Supplemental Agreement No.84toPurchase Agreement No.1810betweenTHE BOEING COMPANYandSOUTHWEST AIRLINES CO.Relating to Boeing Model 737-7H4 and 737-8H4 Aircraft
EX-10.1 2 sa-84topax1810redacted.htm SUPPLEMENTAL AGREEMENT NO. 84 SA-84 to PA-1810 redacted
Supplemental Agreement No. 84 |
to |
Purchase Agreement No. 1810 |
between |
THE BOEING COMPANY |
and |
SOUTHWEST AIRLINES CO. |
Relating to Boeing Model 737-7H4 and 737-8H4 Aircraft |
THIS SUPPLEMENTAL AGREEMENT, entered into as of September 20, 2013, 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);
Buyer and Boeing entered into Purchase Agreement No. 1810 dated January 19, 1994 as amended, and supplemented, (Purchase Agreement) relating to the purchase and sale of Boeing Model 737-7H4 aircraft (737-7H4 Aircraft) and 737-8H4 aircraft (737-8H4 Aircraft); and this Supplemental Agreement is an amendment to and is incorporated into the Purchase Agreement; and
WHEREAS, Boeing offered and Buyer agreed to accelerate delivery of three (3) 737-8H4 Aircraft bearing Manufacturing Serial Numbers 36912 and 36914 (both from October 2013 to September 2013) and 42523 (from July 2014 to June 2014) (collectively, Subject Aircraft).
NOW THEREFORE, in consideration of the mutual covenants herein contained, the parties agree to amend the Purchase Agreement as follows:
1.The Table of Contents of the Purchase Agreement is deleted in its entirety and a new Table of Contents is attached hereto and incorporated into the Purchase Agreement by this reference.
2.Table 1c, “Aircraft Information Table - Block 800LUV Aircraft (non-ETOPS Configuration),” is deleted in its entirety and a new Table 1c is attached hereto and incorporated into the Purchase Agreement by this reference. The new Table 1c reflects the revised delivery month for the Subject Aircraft.
3.Exhibit A-7 , “Aircraft Configuration - Block 800LUV Aircraft (non-ETOPS Configuration),” is deleted in its entirety and replaced with a revised Exhibit A-7, attached
***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-84-1 |
hereto and incorporated in the Purchase Agreement by this reference. The revised Exhibit A-7 contains additional pricing information erroneously omitted from the original exhibit.
4.Attachment A to Letter Agreement SWA-PA-1810-LA-1001315R2, *** is deleted in its entirety and replaced with a revised Attachment A, attached hereto and incorporated in the Purchase Agreement by this reference. The revised Attachment A reflects the revised delivery month for the MSN 42523.
5.Letter Agreement SWA-PA-1810-LA-1105885R1, *** is deleted in its entirety and replaced with a revised Letter Agreement SWA-PA-1810-LA-1105885R2, attached hereto and incorporated in the Purchase Agreement by this reference. The revised letter agreement corrects a typographical error in paragraph 1.2.
6.As a result of the revised delivery month of the MSN 42523, an excess in Advance Payments made by Buyer to Boeing exists in the amount of ***. Boeing will retain such excess amounts until the next Advance Payment is due, at which time Buyer may reduce the amount of such Advance Payment by ***. Buyer’s election to not reduce such next Advance Payment shall not preclude Buyer from using such excess amount on any following Advance Payment. A reconciliation regarding changes in Advance Payments arising from this Supplemental Agreement will be provided separately to Buyer by Boeing.
The Purchase 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/ Jeff Solomon | By: /s/ Tammy Romo | |
Its: Attorney‑In‑Fact | Its: SVP & CFO |
P.A. No. 1810 | SA-84-2 |
TABLE OF CONTENTS |
Page | SA | ||
ARTICLES | Number | Number | |
1. | Subject Matter of Sale | 1-1 | SA-82 |
2. | Delivery, Title and Risk | ||
of Loss | 2-1 | SA-28 | |
3. | Price of Aircraft | 3‑1 | SA-82 |
4. | Taxes | 4-1 | |
5. | Payment | 5‑1 | |
6. | Excusable Delay | 6‑1 | |
7. | Changes to the Detail | ||
Specification | 7-1 | SA-73 | |
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-84 |
TABLE OF CONTENTS |
SA | ||
TABLE | Number | |
1a | Aircraft Information Table - Block 700LUV Aircraft | SA-83 |
1b | Aircraft Information Table - Block 800LUV Aircraft | SA-82 |
1c | Aircraft Information Table - Block 800LUV Aircraft | SA-84 |
(non-ETOPS Configuration) |
EXHIBITS
A-5 | Aircraft Configuration - Block 700LUV Aircraft | SA-75 | |
A-6 | Aircraft Configuration - Block 800LUV Aircraft | SA-75 | |
A-7 | Aircraft Configuration - Block 800LUV Aircraft | SA-84 | |
(non-ETOPS Configuration) | |||
B | *** | SA-75 | |
C | Customer Support Document | ||
C-2 | 737-800 Customer Support Document | SA-75 | |
D-2 | Economic Price Adjustment | SA-75 | |
ECI-MFG/CPI (July 2011 Base Price) | |||
E | Buyer Furnished Equipment | SA-75 | |
Provisions Document | |||
Attachment A - 737-7H4 Aircraft (through 2012) | |||
Attachment B - 737-8H4 Aircraft (2012-2018) | SA-83 | ||
F | Defined Terms Document |
LETTER AGREEMENTS
1810-1R1 | Waiver of Aircraft Demonstration Flight | SA-75 |
P.A. No. 1810 | ii |
K/SWA | SA-84 |
TABLE OF CONTENTS |
SA | ||
RESTRICTED LETTER AGREEMENTS | Number | |
6‑1162‑RLL‑932R3 | *** | SA-75 |
6‑1162‑RLL‑934R5 | Disclosure of Confidential | SA-75 |
Information | ||
6‑1162‑RLL‑941R3 | Other Matters | SA-75 |
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 |
SWA-PA-1810-LA-1001315R2 | *** | SA-83 |
Attachment A | SA-84 | |
SWA-PA-1810-LA-1003498 R1 | *** | SA-75 |
SWA-PA-1810-LA-1003490R2 | *** | SA-82 |
SWA-PA-1810-LA-1003367R1 | *** | SA-75 |
SWA-PA-1810-LA-1105883 | Aircraft Model Substitution | SA-75 |
SWA-PA-1810-LA-1105884R1 | Option Aircraft | SA-75 |
Attachment B - Option Aircraft Information Table | SA-83 | |
SWA-PA-1810-LA-1105885R2 | *** | SA-84 |
SWA-PA-1810-LA-1105886R1 | *** | SA-82 |
SWA-PA-1810-LA-1105887 | *** | SA-75 |
P.A. No. 1810 | iii |
K/SWA | SA-84 |
TABLE OF CONTENTS |
SA | ||
Number | ||
SWA-PA-1810-LA-1105888R3 | *** | SA-83 |
SWA-PA-1810-LA-1105889 | *** | SA-75 |
SWA-PA-01810/03729-LA-1301169 | *** | SA-83 |
ADDITIONAL LETTERS (FOR REFERENCE) - INACTIVE (as of SA-82) | |
6-1162-MSA-288 | Business Offer - Enhanced Ground Proximity |
Warning System (EGPWS) - Activiation - Peaks | |
and Obstacles Feature | |
(Not applicable to Block 700LUV & Block 800LUV Aircraft) | |
6-1162-JMG-501R2 | Business Offer - ACARS package |
(Not applicable to Block 700LUV & Block 800LUV Aircraft) |
INACTIVE / DELETED TABLES, EXHIBITS, AND LETTER AGREEMENTS
TABLE
Table | Title | Last Updated under SA | Current Status |
1 | Aircraft Information Table | SA-75 | Inactive |
2 | Option Aircraft Information Table | SA-74 | Deleted under SA-75 |
EXHIBITS
Exhibits | Title | Last Updated under SA | Current Status |
A | Aircraft Configuration - 737-700 | SA-36 | Inactive |
A-Winglet | Aircraft Configuration | SA-36 | Inactive |
A-1-Winglet | Aircraft Configuration | SA-36 | Inactive |
A-1A | Aircraft Configuration - 737-700 Block T-W-2c | SA-36 | Inactive |
A-2 | Aircraft Configuration - 737-700 Block T-W-2 / T-W-2a | SA-47 | Inactive |
A-3 | Aircraft Configuration - 737-700 Block T-W-2 / T-W-2a | SA-61 | Inactive |
A-4 | Aircraft Configuration - 737- | SA-66 | Inactive |
P.A. No. 1810 | iv |
K/SWA | SA-84 |
TABLE OF CONTENTS |
Exhibits | Title | Last Updated under SA | Current Status |
700 Block T-W-2b Aircraft | |||
