SupplementalAgreement No.61 to PurchaseAgreement No.1810 between THEBOEING COMPANY and SOUTHWESTAIRLINES CO. Relatingto Boeing Model 737-7H4 Aircraft (the Aircraft)
EX-10.1 2 ex10_1.htm EXHBIT 10.1 SUPPLEMENTAL AGREEMENT NO. 61 ex10_1.htm
Exhibit 10.1
CONFIDENTIAL TREATMENT
Supplemental Agreement No. 61
to
Purchase Agreement No. 1810
between
THE BOEING COMPANY
and
SOUTHWEST AIRLINES CO.
Relating to Boeing Model 737-7H4 Aircraft (the Aircraft)
THIS SUPPLEMENTAL AGREEMENT, entered into as of September 30, 2008, by and between THE BOEING COMPANY, a Delaware corporation with principal offices in Seattle, Washington, (Boeing) and SOUTHWEST AIRLINES CO., a Texas corporation with principal offices in Dallas, Texas (Buyer);
WHEREAS, the parties hereto entered into Purchase Agreement No. 1810 dated January 19, 1994, relating to Boeing Model 737-7H4 aircraft (the Agreement) and;
WHEREAS, Buyer has requested and Boeing has agreed to slide the Contract Delivery Month of certain four (4) Firm Aircraft as follows (2016 Firm Aircraft):
Was | New | MSN | ||
June 2009 | January 2016 | 36650 | ||
July 2009 | February 2016 | 36904 | ||
July 2009 | March 2016 | 36651 | ||
August 2009 | April 2016 | 36653 |
and;
WHEREAS, Notwithstanding the Letter agreement No. 6-1162-NIW-1947 which was fully executed on May 2, 2008, Boeing and Buyer have agreed to revise the incorporation point of Record Option Number 2525C882G60 entitled “Replacement of BFE B/E Aerospace Passenger
***Pursuant to 17 CFR 240.24b-2, confidential information has been omitted and has been filed separately with the Securities and Exchange Commission pursuant to a Confidential Treatment Application filed with the Commission.
P.A. No. 1810 SA-61-1
K/SWA
Seats” to the Aircraft delivering in January 2010 from August 2009 due to slide of the Contract Delivery Month relating to the 2016 Firm Aircraft and;
WHEREAS, Boeing and Buyer have agreed to use the latest escalation forecast (4th Quarter 2007 Forecast) to calculate the Advance Payment Base Price for the *** Firm Aircraft in Table 1; and
NOW THEREFORE, in consideration of the mutual covenants herein contained, the parties agree to amend the Agreement as follows:
1. The Table of Contents of the Agreement is deleted in its entirety and a new Table of Contents is attached hereto and incorporated into the Agreement by this reference.
2. Table 1 is deleted in its entirety and replaced by a new Table 1 which is attached hereto to reflect the revision to the Contract Delivery Month of four (4) Firm Aircraft from year 2009 to year 2016.
3. Exhibit A-3 is added as part of Exhibit A suite to reflect incorporation of Record Option Number 2525C882G60 entitled “Replacement of BFE B/E Aerospace passenger Seats” (Record Option) into the configuration of the second Aircraft delivering in January 2010 and thereafter. The incorporation of such Record Option on the first Aircraft delivering in January 2010 will be done using a Boeing internal process and a one time charge associated with the Record Option in the amount of *** (in 1999$ Subject to Escalation) will be invoiced to Buyer as part of the Aircraft Delivery Invoice of the first Aircraft delivering in January 2010.
4. All references in the Letter Agreements associated with Purchase Agreement No. 1810 shall be deemed to refer to the purchase by Buyer of four hundred nineteen (419) Model 737-7H4 Aircraft, sixty-seven (67) Model 737-7H4 Option Aircraft and fifty-four (54) Model 737-7H4 Purchase Right Aircraft, to the extent such reference is not specifically addressed herein.
5. Boeing and Buyer have agreed that Boeing will ***:
P.A. No. 1810 SA-61-2
K/SWA
***
6. Boeing’s labor contract renewal date with its principal employee union (the IAM) expired at midnight on September 3, 2008. After a 48 hour mediation effort, the IAM initiated a strike on September 6, 2008. (IAM Action). The Customer acknowledges that (i) the obligations of Boeing described in this Supplemental Agreement are premised upon Boeing’s manufacturing capability prior to the IAM Action; and (ii) delay in the performance of any obligation of Boeing under this Purchase Agreement resulting from the IAM Action is an excusable delay under the provisions of Article 6 of the Agreement.
The Agreement will be deemed to be supplemented to the extent herein provided and as so supplemented will continue in full force and effect.
EXECUTED IN DUPLICATE as of the day and year first above written.
THE BOEING COMPANY | SOUTHWEST AIRLINES CO. |
By: /s/ Nobuko Wiles | By:/s/ Scott Toppping |
