EX-10.2 3 exhibit102sa-17topax3729re.htm EX-10.2 BOEING SUPPLEMENTAL AGREEMENT NO. 17 Document


SUPPLEMENTAL AGREEMENT NO. 17
to
PURCHASE AGREEMENT NO. 03729
between
THE BOEING COMPANY
and
SOUTHWEST AIRLINES CO.
Relating to Boeing Model 737-8 and 737-7 Aircraft

THIS SUPPLEMENTAL AGREEMENT NO. 17 (SA-17), entered into as of June 3, 2022, is made between THE BOEING COMPANY, a Delaware corporation (Boeing), and SOUTHWEST AIRLINES CO., a Texas corporation (Customer).
RECITALS:
WHEREAS, Customer and Boeing entered into Purchase Agreement Number PA-03729 dated December 13, 2011 (as amended and supplemented, Purchase Agreement) relating to the purchase and sale of Boeing model 737-8 (737-8 Aircraft) and model 737-7 aircraft (737-7 Aircraft) (737-8 Aircraft and 737-7 Aircraft collectively, the “Aircraft”). This SA-17 is an amendment to and is incorporated into the Purchase Agreement. Capitalized terms used herein but not otherwise defined will have the meaning set forth in the Purchase Agreement; and
WHEREAS, Customer and Boeing agree to incorporate into the Remarket Aircraft documents the amendments and additions to certain Letter Agreements and Exhibits provided in this SA-17.

NOW, THEREFORE, the parties agree that the Purchase Agreement is amended as set forth below and otherwise agree as follows:

1.TABLE OF CONTENTS.

The Table of Contents of the Purchase Agreement is hereby deleted in its entirety and replaced by a new Table of Contents (attached), which lists the Tables, Exhibits, and Letter Agreements revised or added by this SA-17 and is identified by “SA-17”. Such revised Table of Contents is incorporated into the Purchase Agreement by this reference.
[***] = Certain identified information has been excluded from the exhibit because it is both not material and is of the type that the registrant treats as private or confidential.

SWA-PA-03729
1
SA-17
BOEING PROPRIETARY



2.TABLES.

There are no changes to the Tables as a result of this SA-17.

3.LETTER AGREEMENTS.

3.1.Letter Agreement No. SWA-PA-03729-LA-2100594 entitled 737-8 Remarket Aircraft, is hereby deleted in its entirety and replaced by Letter Agreement No. SWA-PA-03729-LA-2100594R1.

3.2.Letter Agreement No. SWA-PA-03729-LA-2100700 entitled Remarket Aircraft – Open Matters, is hereby deleted in its entirety and replaced by Letter Agreement No. SWA-PA-03729-LA-2100700R1 entitled Remarket Aircraft – Configuration Matters.


4.EXHIBITS.
4.1.New Exhibit A-3, “Supplemental Aircraft Delivery Configuration”, is attached hereto and incorporated into the Purchase Agreement by this reference, containing the aircraft configuration for the modified Remarket Aircraft.

4.2.The Exhibit B-1, “Remarket Aircraft Technical Acceptance and Delivery Requirements and Responsibilities” is hereby deleted in its entirety and replaced by a new Exhibit B-1 (identified by “SA-17”) attached hereto and incorporated into the Purchase Agreement by reference.

5.[***] IMPACT.

There are no impacts to [***] as a result of this SA-17.


The Purchase Agreement is amended and supplemented to the extent herein provided and as so amended and supplemented will continue in full force and effect.


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

THE BOEING COMPANYSOUTHWEST AIRLINES CO.
By:     /s/Carson J. May
By:    /s/ Chris Monroe
Name: Carson J. May
Name: Chris Monroe
Its:     Attorney-In-Fact
Its:    SVP Finance and Treasurer
SWA-PA-03729
2
SA-17
BOEING PROPRIETARY



TABLE OF CONTENTS
ARTICLESTITLES
Article 1Quantity, Model and DescriptionSA-2
Article 2Delivery Schedule
Article 3Price
Article 4PaymentSA-2
Article 5Additional Terms
TABLETITLE
1A737-8 Aircraft Information TableSA-16
1B737-7 Aircraft Information TableSA-16
EXHIBIT
A1737-8 Aircraft ConfigurationSA-11
A2737-7 Aircraft ConfigurationSA-8
A-3737-8 Remarket Aircraft Configuration
SA-17
B*Aircraft Delivery Requirements and Responsibilities
B-1Remarket Aircraft TechnicalSA-17
Acceptance and Delivery Requirements and Responsibilities
SUPPLEMENTAL EXHIBITSTITLES
AE1*Escalation Adjustment/Airframe and Optional Features
BFE1BFE Variables for 737-8SA-7
BFE2BFE Variables for 737-7SA-8
CS1Customer Support Variables
CS1-7MAXCustomer Support VariablesSA-2
EE1*Engine Escalation/Engine Warranty and Patent Indemnity
SWA-PA-03729SA-17
Page 1
BOEING PROPRIETARY



SLP1*Service Life Policy Components
LETTER AGREEMENTSTITLES
SWA-PA-03729-LA-1106463R3Open MattersSA-8
SWA-PA-03729-LA-1106464*[***]
SWA-PA-03729-LA-1106465*[***]
SWA-PA-03729-LA-1106466[***]
SWA-PA-03729-LA-1106467R2[***]SA-8
SWA-PA-03729-LA-1106468*[***]
SWA-PA-03729-LA-1106469R1[***]SA-2
SWA-PA-03729-LA-1106470R1[***]SA-2
SWA-PA-03729-LA-1106471R2Substitute AircraftSA-12
SWA-PA-03729-LA-1106473R2[***]SA-12
SWA-PA-03729-LA-1106474R7Option AircraftSA-16
SWA-PA-03729-LA-1106475R5[***]SA-14
SWA-PA-03729-LA-1106476R2[***]SA-8
SWA-PA-03729-LA-1106477*[***]
SWA-PA-03729-LA-1106478[***]
SWA-PA-03729-LA-1106479R1[***]SA-2
SWA-PA-03729-LA-1106480R1[***]SA-2
SWA-PA-03729-LA-1106481R2[***]SA-2
SWA-PA-03729-LA-1106482*[***]
SWA-PA-03729-LA-1106483*[***]
SWA-PA-03729-LA-1106484R3[***]
SA-16
SWA-PA-03729-LA-1106485*[***]

SWA-PA-03729SA-17
Page 2
BOEING PROPRIETARY




LETTER AGREEMENTSTITLES
SWA-PA-03729-LA-1209080[***]SA-1
SWA-PA-03729-LA-1210419[***]SA-1
SWA-PA-03729-LA-1300943[***]SA-2
SWA-PA-03729-LA-1301168R3[***]SA-6
SWA-PA-03729-LA-1301170R3[***]SA-12
SWA-PA-03729-LA-1400371[***]SA-7
SWA-PA-03729-LA-1503792Service Ready Operational ValidationSA-6
SWA-PA-03729-LA-1500831[***]SA-7
SWA-PA-03729-LA-1602486R1[***]SA-12
SWA-PA-03729-LA-2100594R1
737-8 Remarket Production AircraftSA-17
SWA-PA-03729-LA-2100700R1
737-8 Configuration Matters – Remarket Production AircraftSA-17
SWA-PA-03729-LA-2100811[***]SA-12
SWA-PA-03729-LA-2100812R1[***]SA-16
SWA-PA-03729-LA-2100813[***]SA-12
SWA-PA-03729-LA-2100814R1[***]SA-15
SWA-PA-03729-LA-2100819[***]SA-12
SWA-PA-03729-LA-2100825R1[***]SA-16
SWA-PA-03729-LA-2100841[***]SA-12
SWA-PA-03729-LA-2100984[***]SA-12
SWA-PA-03729-LA-21037552022/2023 Production PlanSA-16
* Denotes revision to Page 1 or Page 2 only to reference 737-7 (SA-2)

SWA-PA-03729SA-17
Page 3
BOEING PROPRIETARY




INACTIVE / DELETED TABLES, EXHIBITS, AND LETTER AGREEMENTS

RESTRICTED LETTER AGREEMENTS

Letter AgreementTitleLast Updated under SACurrent Status
SWA-PA-03729-LA-1106472R1[***]SA-2Deleted under SA-4
SWA-PA-01810/03729-LA-1301169[***]SA-2Deleted under SA-4

SWA-PA-03729SA-17
Page 4
BOEING PROPRIETARY



SUPPLEMENTAL AIRCRAFT DELIVERY CONFIGURATION
between
THE BOEING COMPANY
and
SOUTHWEST AIRLINES CO
EXHIBIT A-3 to PURCHASE AGREEMENT
NUMBER PA-03729

Page 1
BOEING PROPRIETARY

EXHIBIT A-3
SUPPLEMENTAL AIRCRAFT DELIVERY CONFIGURATION
DATED JUNE 3, 2022
relating to
BOEING MODEL 737-8 AIRCRAFT

The As-Built Configuration of the aircraft with effectivities of 1C691, 1C692-1C694, 1C511-1C513, and 1C514-1C517 (Aircraft) is described in Exhibit A-3. The “Delivery Configuration” of the Aircraft will be comprised of Exhibit A with incorporation of the Master Change Kits (MKs) of this Supplemental Configuration Exhibit A-3 listed below.
A “Delivery Detail Specification” will be provided describing the Delivery Configuration of the Aircraft comprised of Detail Specification D019A008SWA18P-5-(insert MSN: 60186, 60188, 60187, 60219, 60223, 60225, 60226, 60650, 60649, 60652, or 60653) (As-Built Configuration), as amended to incorporate the MKs listed below; including the effects on Manufacturer's Empty Weight (MEW) and Operating Empty Weight (OEW). As soon as practicable, Boeing will provide to Customer the Delivery Detail Specification. [***]



