C.2 | 737-800 Customer Support Variables | SA-71 | Deleted under SA-75 |
D | Price Adjustment Due to Economic Fluctuations - Aircraft Price Adjustment (July 1992 Base Price) | Inactive | |
D-1 | Price Adjustment Due to Economic Fluctuations - Aircraft Price Adjustment (July 1999 Base Price) | SA-13 | Inactive |
E.2 | 737-800 Buyer Furnished Equipment Provisions Document | SA-73 | Deleted under SA-75 |
RESTRICTED LETTER AGREEMENTS
Letter Agreement | Title | Last Updated under SA | Current Status |
6‑1162‑RLL‑933R21 | Option Aircraft | SA-60 | Deleted under SA-75 |
6‑1162‑RLL‑935R1 | Performance Guarantees | SA-1 | Inactive |
6‑1162‑RLL‑936R4 | Certain Contractual Matters | SA-4 | Inactive |
6‑1162‑RLL‑937 | Alternate Advance Payment Schedule | Inactive | |
6‑1162‑RLL‑938 | *** | Inactive | |
6‑1162‑RLL‑939R1 | Certification Flight Test Aircraft | SA-1 | Inactive |
6‑1162‑RLL‑940R1 | Training Matters | SA-1 | Inactive |
6‑1162‑RLL‑942 | Open Configuration Matters | Inactive | |
6‑1162‑RLL‑943R1 | Substitution Rights | SA-6 | Deleted under SA 75 |
6‑1162‑RLL‑944 | *** | Inactive | |
6-1162-RLL-945 | Comparison of 737-7H4 and 737-3H4 Block Fuel Burn | Inactive | |
6-1162-RLL-1855R3 | Additional Contractual Matters | SA-4 | Inactive |
6-1162-RLL-1856 | *** | SA-1 | Inactive |
6-1162-RLL-1857 | Service Ready Validation Program Field Test | SA-1 | Inactive |
6-1162-RLL-1858R1 | Escalation Matters | SA-4 | Inactive |
6-1162-RLL-2036 | Amortization of Costs for Customer Unique Changes | SA-1 | Inactive |
P.A. No. 1810 | v |
K/SWA | SA-84 |
TABLE OF CONTENTS |
Letter Agreement | Title | Last Updated under SA | Current Status |
6-1162-RLL-2037 | Reconciliation of the Aircraft Basic Price | SA-1 | Inactive |
6-1162-RLL-2073 | Maintenance Training Matters | SA-1 | Inactive |
6-1162-KJJ-058R1 | Additional Substitution Rights | SA-71 | Deleted under SA-75 |
6-1162-KJJ-150 | Flight Control Computer & Mode Control Panel Spares Matter | SA-14 | Inactive |
6-1162-MSA-185R3 | Delivery Change Contractual Matters | SA-21 | Inactive |
6-1162-JMG-747R1 | *** | SA-36 | Inactive |
6-1162-CHL-217 | Rescheduled Flight Test Aircraft | SA-32 | Inactive |
6-1162-NIW-606R1 | *** | SA-36 | Inactive |
6-1162-NIW-640 | Early Delivery of Two April 2004 Aircraft | SA-35 | Inactive |
6-1162-NIW-889 | Warranty - Exterior Color Schemes and Markings for YA143 and on | SA-39 | Inactive |
6-1162-NIW-1142 | *** | SA-43 | Inactive |
6-1162-NIW-1369 | *** | SA-46 | Inactive |
6-1162-NIW-1983 | *** | SA-62 | Inactive |
SWA-PA-1810-LA-1000419 | *** | SA-64 | Inactive |
6-1162-NIW-890R1 | *** | SA-75 SA-39 | Inactive |
6-1162-KJJ-054R2 | Business Matters | SA-75 | Inactive |
6-1162-JMG-669R9 | *** | SA-75 SA-75 SA-54 | Inactive |
SWA-PA-1810-LA-02710R1 | *** | SA-72 | Inactive |
P.A. No. 1810 | vi |
K/SWA | SA-84 |
Table 1c Purchase Agreement No. PA 01810 Aircraft Delivery, Description, Price and Advance Payments Block 800LUV Aircraft (non ETOPS Configuration) |
Airframe Model/MTOW: | 737-800 | 174200 pounds | Detail Specification: | D019A001SWA38P-1 Rev C (3/29/2013) | |||
Engine Model/Thrust: | CFM56-7B27 | 27300 pounds | Note 1 | Base Aircraft Price Base Year/Escalation Formula: | Jul-11 | ECI-MFG/CPI | |
Base Aircraft Price: | *** | Engine Price Base Year/Escalation Formula: | N/A | N/A | |||
Special Features: | *** | ||||||
Add'l Features/Changes | *** | ||||||
Total Special Features (Exhibit A-7) | *** | ||||||
Sub-Total of Airframe and Features: | *** | Aircraft Price Escalation Data: | |||||
Engine Price (Per Aircraft): | *** | Base Year Index (ECI): | *** | ||||
Aircraft Basic Price (Excluding BFE/SPE): | *** | Base Year Index (CPI): | *** | ||||
Buyer Furnished Equipment (BFE) Estimate: | *** | ||||||
Seller Purchased Equipment (SPE) Estimate: | *** |
Delivery Date | Number of Aircraft | Escalation Factor (Airframe) | Aircraft Serial Number | Escalation Forecast | Sub-Block Note 2 | Escalation Estimate Adv Payment Base Price Per A/P | Advance Payment Per Aircraft (Amts. Due/Mos. Prior to Delivery): | |||
At Signing *** | 24 Mos. *** | 21/18/12/9/6 Mos. *** | Total *** | |||||||
Sep-2013 | 3 | *** | 36933, 36912, 36914 | *** | *** | *** | *** | *** | *** | |
Nov-2013 | 3 | *** | 36915, 33939, 42526 | *** | *** | *** | *** | *** | *** | |
Dec-2013 | 3 | *** | 36917, 36919, 36731 | *** | *** | *** | *** | *** | *** | |
Mar-2014 | 1 | *** | 37,004 | *** | *** | *** | *** | *** | *** | |
Apr-2014 | 4 | *** | 42384, 36894, 36895, 36896 | *** | *** | *** | *** | *** | *** | |
May-2014 | 3 | *** | 36897, 42385, 42521 | *** | *** | *** | *** | *** | *** | |
Jun-2014 | 4 | *** | 36898, 36905, 42522, 42523 | *** | *** | *** | *** | *** | *** | |
Jun-2014 | 2 | *** | tbd, tbd | *** | OPEX | *** | *** | *** | *** | *** |
Jul-2014 | 1 | *** | 36,911 | *** | *** | *** | *** | *** | *** | |
Jul-2014 | 3 | *** | tbd, tbd, tbd | *** | OPEX | *** | *** | *** | *** | *** |
Aug-2014 | 4 | *** | 36907, 42524,35973, 42525 | *** | *** | *** | *** | *** | *** | |
Sep-2014 | 4 | *** | 36935, 42528, 42527, 42531 | *** | *** | *** | *** | *** | *** |
SWA-PA-01810 | SA-84 | |
63879 / 63887 / 64110 / 64111 | Boeing Proprietary | Page 1 |
Table 1c Purchase Agreement No. PA 01810 Aircraft Delivery, Description, Price and Advance Payments Block 800LUV Aircraft (non ETOPS Configuration) |
Delivery Date | Number of Aircraft | Escalation Factor (Airframe) | Aircraft Serial Number | Escalation Forecast | Sub-Block Note 2 | Escalation Estimate Adv Payment Base Price Per A/P | Advance Payment Per Aircraft (Amts. Due/Mos. Prior to Delivery): | |||
At Signing *** | 24 Mos. *** | 21/18/12/9/6 Mos. *** | Total *** | |||||||
Oct-2014 | 3 | *** | 36909, 36732, 36920 | *** | *** | *** | *** | *** | *** | |
Oct-2014 | 1 | *** | 38,806 | *** | *** | *** | *** | *** | *** | |
Nov-2014 | 2 | *** | 36971, 37043 | *** | *** | *** | *** | *** | *** | |
Dec-2014 | 2 | *** | 37037, 37045 | *** | *** | *** | *** | *** | *** | |
Dec-2014 | 2 | *** | 42529, 42530 | *** | *** | *** | *** | *** | *** |
Total: | 45 |
Notes: |
1) *** |
2) The sub-block identifier is used to denote applicability of certain business terms as referenced in Letter Agreement SWA-PA-1810-LA-1105888R2 to the Purchase Agreement. |
SWA-PA-01810 | SA-84 | |
63879 / 63887 / 64110 / 64111 | Boeing Proprietary | Page 2 |
737-8H4 |
AIRCRAFT CONFIGURATION |
between |
THE BOEING COMPANY |
and |
SOUTHWEST AIRLINES CO. |
Exhibit A-7 to Purchase Agreement Number 1810 |
Block 800LUV Aircraft |
(non-ETOPS Configuration) |
P.A. No. 1810 | A-7- 1 | SA-84 |
AIRCRAFT CONFIGURATION |
Dated September 20, 2013 |
relating to |
BOEING MODEL 737-8H4 AIRCRAFT |
The Detail Specification is Boeing document number D019A001SWA38P-1 Rev C, dated March 29, 2013. The Detail Specification provides further description of Buyer’s configuration set forth in this Exhibit A-7. Such Detail Specification will be comprised of Boeing Configuration Specification D019A001, Rev N dated as of January 29, 2010 as amended to incorporate the Special Features listed in this Exhibit A-7, 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 Special Features. The Aircraft Basic Price reflects and includes all effects of such Special Features, except such Aircraft Basic Price does not include the price effects of any Buyer Furnished Equipment or Seller Purchased Equipment.
