EXHBIT 10.1 SUPPLEMENTAL AGREEMENT NO. 61
Published on October 20, 2008
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
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 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 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
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
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
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
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
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
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 602-4183
|
***
|
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
***
* One time Non-Recurring Price of ***will apply to the first Aircraft
delivering in***.
P.A.
No. 1810
A-3- 8
SA-61