SWA-PA-03729-EX A-3SA-17
Page 2
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
0110-000030MAJOR MODEL 737 AIRPLANEAcceptedAcceptedAcceptedAccepted
0110E131A08MINOR MODEL 737-8 AIRPLANEAcceptedAcceptedAcceptedAccepted
0160F303C15AIRPLANE IDENTIFICATION INFORMATION - TCI/ROJ - 1C511--Accepted-
0160F350A37AIRPLANE IDENTIFICATION INFORMATION - CDX/ROJ - 1C691Accepted---
0160F350B74AIRPLANE IDENTIFICATION INFORMATION - CDX/ROJ - 1C692-Accepted--
0160F350F09RR 97283-24 - AIRPLANE IDENTIFICATION NUMBERS - CDX/ROJ - 1C691Accepted---
0160F351A40AIRPLANE IDENTIFICATION INFORMATION - ROJ - 1C514---Accepted
0170B401A73CLIMATE - NORMAL WEATHER OPERATIONSAcceptedAcceptedAcceptedAccepted
0170B871A31GALLEY AFT COMPLEX - G4B GALLEY - DOMED AFT BULKHEAD (BASELINE)AcceptedAcceptedAcceptedAccepted
0170D387A08AVIONICS - DUAL FMC WITH MULTI-CONTROL DISPLAY UNITAcceptedAcceptedAcceptedAccepted
0170D837A13FLEXIBLE CERTIFICATIONAcceptedAcceptedAcceptedAccepted
0170E432100PC - FORWARD COMPLEX - ADVANCED LAVATORY WITH MINIMUM GALLEY CAPACITY AND WITHOUT CURTAIN AND CURTAIN TRACK - 737 BOEING SKY INTERIORAcceptedAcceptedAcceptedAccepted
0170E432101PC - LAVATORY AFT COMPLEX - TWO ADVANCED LAVATORIES WITH TWO DOUBLE ATTENDANT SEATS AND NO CURTAIN AND CURTAIN TRACKAcceptedAcceptedAcceptedAccepted
0170E516A14COMMUNICATIONS - BASIC COMMUNICATIONS CONFIGURATION WITH HFAcceptedAcceptedAcceptedAccepted
0170E526A94LAVATORY AFT COMPLEX - TWO ADVANCED LAVATORIES WITH TWO DOUBLE ATTENDANT SEATSAcceptedAcceptedAcceptedAccepted
0170E568H37FLIGHT COMPARTMENT - ONE OBSERVER WITH 2-BTP FIRE EXTINGUISHERAcceptedAcceptedAcceptedAccepted
0170E656A04AIRFRAME - 737-8AcceptedAcceptedAcceptedAccepted
0170E806A23CARGO LINERS- HEAVY DUTY - FORWARDAcceptedAcceptedAcceptedAccepted
0170E806A26CARGO LINERS- HEAVY DUTY- AFTAcceptedAcceptedAcceptedAccepted
SWA-PA-03729-EX A-3SA-17
Page 3
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
0170E895B97FORWARD COMPLEX - ADVANCED LAVATORY WITH MINIMUM GALLEY CAPACITY - BOEING SKY INTERIORAcceptedAcceptedAcceptedAccepted
0220E684A09TYPE CERTIFICATE & CERTIFICATE OF AIRWORTHINESSAcceptedAcceptedAcceptedAccepted
0220F350K72MP - TYPE CERTIFICATE & CERTIFICATE OF AIRWORTHINESS - REVISE COUNTRY OF REGISTRATION AND OPERATION - USA IN LIEU OF INDIAAcceptedAcceptedAcceptedAccepted
0221-000026TAKEOFF AND LANDING WITH TAILWIND UP TO 15 KNOTSAcceptedAcceptedAcceptedAccepted
0221A609B52DISPATCH WITH GEAR EXTENDED FOR REVENUE FLIGHTAcceptedAcceptedAcceptedAccepted
0221C483C66ENGINE INOPERATIVE TEN-MINUTE TAKEOFF THRUST OPERATIONAcceptedAcceptedAcceptedAccepted
0224E173A44EXTENDED OPERATIONS (ETOPS) - APU ON DEMANDAcceptedAcceptedAcceptedAccepted
0226-000007CATEGORY IIIA AUTOMATIC APPROACH AND LANDINGAcceptedAcceptedAcceptedAccepted
0226C594A32GNSS LANDING SYSTEM (GLS) - CATEGORY I APPROACH CAPABILITY - ACTIVATIONAcceptedAcceptedAcceptedAccepted
0228E437G77AIRPLANE FLIGHT MANUALAcceptedAcceptedAcceptedAccepted
0252B299A36INSTRUMENTATION, AIRPLANE MANUALS AND FUEL MEASURING STICKS IN METRIC UNITS - TEMPERATURE IN DEGREES CELSIUSAcceptedAcceptedAcceptedAccepted
0253F288A03MP - BUYER FURNISHED EQUIPMENT - PROCUREMENT REVISION - SPE TO BFEAcceptedAccepted--
0254-000003USPHS CERTIFICATE OF SANITARY CONSTRUCTIONAcceptedAcceptedAcceptedAccepted
0315E591E95CERTIFIED OPERATIONAL WEIGHTS AND STRUCTURAL DESIGN WEIGHTSAcceptedRejectedAcceptedAccepted
0315F214J32RR 97283-23 - OPERATIONAL WEIGHTS - REVISION - DECREASE MLW, MTOW, AND MZFW - 1C691Accepted---
0315F263A22CERTIFIED OPERATIONAL WEIGHTS AND STRUCTURAL DESIGN WEIGHTS-Accepted--
0315F263A26MP - CERTIFIED OPERATIONAL WEIGHTS AND STRUCTURAL DESIGN WEIGHTS - REVISION-Accepted--
SWA-PA-03729-EX A-3SA-17
Page 4
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
0315F802A76RR 97029-284 - OPERATIONAL WEIGHTS - REVISION - INCREASE OPERATIONAL WEIGHTSAcceptedAcceptedRejected-
0352-000002CUSTOMIZED LOADING SCHEDULE FOR WEIGHT & BALANCE CONTROL - ALIGNMENT CHART LOADINGAcceptedAcceptedAcceptedAccepted
0352F816A42RR 97029-295 - DELETION OF CUSTOMIZED LOADING SCHEDULE FOR WEIGHT AND BALANCE CONTROL - ALIGNMENT CHART LOADINGAcceptedAcceptedAcceptedAccepted
1110E432048EXTERIOR NON-REGULATORY MARKINGSAcceptedAcceptedAcceptedAccepted
1110E432049EXTERIOR REGULATORY MARKINGS AND COLOR SCHEMEAcceptedAcceptedAcceptedAccepted
1110F802A71RR 97029-283 - EXTERIOR COLOR SCHEMES AND MARKINGS - REPLACEMENT - SOUTHWEST AIRLINES WINGLETS IN LIEU OF EXISTINGAcceptedAccepted--
1110F802A82RR 97029-285 - EXTERIOR COLOR SCHEMES AND MARKINGS -REPLACEMENT - SOUTHWEST AIRLINES ETOPS LIVERY IN LIEU OF SPICE JET AIR LIVERY - SWA - SAME LIVERY AS SWA 1A070AcceptedAcceptedAcceptedAccepted
1110F802A86RR 97029-283 - EXTERIOR COLOR SCHEMES AND MARKINGS - REPLACEMENT - SOUTHWEST AIRLINES WINGLETS IN LIEU OF EXISTING--AcceptedAccepted
1130E432053INTERIOR PLACARDS AND MARKERSAcceptedAcceptedAcceptedAccepted
1130E559D12CARGO COMPARTMENT PLACARDSAcceptedAcceptedAcceptedAccepted
1130E666A17REGISTRY PLACARDAcceptedRejectedAcceptedRejected
1130E970B73LIGHTED SIGNSAcceptedAcceptedAcceptedAccepted
1130F211A25PRR 3M0179 - 737 MAX OWNERSHIP PLACARD IMPRINTING PRODUCTION IMPROVEMENT-Accepted-Accepted
1130F211A26PRR 3M0179 - 737 MAX REGISTRY PLACARD IMPRINTING PRODUCTION IMPROVEMENT-Accepted-Accepted
1130F214J42RR 97260-22 - REVISE OWNERSHIP PLACARDS - 1C511--Accepted-
1130F303C16OWNERSHIP PLACARDS--Accepted-
SWA-PA-03729-EX A-3SA-17
Page 5
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
1130F350A38OWNERSHIP PLACARDSAccepted---
1130F350L12RR 97029-292 - DELETION - OWNERSHIP & REGISTRY PLACARDS - ENGINES, FLIGHT DECK, ENTRY DOOR SILL, AND REGISTRY-Accepted--
1130F350L13RR 97029-291 - DELETION - OWNERSHIP & REGISTRY PLACARDS - ENGINES, FLIGHT DECK, ENTRY DOOR SILL, AND REGISTRYAccepted---
1130F424A01OWNERSHIP PLACARD - AUXILIARY POWER UNIT (APU)-Canceled-Accepted
1130F424A02OWNERSHIP PLACARD - ENGINES-Accepted-Accepted
1130F424A03OWNERSHIP PLACARD - FLIGHT COMPARTMENT-Accepted-Accepted
1130F424A04OWNERSHIP PLACARD - FORWARD LH OVERHEAD DOOR SILL-Accepted-Accepted
1130F424A05REGISTRY PLACARD-Accepted-Accepted
1130F802A78RR 97029-287 - DELETION - OWNERSHIP & REGISTRY PLACARDS- ENGINES, APU, FLIGHT DECK, ENTRY DOOR SILL, AND REGISTRY--Accepted-
1130F802A80RR 97029-289 - DELETION - OWNERSHIP & REGISTRY PLACARDS- ENGINES, APU, FLIGHT DECK, ENTRY DOOR SILL, AND REGISTRY---Accepted
2103D839A04AC HEAT EXCHANGER OUTLET TEMPERATURE MONITORING SENSOR - INSTALLATIONAcceptedAcceptedAcceptedAccepted
2130-000010600 FPM CABIN PRESSURE ASCENT RATEAcceptedAcceptedAcceptedAccepted
2130-000012350 FPM CABIN PRESSURE DESCENT RATEAcceptedAcceptedAcceptedAccepted
2158D839A20ELECTRONIC RACK COOLING SYSTEM - ENHANCED E6 RACKAcceptedAcceptedAcceptedAccepted
2160C703A76CABIN TEMPERATURE CONTROL SYSTEM WITH ATTENDANT PANEL ADJUSTMENT CAPABILITY - 737 BOEING SKY INTERIORAcceptedAcceptedAcceptedAccepted
2170-000021OZONE CONTROL - SPACE PROVISIONS FOR CATALYTIC CONVERTERSAcceptedAcceptedAcceptedAccepted
SWA-PA-03729-EX A-3SA-17
Page 6
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
2210-000003AUTOFLIGHT - INHIBIT GLIDE SLOPE CAPTURE PRIOR TO LOCALIZER CAPTUREAcceptedAcceptedAcceptedAccepted
2210-000124AUTOFLIGHT - FLIGHT DIRECTOR TAKEOFF MODE HEADING SELECTAcceptedAcceptedAcceptedAccepted
2210-000128AUTOFLIGHT - CONTROL WHEEL STEERING WARNINGAcceptedAcceptedAcceptedAccepted
2210-000130AUTOFLIGHT - AIRSPEED DEVIATION WARNINGAcceptedAcceptedAcceptedAccepted
2210-000143AUTOFLIGHT - ALTITUDE ALERT - 200/900 FEETAcceptedAcceptedAcceptedAccepted
2210C175A38AUTOFLIGHT - GO-AROUND ROLL MODE - LNAVAcceptedAcceptedAcceptedAccepted
2230-000137AUTOTHROTTLE - FMCS - TAKEOFF PROFILE THRUST REDUCTION ALTITUDEAcceptedAcceptedAcceptedAccepted
2310B401A33COMMUNICATIONS CONTROL PANELS - TRIPLE GABLES RADIO TUNING PANELS CAPABLE OF TWO HF SYSTEMS AND THREE VHF SYSTEMS (8.33 KHZ CAPABLE) - P/N G7404-124 - BFE/SPEAcceptedAcceptedAcceptedAccepted
2311B401A05HF COMMUNICATIONS - COMPLETE PROVISIONS FOR THE SECOND HF SYSTEMAcceptedAcceptedAcceptedAccepted
2311B401A38HF COMMUNICATIONS - EQUIPMENT INSTALLATION OF SINGLE COLLINS AEROSPACE HF VOICE/DATA TRANSCEIVER - P/N 822-0990-004 - AND DIGITAL HF COUPLER - P/N 822-0987-004 BFE/SPEAcceptedAcceptedAcceptedAccepted
2312-000703VHF COMMUNICATIONS - ACTIVATION OF 8.33 KHZ CHANNEL SPACINGAcceptedAcceptedAcceptedAccepted
2312B401A87VHF COMMUNICATIONS - EQUIPMENT INSTALLATION OF TRIPLE COLLINS AEROSPACE ARINC 750 VHF-2100 TRANSCEIVERS WITH 8.33 KHZ CHANNEL SPACING, VDL MODE 2, AND CMC INTERFACE CAPABILITY - P/N 822-1287-101 - BFE/SPEAcceptedAcceptedAcceptedAccepted
2315E516A58SATCOM - PARTIAL WIRING AND MOUNTING PROVISIONS - L-BAND FLIGHT DECK CONNECTIVITY USING INMARSAT SB200 OR IRIDIUM CERTUSAcceptedAccepted--
SWA-PA-03729-EX A-3SA-17
Page 7
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
2315F197A45MP - SATCOM - INSTALLATION OF PARTIAL WIRING AND MOUNTING PROVISIONS - L-BAND FLIGHT DECK CONNECTIVITY USING INMARSAT SB200 OR IRIDIUM CERTUSAcceptedAccepted--
2321-000063SELCAL - ANNUNCIATION ON AUDIO SELECTOR PANELSAcceptedAcceptedAcceptedAccepted
2321B401A04SELCAL - AVTECH FIVE CHANNEL DECODER - P/N NA138-714C - BFE/SPEAcceptedAcceptedAcceptedAccepted
2322C939A06COMMUNICATIONS MANAGEMENT UNIT (CMU) - DATA LINK RECORDING ACTIVATIONAcceptedAcceptedAcceptedAccepted
2322D347A73CMU - INSTALLATION OF ROCKWELL COLLINS ARINC 758 LEVEL AOA CMU W/ARINC SERVICE PROVIDER - DATA LINK RECORDING CAPABLE - P/N 822-1239-151 - BFE / SPEAcceptedAcceptedAcceptedAccepted
2322E516A28CMU - INSTALLATION OF PARTIAL PROVISIONS FOR A SINGLE CMU IN ACCORDANCE WITH ARINC 758AcceptedAcceptedAcceptedAccepted
2324D197A18EMERGENCY LOCATOR TRANSMITTER (ELT) - ACR ELECTRONICS AUTOMATIC FIXED - WITH NAVIGATION INTERFACE UNIT (NIU) - MODE S BROADCAST - WITH ANTENNA P/N 110-337 - BFE/SPEAcceptedAcceptedAcceptedAccepted
2324E706G43MP - LOW FREQUENCY UNDERWATER LOCATOR DEVICE (LF-ULD) - 8.8 KHZ - INSTALLATIONAcceptedAcceptedAcceptedAccepted