Its: Attorney-In-Fact | Its:Vice President Treasurer |
P.A. No. 1810 SA-61-3
K/SWA
TABLE OF CONTENTS
Page | SA | ||
Number | Number | ||
ARTICLES | |||
1. | Subject Matter of Sale | 1-1 | SA-13 |
2. | Delivery, Title and Risk | ||
of Loss | 2-1 | SA-28 | |
3. | Price of Aircraft | 3-1 | SA-47 |
4. | Taxes | 4-1 | |
5. | Payment | 5-1 | |
6. | Excusable Delay | 6-1 | |
7. | Changes to the Detail | ||
Specification | 7-1 | SA-1 | |
8. | Federal Aviation Requirements and | ||
Certificates and Export License | 8-1 | ||
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 | |
15. | Miscellaneous | 15-1 |
P.A. No. 1810 i
K/SWA & #160; SA-61
TABLE OF CONTENTS CON'T
SA | ||
Number | ||
TABLE | ||
1. | Aircraft Information Table | SA-61 |
2. | Option Aircraft Information Table | SA-60 |
EXHIBITS | ||
A | Aircraft Configuration | SA-61 |
B | Product Assurance Document | SA-1 |
C | Customer Support Document | |
D | Price Adjustments Due to Economic Fluctuations - Aircraft | |
E | Buyer Furnished Equipment | |
Provisions Document | ||
F | Defined Terms Document | |
LETTER AGREEMENTS | ||
1810-1 | Waiver of Aircraft Demonstration Flight |
P.A. No. 1810 ii
K/SWA & #160; SA-61
TABLE OF CONTENTS CON'T
SA | ||
Number | ||
RESTRICTED LETTER AGREEMENTS | ||
6-1162-RLL-932R2 | Promotional Support | SA-13 |
6-1162-RLL-933R21 | Option Aircraft | SA-60 |
6-1162-RLL-934R3 | Disclosure of Confidential | SA-14 |
Information | ||
6-1162-RLL-935R1 | Performance Guarantees | SA-1 |
6-1162-NIW-890 | *** | SA-39 |
6-1162-RLL-936R4 | Certain Contractual Matters | SA-4 |
6-1162-RLL-937 | Alternate Advance Payment Schedule | |
6-1162-RLL-938 | *** | |
6-1162-RLL-939R1 | Certification Flight Test Aircraft | SA-1 |
6-1162-RLL-940R1 | Training Matters | SA-1 |
6-1162-RLL-941R2 | Other Matters | SA-13 |
6-1162-RLL-942 | Open Configuration Matters | |
6-1162-RLL-943R1 | Substitution Rights | SA-6 |
6-1162-RLL-944 | *** | |
6-1162-RLL-945 | Comparison of 737-7H4 and 737-3H4 | |
Block Fuel Burn | ||
6-1162-RLL-1855R3 | Additional Contractual Matters | SA-4 |
6-1162-RLL-1856 | *** | SA-1 |
6-1162-RLL-1857 | Service Ready Validation Program | SA-1 |
Field Test | ||
6-1162-RLL-1858R1 | Escalation Matters | SA-4 |
P.A. No. 1810 iii
K/SWA ; SA-61
TABLE OF CONTENTS CON'T
SA | |||
Number | |||
RESTRICTED LETTER AGREEMENTS | |||
6-1162-RLL-2036 | Amortization of Costs for | ||
Customer Unique Changes | SA-1 | ||
6-1162-RLL-2037 | Reconciliation of the Aircraft | SA-1 | |
Basic Price | |||
6-1162-RLL-2073 | Maintenance Training Matters | SA-1 | |
6-1162-KJJ-054R1 | Business Matters | ||
6-1162-KJJ-055R1 | Structural Matters | SA-25 | |
6-1162-KJJ-056 | Noise and Emission Matters | SA-13 | |
6-1162-KJJ-057 | Product Development Matters | SA-13 | |
6-1162-KJJ-058 | Additional Substitution Rights | SA-13 | |
6-1162-KJJ-150 | Flight Control Computer & Mode | SA-14 | |
Control Panel Spares Matter | |||
6-1162-MSA-185R3 | Delivery Change Contractual | SA-21 | |
Matters | |||
6-1162-JMG-669R9 | *** | SA-54 | |
6-1162-JMG-747R1 | *** | SA-36 | |
6-1162-CHL-217 | Rescheduled Flight Test Aircraft | SA-32 | |
6-1162-NIW-606R1 | *** | SA-36 | |
6-1162-NIW-640 | Early Delivery of Two April 2004 | SA-35 | |
Aircraft | |||
6-1162-NIW-889 | Warranty - Exterior Color Schemes | SA-39 | |
and Markings for YA143 and on | |||
6-1162-NIW-1142 | *** | SA-43 | |
6-1162-NIW-1369 | *** | SA-46 |
P.A. No. 1810 iv
K/SWA & #160; SA-61
Table 1 to
Purchase Agreement No. 1810
Aircraft Information Table
Base Aircraft Price | Special Features | Aircraft Basic Price | Base Year Dollars | |||
Block A, B, C, D & E Aircraft | *** | *** | *** | July 1992 | ||
Block F & G Aircraft | *** | *** | *** | July 1992 | ||
Block H Aircraft | *** | *** | *** | July 1992 | ||
Block I Aircraft | *** | *** | *** | July 1992 | ||
Block J Aircraft | *** | *** | *** | July 1992 | ||
Block K Aircraft | *** | *** | *** | July 1992 | ||
Block K-W Aircraft | *** | *** | *** | July 1992 | ||
Block L Aircraft | *** | *** | *** | July 1992 | ||
Block T Aircraft | *** | *** | *** | July 1999 | ||
Block T-W Aircraft | *** | *** | *** | July 1999 | ||
Block T-W-1 / T-W-1a Aircraft | *** | *** | *** | July 1999 | ||
Block T-W-2 / T-W-2a Aircraft | *** | *** | *** | July 1999 | ||
Block K-W Aircraft: Block K airplanes with production winglets installation | ||||||
Block T-W Aircraft: Block T airplanes with production winglets installation | ||||||
Block T-W-1 / T-W-1a Aircraft: Firm Aircraft contracted to deliver from May 1, 2006 through June 2008 at the signing | ||||||
of SA-47 -- (T-W-1a Aircraft -- Advance Payment Schedule per LA 6-1162-JGM-669) | ||||||