P.A. No. 1810 | A-7- 2 | SA-84 |
BOEING PROPRIETARY |
CR | Title | 2011 $ Price Per A/C |
0110-000029 | MINOR MODEL 737-800 PASSENGER AIRPLANE | *** |
0110-000030 | MAJOR MODEL 737 AIRPLANE | *** |
0170A244C58 | SERVICING FEATURES - BASIC | *** |
0170A425A76 | AVIONICS - DUAL FMC WITH MULTI-CONTROL DISPLAY UNIT | *** |
0170A541A17 | AIRFRAME - 737-800 | *** |
0170B401A26 | COMMUNICATIONS - BASIC COMMUNICATIONS CONFIGURATION WITH HF DATALINK PROVISIONS AND INTEGRATED SELCAL CALL | *** |
0170B401A73 | CLIMATE - NORMAL WEATHER OPERATIONS | *** |
0170B513A51 | PC - PUSH TO TALK (PTT) SWITCH ON GLARESHIELD - REMOVE | *** |
0170B750B43 | 737 BOEING SKY INTERIOR | *** |
0170C430J04 | PC - COMMUNICATIONS - DUAL COMMUNICATIONS CONTROL PANEL WIRING IN LIEU OF TRIPLE COMMUNICATIONS CONTROL PANEL WIRING | *** |
0170C801A81 | GALLEY AFT COMPLEX - G4B GALLEY - DOMED AFT BULKHEAD | *** |
0170C801C76 | LAVATORY AFT COMPLEX - TWO LAVATORIES WITH TWO DOUBLE ATTENDANT SEATS - 737 BOEING SKY INTERIOR | *** |
0170D360B56 | PC - LAVATORY AFT COMPLEX - TWO LAVATORIES WITH TWO DOUBLE ATTENDANT SEATS, NO CURTAIN - BOEING SKY INTERIOR | *** |
0221A599A81 | WET GROOVED RUNWAY OPERATIONS WITH ANTISKID SYSTEM INOPERATIVE | *** |
0221A609B52 | DISPATCH WITH GEAR EXTENDED FOR REVENUE FLIGHT | *** |
0221C588A08 | LANDING PERFORMANCE IMPROVEMENT- SKID RESISTANT RUNWAYS (FOR FAA CERTIFIED CUSTOMERS) | *** |
0222C472A09 | SHORT FIELD PERFORMANCE ENHANCEMENT | *** |
0224-000036 | EXTENDED RANGE TWIN ENGINE OPERATIONS (ETOPS) | *** |
0228-000001 | FLIGHT MANUALS IN FAA FORMAT | *** |
0228-000032 | FLIGHT CREW OPERATIONS MANUAL IN FAA FORMAT | *** |
0252B299A34 | INSTRUMENTATION, AIRPLANE AND FUEL MEASURING STICK MANUALS IN ENGLISH UNITS - TEMPERATURE IN DEGREES FAHRENHEIT | *** |
0254-000003 | USPHS CERTIFICATE OF SANITARY CONSTRUCTION | *** |
0315D292A01 | CERTIFIED OPERATIONAL AND STRUCTURAL DESIGN WEIGHTS 737-800 | *** |
0351D322A15 | TAKEOFF PERFORMANCE IMPROVEMENT - ALTERNATE FORWARD CENTER OF GRAVITY LIMITS | *** |
0370C910B63 | AIR CONDITIONING TRANSITION DUCT UNDER FLOOR - INSTALLATION - 17 MIL DAMPING TAPE FOR NOISE REDUCTION | *** |
1110D360A84 | EXTERIOR NON-REGULATORY MARKINGS | *** |
1110D360A85 | EXTERIOR REGULATORY MARKINGS AND COLOR SCHEME | *** |
1130D360A86 | CARGO COMPARTMENT PLACARDS | *** |
1130D360A88 | LIGHTED SIGNS | *** |
1130D360B61 | INTERIOR PLACARDS AND MARKERS - 737 BOEING SKY INTERIOR | *** |
2130-000010 | 600 FPM CABIN PRESSURE ASCENT RATE | *** |
2130-000015 | 750 FPM CABIN PRESSURE DESCENT RATE | *** |
2170-000021 | OZONE CONTROL - SPACE PROVISIONS FOR CATALYTIC CONVERTERS | *** |
2210-000121 | AUTOFLIGHT - ACTIVATION OF CONTROL WHEEL STEERING REVERSION IN APPROACH MODE | *** |
2210-000123 | AUTOFLIGHT - FLIGHT DIRECTOR TAKEOFF MODE WINGS LEVEL | *** |
2210-000142 | AUTOFLIGHT - ALTITUDE ALERT - 300/900 FEET | *** |
2210-000151 | AUTOFLIGHT - ENABLE GLIDE SLOPE CAPTURE PRIOR TO LOCALIZER CAPTURE | *** |
2210C175A38 | AUTOFLIGHT - GO-AROUND ROLL MODE - LNAV | *** |
2230-000137 | AUTOTHROTTLE - FMCS - TAKEOFF PROFILE THRUST REDUCTION ALTITUDE | *** |
2310B691B85 | COMMUNICATIONS CONTROL PANELS - DUAL GABLES RADIO TUNING PANELS CAPABLE OF (2) HF SYSTEMS AND (3) VHF SYSTEMS (8.33 KHZ CAPABLE) - P/N G7404-124 - BFE/SPE | *** |
2311B401A28 | HF COMMUNICATIONS - EQUIPMENT INSTALLATION OF DUAL HONEYWELL INTERNATIONAL INC. HF TRANSCEIVERS - P/N ###-###-####-012 - AND DIGITAL HF COUPLERS - P/N ###-###-####-011 - BFE/SPE | *** |
2311B401A29 | DUAL HF DATA RADIO - ARINC 753 - ACTIVATION - AIRLINE DATA LINK COMMUNICATIONS ONLY | *** |
2312A213B90 | VHF COMMUNICATIONS - EQUIPMENT INSTALLATION OF TRIPLE HONEYWELL ARINC 750 RTA-44D VHF FM IMMUNE TRANSCEIVERS WITH 8.33 KHZ CHANNEL SPACING, VDL MODE 2, AND CMC INTERFACE CAPABILITY - P/N 064-50000-2000 - BFE/SPE | *** |
2321-000050 | SELCAL - AVTECH FIVE CHANNEL DECODER - P/N 1200008-000 - BFE/SPE | *** |
2322C430J57 | MP - COMMUNICATIONS MANAGEMENT UNIT (CMU) - ACTIVATION - DATA LINK RECORDING | *** |
2322C703A02 | CMU - HONEYWELL ARINC 758 LEVEL AOA MARK III COMMUNICATIONS MANAGEMENT UNIT (CMU) - INSTALLATION INTO EXISTING PARTIAL PROVISIONS - P/N ###-###-####-921 - BFE/SPE | *** |
2322C939A05 | CMU - INSTALLATION OF PARTIAL PROVISIONS FOR A SINGLE CMU IN ACCORDANCE WITH ARINC 758 | *** |
P.A. 1810 SA-84 | BOEING PROPRIETARY | Page 1 |
BOEING PROPRIETARY |
CR | Title | 2011 $ Price Per A/C |
2322D322B88 | MP - CMU - INSTALLATION OF HONEYWELL MARK II ARINC 758 LEVEL AOA CMU W/ARINC SERVICE PROVIDER - DATA LINK RECORDING CAPABLE - P/N ###-###-####-006 IN LIEU OF THE EXISTING HONEYWELL MARK III ARINC 758 LEVEL AOA CMU - P/N ###-###-####- 921 - BFE | *** |
2324B299A26 | EMERGENCY LOCATOR TRANSMITTER (ELT) - WULFSBERG ELECTRONICS AUTOMATIC FIXED WITH NAVIGATION INTERFACE UNIT (NIU) - MODE S BROADCAST - BFE/SPE | *** |
2331B754B15 | PASSENGER ADDRESS (PA) SYSTEM - ARINC 715 - ROCKWELL COLLINS AMPLIFIER - BFE/SPE | *** |
2342D360B00 | CABIN INTERPHONE SYSTEMS - ATTENDANT HANDSETS WITH UNIQUE MARKINGS | *** |