2324E773A11LOW FREQUENCY UNDERWATER LOCATOR DEVICE - 8.8 KHZAcceptedAcceptedAcceptedAccepted
2331-000558PA MIC INSTALLATION IN FLIGHT DECK AT AFT END OF AISLESTANDAcceptedAcceptedAcceptedAccepted
2331B754B15PASSENGER ADDRESS (PA) SYSTEM - ARINC 715 - COLLINS AEROSPACE AMPLIFIER - BFE/SPEAcceptedAcceptedAcceptedAccepted
2331B754B17PASSENGER ADDRESS (PA) SYSTEM - PA-IN-USE INDICATOR IN THE FLIGHT DECKAcceptedAcceptedAcceptedAccepted
2331E097A10PRAM/BMM SYSTEM - PANASONIC - FASTEN SEAT BELT/DECOMPRESSION DISCRETES ACTIVATED - BFE/SPEAcceptedAcceptedAcceptedAccepted
SWA-PA-03729-EX A-3SA-17
Page 8
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
2350B872A08AUDIO CONTROL PANEL - INTEGRATED SELCAL, CREW CALL, AND SATCOM FUNCTIONS - INSTALLATION - 3 VHF/2 HFAcceptedAcceptedAcceptedAccepted
2351-000034HAND HELD MICROPHONE - CAPTAIN AND FIRST OFFICER - ELECTROVOICE - P/N 903-1341 - BFE/SPEAcceptedAcceptedAcceptedAccepted
2351-000036HAND HELD MICROPHONE - FIRST OBSERVER - ELECTROVOICE - P/N 903-1341 - BFE/SPEAcceptedAcceptedAcceptedAccepted
2351-000043CONTROL WHEEL PUSH TO TALK (PTT) SWITCH - THREE POSITION WITH DETENT IN INTERPHONE POSITIONAcceptedAcceptedAcceptedAccepted
2351A213A33AUDIO INTEGRATION - INSTALLATION - TWO-PLUG AUDIO JACKS IN THE FLIGHT DECKAcceptedAcceptedAcceptedAccepted
2371A083A49VOICE RECORDER MICROPHONE/MONITOR PANEL WIRING - BULK ERASE FUNCTION DISABLEDAcceptedAcceptedAcceptedAccepted
2371B628B41VOICE RECORDER - RECORDER INDEPENDENT POWER SUPPLY (RIPS) - AFT LOWERED CEILINGAcceptedAcceptedAcceptedAccepted
2371B696P48COCKPIT VOICE RECORDER - MANUAL(ON) / AUTO(OFF) SWITCH INSTALLATION COMPATIBLE WITH CVR RECORDER INDEPENDENT POWER SUPPLY (RIPS) INSTALLATIONAcceptedAcceptedAcceptedAccepted
2371E716A13VOICE RECORDER AND MICROPHONE/MONITOR - L-3 AVIATION PRODUCTS - 2 HOUR RECORDING TIME - WITH DATALINK RECORDING CAPABILITY - P/N 2100-1925-22 & P/N S152-0020-01 - BFE/SPEAcceptedAcceptedAcceptedAccepted
2371F816A45RR 97029-286 - REPLACE COCKPIT VOICE RECORDER (CVR), CVR CONTROL PANEL, AND DIGITAL FLIGHT DATA RECORDER (DFDR)--AcceptedAccepted
2371F816A48RR 97029-294 - REPLACE COCKPIT VOICE RECORDER (CVR), CVR CONTROL PANEL, AND DIGITAL FLIGHT DATA RECORDER (DFDR) - BFEAcceptedAccepted--
SWA-PA-03729-EX A-3SA-17
Page 9
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
2375E526A61FLIGHT DECK ENTRY VIDEO SURVEILLANCE SYSTEM - PARTIAL PROVISIONS FOR THREE-CAMERA SYSTEMS - MDS INTERFACEAcceptedAcceptedAcceptedAccepted
2375E526A63FLIGHT DECK ENTRY VIDEO SURVEILLANCE SYSTEM - INSTALLATION INTO PARTIAL PROVISIONS - MDS INTERFACE - COLLINS AEROSPACE - BFE/SPEAcceptedAcceptedAcceptedAccepted
2375E861K81MP - VIDEO SURVEILLANCE SYSTEM - REVISION - GOODRICH IN LIEU OF AD AEROSPACE SYSTEM - GOODRICH - SPEAcceptedAcceptedAcceptedAccepted
2451B815K32POWER DISTRIBUTION - WIRING INSTALLATION FOR ADDITIONAL CAPACITYAcceptedAcceptedAcceptedAccepted
2520E432055INTERIOR COLOR AND MATERIAL - STANDARD OFFERINGAcceptedAcceptedAcceptedAccepted
2520F158A43INTERIOR COLOR AND MATERIAL - CUSTOM - ATTENDANT SEAT UPHOLSTERY AND SEAT BELTAcceptedAcceptedAcceptedAccepted
2520F158A44MP - INTERIOR COLOR AND MATERIAL - REVISION - ATTENDANT SEAT UPHOLSTERY AND SEAT BELTAcceptedAcceptedAcceptedAccepted
2523E432056PASSENGER SERVICE UNITS - 737 BOEING SKY INTERIORAcceptedAcceptedAcceptedAccepted
2524E432058FORWARD LEFT HAND FULL HEIGHT WINDSCREEN WITH STOWAGE UNIT - BOEING SKY INTERIORAcceptedAcceptedAcceptedAccepted
2525C204K04HIC AND FEMUR LOAD COMPLIANCE - ECONOMY CLASS SEATSAcceptedAcceptedAcceptedAccepted
2525C204K05HIC AND FEMUR LOAD COMPLIANCE - ATTENDANT SEATSAcceptedAcceptedAcceptedAccepted
2525F198C28MP - PASSENGER COMPARTMENT SEATS - REPLACEMENT - RECARO IN LIEU OF LIFT BY ENCORE - SPEAcceptedAcceptedAcceptedAccepted
2525F198D47ECONOMY CLASS SEATS - BFE/SPEAcceptedAcceptedAcceptedAccepted
2525F198D48MP - PASSENGER SEATS - REVISION - ROW 4, RIGHT HAND, PREMIUM ECONOMY IN LIEU OF ECONOMY - SPEAcceptedAcceptedAcceptedAccepted
2525F288A13MP - PASSENGER COMPARTMENT SEATS - PROCUREMENT - REVISION - SPE TO BFEAcceptedAccepted--
SWA-PA-03729-EX A-3SA-17
Page 10
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
2527F198D45FLOOR COVERING - CARPET - BFE/SPEAcceptedAcceptedAcceptedAccepted
2527F198D46MP - FLOOR COVERING - INSTALLATION - CARPET - MOHAWK - SPEAcceptedAcceptedAcceptedAccepted
2528E432061OVERHEAD STOWAGE BINS - 737 BOEING SKY INTERIORAcceptedAcceptedAcceptedAccepted
2528E432066CHECKLIST HOLDER INSTALLATION - LAVATORIES A, D AND EAcceptedAcceptedAcceptedAccepted
2528E934H13LITERATURE POCKET - 787 STYLEAcceptedAcceptedAcceptedAccepted
2530E432067GALLEY PART NUMBERS - STANDARD EFFORT - BFE/SPEAcceptedAcceptedAcceptedAccepted
2530F198B83GALLEY INSERT PART NUMBERS - BFE/SPEAcceptedAcceptedAcceptedAccepted
2530F198B84MP - GALLEY INSERTS - REPLACEMENT - WATER BOILER - ZODIAC - SPEAcceptedAcceptedAcceptedAccepted
2540E432069LA ADVANCED LAVATORY 2.0 SELECTABLESAcceptedAcceptedAcceptedAccepted
2540E432070LD ADVANCED LAVATORY 2.0 SELECTABLESAcceptedAcceptedAcceptedAccepted
2540E432071LE ADVANCED LAVATORY 2.0 SELECTABLESAcceptedAcceptedAcceptedAccepted
2560B693L40FLASHLIGHTS WITH SHIELDS, TWO - FLIGHT DECK - DME - LED - P/N P2-07-0015-002 - BFE/SPEAcceptedAcceptedAcceptedAccepted
2560E097A48PROTECTIVE GLOVES - FLIGHT DECK - TIGHITCO - BFE/SPEAcceptedAcceptedAcceptedAccepted
2560E526B32PROTECTIVE BREATHING EQUIPMENT - FLIGHT DECK - SECOND OBSERVERS SEAT STANCHIONS - COLLINS AEROSPACE - P/N E28180-20-0006 - BFE/SPEAcceptedAcceptedAcceptedAccepted
2560F197A06CREW LIFE VESTS - FLIGHT DECK, NO SECOND OBSERVER - SWITLIK P/N S-61850-7409-SPJ112 - BFE/SPEAcceptedAcceptedAcceptedAccepted
2560F197A07MP - CREW LIFE VESTS - REPLACEMENT - FLIGHT DECK, NO SECOND OBSERVER - SWITLIK P/N S-61850-7409-SPJ112 IN LIEU OF EASTERN AERO MARINE P/N P01074-101WC - SPEAcceptedAcceptedAcceptedAccepted
SWA-PA-03729-EX A-3SA-17
Page 11
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
2560F197A40MP - PROTECTIVE BREATHING EQUIPMENT - REPLACEMENT - SECOND OBSERVER'S SEAT STANCHIONS - B E AEROSPACE SYSTEMS GMBH - P/N E28180-20-0006 IN LIEU OF BE AEROSPACE - P/N 119003-21 - SPEAcceptedAcceptedAcceptedAccepted
2562F198D76OVERWATER EMERGENCY EQUIPMENT - BFE/SPE - 737 BOEING SKY INTERIORAcceptedAcceptedAcceptedAccepted
2562F198D81MP - OVERWATER EMERGENCY EQUIPMENT - REPLACEMENT - PORTABLE ELT AND BRACKET - HONEYWELL - SPE--AcceptedAccepted
2562F198D82MP - OVERWATER EMERGENCY EQUIPMENT - REPLACEMENT - PORTABLE ELT AND BRACKET - HONEYWELL - BFEAcceptedAccepted--
2564E432204DETACHABLE EMERGENCY EQUIPMENT - PASSENGER COMPARTMENT - BFE/SPE - 737 BOEING SKY INTERIORAcceptedAcceptedAcceptedAccepted
2622E088A14APU FIRE EXTINGUISHER BOTTLE - COMMON WITH ENGINE BOTTLESAcceptedAcceptedAcceptedAccepted
2841-000004STANDARD FUEL SYSTEM ACCURACY - NO FUEL DENSITOMETERSAcceptedAcceptedAcceptedAccepted
2841-000011FUEL QUANTITY PRESELECT CAPABILITY ON RIGHT WING FUELING PANELAcceptedAcceptedAcceptedAccepted
2911-000042ENGINE-DRIVEN HYDRAULIC PUMPS WITH VESPEL SPLINE - EATON (VICKERS) - 10-62167AcceptedAcceptedAcceptedAccepted
2912E704A20AC MOTOR-DRIVEN HYDRAULIC PUMPS - EATON (VICKERS) - S276A100AcceptedAcceptedAcceptedAccepted
3041-000003NO HEATED FLIGHT COMPARTMENT NUMBER 3 WINDOWAcceptedAcceptedAcceptedAccepted
3131-000143ACCELEROMETER - HONEYWELL P/N 971-4193-001 - BFE/SPEAcceptedAcceptedAcceptedAccepted
3131E103A15DIGITAL FLIGHT DATA ACQUISITION UNIT (DFDAU) - CATIIIB/IAN/GLS/NPS CAPABLE - WITH ACMS CAPABILITY - ONS - SFEAcceptedAcceptedAcceptedAccepted
SWA-PA-03729-EX A-3SA-17
Page 12
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
3131E716A09DIGITAL FLIGHT DATA RECORDER (DFDR) - L-3 AVIATION PRODUCTS - 1024 WORD PER SECOND MAXIMUM DATA RATE P/N 2100-4945-22 - BFE/SPEAcceptedAcceptedAcceptedAccepted
3133-000123ARINC 740 PRINTER PROVISIONS IN THE FLIGHT DECK AISLESTANDAcceptedAcceptedAcceptedAccepted
3133E568J10MULTI-INPUT PRINTER -ARINC 740 - ASTRONOVA - P/N 42907100 - BFE/SPEAcceptedAcceptedAcceptedAccepted
3133F183C90MP - FLIGHT COMPARTMENT PRINTER - PROCUREMENT REVISION - BFE TO SPE---Accepted
3133F197A31MP - MULTI-INPUT PRINTER - ARINC 740 - INSTALLATION INTO PARTIAL PROVISIONS - ASTRONOVA - P/N 42907100 - BFEAcceptedAcceptedAcceptedAccepted
3133F288A02MP - FLIGHT COMPARTMENT PRINTER - PROCUREMENT - REVISION - BFE TO SPEAcceptedAccepted--
3135E526B33ONBOARD NETWORK SYSTEM - QUICK ACCESS RECORDER - DAR OUTPUTAcceptedAcceptedAcceptedAccepted
3161-000070ENGINE OIL QUANTITY DISPLAY - QUARTS - ENGINE DISPLAYAcceptedAcceptedAcceptedAccepted
3161-000133ENGINE FUEL FLOW - FULL TIME DISPLAY - PRIMARY ENGINE DISPLAY UNITAcceptedAcceptedAcceptedAccepted
3161E568A38CDS - FUEL QUANTITY DISPLAY WITH NUMERIC READOUT ONLY - ENABLEAcceptedAcceptedAcceptedAccepted
3162-000018ATTITUDE COMPARATOR - FLASHING - ADIAcceptedAcceptedAcceptedAccepted
3162-000022FLIGHT DIRECTOR COMMAND DISPLAY - SPLIT AXIS - ADIAcceptedAcceptedAcceptedAccepted
3162-000028RADIO ALTITUDE - BELOW ADIAcceptedAcceptedAcceptedAccepted
3162-000030RISING RUNWAY - DISPLAYED ON THE ADIAcceptedAcceptedAcceptedAccepted
3162-000036LANDING ALTITUDE REFERENCE BAR - PRIMARY FLIGHT DISPLAYAcceptedAcceptedAcceptedAccepted
3162-000040BARO MINIMUMS POINTER - DISPLAYED ON SELECTION OF RADIO ALTITUDE MINIMUMS - PRIMARY FLIGHT DISPLAYAcceptedAcceptedAcceptedAccepted
3162-000044TCAS RESOLUTION ADVISORY - VSIAcceptedAcceptedAcceptedAccepted
3162-000046SINGLE CHANNEL AUTOPILOT ANNUNCIATION - ABOVE ADIAcceptedAcceptedAcceptedAccepted
SWA-PA-03729-EX A-3SA-17
Page 13
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
3162-000051ILS LOCALIZER DEVIATION EXPANDED SCALE - AUTOPILOT OR FLIGHT DIRECTOR MODEAcceptedAcceptedAcceptedAccepted
3162-000059MAP MODE ORIENTATION - TRACK UP - NAVIGATION DISPLAYAcceptedAcceptedAcceptedAccepted
3162-000064RANGE ARCS - NAVIGATION DISPLAYAcceptedAcceptedAcceptedAccepted
3162-000079MANUALLY TUNED VOR SELECTED COURSE LINES DISPLAYED - NAVIGATION DISPLAYAcceptedAcceptedAcceptedAccepted