Block T-W-2 / T-W-2a Aircraft: U-W-1 Option Aircraft which became Firm Aircraft after signing of SA-47 and | ||||||
Firm Aircraft contracted to deliver in July 2008 forward at the signing of SA47 -- | ||||||
(T-W-2a Aircraft -- Advance Payment Schedule per LA 6-1162-JGM-669) | ||||||
* Exhibit A-2 applies to Block T-W-2 / T-W-2a Aircraft delivering through Dec 2009 and the first Aircraft delivering in Jan 2010 | ||||||
* Exhibit A-3 applies to Block T-W-2 / T-W-2a Aircraft the second Aircraft delivering in Jan 2010 and on |
SWA & #160; Page 1 SA-61
Escalation Estimate | |||||
Delivery | Number of | Aircraft | Adv Payment Base | ||
Date | Aircraft | Block | Price Per A/P | Serial Number | |
Dec-2000 | 2 | E | *** | ||
Jan-2001 | 1 | E | *** | ||
Feb-2001 | 1 | E | *** |
Mar-2001 | 2 | E | *** | ||
Jun-2001 | 3 | E | *** | ||
Sep-2001 | 3 | E | *** | ||
Oct-1998 | 1 | F | *** | ||
Nov-1998 | 2 | F | *** | ||
Dec-1998 | 2 | F | *** | ||
Mar-1999 | 2 | G | *** | ||
Jun-1999 | 2 | H | *** | ||
Jul-1999 | 1 | H | *** | ||
Aug-1999 | 1 | H | *** | ||
Sep-1999 | 2 | H | *** | ||
Oct-1999 | 1 | H | *** | ||
Mar-2000 | 1 | H | *** | ||
Apr-2000 | 2 | H | *** | ||
Sep-2000 | 1 | H | *** | ||
Oct-2000 | 2 | H | *** | ||
Mar-2001 | 2 | H | *** | ||
Apr-2001 | 1 | H | *** | ||
Oct-2001 | 3 | H | *** | ||
Nov-2001 | 2 | I | *** | ||
Dec-2001 | 1 | I | *** | ||
Jan-2002 | 1 | I | *** | ||
Mar-2002 | 4 | I | *** | ||
Apr-2002 | 2 | I | *** | ||
Dec-2002 | 2 | I | *** | ||
May-2003 | 1 | I | *** | ||
Jun-2003 | 2 | I | *** | ||
Jul-2003 | 1 | I | *** | ||
Aug-2003 | 1 | I | *** | ||
Sep-2003 | 3 | I | *** | ||
Nov-2002 | 1 | J | *** | ||
Dec-2002 | 1 | J | *** | ||
Nov-2003 | 2 | J | *** | ||
Dec-2003 | 2 | J | *** | ||
Mar-2004 | 1 | J | *** | ||
Mar-2004 | 1 | K | *** | ||
Apr-2004 | 3 | K | *** | ||
May-2004 | 1 | K | *** | ||
Jun-2004 | 2 | K | *** | ||
Jul-2004 | 2 | K | *** | ||
Sep-2004 | 1 | K-W | *** | ||
Oct-2004 | 4 | K-W | *** | ||
Oct-1999 | 1 | L | *** | ||
Nov-1999 | 2 | L | *** | ||
Dec-1999 | 1 | L | *** | ||
Jun-2000 | 3 | L | *** | ||
Jul-2000 | 3 | L | *** | ||
Sep-2000 | 1 | L | *** | ||
Oct-2000 | 1 | L | *** | ||
Nov-2000 | 4 | L | *** | ||
Dec-2000 | 1 | L | *** | ||
Jan-2001 | 1 | L | *** |
SWA & #160; Page 2 SA-61
Feb-2001 | 1 | L | *** | ||
Jul-2001 | 1 | L | *** | ||
Sep-2001 | 1 | L | *** | ||
Oct-2001 | 1 | L | *** | ||
Mar-2003 | 2 | L | *** | ||
Jul-2003 | 1 | L | *** | ||
Aug-2003 | 2 | L | *** | ||
Nov-2001 | 1 | T | *** | ||
Feb-2002 | 1 | T | *** | ||
Jan-2004 | 2 | T | *** | ||
Feb-2004 | 1 | T | *** | ||
Apr-2004 | 3 | T | *** | ||
May-2004 | 1 | T | *** | ||
Jun-2004 | 6 | T | *** | ||
Jul-2004 | 2 | T | *** | ||
Aug-2004 | 6 | T-W | *** | ||
Sep-2004 | 4 | T-W | *** | ||
Oct-2004 | 0 | T-W | *** | ||
Nov-2004 | 3 | T-W | *** | ||
Dec-2004 | 3 | T-W | *** | ||
Jan-2005 | 5 | T-W | *** | ||
Feb-2005 | 3 | T-W | *** | ||
Mar-2005 | 4 | T-W | *** | ||
Apr-2005 | 4 | T-W | *** | ||
May-2005 | 2 | T-W | *** | ||
Jun-2005 | 4 | T-W | *** | ||
Jul-2005 | 2 | T-W | *** | ||
Aug-2005 | 2 | T-W | *** | ||
Sep-2005 | 3 | T-W | *** | ||
Oct-2005 | 2 | T-W | *** | ||
Nov-2005 | 2 | T-W | *** | ||
Dec-2005 | 1 | T-W | *** | ||
Jan-2006 | 1 | T-W | *** | ||
Feb-2006 | 4 | T-W | *** | ||
Mar-2006 | 3 | T-W | *** | ||
Apr-2006 | 2 | T-W | *** | ||
May-2006 | 5 | T-W-1 | *** | ||
Jun-2006 | 5 | T-W-1 | *** | ||
Jul-2006 | 3 | T-W-1 | *** | ||
Aug-2006 | 3 | T-W-1 | *** | ||
Sep-2006 | 3 | T-W-1 | *** | ||
Oct-2006 | 1 | T-W-1 | *** | ||
Nov-2006 | 2 | T-W-1 | *** | ||
Dec-2006 | 2 | T-W-1 | *** | ||
Jan-2007 | 2 | T-W-1 | *** | ||
Feb-2007 | 3 | T-W-1 | *** | ||
Mar-2007 | 2 | T-W-1 | *** | ||
Apr-2007 | 3 | T-W-1 | *** | ||
May-2007 | 3 | T-W-1 | *** | ||
Jun-2007 | 2 | T-W-1 | *** | ||
Jun-2007 | 1 | T-W-1a | *** | 36528 |
SWA & #160; Page 3 SA-61
Jul-2007 | 2 | T-W-1 | *** | ||
Jul-2007 | 1 | T-W-1a | *** | 36610 | |
Aug-2007 | 2 | T-W-1 | *** | ||
Aug-2007 | 3 | T-W-1a | *** | 36611, 36632 & 36633 | |
Sep-2007 | 2 | T-W-1 | *** | ||
Sep-2007 | 1 | T-W-1a | *** | 36612 | |
Oct-2007 | 3 | T-W-1 | *** | ||
Oct-2007 | 1 | T-W-1a | *** | 36613 | |
Nov-2007 | 1 | T-W-1 | *** | ||
Nov-2007 | 1 | T-W-1a | *** | 36614 | |
Dec-2007 | 2 | T-W-1 | *** | ||
Dec-2007 | 1 | T-W-1a | *** | 36615 | |
Jan-2008 | 1 | T-W-1 | *** | ||
Jan-2008 | 2 | T-W-1a | *** | 36616 & 36617 | |
Jan-2008 | 1 | T-W-2 | *** | 36887 | |
Feb-2008 | 1 | T-W-1 | *** | ||
Feb-2008 | 3 | T-W-1a | *** | 36618, 36619 & 36620 | |
Mar-2008 | 1 | T-W-1 | *** | ||
Mar-2008 | 2 | T-W-1a | *** | 36621 & 36622 | |