2350A150D50 | AUDIO INTEGRATING - INHIBIT AURAL ALERT TRANSMISSIONS THROUGH CAPTAIN, FIRST OFFICER'S AND FIRST OBSERVER'S HEADPHONES | *** |
2350B872A08 | AUDIO CONTROL PANEL - INTEGRATED SELCAL, CREW CALL, AND SATCOM FUNCTIONS INSTALLATION - 3 VHF/2 HF | *** |
2351-000043 | CONTROL WHEEL PUSH TO TALK (PTT) SWITCH - THREE POSITION WITH DETENT IN INTERPHONE POSITION | *** |
2351A213A33 | AUDIO INTEGRATION - INSTALLATION - TWO-PLUG AUDIO JACKS IN THE FLIGHT DECK | *** |
2351A213B77 | BOOM MICROPHONE HEADSETS - CAPTAIN AND FIRST OFFICER - TELEX AIRMAN 750 - P/N 64300-200 - BFE/SPE | *** |
2351B696M34 | AUDIO INTEGRATION - INSTALLATION - 2J HAND MICROPHONE JACKS IN THE FLIGHT DECK | *** |
2351D360C80 | PASSENGER CABIN MEDICAL COMMUNICATIONS SYSTEM - BOEING SKY INTERIOR | *** |
2371B628B32 | VOICE RECORDER AND MICROPHONE/MONITOR - HONEYWELL - 2 HOUR RECORDING TIME - WITH DATALINK RECORDING CAPABILITY - P/N ###-###-####-001 & P/N ###-###-####-001 - BFE/SPE | *** |
2371B628B41 | VOICE RECORDER - RECORDER INDEPENDENT POWER SUPPLY (RIPS) - AFT LOWERED CEILING | *** |
2433-000010 | STANDBY POWER - 60-MINUTE CAPABILITY | *** |
2451B572D03 | GALLEY G1 POWER - 6.9 KVA | *** |
2510C910B65 | TRIP COUNTER - INSTALLATION - SFE - DEXTER WILSON | *** |
2511-000271 | SECOND OBSERVER STATION, WITHOUT ARMRESTS - ADDITION | *** |
2511B696M36 | FLIGHT COMPARTMENT SEATS - INSTALL CAPTAIN AND FIRST OFFICER SEATS WITH FLOTATION CUSHIONS | *** |
2513-000420 | NO ROLLER SUNSHADES - FLIGHT DECK | *** |
2513B696E89 | LOG BOOK HOLDER - INSTALLATION - ON AFT FACE OF P8 AISLESTAND | *** |
2513B696E95 | FLIGHT COMPARTMENT ACCOMMODATIONS - INSTALL A FUEL CONVERSION PLACARD ON THE FACE OF CAPTAIN AND FIRST OFFICER'S CLIPBOARDS | *** |
2513C410C22 | FLIGHT COMPARTMENT ACCOMMODATIONS - EMERGENCY EVACUATION CHECKLIST PLACARD ON THE CAPTAIN AND FIRST OFFICER'S CONTROL COLUMNS | *** |
2520D360A90 | INTERIOR COLOR AND MATERIAL - STANDARD OFFERING | *** |
2523D360F87 | PASSENGER SERVICE UNITS - 737 BOEING SKY INTERIOR | *** |
2524D360A79 | CLOSET - AFT OF DOOR 1, LEFT - BFE/SPE | *** |
2524D360B01 | FULL HEIGHT WINDSCREEN/STOWAGE UNIT - RHS - STA 336.75 - BFE/SPE | *** |
2525A627A07 | DOUBLE ATTENDANT SEAT - WALL MOUNTED - STA 304 | *** |
2525C204K04 | HIC AND FEMUR LOAD COMPLIANCE - ECONOMY CLASS SEATS | *** |
2525C204K05 | HIC AND FEMUR LOAD COMPLIANCE - ATTENDANT SEATS | *** |
2525D360F41 | ECONOMY CLASS SEATS - BFE/SPE | *** |
2527D360C81 | FLOOR COVERING - GALLEY MAT AND CARPET - BFE | *** |
2528C204J16 | FORWARD CENTER OVERHEAD STOWAGE COMPARTMENT - PROVISIONED FOR PALLETIZED EQUIPMENT AND LIFE RAFTS - 737 BOEING SKY INTERIOR | *** |
2528C204J18 | SECOND FORWARD CENTER OVERHEAD STOWAGE COMPARTMENT - PROVISIONED FOR PALLETIZED EQUIPMENT AND LIFE RAFTS - 737 BOEING SKY INTERIOR | *** |
2528C204J20 | FIRST MID CABIN CENTER OVERHEAD STOWAGE COMPARTMENT - PROVISIONED FOR PALLETIZED EQUIPMENT AND LIFE RAFTS - 737 BOEING SKY INTERIOR | *** |
2528C204J22 | SECOND MID-CABIN CENTER OVERHEAD STOWAGE COMPARTMENT - PROVISIONED FOR PALLETIZED EQUIPMENT AND LIFE RAFTS - 737 BOEING SKY INTERIOR | *** |
2528D360A93 | LITERATURE POCKETS - BFE/SPE | *** |
2528D360B64 | OVERHEAD STOWAGE BINS - ADDITIONAL FEATURES - 737 BOEING SKY INTERIOR | *** |
2529A802A86 | DOOR WARNING STRAP - SHOCK CORD | *** |
2529D360B52 | FORWARD ATTENDANT WORKSTATION - PANEL & HANDSET - UNIQUE FACEPLATE DISPLAY | *** |
2530C882K34 | GALLEY G1 - AFT STATION 293 | *** |
2530D360B03 | GALLEY PART NUMBERS - BFE/SPE | *** |
2530D360B04 | GALLEY INSERT PART NUMBERS - BFE/SPE | *** |
2540B873A66 | LA LAVATORY | *** |
2540D360A81 | LA LAVATORY SELECTABLES | *** |
P.A. 1810 SA-84 | BOEING PROPRIETARY | Page 2 |
BOEING PROPRIETARY |
CR | Title | 2011 $ Price Per A/C |
2540D360A82 | LE LAVATORY SELECTABLES | *** |
2540D360C84 | LD LAVATORY SELECTABLES | *** |
2552-000117 | CARGO COMPARTMENT NETS WITH NYLON TYPE WEB SUPPORTS | *** |
2552-000216 | LOWER SIDEWALL LINER - FOWARD AND AFT CARGO COMPARTMENT - .060 THICKNESS | *** |
2552B491A05 | FLOOR PANELS - FORWARD CARGO COMPARTMENT - 0.090 INCH THICKNESS, BMS 8-2, CONOLITE | *** |
2552B491A06 | FLOOR PANELS - AFT CARGO COMPARTMENT - 0.090 INCH THICKNESS BMS 8-2, CONOLITE | *** |
2552B491A07 | CEILING LINER - FORWARD CARGO COMPARTMENT - 0.031 INCH THICKNESS, BMS 8-2, CONOLITE | *** |
2552B491A10 | CEILING LINER - AFT CARGO COMPARTMENT - 0.031 INCH THICKNESS, BMS 8-2, CONOLITE | *** |
2552B491A11 | STA 731 BULKHEAD - .060 INCH THICKNESS, BMS 8-2, CONOLITE | *** |
2552B491A13 | UPPER SIDEWALL LINER - AFT CARGO COMPARTMENT - 0.045 INCH THICKNESS, BMS 8-2, CONOLITE | *** |
2560-000176 | HALON FIRE EXTINGUISHER - FLIGHT DECK - WALTER KIDDE | *** |
2560-000269 | CREW LIFE VEST STOWAGE - FLIGHT DECK, SECOND OBSERVER - CAPTAIN'S SEAT BACK | *** |
2560C410D09 | CREW LIFE VESTS - FLIGHT DECK, WITH SECOND OBSERVER - EASTERN AERO MARINE INC - P/N P01202-301C - BFE/SPE | *** |
2562D360B66 | OVERWATER EMERGENCY EQUIPMENT - BFE/SPE - 737 BOEING SKY INTERIOR | *** |