3162-000084TCAS 3 NM RANGE RING - NAVIGATION DISPLAYAcceptedAcceptedAcceptedAccepted
3162-000088AIRSPEED BUG - ENABLED - 80 KNOT SETTING - MACH AIRSPEED INDICATORAcceptedAcceptedAcceptedAccepted
3162-000355V1 AURAL CALLOUT - FLIGHT DECKAcceptedAcceptedAcceptedAccepted
3162A627A32SOFTWARE ACTIVATION - DOUBLE DERATE INDICATION - ENABLEAcceptedAcceptedAcceptedAccepted
3162A627A38CDS - SOFTWARE ACTIVATION - HORIZON LINE HEADING SCALE - ENABLEAcceptedAcceptedAcceptedAccepted
3162A627A42CDS - SOFTWARE ACTIVATION - REF FLAP/SPEED ANNUNCIATION - ENABLEAcceptedAcceptedAcceptedAccepted
3162C594A29CDS - SOFTWARE ACTIVATION - NAVIGATION PERFORMANCE SCALES - ENABLEAcceptedAcceptedAcceptedAccepted
3162E967A02RSAT - SPEEDBRAKE WARNINGAcceptedAcceptedAcceptedAccepted
3244-000009PARKING BRAKE WARNING LIGHT - NOSE LANDING GEAR AREAAcceptedAcceptedAcceptedAccepted
3245B290A77WHEELS AND TIRES - NOSE LANDING GEAR - WHEELS - COLLINS AEROSPACE - INSTALLATION WITH SFE 12 PR, 235 MPH RATED RADIAL TIRESAcceptedAcceptedAcceptedAccepted
3245B290A92BRAKES - CARBON - COLLINS AEROSPACEAcceptedAcceptedAcceptedAccepted
3245F216A01WHEELS AND TIRES - MAIN LANDING GEAR - WHEELS FOR CARBON BRAKES - GOODRICH - INSTALLATION WITH 32 PR, 235 MPH RADIAL TIRESAcceptedAcceptedAcceptedAccepted
3245F216A02MP - WHEELS, TIRES AND BRAKES - REPLACEMENT - MAIN LANDING GEAR - WHEELS AND TIRES FOR CARBON BRAKES - GOODRICH - MAX9 WHEELS AND 32-PR TIRES IN LIEU OF MAX8 WHEELS AND 30-PL TIRESAcceptedAcceptedAcceptedAccepted
SWA-PA-03729-EX A-3SA-17
Page 14
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
3245F802B24RR 97029-293 - REPLACEMENT - WHEELS AND TIRES - MAIN AND NOSE LANDING GEAR WHEELS AND TIRES WITHOUT TPIS IN LIEU OF WHEELS AND TIRES WITH TPISAcceptedAcceptedAcceptedAccepted
3249E173A73TIRE PRESSURE INDICATION SYSTEM - INSTALLATIONAcceptedAcceptedAcceptedAccepted
3321C869A65PASSENGER CABIN LIGHTING - SINGLE-ZONE CONTROL - 737 BOEING SKY INTERIORAcceptedAcceptedAcceptedAccepted
3324C195A05NO SMOKING SIGN - SILK SCREENED SYMBOLAcceptedAcceptedAcceptedAccepted
3350A704A19EMERGENCY ESCAPE PATH LIGHTING - FLOOR MOUNTED - PHOTOLUMINESCENTAcceptedAcceptedAcceptedAccepted
3412E437F31DUAL ELEMENT ASPIRATED TAT PROBE (FOR FMC) - INSTALLED IN A NON-ASPIRATED CONFIGURATIONAcceptedAcceptedAcceptedAccepted
3430F197A39MP - MULTI-MODE RECEIVER (MMR) AND VOR/MARKER BEACON - REPLACEMENT - ROCKWELL COLLINS 3G MMR P/N 822-2532-100 IN LIEU OF EXISTING ROCKWELL COLLINS MMR P/N 822-1821-332 AND ROCKWELL COLLINS VOR/MARKER BEACON P/N 822-0297-001 - SPEAcceptedAcceptedAcceptedAccepted
3430F211A42PRR 3M8275-6S - ROCKWELL COLLINS AEROSPACE GLU-2100 MMR SOFTWARE UPDATE--AcceptedAccepted
3430F302B75MP - SOFTWARE REPLACEMENT - 3G MULTI-MODE RECEIVER (3G MMR) - COLLINS AEROSPACE - P/N 822-2532-100 - BFEAcceptedAccepted--
3430F608A043G MULTI-MODE RECEIVER (3G MMR) - COLLINS AEROSPACE - P/N 822-2532-100 - BFE/SPEAcceptedAcceptedAcceptedAccepted
3431C175A06NAVIGATION CONTROL PANEL (NCP) - GNSS LANDING SYSTEM (GLS) CAPABLE - GABLES - P/N G7501-01- BFE/SPEAcceptedAcceptedAcceptedAccepted
3433C594A24RADIO ALTIMETER (RA) - CAT IIIB CAPABLE - COLLINS AEROSPACE - P/N 822-0334-003 - BFE/SPEAcceptedAcceptedAcceptedAccepted
SWA-PA-03729-EX A-3SA-17
Page 15
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
3436D972A01HEAD-UP DISPLAY (HUD) - PARTIAL PROVISIONS FOR SINGLE COLLINS AEROSPACE HEAD-UP GUIDANCE SYSTEM (HGS) MODEL 6000 WITH MCDU INTERFACEAcceptedAcceptedAcceptedAccepted
3436D972A02HEAD-UP DISPLAY (HUD) - INSTALLATION OF SINGLE COLLINS AEROSPACE HEAD-UP GUIDANCE SYSTEM (HGS) MODEL 6000 WITH MCDU INTERFACE - STC CERTIFIED - BFE/SPEAcceptedAcceptedAcceptedAccepted
3443A065B18SINGLE WEATHER RADAR CONTROL PANEL - WITH MULTISCAN FUNCTIONALITY - COLLINS AEROSPACE P/N 622-5129-802 - BFE/SPEAcceptedAcceptedAcceptedAccepted
3443E568A02SINGLE WEATHER RADAR SYSTEM - WITH PREDICTIVE WINDSHEAR AND MULTISCAN CAPABILITY WITH V2.0 HAZARD DISPLAY FEATURES - COLLINS AEROSPACE WRP-2100A PROCESSOR P/N 822-3150-101 - BFE/SPEAcceptedAcceptedAcceptedAccepted
3445E724A21TCAS SYSTEM - COLLINS AEROSPACE TCAS COMPUTER P/N 822-2911-002 - TCAS CHANGE 7.1 COMPLIANT - BFE/SPEAcceptedAcceptedAcceptedAccepted
3446-000046LOW VOLUME FOR ALTITUDE CALLOUTSAcceptedAcceptedAcceptedAccepted
3446-000050500 SMART CALLOUTAcceptedAcceptedAcceptedAccepted
3446B693F93GROUND PROXIMITY WARNING SYSTEM ALTITUDE CALLOUTS - 2500, 1000, 500, 100, 50, 40, 30, 20, 10. APPROACHING MINIMUMS, MINIMUMSAcceptedAcceptedAcceptedAccepted
3446C174A14ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) - BANK ANGLE CALLOUT (VARIABLE CALLOUT BELOW 130 FT) - ENABLEAcceptedAcceptedAcceptedAccepted
3453E437A58ATC SYSTEM - ROCKWELL COLLINS ATC TRANSPONDER P/N 822-1338-205 - ADS-B OUT DO-260B COMPLIANT - GABLES CONTROL PANEL P/N G6992-40 - BFE/SPEAcceptedAcceptedAcceptedAccepted
SWA-PA-03729-EX A-3SA-17
Page 16
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
3453F197A93MP - AIR TRAFFIC CONTROL TRANSPONDER SYSTEM - REPLACEMENT - GABLES CONTROL PANEL P/N G6992-40 IN LIEU OF P/N G6992-02 - SPEAcceptedAcceptedAcceptedAccepted
3455E717A12DISTANCE MEASURING EQUIPMENT (DME) - COLLINS AEROSPACE INTERROGATOR P/N 822-2325-001 - BFE/SPEAcceptedAcceptedAcceptedAccepted
3461A425A09FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - NAVIGATION DATABASE - BOEING SUPPLIEDAcceptedAcceptedAcceptedAccepted
3461A425A33FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - RUNWAY DISTANCE REMAINING - FEETAcceptedAcceptedAcceptedAccepted
3461A425A40FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS)- VERTICAL NAVIGATION PROFILE- "VNAV ALT"- ENABLEAcceptedAcceptedAcceptedAccepted
3461A425A48FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - ACTIVATE COLOR OPERATIONAcceptedAcceptedAcceptedAccepted
3461A890A76FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - NAVIGATION DISPLAY - MISSED APPROACH IN CYAN UNTIL ACTIVE - ENABLEAcceptedAcceptedAcceptedAccepted
3461B403A13FLIGHT MANAGEMENT COMPUTING SYSTEM (FMCS) - INTEGRATED APPROACH NAVIGATION (IAN)AcceptedAcceptedAcceptedAccepted
3461C175A11FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - AIR TRAFFIC SERVICES DATA LINK (ATS DL) - FANS FEATURE ACTIVATIONAcceptedAcceptedAcceptedAccepted
3461C175A14FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - FANS CAPABLE MCDU WITH ATC KEYBOARD - INSTALLATION-SFEAcceptedAcceptedAcceptedAccepted
3461C175A32FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - COMMON VNAV - ENABLEAcceptedAcceptedAcceptedAccepted
3511B873B97CREW OXYGEN MASKS - FULL FACE MASK WITH BUILT-IN SMOKE GOGGLES - FIRST OBSERVER - COLLINS AEROSPACE - BFE/SPEAcceptedAcceptedAcceptedAccepted
SWA-PA-03729-EX A-3SA-17
Page 17
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
3511B873B98CREW OXYGEN MASKS - FULL FACE MASK WITH BUILT-IN SMOKE GOGGLES - CAPTAIN AND FIRST OFFICER - COLLINS AEROSPACE - BFE/SPEAcceptedAcceptedAcceptedAccepted
3811-000019POTABLE WATER - SERVICEABLE TO 60 GALLONSAcceptedAcceptedAcceptedAccepted
3812-000002NO WATER QUANTITY GAUGE - WATER SERVICE PANELAcceptedAcceptedAcceptedAccepted
3832-000076NO SENSOR FOULED LIGHT - COVER PLATEAcceptedAcceptedAcceptedAccepted
3832-000078NO WASTE QUANTITY GAUGE - COVER PLATEAcceptedAcceptedAcceptedAccepted
3910F197A33AFT ELECTRONICS PANEL ARRANGEMENTAcceptedAcceptedAcceptedAccepted
3910F197A34MP - AFT ELECTRONICS PANEL - REVISIONAcceptedAcceptedAcceptedAccepted
4400F186A15MP - HIGH-SPEED COMMUNICATIONS - INSTALLATION - ADDITIONAL PARTIAL PROVISIONS - HONEYWELL GX KA EQUIPMENT AS FURNITURE AND ROCKWELL COLLINS GX JETWAVE KA BAND UNIQUE WIRING AND EQUIPMENT TRAYS - ROCKWELL COLLINS - CSE/SPEAcceptedAcceptedAcceptedAccepted
4420E895E05IFE SYSTEM - PARTIAL PROVISIONS FOR IN-FLIGHT ENTERTAINMENT AND CONNECTIVITY SYSTEM MAIN EQUIPMENT - 737 MAXAcceptedAcceptedAcceptedAccepted
4435E526E63HIGH-SPEED COMMUNICATIONS - STRUCTURAL PROVISIONS - TRI-BAND RADOMEAcceptedAcceptedAcceptedAccepted
4435E837C84HIGH-SPEED COMMUNICATIONS - TRI-BAND RADOME INSTALLATION - WHITE COLOR (BAC 7945)AcceptedAcceptedAcceptedAccepted
4435E861A83HIGH-SPEED COMMUNICATIONS - PARTIAL PROVISIONS FOR KU/KA-BAND OFFBOARD CONNECTIVITY SYSTEMS - 737 MAXAcceptedAcceptedAcceptedAccepted
4435E861A88HIGH-SPEED COMMUNICATIONS - PARTIAL PROVISIONS FOR CABIN WIRELESS NETWORK SYSTEMS WITH 4 WAPS - 737 MAXAcceptedAcceptedAcceptedAccepted
SWA-PA-03729-EX A-3SA-17
Page 18
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
4435E926A65HIGH-SPEED COMMUNICATIONS - GATE-TO-GATE ACTIVATION-Accepted-Accepted
4435E926B26HIGH-SPEED COMMUNICATIONS - BROADBAND CONTROL PANEL WITH TWO POSITION SWITCH-Accepted-Accepted
4435F127A23HIGH-SPEED COMMUNICATIONS - INSTALLATION - HONEYWELL GX KA EQUIPMENT AS FURNITURE - ROCKWELL COLLINS - CSE/SPEAcceptedAcceptedAcceptedAccepted
4435F186A96HIGH-SPEED COMMUNICATIONS - INSTALLATION - ADDITIONAL PARTIAL PROVISIONS - ROCKWELL COLLINS GX JETWAVE KA BAND UNIQUE WIRING AND EQUIPMENT TRAYSAcceptedAcceptedAcceptedAccepted
4435F186A97MP - EXTERNAL COMMUNICATION SYSTEM - DELETE - PARTIAL PROVISIONS FOR A GROUND CELLULAR MODEM LOCATED IN THE G4 GALLEY - 737 MAXAcceptedAcceptedAcceptedAccepted
4435F186B82HIGH-SPEED COMMUNICATIONS - INSTALLATION - OPERATIONAL SOFTWARE - ROCKWELL COLLINS INC - CSE/SPE-Accepted-Accepted
4435F186C78HIGH-SPEED COMMUNICATIONS - INSTALLATION - INSTALL ROCKWELL COLLINS GX JETWAVE KA BAND EQUIPMENT INTO PROVISIONS AND ACTIVATE THE SYSTEM - ROCKWELL COLLINS INC - CSE/SPE-Accepted-Accepted
4435F186C79MP - HIGH-SPEED COMMUNICATIONS - INSTALLATION - INSTALL ROCKWELL COLLINS GX JETWAVE KA BAND EQUIPMENT INTO PROVISIONS AND ACTIVATE THE SYSTEM - ROCKWELL COLLINS INC - CSE/SPE-Accepted-Accepted
4610E526A81ONBOARD NETWORK SYSTEM - PARTIAL PROVISIONS - GROUND BASED CONNECTIVITYAcceptedAcceptedAcceptedAccepted
4610E526B92ONBOARD NETWORK SYSTEM - CELLULAR AND WIFI GROUND BASED CONNECTIVITY - WIRELESS WIDE AREA NETWORK UNIT (WWU) - BFE/SPEAcceptedAcceptedAcceptedAccepted
SWA-PA-03729-EX A-3SA-17
Page 19
BOEING PROPRIETARY