Mar-2008 | 1 | T-W-2 | *** | 36888 | |
Apr-2008 | 1 | T-W-1 | *** | ||
Apr-2008 | 2 | T-W-1a | *** | 36623 & 36624 | |
May-2008 | 1 | T-W-1 | *** | ||
May-2008 | 2 | T-W-1a | *** | 36625 & 36626 | |
Jun-2008 | 1 | T-W-1 | *** | ||
Jun-2008 | 2 | T-W-1a | *** | 36627 & 36628 | |
Jul-2008 | 2 | T-W-2a | *** | ||
Jul-2008 | 2 | T-W-2 | *** | 36889 & 36890 | |
Aug-2008 | 1 | T-W-2a | *** | ||
Oct-2008 | 1 | T-W-2a | *** | ||
Nov-2008 | 1 | T-W-2a | *** | ||
Dec-2008 | 1 | T-W-2a | *** | ||
Jan-2009 | 1 | T-W-2a | *** | ||
Feb-2009 | 2 | T-W-2a | *** | ||
Mar-2009 | 2 | T-W-2a | *** | ||
Apr-2009 | 2 | T-W-2a | *** | ||
Apr-2009 | 1 | T-W-2 | *** | 36900 | |
May-2009 | 2 | T-W-2a | *** | ||
Jan-2010 | 1 | T-W-2a | *** | ||
Jan-2010 | 1 | T-W-2 | *** | 36913 | |
Feb-2010 | 1 | T-W-2a | *** | ||
Feb-2010 | 1 | T-W-2 | *** | 36916 | |
Mar-2010 | 1 | T-W-2a | *** | ||
Mar-2010 | 1 | T-W-2 | *** | 36918 | |
Apr-2010 | 1 | T-W-2a | *** | ||
Apr-2010 | 1 | T-W-2 | *** | 36921 | |
May-2010 | 1 | T-W-2a | *** | ||
May-2010 | 2 | T-W-2 | *** | 36923, 36924 | |
Jun-2010 | 1 | T-W-2a | *** | ||
Jul-2010 | 1 | T-W-2a | *** | ||
Aug-2010 | 1 | T-W-2a | *** |
SWA & #160; Page 4 SA-61
Sep-2010 | 1 | T-W-2a | *** | ||
Oct-2010 | 1 | T-W-2a | *** | ||
Jan-2011 | 1 | T-W-2a | *** | ||
Feb-2011 | 1 | T-W-2a | *** | ||
Mar-2011 | 1 | T-W-2a | *** | ||
Apr-2011 | 1 | T-W-2a | *** | ||
May-2011 | 1 | T-W-2a | *** | ||
Jun-2011 | 1 | T-W-2a | *** | ||
Jul-2011 | 1 | T-W-2a | *** | ||
Aug-2011 | 1 | T-W-2a | *** | ||
Sep-2011 | 1 | T-W-2a | *** | ||
Oct-2011 | 1 | T-W-2a | *** | ||
Oct-2011 | 1 | T-W-2 | *** | 36966 | |
Nov-2011 | 1 | T-W-2 | *** | 36968 | |
Dec-2011 | 1 | T-W-2 | *** | 36971 | |
Jan-2012 | 1 | T-W-2a | *** | ||
Feb-2012 | 1 | T-W-2a | *** | ||
Mar-2012 | 1 | T-W-2a | *** | ||
Apr-2012 | 1 | T-W-2a | *** | ||
May-2012 | 1 | T-W-2a | *** | ||
Jun-2012 | 1 | T-W-2a | *** | ||
Jul-2012 | 1 | T-W-2a | *** | ||
Aug-2012 | 1 | T-W-2a | *** | ||
Sep-2012 | 1 | T-W-2a | *** | ||
Oct-2012 | 1 | T-W-2a | *** | ||
Oct-2012 | 1 | T-W-2 | *** | 36997 | |
Nov-2012 | 1 | T-W-2 | *** | 37005 | |
Dec-2012 | 1 | T-W-2 | *** | 37006 | |
Jan-2013 | 1 | T-W-2 | *** | 36891 | |
Jan-2013 | 1 | T-W-2a | *** | ||
Feb-2013 | 1 | T-W-2a | *** | ||
Mar-2013 | 1 | T-W-2a | *** | ||
Mar-2013 | 1 | T-W-2 | *** | ||
Apr-2013 | 1 | T-W-2 | *** | ||
May-2013 | 1 | T-W-2 | *** | ||
Jun-2013 | 2 | T-W-2 | *** | ||
Jul-2013 | 1 | T-W-2 | *** | ||
Aug-2013 | 2 | T-W-2 | *** | ||
Sep-2013 | 2 | T-W-2 | *** | ||
Oct-2013 | 2 | T-W-2 | *** | ||
Nov-2013 | 1 | T-W-2 | *** | ||
Dec-2013 | 2 | T-W-2 | *** | ||
Jan-2014 | 1 | T-W-2 | *** | ||
Feb-2014 | 1 | T-W-2 | *** | ||
Mar-2014 | 1 | T-W-2 | *** | ||
Apr-2014 | 1 | T-W-2 | *** | ||
May-2014 | 1 | T-W-2 | *** | ||
Jun-2014 | 1 | T-W-2 | *** | ||
Jul-2014 | 1 | T-W-2 | *** | ||
Aug-2014 | 1 | T-W-2 | *** | ||
Sep-2014 | 1 | T-W-2 | *** |
SWA & #160; Page 5 SA-61
Oct-2014 | 1 | T-W-2 | *** | ||
Jan-2015 | 1 | T-W-2 | *** | 36899 | |
Feb-2015 | 1 | T-W-2 | *** | 36901 | |
Mar-2015 | 1 | T-W-2 | *** | 36902 | |
Apr-2015 | 2 | T-W-2a | *** | 36649, 36652 | |
May-2015 | 1 | T-W-2 | *** | 36903 | |
Jun-2015 | 1 | T-W-2 | *** | 36906 | |
Jun-2015 | 1 | T-W-2a | *** | 36654 | |
Jul-2015 | 1 | T-W-2a | *** | 36655 | |
Aug-2015 | 1 | T-W-2a | *** | 36656 | |
Sep-2015 | 1 | T-W-2a | *** | 36657 | |
Jan-2016 | 1 | T-W-2a | *** | 36650 | |
Feb-2016 | 1 | T-W-2 | *** | 36904 | |
Mar-2016 | 1 | T-W-2a | *** | 36651 | |
Apr-2016 | 1 | T-W-2a | *** | 36653 |
SWA & #160; Page 6 SA-61
AIRCRAFT CONFIGURATION
Dated __________________, 2008
relating to
BOEING MODEL 737-7H4 AIRCRAFT
The Detail Specification is Boeing Detail Specification D6-38808-1, Rev G dated as of July 26, 2005. Such Detail Specification will be comprised of Boeing Configuration Specification D019A001, Rev H dated as of November 18, 2005 as amended to incorporate the Options listed below, including the effects on Manufacturer's Empty Weight (MEW) and Operating Empty Weight (OEW). As soon as practicable, Boeing will furnish to Buyer copies of the Detail Specification, which copies will reflect such Options. The Aircraft Basic Price reflects and includes all effects of such Options, except such Aircraft Basic Price does not include the price effects of any Buyer Furnished Equipment or Seller Purchased Equipment. The effects of all Options which are mutually agreed upon between Boeing and Buyer for incorporation into the Aircraft Configuration will be incorporated into an applicable suit of Exhibit A of the Purchase Agreement by written amendment.