2564D360G72 | DETACHABLE EMERGENCY EQUIPMENT - PASSENGER COMPARTMENT - BFE/SPE - 737 BOEING SKY INTERIOR | *** |
2622-000047 | APU FIRE EXTINGUISHER BOTTLE - COMMON WITH ENGINES | *** |
2841-000004 | STANDARD FUEL SYSTEM ACCURACY - NO FUEL DENSITOMETERS | *** |
2911-000042 | ENGINE-DRIVEN HYDRAULIC PUMPS WITH VESPEL SPLINE - EATON (VICKERS) - 10-62167 | *** |
2911-000044 | AC MOTOR-DRIVEN HYDRAULIC PUMPS - EATON (VICKERS) - 10-60556 | *** |
3041-000003 | NO HEATED FLIGHT COMPARTMENT NUMBER 3 WINDOW | *** |
3042B696M33 | WINDSHIELD WIPER SYSTEM - REVISION - SINGLE SWITCH FOR BOTH WIPERS | *** |
3120C910B67 | CLOCK WIRING - INSTALLATION - FMC, DFDAU AND VOICE RECORDER INPUT FROM FIRST OFFICER'S CLOCK | *** |
3131-000143 | ACCELEROMETER - HONEYWELL P/N ###-###-####-001 - BFE/SPE | *** |
3131B628B16 | DIGITAL FLIGHT DATA RECORDER (DFDR) - HONEYWELL - 1024 WORDS PER SECOND MAXIMUM DATA RATE - P/N ###-###-####-009 - BFE/SPE | *** |
3131D217A10 | DIGITAL FLIGHT DATA ACQUISITION UNIT (DFDAU) - CAT IIIB/IAN/GLS/NPS CAPABLE - WITH ACMS CAPABILITY AND INTEGRATED PCMCIA MEDIA INTERFACE - TELEDYNE CONTROLS - 512 WPS CAPABLE - 737-7 DATA FRAME ACTIVE - P/N ###-###-####-916 - BFE/SPE | *** |
3132-000014 | PORTABLE DATA LOADER/RECORDER CONNECTOR IN FLIGHT DECK-ARINC 615-SFE | *** |
3133A150E33 | MP-INSTL OF ARINC 740 PRINTER PROVISIONS IN THE FLIGHT DECK AISLESTAND | *** |
3161-000133 | ENGINE FUEL FLOW - FULL TIME DISPLAY - PRIMARY ENGINE DISPLAY UNIT | *** |
3161A627A40 | CDS - SOFTWARE ACTIVATION - SELECTABLE COMPACTED ENGINE FORMAT - ENABLE | *** |
3161C175A22 | ENGINE OIL QUANTITY DISPLAY - PERCENT - ENGINE DISPLAY | *** |
3162-000018 | ATTITUDE COMPARATOR - FLASHING - ADI | *** |
3162-000023 | FLIGHT DIRECTOR COMMAND DISPLAY - FILLED INTEGRATED CUE - ADI | *** |
3162-000028 | RADIO ALTITUDE - BELOW ADI | *** |
3162-000030 | RISING RUNWAY - DISPLAYED ON THE ADI | *** |
3162-000036 | LANDING ALTITUDE REFERENCE BAR - PRIMARY FLIGHT DISPLAY | *** |
3162-000040 | BARO MINIMUMS POINTER - DISPLAYED ON SELECTION OF RADIO ALTITUDE MINIMUMS - PRIMARY FLIGHT DISPLAY | *** |
3162-000044 | TCAS RESOLUTION ADVISORY - VSI | *** |
3162-000051 | ILS LOCALIZER DEVIATION EXPANDED SCALE - AUTOPILOT OR FLIGHT DIRECTOR MODE | *** |
3162-000059 | MAP MODE ORIENTATION - TRACK UP - NAVIGATION DISPLAY | *** |
3162-000079 | MANUALLY TUNED VOR SELECTED COURSE LINES DISPLAYED - NAVIGATION DISPLAY | *** |
3162-000088 | AIRSPEED BUG - ENABLED - 80 KNOT SETTING - MACH AIRSPEED INDICATOR | *** |
3162-000218 | GROUND SPEED - DISPLAYED BELOW AIRSPEED TAPE WHEN MACH NUMBER IS NOT DISPLAYED - PRIMARY FLIGHT DISPLAY | *** |
3162A066A17 | COMMON DISPLAY SYSTEMS FAULT MESSAGE - REVERSE VIDEO DISPLAY | *** |
3162A213A02 | CDS DISPLAY - PFD/ND FORMAT - OVER AND UNDER ENGINE PRESENTATION | *** |
3162A627A36 | CDS - SOFTWARE ACTIVATION - VNAV SPEED BANDS - ENABLE | *** |
3162C594A29 | CDS - SOFTWARE ACTIVATION - NAVIGATION PERFORMANCE SCALES - ENABLE | *** |
3244-000008 | SERVICE INTERPHONE CONNECTOR - EXTERNAL POWER PANEL | *** |
3245-000098 | WHEELS AND TIRES - NOSE LANDING GEAR - WHEELS - BFGOODRICH - INSTALLATION WITH SFE 12 PR, 225 MPH RADIAL TIRES | *** |
3245B290A92 | BRAKES - CARBON - GOODRICH | *** |
P.A. 1810 SA-84 | BOEING PROPRIETARY | Page 3 |
BOEING PROPRIETARY |
CR | Title | 2011 $ Price Per A/C |
3245B290A94 | WHEELS AND TIRES - MAIN LANDING GEAR - WHEELS FOR CARBON BRAKES - GOODRICH - INSTALLATION WITH SFE 28 PR, 225 MPH TIRES | *** |
3321C869A65 | PASSENGER CABIN LIGHTING - SINGLE-ZONE CONTROL - 737 BOEING SKY INTERIOR | *** |
3324C195A04 | NO SMOKING SIGN - SILK SCREENED SYMBOL AND RETAIN CHIME FUNCTION | *** |
3342-000033 | NOSE GEAR TAXI LIGHT - NO AUTOMATIC SWITCHOFF AT RETRACTION | *** |
3342-000035 | NOSE GEAR TAXI LIGHT - 250-WATT | *** |
3344C910B68 | ANTI-COLLISION LIGHT - INSTALLATION - SWITCH NOMENCLATURE | *** |
3350C869A05 | EMERGENCY ESCAPE PATH LIGHTING - FLOOR MOUNTED - COLOR PHOTOLUMINESCENT | *** |
3350D360K03 | RO - EMERGENCY LIGHTING - REPLACEMENT - EMERGENCY ESCAPE PATH LIGHTING - NARROW COLORED PHOTOLUMINESCENT IN LIEU OF STANDARD WIDTH | *** |
3412-000022 | DUAL ELEMENT NON-ASPIRATED TAT PROBE | *** |
3414-000035 | STANDBY ALTIMETER/AIRSPEED INDICATOR - FLIGHT DECK | *** |
3423-000023 | STANDBY ATTITUDE INDICATOR - SEXTANT AVIONIQUE - SFE | *** |
3430B866A28 | ILS/GPS MULTI-MODE RECEIVER (MMR) - HONEYWELL INTERNATIONAL INC. - P/N 066- 50029-1201 - BFE/SPE | *** |
3431A065B03 | VHF NAV/DME CONTROL PANEL - GABLES ENGINEERING - P/N G7500-03 - BFE/SPE | *** |
3433A732A13 | RADIO ALTIMETER (RA) - CAT IIIB CAPABLE - HONEYWELL INTERNATIONAL INC - P/N 066-50007-0111 - BFE/SPE | *** |
3436A218A66 | HEAD-UP DISPLAY (HUD) - PARTIAL PROVISIONS FOR A COMMON HUD SYSTEM WITH CONTROL PANEL INTERFACE | *** |
3436C594A68 | HEAD UP DISPLAY (HUD) - INSTALLATION OF ROCKWELL COLLINS PHASE 3 HGS4000 SYSTEM WITH CONTROL PANEL - STC CERTIFIED - BFE/SPE | *** |