OptionOption Title1C6911C692-1C6941C511-1C5131C514-1C517
4610E526E60ONBOARD NETWORK SYSTEM - ACTIVATION OF ONS-ACARS CMU INTERFACEAcceptedAcceptedAcceptedAccepted
4610E855A25CREW WIRELESS NETWORK - FORWARD WIRELESS ACCESS POINT (WAP) - PROVISIONSAcceptedAcceptedAcceptedAccepted
4610E855A26CREW WIRELESS NETWORK - FORWARD WIRELESS ACCESS POINT (WAP) - INSTALLATIONAcceptedAcceptedAcceptedAccepted
4610F197A70MP - CREW WIRELESS NETWORK - REVISION - CWLU2 FORWARD WIRELESS ACCESS POINT IN LIEU OF EXISTING CWLU1 FORWARD AND AFT WIRELESS ACCESS POINT PROVISIONSAcceptedAcceptedAcceptedAccepted
5231A561C54CARGO DOOR - SOLID SKINAcceptedAcceptedAcceptedAccepted
5300-000027UNDERSEAT FLOOR PANELS, LOW TRAFFIC CAPABILITYAcceptedAcceptedAcceptedAccepted
5352A298A28RADOME- NORDAM- SFEAcceptedAcceptedAcceptedAccepted
7200D422A03CFM LEAP-1B ENGINES - 1B25 RATINGAcceptedAcceptedAcceptedAccepted
7200F278D81RR 97226-119 - CFM LEAP-1B ENGINES - ENGINE THRUST RATE INCREASE - 1B27 RATING IN LIEU OF 1B25 RATING---Accepted
7200F816A44RR 97029-296 - REVISION - CFM LEAP-1B ENGINES - 1B28 RATING IN LIEU OF 1B25 RATINGAcceptedAcceptedAcceptedRejected
7200F816A47RR 97029-297 - REVISION - CFM LEAP-1B ENGINES - 1B28 RATING IN LIEU OF 1B27 RATINGRejectedRejected-Accepted
7900-000116LUBRICATING OIL - MOBIL JET IIAcceptedAcceptedAcceptedAccepted