P.A. No. 1810 A-3- 1 SA-61
Exhibit A-3 – Applicable to the second Aircraft Delivering January 2010 and on
Change No. | Title | *** |
0000DC3182 | MISCELLANEOUS DEVELOPEMENT CHANGES | *** |
0110CG3018 | 737-700 CONFIGURATION | *** |
0252MP3132 | DISPATCH W/GEAR DWN FOR REVENUE FLT | *** |
0310CH3332 | MTOGW TO 138,500 | *** |
0352CG3023 | A/P LOAD SYS WT. & BALANCE CONTROL | *** |
0370CH3014 | AIR CONDITIONING TRANSITION DUCT UNDER FLOOR - ADD 17 MIL DAMPINGTAPE FOR NOISE REDUCTION | *** |
0370CH3019 | INSTALLATION OF STRINGER DAMPING FROM STATION 540-727 | *** |
1110A034B37 | EXTERIOR COLOR REVISION | *** |
1110A077A10 | EXT MARKINGS PRIMER REVISIONS | *** |
1110CH3003 | EXT DECOR PAINT-CROWN METRO | *** |
1110MP3290 | EXT DECO FNSH-DESOTO H.S TPCOAT | *** |
1110MP3354 | EXTERIOR DECOR.FINISH-HS TOPCOATIN LIEU OF EXISTING TOPCOAT | *** |
1110MP3388 | FLAP TRACK FAIRINGS -PAINT | *** |
2123CH3042 | AIR CONDITIONING SYSTEM REVISION -737-200 TYPE GASPER SYSTEM | *** |
2160CG3011 | CABIN TEMPERATURE INDICATOR - DEGREES FAHRENHEIT IN LIEU OFCELSIUS | *** |
2210CG3204 | DIGITAL FLIGHT CONTROL SYSTEM (DFCS) - PADDLE AUTOPILOT ENGAGEMODE CONTROL PANEL | *** |
2210MP3227 | DFCS PUSH BUTTON AUTOPILOT ENGAGE | *** |
2230CH3028 | AUTOTHROTTLE DEACTIVATION - UNIT TO REMAIN INSTALLED AND BITEFEATURES OPERATIONAL | *** |
2312CH3284 | DUAL VHF COMMUNICATIONS - INSTALLATION - BFE ALLIEDSIGNAL/GABLESENGINEERING INC | *** |
2319CH3020 | CLAIRCOM AIR TO GROUND PASSENGER COMMUNICATION SYSTEM - COMPLETEBFE INSTALLATION PROVISIONS | *** |
2319MP3021 | CLAIRCOM PHONES - CANCEL INSTALL. | *** |
2319MP3043 | AT&T WIRELESS PHN SYST. INSTAL&CERT | *** |
2319MP3051 | AT&T WIRELESS PHN SYSTEM-PART. REV. | *** |
2319MP3105 | AT&T WIRELESS AIR TO GRND PHONE SYS | *** |
2320CH3020 | ATSCALL INSTALLATION - PARTIAL PROVISIONS - AFT ELECTRONICS PANEL | *** |
2321CH3498 | SELECTIVE CALLING EQUIPMENT - SELCAL - DELETE PARTIAL PROVISIONS | *** |
2331CH3158 | DELETION OF BFE MATSUSHITA PASSENGER ADDRESS TAPE REPRODUCER | *** |
2331CH3159 | PASSENGER ADDRESS SYSTEM - COLLINSARINC 700 IN LIEU OF COLLINSARINC 560 | *** |
2340MP3095 | REV BFE BOOM MICROPHONE/HEADSET | *** |
2342MP3011 | FLT ATT HNDSET REV TO FUNCT & FACEP | *** |
2350CH3139 | PA MICROPHONE - ADD ELECTROVOICE P/N ###-###-#### | *** |
2350CH3162 | DTMF MICROPHONE INSTALLATION - FIRST OBSERVER | *** |
2350CH3163 | DIGITAL AUDIO REMOTE ELECTRONICS UNIT REVISION TO DELETE HEADSETAURAL ALERTS | *** |
2350MP3220 | DIGITAL AUDIO REMOTE ELETRON-ADD | *** |
2370CG3166 | SOLID STATE VOICE RECORDER - INSTALLATION - BFE ALLIEDSIGNAL INC | *** |
2371A051B44 | SOLID STATE VOIC RECORDER | *** |
P.A. No. 1810 A-3- 2 SA-61
2500CH3453 | DOOR WARNING STRAP - SHOCK CORD | *** |
2501CH3076 | FORWARD MODULE WITH GALLEY G1 AND LAVATORY LA | *** |
2501MP3080 | REVISE FORWARD MODULE WITH GALLEY G1 AND LAVATORY LA FROM SEATTRACK MOUNT TO HARDPOINT | *** |
2502CH3066 | AFT MODULE WITH GALLEY G3, G4 AND LAVATORY LB | *** |
2502MP3069 | REV MODUL WITH GALLEY G3, 4, & LAV | *** |
2510CH3058 | FLIGHT COMPARTMENT - MISCELLANEOUSREVISIONS | *** |
2510CH3059 | TRIP COUNTER REVISION - SFE - DEXTER WILSON | *** |
2510CH3060 | CONTROL COLUMN CHECKLIST DELETION | *** |
2511A599A02 | FLIGHT DECK-PADDED ROTARY BUCKLE | *** |
2511CG3057 | SECOND OBSERVER'S STATION | *** |
2511CH3059 | LOG BOOK POCKET INSTALLATION - ON SECOND OBSERVERS SEAT LEGS | *** |
2520A092I19 | INTERIOR COLOR AND MATERIAL REV | *** |
2520CH3538 | INTERIOR ARRANGEMENT - 137 TOURISTCLASS AT 33/32" PITCH WITH LAVSLA AND LB AND GALLEYS G1, G3 AND G4 | *** |
2520MP3667 | REV. STOW BIN ADD BULLNOSE ON INBRD | *** |
2523CH3109 | PSU REVISION - ADD PLACARD TO PASSENGER VIEWING SURFACE IN LOUNGEAREAS ONLY | *** |
2523CH3112 | INSTALL NON STANDARD COLOR PSU | *** |
2523MP3119 | REVISION INTERIOR ARRANGEMENT | *** |
2524CH3431 | BFE FWD RIGHT HAND WINDSCREEN/STOWAGE UNIT IN LIEU OF SFE | *** |
2524MP3488 | FULL HGT BFE STOW UNIT REV ADD BFE | *** |
2524MP3500 | REV PARTITION DECOR COVERNING ULTRA | *** |
2524MP3513 | EMERGENCY QUIPMENT BRACKET COMMONALITY-SFE | *** |
2525MP3159 | REV PAX SEAT ALL F/W FACING W/ 137 | *** |
2528CH3189 | SFE HALF HEIGHT STOWAGE UNIT/WINDSCREEN - AFT LH CABIN WITH THEAFT FACE AT STATION 955 - WITH MEGAPHONE | *** |
2528CH3191 | SFE FULL HEIGHT STOWAGE UNIT/WINDSCREEN - FWD LH CABIN WITH THEAFT FACE AT STATION 355 | *** |
2528CH3194 | BFE HALF HEIGHT STOWAGE UNIT/WINDSCREEN - AFT LH CABIN WITH THEAFT FACE AT STATION 955 - WITH MEGAPHONE | *** |