3443B696L72 | SINGLE WEATHER RADAR SYSTEM - HONEYWELL INTERNATIONAL INC. - MODEL RDR- 4000 WEATHER RADAR - INSTALLATION - BFE/SPE | *** |
3443B696L73 | SINGLE WEATHER RADAR SYSTEM CONTROL PANEL - HONEYWELL RDR-4000 RADAR SYSTEM - P/N ###-###-####-001 - BFE/SPE | *** |
3445B866A10 | TCAS SYSTEM - HONEYWELL INTERNATIONAL INC TCAS COMPUTER P/N ###-###-####-001 - TCAS CHANGE 7 COMPLIANT - BFE/SPE | *** |
3446-000046 | LOW VOLUME FOR ALTITUDE CALLOUTS | *** |
3446-000048 | ENHANCED GROUND PROXIMITY WARNING SYSTEM (EGPWS) - BANK ANGLE CALLOUT ENABLE | *** |
3446-000050 | 500 SMART CALLOUT | *** |
3446-000057 | GROUND PROXIMITY WARNING SYSTEM ALTITUDE CALLOUTS - 100, 50, 30, 10 | *** |
3451-000023 | VOR/MARKER BEACON - ALLIEDSIGNAL RECEIVER P/N 066-50012-0101 - BFE/SPE | *** |
3453B866A17 | ATC SYSTEM - HONEYWELL INTERNATIONAL INC ATC TRANSPONDER P/N 066-01127- 1602 - ELS/EHS/ES AND TCAS CHANGE 7 COMPLIANT - HONEYWELL INTERNATIONAL INC CONTROL PANEL P/N ###-###-#### - BFE/SPE | *** |
3455-000020 | DISTANCE MEASURING EQUIPMENT (DME) - ALLIEDSIGNAL INTERROGATOR P/N 066- 50013-0101 - BFE/SPE | *** |
3457B696A24 | AUTOMATIC DIRECTION FINDING (ADF) SYSTEM - PARTIAL PROVISIONS | *** |
3461A150B73 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - ENGINE-OUT STANDARD INSTRUMENT DEPARTURES (SID'S) - ENABLE | *** |
3461A425A10 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - NAVIGATION DATABASE - CUSTOMER SUPPLIED | *** |
3461A425A17 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - AIRLINE OPERATIONAL COMMUNICATIONS DATA LINK (AOC DL) - FANS FEATURE ACTIVATION | *** |
3461A425A30 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS)- ABEAM WAYPOINTS- ENABLE | *** |
3461A425A48 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - ACTIVATE COLOR OPERATION | *** |
3461A890A76 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - NAVIGATION DISPLAY - MISSED APPROACH IN CYAN UNTIL ACTIVE - ENABLE | *** |
3461B696D59 | MP - FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) -AIR TRAFFIC SERVICES DATA LKINK (ATS DL) -FANS FEATURE ACTIVATION | *** |
3461B696K97 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - VERTICAL RNP DEFAULT VALUE - REVISION | *** |
3461B696M48 | FLIGHT MANAGEMENT COMPUTING SYSTEM (FMCS) - INTENT DATA TRANSMITTED VIA THE FMC INTENT DATA DEDICATED OUTPUT BUS - ENABLE | *** |
3461C175A14 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - FANS CAPABLE MCDU WITH ATC KEYBOARD - INSTALLATION-SFE | *** |
3461C175A32 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - COMMON VNAV - ENABLE | *** |
3461C175A34 | FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - SPEED PROPAGATION FROM THE CRUISE PAGE TO THE DESCENT PAGE - ENABLE | *** |
3461C430J05 | FLIGHT MANAGEMENT COMPUTING SYSTEM (FMCS) - VOR INHIBIT | *** |
3461C594A26 | FLIGHT MANAGEMENT COMPUTING SYSTEM (FMCS) - INTENT DATA TRANSMITTED TO ACARS - ENABLE | *** |
3511-000011 | NO REMOTE CREW OXYGEN FILL STATION | *** |
3511B696M31 | CREW OXYGEN MASKS AND SMOKE GOGGLES - CAPTAIN, FIRST OFFICER, FIRST OBSERVER AND SECOND OBSERVER - BFE/SPE | *** |
P.A. 1810 SA-84 | BOEING PROPRIETARY | Page 4 |
BOEING PROPRIETARY |
CR | Title | 2011 $ Price Per A/C |
3511D322B89 | MP - CREW OXYGEN MASKS - WITH SECOND OBSERVER - REPLACEMENT - AVOX FULL FACE MASKS WITH BUILT-IN GOGGLES IN LIEU OF THE EXISTING AVOX MASKS WITH SEPARATE SMOKE GOGGLES - BFE | *** |
3811-000017 | POTABLE WATER - SERVICEABLE TO 40 GALLONS | *** |
3830C882K61 | WASTE DISPOSAL - 4"" SERVICE PANEL LAVATORY DRAIN VALVE | *** |
3832-000032 | VACUUM WASTE SYSTEM - MONOGRAM TOILET ASSEMBLIES | *** |
3910D322A11 | AFT ELECTRONICS PANEL ARRANGEMENT | *** |
5231A561C54 | CARGO DOOR - SOLID SKIN | *** |
5300-000027 | UNDERSEAT FLOOR PANELS, LOW TRAFFIC CAPABILITY | *** |
5352A298A28 | RADOME- NORDAM- SFE | *** |
5730B290A42 | PARTIAL PROVISIONS FOR AVIATION PARTNERS BOEING (APB) WINGLET INSTALLATION | *** |
5730C581A10 | WINGLET INSTALLATION - AVIATION PARTNERS BOEING (APB) - BFE/SPE (737-800) | *** |
7200-000125 | CFM56-7 ENGINES - 7B26 RATING | *** |
7900-000116 | LUBRICATING OIL - MOBIL JET II | *** |
MISC | INTERIOR ALLOWANCE | *** |
MISC DOOR | FAA FLIGHT DECK DOOR | *** |
MISC P & O | PEAKS & OBSTACLES | *** |
MISC/FAA4 | FLAME PROPAGATION - INSULATION BLANKETS (FAA) | *** |
MISC/FAA5 | FIRE PENETRATION - BURNTHROUGH, FAR 25.856(b) | *** |
OPTIONS: 200 | TOTALS: | *** |
ADDITIONAL PRODUCTION CHANGES, INCLUDING CHANGES FOR NON-ETOPS (AS OF SA-82):
0224B372J97 | RO - EXTENDED RANGE TWIN ENGINE OPERATIONS (ETOPS) - DELETION | *** |
0252D322D01 | MP - INSTRUMENTATION, AIRPLANE AND FUEL MEASURING STICK MANUALS IN ENGLISH UNITS - TEMPERATURE IN DEGREES CELSIUS IN LIEU OF TEMPERATURE IN DEGREES FAHRENHEIT | *** |
1110D185K68 | MP - EXTERIOR COLOR SCHEMES AND MARKINGS - ADDITION - ETOPS MAINTENANCE MARKING | *** |
1110D360N93 | RO - EXTERIOR COLOR SCHEMES AND MARKINGS - DELETION - ETOPS MAINTENANCE MARKING | *** |
2300D322C81 | RO - FPO - COMMUNICATIONS - DELETION OF DUAL HONEYWELL HF COMMUNICATIONS SYSTEM INCLUDING PROVISIONS AND DELETE E6 EQUIPMENT RACK - RETAIN INTEGRATED AUDIO SELECTOR PANEL WIRING - BFE | *** |