SWA-PA-03729-EX A-3SA-17
Page 20
BOEING PROPRIETARY



REMARKET AIRCRAFT TECHNICAL ACCEPTANCE AND DELIVERY REQUIREMENTS AND RESPONSIBILITIES
between
THE BOEING COMPANY
and
SOUTHWEST AIRLINES CO.
EXHIBIT B-1 to PURCHASE AGREEMENT
NUMBER PA-03729


Page 1
SA-17
BOEING PROPRIETARY

EXHIBIT B-1
REMARKET AIRCRAFT TECHNICAL ACCEPTANCE AND
DELIVERY REQUIREMENTS AND RESPONSIBILITIES
relating to
BOEING MODEL 737-8 REMARKET AIRCRAFT

Both Boeing and Customer have certain documentation and approval responsibilities at various times during the construction and delivery cycle of the Remarket Aircraft that are critical to accomplishing Initial Technical Acceptance (defined in Article 3.1 below), Final Technical Acceptance (defined in Article 3.6 below), and Delivery (as defined below) of the Reconfigured Remarket Aircraft, and ensuring a positive experience for both parties. This Exhibit B-1 documents those responsibilities and indicates recommended completion deadlines for the actions to be accomplished.

    Boeing and Customer acknowledge that each Remarket Aircraft is built and will be delivered to Customer based on terms specified in Letter Agreement No. SWA-PA-03729-LA-2100594 entitled “737-8 Remarket Aircraft” (Remarket Aircraft Letter Agreement). Boeing has manufactured the Remarket Aircraft as described in their respective As-Built Configurations, as that term is defined in the Remarket Aircraft Letter Agreement and the applicable Exhibit A to the Purchase Agreement.

Following Customer’s Initial Technical Acceptance of the Remarket Aircraft in their respective As-Built Configurations, Boeing will manage the Reconfiguration of the Remarket Aircraft to the Delivery Configuration, as each term is defined in the Remarket Aircraft Letter Agreement. Customer’s Delivery Configuration, once finalized, will be described and incorporated into the Purchase Agreement as Exhibit A documents by way of supplemental agreement.

Upon the completion of the Reconfiguration to conform to the Delivery Configuration, the reconfigured Remarket Aircraft (Reconfigured Remarket Aircraft) will be presented for final inspection and Final Technical Acceptance and Delivery to Customer by Boeing in conformance with the Purchase Agreement.

1.GOVERNMENT DOCUMENTATION REQUIREMENTS.
Certain actions are required to be taken by Customer in advance of the scheduled Initial Technical Acceptance and/or Delivery with respect to obtaining certain government issued documentation.
1.1Airworthiness and Registration Documents. Boeing and Customer agree that the registration number provided by Customer shall be utilized for each Remarket Aircraft for the process of aircraft certification. Not later than six (6) months prior to Initial Technical Acceptance and upon Boeing request, Customer will notify Boeing



SWA-PA-03729-EX B-1SA-17
Page 2
BOEING PROPRIETARY

of the registration number to be painted on the side of the Remarket Aircraft. In addition, and not later than three (3) months prior to Initial Technical Acceptance and upon Boeing request, Customer will authorize, by letter to the regulatory authority having jurisdiction, the temporary use of such registration numbers by Boeing during the pre-delivery testing of the Remarket Aircraft. To the extent insufficient time exists between Customer’s purchase of the Remarket Aircraft and the deadlines in this paragraph, Customer will provide the information required as soon as possible following such purchase.
Customer is responsible for furnishing any temporary or permanent registration certificates required by any governmental authority having jurisdiction to be displayed aboard each Remarket Aircraft after Delivery.
1.2Certificate of Sanitary Construction.
1.2.1U.S. Registered Remarket Aircraft. Post modification, Boeing will or will arrange to obtain from the United States Public Health Service, a United States Certificate of Sanitary Construction to be displayed aboard the Remarket Aircraft after Delivery to Customer.