2528CH3195 | BFE FULL HEIGHT STOWAGE UNIT/WINDSCREEN IN LIEU OF SFE - FWD LHCABIN WITH THE AFT FACE AT STATION355 | *** |
2528MP3205 | CREW LUGGAGE SECURITY DEVISE | *** |
2528MP3217 | CREW LUGGAGE SECURITY DEVICE | *** |
2530MP3613 | REV G3 EXT DECOR COVERING ULTRALEAT | *** |
2530MP3860 | BFE GALLEY REV COMOSITES UNLIM | *** |
2541CH3034 | LIQUID SOAP DISPENSER INSTALLATION | *** |
2550CH3153 | CARGO COMPARTMENT LINING REVISION | *** |
2550CH3233 | FWD AND AFT CARGO COMPARTMENT FLOOR PANEL REVISION - ALUMINUMPANELS IN LIEU OF CONOLITE AT ENTRYWAY | *** |
2550MP3259 | TRANSVERSE CARGO NET INSTALLATION - FORWARD AND AFT CARGOCOMPARTMENTS | *** |
2550MP3267 | FORWARD AND AFT CARGO COMPARTMENT CARGO RESTRAINT SYSTEM | *** |
2550MP3355 | FRWRD & AFT CARGO CMPRTMNT | *** |
2566A077A03 | ESCAPE SLIDES COMPARTMENTS SFE TOBFE B.GOODRICH INSTALLED | *** |
2622CH3013 | APU FIRE BOTTLE REVISION - INTERCHANGEABLE WITH ENGINE BOTTLE | *** |
2841CG3095 | FUEL QUANTITY INDICATORS ON RIGHT WING FUELING PANEL | *** |
2844CG3038 | MEASURING STICK CONVERSION TABLES TO U.S. GALLONS | *** |
2910CG3087 | ENGINE DRIVEN HYDRAULIC PUMP WITH VESPEL SPLINE - VICKERS10-62167-3 IN LIEU OF ABEX 10-62167-2 | *** |
P.A. No. 1810 A-3- 3 SA-61
2910CH3082 | HYDRAULIC PUMPS - AC ELECTRIC MOTOR DRIVEN - VICKERS IN LIEU OFABEX | *** |
3040CH3041 | INSTALL A TWO LRU WINDOW HEAT CONTROL SYSTEM - PED 1231-1 IN LIEUOF TBD | *** |
3040MP3049 | INSTL 4 UNIT WINDOW HEAT CNTRL SYS | *** |
3040MP3053 | INSTALL A BFE WINDOW HEAT CONTROLSYSTEM OLIN 231-3 IN LIEU OF 231-2 | *** |
3041A034B24 | INSTALL PRIMEX WINDOW HEAT CONT SYS | *** |
3043MP3022 | REV WINDSHIELD WIPER SWTCH SINGLE | *** |
3120CH3016 | CLOCK WIRING REVISION - FMC, DFDAUAND VOICE RECORDER INPUT FROMFIRST OFFICER'S CLOCK IN LIEU OF CAPTAIN'S CLOCK | *** |
3131CG3673 | ACCELEROMETER - INSTALLATION - BFEALLIEDSIGNAL INC | *** |
3131CG3692 | SOLID STATE DIGITAL FLIGHT DATA RECORDER - INSTALLATION - BFESUNDSTRAND - 128 WPS | *** |
3131CH3721 | DIGITAL FLIGHT DATA ACQUISITION UNIT (DFDAU) - INSTALLATION - BFEALLIEDSIGNAL | *** |
3162A066A15 | REVERSE VIDEO DISPLAY-COMMON DISPLASYS FAULT MESSAGE | *** |
3162A066A27 | ILF LOCALIZER DEVIATION EXPANDEDSCALE | *** |
3162CG3013 | EFIS/MAP DISPLAY FORMAT | *** |
3162CG3016 | FLT DRCTR COMND DSPL-FIL INTGRT CUE | *** |
3162CG3017 | MACH AIRSPEED DISPLAY | *** |
3162CG3019 | RADIO ALTITUDE DISPLAY - ROUND DIAL | *** |
3162CG3020 | RADIO ALTITUDE - ABOVE ADI | *** |
3162CG3022 | RISING RUNWAY DISPLAY | *** |
3162CG3025 | RADIO ALTITUDE HEIGHT ALERT DISPLAY - 2500 FEET | *** |
3162CG3026 | ATTITUDE COMPARATOR - STEADY | *** |
3162CG3029 | LOCALIZER BACKCOURSE POLARITY - REVERSAL | *** |
3162CG3032 | MAP MODE ORIENTATION - TRACK UP | *** |
3162CG3038 | MANUALLY TUNED VOR SELECTED COURSELINES - DISPLAYED | *** |
3162CG3041 | ADF POINTER(S) IN MAP MODE - SUPPRESSED | *** |
3162CG3042 | POSITION DIFFERENCE - AUTOMATIC DISPLAY | *** |
3162CG3046 | WEATHER RADAR MODE/GAIN/TILT ANGLE- DISPLAYED | *** |
3162CG3050 | TCAS TRAFFIC ON MAP | *** |
3162CG3052 | TCAS RESOLUTION ADVISORY ON ADI | *** |
3162CG3053 | TCAS RESOLUTION ADVISORY ON IVSI | *** |
3162CG3057 | ANALOG FAILURE FLAGS-DISPLAYED | *** |
3162CH3066 | MACH AIRSPEED INDICATOR BUG #5 - 80 KNOTS | *** |
3162CH3068 | SUPPLEMENTAL METRIC DATA INDICATIONS - DEACTIVATION | *** |
3162CH3075 | EFIS CONTROL PANEL - EFIS/MAP DISPLAY FORMAT | *** |
3162MP3128 | DELETE ANALOG FAILURE FLAG | *** |
3162MP3129 | SUPP METRIC DATA INDICATIONS ACTIV | *** |
3162MP3131 | ENHANCED MACHINE AIRSPEED DISPLAY | *** |
3162MP3132 | WX RADAR RANGE INDICATORS RANGE MRK | *** |
3240CH3220 | NOSE LANDING GEAR WHEELS - BENDIX | *** |
3240CH3221 | MAIN LANDING GEAR WHEELS AND BRAKES - BENDIX | *** |
3240MP3258 | INSTL NOSE LANDING GEAR ALLIED SIGN | *** |
3240MP3288 | NOSE LDG GEAR INSTL - 700 WHEELSILO -300 WHEELS | *** |
3245CH3029 | TIRES - INSTALLATION OF SFE GOODYEAR TIRES | *** |
3324A092K63 | PASS CAB INSTALL-NO SMOKING PERMANILLUMINATION | *** |
3324CH3010 | CEILING MOUNTED LIGHTED EXIT SIGN - RELOCATION | *** |
3343CH3034 | ANTI-COLLISION LIGHT - SWITCH NOMENCLATURE REVISION | *** |
3345CH3020 | LOGO LIGHTS - SYSTEM DEACTIVATION | *** |
P.A. No. 1810 A-3- 4 SA-61
3345MP3029 | REACTIVATION OF LOGO LIGHTS | *** |
3350MP3079 | EGRESS LIGHTING REVISION TOACCOMODATE ALL FOWARD FACINGSEAT CONFIGURATION. | *** |
3423CH3021 | INSTALL BFE STANDBY ATTITUDE INDICATOR WITHOUT ILS DEVIATIONDISPLAY IN LIEU OF SFE INDICATOR | *** |