2312C028G60 | MP - VHF COMMUNICATIONS SYSTEM - ACTIVATION OF KEYLINE TIMER | *** |
2500D360N91 | RO - PASSENGER COMPARTMENT - DELETION - EMERGENCY EQUIPMENT AND CENTER OVERHEAD STOWAGE - BFE | *** |
2520D185M20 | MP - PASSENGER COMPARTMENT - REPLACEMENT - GALLEY AND ENTRYWAY MAT MATERIAL - SCHNELLER - BFE | *** |
2525D360N76 | MP - PASSENGER COMPARTMENT SEATS - REVISION - B/E AEROSPACE - BFE | *** |
2525D360T83 | MP - PASSENGER COMPARTMENT SEATS - REVISION - TRAY TABLE LATCH - B E AEROSPACE - BFE | *** |
2527D360L35 | MP - FLOOR COVERING - REPLACEMENT - CARPET TILES IN PASSENGER CABIN - WITH 18MM WIDE PHOTOLUM - INTERFACEFLOR IN LIEU OF MOHAWK - BFE | *** |
2527D360T79 | MP - FLOOR COVERING - REVISION - CARPET AND GALLEY MAT - BFE | *** |
2527D360T90 | MP - FLOOR COVERING - REVISION - CARPET TILES - INTERFACEFLOR - BFE | *** |
2529D384F68 | MP - DOOR WARNING STRAP - REPLACEMENT - FORWARD LH DOOR | *** |
2530D360T82 | MP - GALLEY - REPLACEMENT - WASTE CONTAINER - COMPOSITES UNLIMITED - BFE | *** |
2552D560A01 | MP - FPO - LOWER LOBE (CONTAINERIZED) CARGO COMPARTMENT - REPLACEMENT - FWD AND AFT CARGO LINERS | *** |
2562D360N20 | MP - OVERWATER EMERGENCY EQUIPMENT - ADDITION - LIFE RAFTS IN CENTER OVERHEAD STOWAGE - EASTERN AERO MARINE - BFE | *** |
2564D185K61 | MP - DETACHABLE EMERGENCY EQUIPMENT - PASSENGER COMPARTMENT - ADDITION - OXYGEN BOTTLE AND MASK - SCOTT AVIATION - BFE | *** |
2564D360M44 | MP - DETACHABLE EMERGENCY EQUIPMENT - REVISION - PASSENGER COMPARTMENT - BFE | *** |
2564D360M82 | MP - DETACHABLE EMERGENCY EQUIPMENT - PASSENGER COMPARTMENT - ADDITION - PBE IN FWD LH MONUMENT - ESSEX - BFE | *** |
2564D360P90 | MP - DETACHABLE EMERGENCY EQUIPMENT - DELETION - SMOKE HOODS - ESSEX CORPORATION - BFE | *** |
2564D360T14 | MP - DETACHABLE EMERGENCY EQUIPMENT - FIRST AID KIT - PROCUREMENT REVISION - BFE TO BFBI | *** |
2732D322C99 | MP - STALL WARNING SYSTEM - STALL MANAGEMENT YAW DAMPER COMPUTERS (SMYD) - REPLACEMENT- SMYD COMPUTERS WITH AUTOSTOW FUNCTIONALITY, P/N 285A1010-109 IN LIEU OF THE EXISTING SMYD COMPUTERS, P/N 285A1010-9 - SFE | *** |
3133A051B38 | MP - MULTI-INPUT PRINTER - ARINC 740 - MILTOPE P/N 497126-31 - BFE | *** |
3133B694B49 | RO - ARINC 740 MULTI-INPUT PRINTER REMOVAL FROM PROVISIONS IN THE AFT AISLE STAND - HONEYWELL - P/N ###-###-#### - BFE | *** |
P.A. 1810 SA-84 | BOEING PROPRIETARY | Page 5 |
BOEING PROPRIETARY |
CR | Title | 2011 $ Price Per A/C |
3133D322C34 | MP - ARINC 740 MULTI-INPUT PRINTER - REPLACEMENT - HONEYWELL P/N ###-###-#### IN LIEU OF MILTOPE P/N 497126-31 - BFE | *** |
3211D830A06 | MP - MAIN GEAR - REVISION - STRENGTHENED MAIN LANDING GEAR AXLES | *** |
3430B694H08 | MP - ILS/GPS MULTI-MODE RECEIVER (MMR) - INSTALLATION - SEXTANT IN LIEU OF HONEYWELL - BFE | *** |
3433D354B57 | MP - RADIO ALTIMETER SYSTEM - REPLACEMENT - HONEYWELL LOW RANGE RADIO ALTIMETER P/N 066-50007-0531 IN LIEU OF EXISTING P/M 066-500007-0111 - BFE | *** |
3455D354B43 | MP - DISTANCE MEASURING EQUIPMENT (DME) SCANNING INTERROGATOR - REPLACEMENT - HONEYWELL P/N 066-50013-0111 IN LIEU OF P/N 066-50013-0101 - BFE | *** |
3461D322C75 | RO - FLIGHT MANAGEMENT COMPUTER SYSTEM (FMCS) - DEACTIVATION - AIR TRAFFIC SERVICES DATA LINK (ATS DL) | *** |
3910D322C28 | MP - AFT ELECTRONICS PANEL ARRANGEMENT - REVISION - AFT ELECTRONICS PANEL ARRANGEMENT WITH ARINC 740 PRINTER INSTALLATION IN LIEU OF THE EXISTING AFT ELECTRONICS PANEL ARRANGEMENT | *** |
3910D322C77 | RO - AFT ELECTRONICS PANEL - REVISION | *** |
7200A367A61 | MP - CFM56-7 ENGINES - 7B27 RATING IN LIEU OF 7B26 RATING | *** |
7200D977A01 | MP - CFM56-7 ENGINES - 7B27/F THRUST RATING IN LIEU OF THE EXISTING 7B27 THRUST RATING | *** |
OPTIONS: 35 | TOTALS: | *** |
GRAND TOTALS: | *** |
P.A. 1810 SA-84 | BOEING PROPRIETARY | Page 6 |
Attachment A to SWA-PA-1810-LA1001315R2 | ||
Page 1 of 2 |
***
Letter Agmt SWA-PA-1810-LA-1001315R2; paragraph 3
No. | Model | Aircraft Block | MSN's | Current Delivery Mo. | Base Year | *** | |||
1 | 737-700 | T-W-2b | 36,962 | July-11 | 1999 | *** | |||
2 | 737-700 | T-W-2b | 36,963 | July-11 | 1999 | *** | |||
3 | 737-700 | T-W-2b | 36,965 | August-11 | 1999 | *** | |||
4 | 737-700 | T-W-2b | 36,967 | October-11 | 1999 | *** | |||
5 | 737-800 | 800LUV | 36,980 | March-12 | 2011 | *** | |||
6 | 737-800 | 800LUV | 36,983 | April-12 | 2011 | *** | |||
7 | 737-800 | 800LUV | 36,985 | May-12 | 2011 | *** | |||
8 | 737-800 | 800LUV | 36,987 | May-12 | 2011 | *** | |||
9 | 737-800 | 800LUV | 36,990 | July-12 | 2011 | *** | |||
10 | 737-800 | 800LUV | 36,992 | August-12 | 2011 | *** | |||
11 | 737-800 | 800LUV | 36,994 | September-12 | 2011 | *** | |||
12 | 737-800 | 800LUV | 37,003 | November-12 | 2011 | *** | |||
13 | 737-800 | 800LUV | 37,009 | December-12 | 2011 | *** | |||
14 | 737-800 | 800LUV | 36,973 | March-13 | 2011 | *** | |||
15 | 737-800 | 800LUV | 36,998 | March-13 | 2011 | *** | |||
16 | 737-800 | 800LUV | 36,908 | April-13 | 2011 | *** | |||