2.INSURANCE CERTIFICATES.
Unless provided earlier, Customer will provide to Boeing not later than thirty (30) days prior to Delivery, a copy of the requisite annual insurance certificate in accordance with the requirements of Article 8.2 of the AGTA.
3.TECHNICAL ACCEPTANCE OF AS-BUILT CONFIGURED REMARKET AIRCRAFT; REMARKET AIRCRAFT REPOSITION.
3.1Schedule Remarket Aircraft for Initial Technical Acceptance. Boeing and Customer shall agree, in advance, on a detailed listing of documents and process steps necessary for initial and final technical acceptance (the Delivery Agenda). In the event that anything in the Delivery Agenda or the Purchase Agreement conflict, the provisions of the Delivery Agenda shall prevail. Each Remarket Aircraft in As-Built Configuration will be available for inspection and an initial technical acceptance by Customer as of the month specified in Letter Agreement No. SWA-PA-03729-LA-1106474R7 entitled “Option Aircraft” of the Purchase Agreement, prior to Reconfiguration (Initial Technical Acceptance), at the Seattle Delivery Center (SDC). Boeing will provide notice of the target date of Initial Technical Acceptance at least forty-five (45) calendar days prior to the scheduled month of Initial Technical Acceptance. Boeing will give Customer at least seven (7) calendar days’ notice of the specific date for review and inspection of the As-Built Configuration of the Remarket Aircraft and will provide the associated technical documents, reports and manuals no later than sixty (60) days prior to the target date. Such reports shall, in addition to other required documentation, include a report on the customer inspection plan (Customer Inspection Report) for the original purchaser of the Remarket Aircraft. At a minimum, the Customer Inspection Report shall include:
3.1.1The areas that were inspected;







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3.1.2The name of the individual conducting the inspection;
3.1.3Details on any inspections that were waived; and
3.1.4Findings and associated corrective actions.

3.2Scope of Initial Inspection. The initial inspection of the Remarket Aircraft shall be equal in scope to that of any other Aircraft under the Purchase Agreement reasonably necessary for Customer to provide its Initial Technical Acceptance in the form substantially similar to Attachment A hereto. Customer recognizes that the Remarket Aircraft are already built and, as a result, not all of the inspection activity that Customer may be accustomed to engaging in during the build process will be available to Customer. Boeing will make reasonable accommodations to provide Customer access for additional inspections as agreed upon.
3.3Delivery Condition Required for Initial Technical Acceptance. The Remarket Aircraft in their As-Built Configuration will be certified by the Federal Aviation Administration (FAA) to the configuration specification described in Exhibit A documents and will conform to Type Certification. Upon Boeing’s presentation of the Remarket Aircraft in the As-Built Configuration, Customer will then provide to Boeing written Initial Technical Acceptance of the As-Built Configuration of each Remarket Aircraft, when:
3.3.1The Remarket Aircraft has the Limited Configuration Revisions incorporated in the As-Built Configuration;
3.3.2The FAA has issued a Standard Airworthiness Certificate for each Remarket Aircraft in its As-Built Configuration;
3.3.3Customer has reviewed, inspected and accepted the technical documents, manuals and Boeing quality reports for each Remarket Aircraft in the As-Built Configuration;
3.3.4Customer has inspected the As-Built Configuration of the Remarket Aircraft;
3.3.5Customer has waived the demonstration flight in accordance with Letter Agreement No. SWA-PA-03729-LA-1106468 entitled “Demonstration Flight Waiver” of the Purchase Agreement; and
3.3.6Customer and Boeing will document any material quality and/or production issues with respect to the As-Built Configuration of the Remarket Aircraft and will execute an Initial Technical Acceptance Commitments Letter. Note that a separate Delivery Commitments Letter will be prepared for the Delivery following completion of Reconfiguration of the Remarket Aircraft to meet the Delivery Configuration.
3.4Re-location of the Remarket Aircraft to the Reconfiguration Site Following Initial Technical Acceptance of the Remarket Aircraft by Customer. Following Customer’s Initial Technical Acceptance, Boeing may, at its discretion, reposition the Remarket Aircraft to the MRO (as defined in the Remarket Aircraft Letter Agreement) that will perform the Reconfiguration. Reconfiguration of the Remarket Aircraft shall be
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performed with the goal of allowing sufficient time for (a) Customer to conduct the Final Technical Acceptance, (b) the MRO to address and/or remediate quality issues related to the Reconfiguration, and (c) Customer to take Delivery of the Remarket Aircraft during the Delivery Month noted in to Letter Agreement No. SWA-PA-03729-LA-1106474R7 entitled “Option Aircraft“, Attachment 1-A. As part of Reconfiguration activities, and to facilitate delivery, all changes to part numbers and serial numbers shall be communicated to Customer as they occur in a mutually acceptable format and timing.
3.5Scope of Final Inspection. The final inspection of the Remarket Aircraft shall be limited to an inspection of the Reconfiguration work performed; provided, however, (i) that, if during the Reconfiguration, and in order to accomplish the Reconfiguration work, there are areas affected beyond those that would normally be accessed or which were previously closed, during original production and/or (ii) if any areas of the Remarket Aircraft that are inspected by Customer for Aircraft were not inspected during original production, subject to Section 3.2, Customer shall be entitled to inspect those additional areas to ensure they comply with the Initial Technical Acceptance.
3.6Final Technical Acceptance. The Remarket Aircraft, in their respective Delivery Configuration shall be made available for a final inspection and technical acceptance of the Reconfiguration work (the Final Technical Acceptance) at the MRO.
3.7Delivery Condition Required for Final Technical Acceptance. Each Remarket Aircraft shall have incorporated all Service Bulletins related to the Reconfiguration, with the touch-labor and work performed as required for completion of the Reconfiguration into the Delivery Configuration. Boeing shall provide Customer with preliminary delivery documents in advance as is customary for Customer’s Aircraft and final, updated versions of the delivery documents shall be provided at Final Technical Acceptance. All documents shall be provided in the same format as is customary for delivery of Customer’s Aircraft. Customer will provide to Boeing written Final Technical Acceptance of the Remarket Aircraft, when:
3.7.1Customer has reviewed, inspected and accepted the Remarket Aircraft’s updated technical documents, manuals and quality reports, as well as an updated weight and balance manual to capture the Remarket Aircraft in its Delivery Configuration. All technical documents and manuals shall be in a post-modification configuration and as applicable, shall possess unique Customer Effectivity Codes.
3.7.2Customer has reviewed and accepted, such acceptance shall not be unreasonably withheld, any Maintenance Review Board and/or Significant Rework Log repairs that were completed during production and/or Reconfiguration.
3.7.3Customer has inspected and accepted the Reconfigured Remarket Aircraft after a post-Reconfiguration functional check flight (Functional Check Flight).
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3.7.3.1If delivery will not occur at the MRO, the Functional Check Flight will be conducted, unless otherwise agreed by the Parties, during the repositioning flight from the MRO to the site of delivery. The Parties agree that the purpose and intent of the Functional Check Flight is to ensure that the functionality of the Remarket Aircraft complies with the Initial Technical Acceptance and the Delivery Configuration. The Remarket Aircraft shall not be flown after the Functional Check Flight without the explicit, prior agreement of Customer.
3.7.3.2Upon completion of the Functional Check Flight, Boeing will address any flight squawks encountered during the Functional Check Flight and Customer will be provided an opportunity to inspect the Remarket Aircraft, in the form of a walk around. Boeing will ensure that all flight squawks and new issues identified by the walk around will be addressed prior to transfer of title.
3.7.3.3Customer will complete its Final Technical Acceptance inspections at the MRO prior to the Functional Check Flight, and Boeing will likewise ensure that all repairs identified during said inspections will be completed prior to the Functional Check Flight or a repositioning flight.
3.7.4Customer and Boeing have documented any material quality and/or production issues with respect to the post-Reconfiguration Configuration of the Remarket Aircraft and executed a Final Technical Acceptance Commitments Letter (A separate Delivery Commitments Letter will be prepared for the Delivery following completion of changes to meet the Delivery Configuration).

3.8Repositioning Upon completion of the Reconfiguration of the Remarket Aircraft, if the Completed Remarket Aircraft will be stored prior to Delivery, Boeing may reposition the Aircraft from the MRO to a storage location and possibly reposition again to support Customer’s Final Technical Acceptance and Delivery.

4.FINAL TECHNICAL ACCEPTANCE AND DELIVERY ACTIONS BY BOEING.
4.1Schedule of Inspections. All FAA, Boeing, Customer and, if required, CBP inspections will be scheduled by Boeing for completion prior to Delivery of the Remarket Aircraft. Customer will be informed of such schedules.
4.2Schedule of Demonstration Flights. All FAA demonstration flights will be scheduled by Boeing for completion prior to Delivery. [***]


4.3[***]


4.4Delivery Papers, Documents and Data. Boeing will have available at the time of Delivery, as the case may be, certain delivery papers, documents and data for




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execution and delivery. Such documents shall include, but not be limited to, a maintenance release from the MRO evidencing the airworthiness of the Remarket Aircraft and a post-modification letter verifying that the Air Traffic Control transponder and altimeter system comply with FAA regulations. If the Remarket Aircraft will be registered with the FAA, Boeing will pre-position in Oklahoma City, Oklahoma, for filing with the FAA at the time of Delivery of the Remarket Aircraft an executed original Form 8050-2, Aircraft Bill of Sale, indicating transfer of title to the Remarket Aircraft from Boeing to Customer.
4.5Delegation of Authority. Boeing will present a certified copy of a delegation of authority, designating and authorizing certain persons to act on its behalf in connection with Delivery of the Completed Remarket Aircraft.
4.6Aircraft Flight Log. Boeing will provide the Remarket Aircraft flight log for repositioning flights where Boeing provides flight crew personnel.

5.ADDITIONAL DELIVERY ACTIONS BY CUSTOMER.
5.1Aircraft Radio Station License. At Delivery Customer will provide its radio station license to be placed on board the Reconfigured Remarket Aircraft following Delivery.
5.2Delegation of Authority. Customer will present to Boeing at Delivery of the Remarket Aircraft an original or certified copy of Customer's delegation of authority designating and authorizing certain persons to act on its behalf in connection with the Delivery.
5.3TSA Waiver Approval. Customer may be required to have an approved Transportation Security Administration (TSA) waiver for the post-Delivery repositioning flight depending on Customer’s en-route stop(s) and destination unless the Customer already has a TSA-approved security program in place. Customer is responsible for application of the TSA waiver and obtaining TSA approval. Customer will provide a copy of the approved TSA waiver to Boeing upon arrival at the delivery location.
5.4Electronic Advance Passenger Information System. Should the post-Delivery repositioning flight of a Remarket Aircraft leave the United States, the Department of Homeland Security office requires Customer to comply with the Electronic Advance Passenger Information System (eAPIS). Customer needs to establish their own account with CBP in order to file for departure.





