002

 

Subject: Privileged and Confidential Matters

 

Reference: Purchase Agreement No. PA-1951 (Purchase Agreement) between The
Boeing Company (Boeing) and Continental Airlines, Inc. (Customer) relating to
Model 737-924ER aircraft (Aircraft)

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

Boeing and Customer agree that certain commercial and financial information
contained in or transmitted pursuant to the Purchase Agreement and the Aircraft
General Terms Agreement (AGTA) (together the “Purchase Agreement”) between
Boeing and Customer and all letter agreements made a part of the Purchase
Agreement, including exhibits or attachments thereto are considered by Boeing
and Customer as privileged and confidential and the parties agree that the
information contained therein or transmitted pursuant to (Information)
represents confidential business information. Except as specified below, each of
Boeing and Customer is prohibited from disclosing the Information to any person,
entity, or government agency. Each party shall protect the confidentiality of
such Information in the manner similar to how a party protects its own
Information of a similar nature, but with no less than a reasonable standard of
care. This provision shall not restrict a party from taking any steps necessary
to protect and safeguard its interests relating to the Information, including
obtaining a protective order or other injunctive relief, where appropriate.

 

  (a) Employees. A party may disclose the Information to its own employees (as
well as the employees of United Continental Holdings, Inc. and United Air Lines,
Inc.) who (i) have a need to know the Information for purposes of assisting said
party in the evaluation or administration of the Purchase Agreement or such
party’s business operations and (ii) have been instructed to not disclose the
Information except as provided by this Letter Agreement.

 

  (b) Professional Advisors. A party may disclose the Information to its
auditors, insurers, financial advisors, *** and attorneys (“Professional
Advisors”) who have a need to know the Information in connection with providing
services to said party only when said party has first obtained from the
Professional Advisor a written obligation of confidentiality and restricted use
that is no less restrictive than the terms of this Letter Agreement. Each party
shall be fully responsible to the other party for the Professional Advisors’
compliance with such obligations.

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

CAL-PA-1951-LA-1209110

Privileged and Confidential Matters

  Page 1

--------------------------------------------------------------------------------

LOGO [g408868g13d55.jpg]

 

  (c) Regulatory Requirements. A party may disclose in a regulatory or other
government filing that part of the Information which is required by applicable
law or regulation to be disclosed in such regulatory or other governmental
filings, including filings with the Securities and Exchange Commission (“SEC”),
but only in accordance with the following requirements:

 

  (i) The disclosing party shall advise the other party in writing of such
disclosure requirement prior to making such disclosure to enable the other party
to take those steps it deems necessary to protect the Information; and

 

  (ii) The disclosing party shall, as requested by the other party, seek
redaction and/or confidential treatment for the Information or parts thereof
from the SEC or other applicable regulators.

Very truly yours,

 

THE BOEING COMPANY By   /s/ *** Its   Attorney-In-Fact ACCEPTED AND AGREED TO
this Date:   July 12, 2012 Continental Airlines, Inc. By   /s/ Gerald Laderman
Its   Senior Vice President – Finance and Treasurer

 

BOEING / CONTINENTAL AIRLINES, INC. PROPRIETARY

CAL-PA-1951-LA-1209110

Privileged and Confidential Matters

  Page 2