17 | 737-800 | 800LUV | 36,933 | September-13 | 2011 | *** | |||
18 | 737-800 | 800LUV | 42,526 | November-13 | 2011 | ||||
19 | 737-800 | 800LUV | 37,004 | March-14 | 2011 | ||||
20 | 737-800 | 800LUV | 42,521 | May-14 | 2011 | ||||
21 | 737-800 | 800LUV | 42,522 | June-14 | 2011 | ||||
22 | 737-800 | 800LUV | tbd | June-14 | 2011 | ||||
23 | 737-800 | 800LUV | tbd | June-14 | 2011 | ||||
24 | 737-800 | 800LUV | 42,523 | June-14 | 2011 | ||||
25 | 737-800 | 800LUV | tbd | July-14 | 2011 | ||||
26 | 737-800 | 800LUV | tbd | July-14 | 2011 | ||||
27 | 737-800 | 800LUV | tbd | July-14 | 2011 | ||||
28 | 737-800 | 800LUV | 42,524 | August-14 | 2011 | ||||
29 | 737-800 | 800LUV | 42,525 | August-14 | 2011 | ||||
30 | 737-800 | 800LUV | 36,935 | September-14 | 2011 | ||||
31 | 737-800 | 800LUV | 42,527 | September-14 | 2011 | ||||
32 | 737-800 | 800LUV | 42,528 | September-14 | 2011 | ||||
33 | 737-800 | 800LUV | 42,531 | September-14 | 2011 | ||||
34 | 737-800 | 800LUV | 36,909 | October-14 | 2011 | ||||
35 | 737-800 | 800LUV | 37,043 | November-14 | 2011 | ||||
36 | 737-800 | 800LUV | 42,529 | December-14 | 2011 | ||||
37 | 737-800 | 800LUV | 42,530 | December-14 | 2011 | ||||
38 | 737-800 | 800LUV | 37,045 | December-14 | 2011 | ||||
39 | 737-800 | 800LUV | 37,037 | December-14 | 2011 | ||||
40 | 737-700 | 700LUV | 42,535 | January-15 | 2011 | ||||
41 | 737-700 | 700LUV | 42,536 | February-15 | 2011 | ||||
42 | 737-700 | 700LUV | 42,537 | March-15 | 2011 | ||||
43 | 737-700 | 700LUV | 42,538 | April-15 | 2011 | ||||
44 | 737-700 | 700LUV | 42,539 | May-15 | 2011 | ||||
45 | 737-700 | 700LUV | 42,540 | June-15 | 2011 | ||||
46 | 737-700 | 700LUV | 42,541 | July-15 | 2011 | ||||
47 | 737-700 | 700LUV | 42,542 | August-15 | 2011 | ||||
48 | 737-700 | 700LUV | 42,543 | September-15 | 2011 |
SA-84 |
Attachment A to SWA-PA-1810-LA1001315R2 | ||
Page 2 of 2 |
49 | 737-700 | 700LUV | 36,940 | November-15 | 2011 | |
50 | 737-700 | 700LUV | 36,938 | April-16 | 2011 | |
51 | 737-700 | 700LUV | 36,939 | May-16 | 2011 | |
52 | 737-700 | 700LUV | 36,945 | July-16 | 2011 | |
53 | 737-700 | 700LUV | 36,977 | September-16 | 2011 | |
54 | 737-700 | 700LUV | 42,532 | January-17 | 2011 | |
55 | 737-700 | 700LUV | 36,910 | January-17 | 2011 | |
56 | 737-700 | 700LUV | 36,970 | February-17 | 2011 | |
57 | 737-700 | 700LUV | 36,969 | February-17 | 2011 | |
58 | 737-700 | 700LUV | 36,972 | March-17 | 2011 | |
59 | 737-700 | 700LUV | 36,927 | April-17 | 2011 | |
60 | 737-700 | 700LUV | 36,974 | April-17 | 2011 | |
61 | 737-700 | 700LUV | 36,925 | May-17 | 2011 | |
62 | 737-700 | 700LUV | 36,975 | May-17 | 2011 | |
63 | 737-700 | 700LUV | 36,976 | June-17 | 2011 | |
64 | 737-700 | 700LUV | 36,926 | January-18 | 2011 | |
65 | 737-700 | 700LUV | 42,533 | February-18 | 2011 | |
66 | 737-700 | 700LUV | 42,545 | February-18 | 2011 | |
67 | 737-700 | 700LUV | 42,534 | March-18 | 2011 | |
68 | tbd | |||||
69 | tbd | |||||
70 | tbd | |||||
71 | tbd |
SA-84 |
The Boeing Company | ||
P.O. Box 3707 | ||
Seattle, WA 98124-2207 | ||
SWA-PA-1810-LA-1105885R2
Southwest Airlines Co.
2702 Love Field Drive
P.O. Box 36611
Dallas, Texas ###-###-####
Subject: | *** |
Reference: | a) Purchase Agreement No. 1810 (Purchase Agreement) between The Boeing Company (Boeing) and Southwest Airlines Co. (Buyer) relating to Model 737-7H4 and 737-8H4 aircraft |
This letter agreement (Letter Agreement) amends and supplements the Purchase Agreement. Unless otherwise noted, this Letter Agreement is solely applicable to the Block 700LUV Aircraft identified in Table 1a of the Purchase Agreement (Block 700LUV Aircraft). All terms used but not defined in this Letter Agreement shall have the same meaning as in the Purchase Agreement.
1. ***
SWA-PA-1810-LA-1105885R2 | Page 1 | |
*** | SA-84 | |
BOEING PROPRIETARY |
2. ***
SWA-PA-1810-LA-1105885R2 | Page 2 | |
*** | SA-84 | |
BOEING PROPRIETARY |
3. ***
4. ***
5. Assignment.
Unless otherwise noted herein, *** This Letter Agreement cannot be assigned, in whole or in part, without the prior written consent of Boeing.
SWA-PA-1810-LA-1105885R2 | Page 3 | |
*** | SA-84 | |
BOEING PROPRIETARY |
6. Confidentiality
Buyer understands that certain commercial and financial information contained in this Letter Agreement including any attachments hereto is considered by Boeing as confidential. Buyer agrees that it will treat this Letter Agreement and the information contained herein as confidential and will not, without the prior written consent of Boeing, disclose this Letter Agreement or any information contained herein to any other person or entity except as provided in Letter Agreement No. 6-1162-RLL-934, as amended.
Very truly yours,
THE BOEING COMPANY | ||
By | /s/ Jeff Solomon | |
Its | Attorney-In-Fact | |
ACCEPTED AND AGREED TO this | ||
Date: | September 20, 2013 | |
SOUTHWEST AIRLINES CO. | ||
By | /s/ Tammy Romo | |
Its | SVP & CFO |
SWA-PA-1810-LA-1105885R2 | Page 4 | |
*** | SA-84 | |
BOEING PROPRIETARY |