ATTACHMENT A TO EXHIBIT B-1






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CERTIFICATE OF INITIAL TECHNICAL ACCEPTANCE
BOEING MODEL 737-8
Southwest Airlines Co.

1.
REMARKET AIRCRAFT IDENTIFICATION
REGISTRATION IDENTIFICATION NO.:<RegNo>
BLOCK NO.:<Block>
MANUFACTURER'S SERIAL NO.:<MSN>
<EngMfg> <EngModel> ENGINE SERIAL NOS.:
POSITION #1POSITION #2
<EngMSN1><EngMSN2>
2.REMARKET AIRCRAFT INSPECTION
INSPECTED AT: The State of <DeliveryLocation>

DATE: ___________________ TIME___________________

Southwest Airlines Co. does hereby acknowledge and agree that the above described Remarket Aircraft together with all equipment installed therein and documents related thereto has been inspected by Southwest Airlines Co. to its satisfaction except as noted below, as applicable, and that the Remarket Aircraft complies with the provisions of Purchase Agreement No. 03729 dated December 13, 2011, as amended and supplemented relevant to the Remarket Aircraft, and Southwest Airlines Co. hereby technically accepts such Remarket Aircraft.

EXECUTED this _____ day of <DelMonthYear>.
SOUTHWEST AIRLINES CO.
Signature

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Printed name
Title


Exceptions to Technical Acceptance



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The Boeing Company
    P.O. Box 3707
    Seattle, WA 98124 2207
SWA-PA-03729-LA-2100594R1

Southwest Airlines Co.
2702 Love Field Drive
P.O. Box 36611
Dallas, Texas 75235-1611

Subject:    737-8 Remarket Aircraft

Reference:    a) Purchase Agreement No. PA-03729 (Purchase Agreement) between The Boeing Company (Boeing) and Southwest Airlines Co. (Customer) relating to models 737-8 and 737-7 aircraft (Aircraft).
b) Letter Agreement No. SWA-PA-03729-LA-2100700R1 entitled “Remarket Aircraft - Configuration Matters” (Remarket Aircraft – Configuration Matters Letter Agreement) to the Purchase Agreement relating to the purchase of model 737-8 Remarket Aircraft.

    This letter agreement (Letter Agreement) amends and supplements the Purchase Agreement and governs Customer’s purchase of sixty (60) remarket Boeing model 737-8 Aircraft with CFMI engines (Remarket Aircraft), under the terms and conditions described in this Letter Agreement and the Purchase Agreement. All capitalized terms which are not otherwise defined herein shall have the definitions specified in the Purchase Agreement and other letter agreements specifically addressing the Remarket Aircraft.

    This Letter Agreement incorporates in the Purchase Agreement those terms applicable only to the Remarket Aircraft. Except as expressly amended by the terms of this Letter Agreement, Remarket Aircraft are in all other respects “Aircraft” under the terms of the Purchase Agreement.

    [***]








    [***]












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    [***]







1.    [***]












































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2.    [***]
    









3.    [***]










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4.    [***]

































5.    [***]

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6.    Miscellaneous.

    [***]

























7.    [***]










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8.    Assignment.

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

9.    Confidential Treatment.

Customer understands that certain commercial and financial information contained in this Letter Agreement is considered by Boeing as confidential and has value precisely because it is not available generally or to other parties. Customer agrees to limit the disclosure of the contents of this Letter Agreement to (a) its directors and officers, (b) employees of Customer with a need to know the contents for performing its obligations (including, without limitation, those employees performing accounting, finance, administration and other functions necessary to finance and purchase, deliver or lease the Remarket Aircraft) and who understand they are not to disclose its contents to any other person or entity (other than those to whom disclosure is permitted by this Article) without the prior written consent of Boeing and (c) any auditors and attorneys of Customer who have a need to know such information and have signed a confidentiality agreement in the same form and substance similar to this Article, or are otherwise bound by a confidentiality obligation. Disclosure to other parties is not permitted without Boeing’s consent except as may be required by applicable law or governmental regulations. Customer shall be fully responsible to Boeing for compliance with such obligations.

    

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Very truly yours,


THE BOEING COMPANY
By/s/ Carson J. May
Name
Carson J. May
ItsAttorney-In-Fact
ACCEPTED AND AGREED TO this
Date:June 3, 2022
SOUTHWEST AIRLINES CO.
By/s/ Chris Monroe
Name
Chris Monroe
ItsSVP Finance and Treasurer



            
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SWA-PA-03729-LA-2100700R1


Southwest Airlines Co.
2702 Love Field Drive
P.O. Box 36611
Dallas, Texas 75235-1611

Subject:    Remarket Aircraft – Configuration Matters

References:    a) Purchase Agreement No. PA-03729 (Purchase Agreement) between The Boeing Company (Boeing) and Southwest Airlines Co. (Customer) relating to models 737-8 and 737-7 aircraft (Aircraft); and

b) Letter Agreement No. SWA-PA-03729-LA-2100594R1 entitled “737-8 Remarket Aircraft” (737-8 Remarket Aircraft Letter Agreement) to the Purchase Agreement relating to the purchase of model 737-8 Remarket Aircraft.

This letter agreement (Letter Agreement) amends and supplements the Purchase Agreement. All terms used but not defined in this Letter Agreement will have the same meaning as in the Purchase Agreement.
1.Additional Delivery Configuration Revisions.
1.1The As-Built Configurations (which will include the Limited Configuration Revisions and As-Installed SPE/BFE, each as described in the 737-8 Remarket Aircraft Letter Agreement) for the Remarket Aircraft are described in the applicable Exhibit A to the Purchase Agreement shall be provided at least sixty (60) days prior to the target date for Initial Technical Acceptance. At Initial Technical Acceptance, Boeing will present each Remarket Aircraft to Customer in the respective As-Built Configuration for inspection and acceptance prior to Reconfiguration (as described in the 737-8 Remarket Aircraft Letter Agreement).
1.2 Following Initial Technical Acceptance by Customer of a Remarket Aircraft in its As-Built Configuration, Boeing will effect the Reconfiguration of such Remarket Aircraft into the Delivery Configuration, subject to minor, aesthetic and part-number differences between the Delivery Configuration of the Remarket Aircraft and the configuration of other Aircraft covered by the Purchase Agreement. Customer shall have the right to refuse any deviation or non-routine repair that would result in a change to the Customer’s maintenance program Once established by the Parties, the Delivery Configuration will be ultimately be defined for each Remarket Aircraft in an Exhibit A to the Purchase Agreement and incorporated into the Purchase Agreement by way of a supplemental agreement.








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1.3[***]



Boeing and Customer will consult together with regard to (i) the master kit changes required in the Change Proposal Packages for Reconfiguration of the Remarket Aircraft to the Delivery Configuration, and (ii) Customer’s BFE required from Customer for certification of each Remarket Aircraft in the Delivery Configuration (Configuration Coordination).
1.3.1Following the Configuration Coordination, Customer will have the opportunity to i) review the detailed descriptions in the Change Proposal Packages and/or ii) meet with Boeing to discuss and amend, as required, the Change Proposal Packages. Such review and/or meeting will not cause a delay to the acceptance timing of the Change Proposal Packages
1.3.2The Change Proposal Package for each Remarket Aircraft will be provided to Customer within thirty (30) days of the Configuration Coordination. Customer will provide acceptance within thirty (30) days of the receipt of the Change Proposal Package.
1.3.3For each Remarket Aircraft, Customer will provide a shipset of Customer’s BFE to Boeing, at the MRO selected to do the Reconfiguration of a Remarket Aircraft, for installation on and certification of the Delivery Configuration of each Remarket Aircraft. Boeing will provide the BFE on-dock dates as referenced in My Boeing Fleet (MBF).
1.3.4The Parties will work together to finalize the respective Delivery Configuration of each Remarket Aircraft, and each Delivery Configuration will be incorporated into the Purchase Agreement as Exhibit A-3 entitled “737-8 Remarket Aircraft Configuration”, with references to each Remarket Aircraft by manufacturer’s serial number (MSN).
1.3.5The Change Proposal Packages, once accepted and incorporated into the Purchase Agreement, will [***]


1.4The Parties agree to cooperate in good faith during the Configuration Coordination so that a mutually agreeable Delivery Configuration can be reached. Any delay in Customer’s acceptance of the Change Proposal Package may affect the schedule for induction of such Remarket Aircraft’s induction into the reconfiguration process and Boeing reserves the right to adjust the scheduled delivery date based on such delay in acceptance due to Customer.









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2.[***]







3.    Confidential Treatment.

Customer understands that certain commercial and financial information contained in this Letter Agreement is considered by Boeing as confidential and has value precisely because it is not available generally or to other parties. Customer agrees to limit the disclosure of the contents of this Letter Agreement to (a) its directors and officers, (b) employees of Customer with a need to know the contents for performing its obligations (including, without limitation, those employees performing accounting, finance, administration and other functions necessary to finance and purchase, deliver or lease the Remarket Aircraft) and who understand they are not to disclose its contents to any other person or entity (other than those to whom disclosure is permitted by this Article) without the prior written consent of Boeing and (c) any auditors and attorneys of Customer who have a need to know such information and have signed a confidentiality agreement in the same form and substance similar to this Article, or are otherwise bound by a confidentiality obligation. Disclosure to other parties is not permitted without Boeing’s consent except as may be required by applicable law or governmental regulations. Customer shall be fully responsible to Boeing for compliance with such obligations.


















Very truly yours,


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THE BOEING COMPANY
By/s/ Carson J. May
Name
Carson J. May
ItsAttorney-In-Fact
ACCEPTED AND AGREED TO this
Date:June 3, 2022
SOUTHWEST AIRLINES CO.
By/s/ Chris Monroe
Name
Chris Monroe
ItsSVP Finance and Treasurer






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