3423CH3026 | STANDBY INDICATOR - SFE SEXTANT INLIEU OF BFE JET | *** |
3430MP3061 | MULTI-MODE RECEIVER (MMR) - INSTALLATION OF ILS/GPS - BFEALLIEDSIGNAL INC | *** |
3430MP3069 | MMR-GPS PROVISIONS-REP OF OH GPS | *** |
3431CG3051 | ILS - INSTALLATION - BFE ALLIEDSIGNAL INC | *** |
3431MP3072 | ILS-DELETION OF EXISTING ILS RECEIV | *** |
3433CG3058 | LOW RANGE RADIO ALTIMETER (LRRA) -INSTALLATION - BFE ALLIEDSIGNALINC | *** |
3435CH3028 | FLIGHT DYNAM.CAPTAIN ONLY HEAD UPGUIDANCE SYSTEM-PART PROVISIONS | *** |
3435MP3035 | HEAD UP GUIDANCE SYS - BFE INSTL | *** |
3436A034B19 | INSTALL 1500-1730-002 HUD COMPUTER | *** |
3443CH3118 | WEATHER RADAR SYSTEM - ARINC 708A SINGLE WEATHER RADAR SYSTEM WITHPREDICTIVE WINDSHEAR - PARTIAL PROVISIONS | *** |
3443CH3154 | ARINC 708 WEATHER RADAR SYSTEM - INSTALLATION - BFE ALLIEDSIGNALINC (WITH DEACTIVATED PREDICTIVE WINDSHEAR FEATURE R/T RDR-4B) | *** |
3445CH3197 | TCAS II - INSTALLATION - BFE ALLIEDSIGNAL INC | *** |
3451CG3005 | VOR/MARKER BEACON - INSTALLATION -BFE ALLIEDSIGNAL INC | *** |
3455CG3120 | DISTANCE MEASURING EQUIPMENT (DME)- INSTALLATION - BFEALLIEDSIGNAL INC (SCANNING) | *** |
3457CG3088 | AUTOMATIC DIRECTION FINDER (ADF) -INSTALLATION - BFE ALLIEDSIGNALINC | *** |
3457CG3092 | AUTOMATIC DIRECTION FINDER (ADF) CONTROL PANEL - INSTALLATION -BFE GABLES ENGINEERING INC | *** |
3457MP3132 | ADD ADF CNTRL PANEL REV GABLES ILO | *** |
3457MP3133 | ADD ADF ANTENNA REV ALLIED SIG ILO | *** |
3458CH3091 | GPS PROVISIONS - ADD COMPONENTS REQUIRED TO PROVIDE COMPLETEPROVISIONS | *** |
3458CH3091.1 | GPS PROVISIONS - ADD COMPONENTS REQUIRED TO PROVIDE COMPLETEPROVISIONS | *** |
3458CH3092 | GLOBAL POSITIONING SYSTEM (GPS) - INSTALLATION - HONEYWELL INC(SUPPLEMENTAL NAVIGATION CERTIFICATION) | *** |
3461CG3403 | BUYER FURNISHED NAVIGATION DATA BASE | *** |
3461CH3485 | VERTICAL NAVIGATION (VNAV) ACTIVATE/DEACTIVATE SERVICE BULLETIN | *** |
3461CH3489 | FLIGHT MANAGEMENT COMPUTER SYSTEM REVISION - CERTIFICATION FORSINGLE COMPUTER OPERATION ONLY | *** |
3461MP3496 | INSTALL FMC-SECOND 4MCU, UPDATE10 FMC W/256K NAVAGATION DATABASEINTO EXISITING PARTIAL PROVISIONS | *** |
3510CG3089 | CREW OXYGEN - 114 CU. FT. IN LIEU OF 76 CU. FT. CYLINDER | *** |
3830MP3025 | INSTL PNEUDRAULICS 4" SERV PANL LAV | *** |
3831MP3019 | REV GRAY WATER DRAIN ROUT LEVEL LIN | *** |
3832CH3071 | VACUUM LAVATORY SYSTEM IN LIEU OF RECIRCULATING LAVATORY - LAVS AAND B | *** |
3910CH3113 | RELOCATE ATC CONTROL PANEL | *** |
3910CH3122 | AFT ELECTRONICS PANEL ARRANGEMENT | *** |
4960MP3024 | APU SOFTWARE LOADING-ONBOARD FROMFLIGHT DECK | *** |
5100CH3026 | ADDITIONAL CORROSION PROTECTION BENEATH GALLEYS AND LAVS | *** |
P.A. No. 1810 A-3- 5 SA-61
5100CH3027 | FWD AND AFT CARGO DOOR REVISION - INSTALL HEAVY DUTY SKIN | *** |
5100MP3030 | REMOVE ADD CORR PROT. ADDED BY CR | *** |
5220MP3012 | OVER/WNG HATCH ASSIST HNDLE REV INS | *** |
5312MP3004 | INSTAL OF SFE WEATHERMASTER RADOMEIN LIEU OF SFE BASIC RADOME | *** |
5730B502D20 | PRODUCTION INSTALLATION OF BFE WINGLETS | *** |
7200CG3244 | A/P PRFRMC:CFM56-7 ENG W/THRUST 22K | *** |
7731MP3049 | EVM SYST WITH ON-BOARD TRIM & BAL | *** |
7900CG3026 | LUBRICATING OIL - ESSO/EXXON TURBOOIL 2380 | *** |
Sub-Total Changes - Special Features -- the same as in Exhibit A-1-Winglet ***
Additional Master Changes | ||
0221A599A80 | WET GROOVED RUNWAY OPERATIONS WITHANTISKID SYSTEM INOPERATIVE CERT. | *** |
0315B572C40 | MP - OPERATIONAL WEIGHTS - INCREASE MTOW | *** |
0370B572B79 | MP - STRINGER DAMPING - REMOVE BETWEEN STATIONS 540-727 | *** |
1110B458A27 | MP - EXTERIOR MARKINGS AND PLACARDS REVISION | *** |
1110B642K10 | MP - EXTERIOR COLOR SCHEMES AND MARKINGS - REVISION - PAINT SYSTEM PRIMER - SPE | *** |
1110B645J06 | MP - EXTERIOR COLOR SCHEMES AND MARKINGS - REVISION - PRC DESOTO CA8800 DECORATIVE PAINT TOPCOAT | *** |
1130A599A55 | AFT CLOSET PLACARD-COLOR CHANGE | *** |
1130C410C11 | MP - PLACARDS AND MARKINGS - INSTALLATION - INTERIOR PLACARDS - SWA | *** |
2130A610B77 | CABIN PRESSURE DESCENT RATE REV | *** |
2312B696C02 | MP - VHF COMMUNICATIONS - INSTALLATION OF TRIPLE HONEYWELL RTA-44D VHF SYSTEM WITH ARINC 750 VDL MODE 2 CAPABLE TRANSCEIVERS P/N 064-50000-2000 - BFE | *** |
2318A599A08 | CABIN TELECOMMUNICATION-REV-PHONECABLES-BFE | *** |
2318A599A67 | PHONE SYS COMPONENT DELETION | *** |
2318B815C19 | MP - TELEPHONE AND BEARER RADIO - PARTIAL PROVISIONS - DELETE | *** |
2320A150E34 | MP- DELETION OF ATSCALL PARTIAL PROVISIONS FROM AFT ELECTRONICS PANEL | *** |
2322A150E39 | MP- COMMUNICATIONS MANAGEMENT UNIT (CMU) -PARTIAL PROVISIONS FOR SINGLE ARINC 758 CMU | *** |
2322B696C01 | MP - ACARS - HONEYWELL ARINC 758 LEVEL AOA MARK III COMMUNICATIONS MANAGEMENT UNIT (CMU) - INSTALLATION INTO EXISTIN PARTIAL PROVISIONS - BFE | *** |
2351A599A29 | BSS-HEADPHONE 1ST OBSERVER-REPLACE | *** |
2351A802B31 | HAND HELD MICROPHONE CAP AND IST OFFICER DELETE | *** |
2351B162A52 | HEADPHONE TELEX 616500-001 | *** |
2400C410B99 | MP - ELECTRICAL POWER - SPARE WIRE INSTALLATION TO FACILITATE POST DELIVERY MEDICAL COMMUNICATIONS SYSTEM | *** |
2500C547A51 | MP - ATTENDANT AND PASSENGER LIFE VESTS - INSTALLATION - HOOVER INDUSTRIES - BFE | *** |
2513B696E90 | MP - LOG BOOK HOLDER - RELOCATION - FROM SECOND OBSERVER'S SEAT LEGS TO AFT FACE OF P8 AISLESTAND | *** |
2513B696E96 | MP - FLIGHT COMPARTMENT ACCOMMODATIONS - INSTALLATION - FUEL CONVERSION PLACARD ON THE FACE OF CAPTAIN AND FIRST OFFICER'S CLIPBOARDS | *** |
P.A. No. 1810 A-3- 6 SA-61
2513C410C23 | MP - FLIGHT COMPARTMENT ACCOMMODATIONS - INSTALLATION - EMERGENCY EVACUATION CHECKLIST PLACARD ON THE CAPTAIN AND FIRST OFFICERS CONTROL COLUMNS | *** |
2520B642I61 | MP - GALLEY MAT REVISION - REVISION - BFE | *** |
2520B642N11 | MP - INTERIOR COLOR REVISION - AFT LEFTHAND CLOSET | *** |
2524A599A45 | DECO LAMINATE W/GRAPHIC FOR BFEWINDSCREEN | *** |
2524A694H23 | AFT CENTERLINE CLOSET REVISION FROMMISC STOWAGE TO TRASH STOWAGE | *** |
2524B643D06 | MP - FULL HEIGHT WINDSCREEN/CLOSET - AFT LH - REVISION - BFE | *** |
2525A599A17 | ECONO CLASS PASS SEATING-REV | *** |
2525B645F30 | MP - ECONOMY CLASS PASSENGER SEATS - REVISION - 3 INCH RECLINE IN LIEU OF 4 INCH RECLINE | *** |
2529A699A57 | ASSIST HANDLE-COLOR CHANGE | *** |
2529A802A85 | WARNING STRAP RING-COLOR CHANGE | *** |
2540C426C65 | MP - LA LAVATORY SELECTABLES - INSTALLATION - BABY CARE TABLE | *** |
2540C547C53 | MP - LA AND LB LAVATORIES - REVISION - ADD DEODRANT DISC BRACKET AND DELETE BAR SOAP AND PAPER CUP PROVISIONS | *** |
2560B696E74 | MP - CREW LIFE VESTS - INSTALLATION - FLIGHT DECK WITH SECOND OBSERVER - HOOVER INDUSTRIES P/N HS3701C-SWA - BFE | *** |
2566A802C31 | MP - ESCAPE SLIDES/COMPARTMENTS - CHANGE FROM BFE TO SFE - BF GOODRICH - INSTALLED | *** |
3041B458A01 | WINDOW HEAT CONTROL STANDARD BFE | *** |
3131A802B13 | D.F.D.A.U.-HONEYWELL-BFE | *** |
3133A150E33 | MP - INSTALLATION OF ARNIC 740 PRINTER PROVISIONS IN THE FLIGHT DECK AISLESTAND | *** |
3321A694H26 | COOL WHITE LIGHTS IN LIEU OF WARMWHITE PASSENGER CABIN | *** |
3321A802A50 | PASS CABIN LIGHTING-TRIM COLOR CHGE | *** |
3324C547B16 | MP - INFORMATION SIGNS - DEACTIVATION - PERMANENT SILKSCREENING OF NO SMOKING SYMBOL AND ADDITION IF KUFE VEST PLACARDING | *** |
3430B696D36 | MP - ILS/GPS MULTI-MODE RECEIVER (MMR) - REVISION - HONEYWELL MMR IN LEIU OF ALLIEDSIGNAL MMR - BFE | *** |
3436A150D47 | HEAD UP GUIDANCE SYS-INSTALL FLTDYNAMICS HGS COMPUTER | *** |
3436A599A59 | HEAD UP DISPLAY (HUD) PARTIAL PROVIS FOR CAT IIIA HGS 2350 FLT DYNAMIC | *** |
3436B572D13 | MP - HEAD UP DISPLAY (HUD) SYSTEM - REPLACEMENT - FLIGHT DYNAMICS PHASE 3 HGS4000 SYSTEM INTO EXISTING COMMON HUG PARTIAL PROVISIONS IN LIEU OF HGS2350 HUD SYSTEM - BFE | *** |
3445B363B10 | TRAFFIC ALERT & AVOIDANCE SYSTEM | *** |
3445B370E27 | MP - TCAS SYSTEM - REPLACEMENT - HONEYWELL TCAS COMPUTER - TCAS CHANGE 7 COMPLIANT - HONEYWELL - BFE | *** |
3446A561D04 | EGPWS-ACTIVATION-PEAKS & OBSTACLESFEATURE | |
3457B696A23 | ADF PARTIAL PROVS ILO SGL SYS | *** |
3461A051B70 | FMC COLOR CDU/MCDU OPERATION ENABLE | *** |
3461A150D31 | MP - FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - INSTALLATION OF DUAL FMC'S AND MCDU'S IN LIEU OF EXISTING DUAL FMC'S AND CDU'S - SFE | *** |
3461A150D32 | FMC SYS AIRLINE OPERATIOINALCOMMUNICATIONS DATA LINK | *** |
3910A150E36 | MP- AFT ELECTRONICS PANEL ARRANGEMENT-SOUTHWEST AIRLINES | *** |
5310A599A04 | RADOME-WEATHERMASTER-REV-EXT MKG | *** |
5352A599A07 | MP - RADOME INSTALL-REV-WEATHERMASTER UNPAINTED | *** |
7200B572C87 | MP - ENGINE - CFM56-7 ENGINES - 7B24 RATING IN LIEU OF 7B22 | *** |
MISC DOOR | FAA FLIGHT DECK DOOR | *** |
MISC/FAA4 | FLAME PROPAGATION - INSULATION BLANKETS | *** |
P.A. No. 1810 A-3- 7 SA-61
Total Additional Master Changes ***
2525C882G60 REPLACEMENT OF BFE B/E AEROSPACE PASSENGER SEATS***
Exhibit A-3 Total 60; ***
* One time Non-Recurring Price of ***will apply to the first Aircraft delivering in***.
P.A. No. 1810 A-3- 8 SA-61