Service Bulletin B787-81205-SB380009-00 WATER/WASTE - Water System

- Potable Water System - Couplings Replacement

Publication: B787-81205-SB380009-00 Issue 002, 09 Dec 2015

BOEING PROPRIETARY, CONFIDENTIAL AND/OR TRADE SECRET

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ECCN: 9E991

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PM Applicability (Publication Module applicability)

787-8 Airplanes. Refer to Data Module SB B787-A-38-00-0009-00A-932A-D, Paragraph 1., Effectivity for the

list of affected airplanes.

TITLE PAGE B787-81205-SB380009-00

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2.0

B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

Table of Contents

Page

Revision Transmittal Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

PLANNING INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18

1. Effectivity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

A. Airplanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

B. Spares Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

2. Concurrent Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

3. Reason . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

4. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

5. Compliance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22

6. Approval . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22

7. Manpower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22

8. Weight and Balance Changes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30

9. Electrical Load Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30

10. References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30

A. Existing Data: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30

B. Data Supplied with this Service Bulletin: . . . . . . . . . . . . . . . . . . . . . . . . . . 31

C. Installation Requirement Modules Used in the Preparation of this Service Bulletin: . . . 31

11. Publications Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

12. Interchangeability and Intermixability of Parts . . . . . . . . . . . . . . . . . . . . . . . . . 31

13. Software Accomplishment Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31

MATERIAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32

1. Material - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32

2. Industry Support Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38

3. Parts Necessary for Each Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38

A. Kits/Parts: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38

B. Parts and Materials Supplied by the Operator: . . . . . . . . . . . . . . . . . . . . . . . 47

C. Parts Modified and Reidentified: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47

D. Parts Removed and Not Replaced: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47

4. Parts Necessary to Change Spares . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47

5. Special Tooling - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 47

6. Special Tooling Necessary to do this Service Bulletin . . . . . . . . . . . . . . . . . . . . . 47

ACCOMPLISHMENT INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 48

1. GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 50

2. WORK INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 51

Task 1 – REPLACEMENT OF COUPLINGS LOCATED ABOVE FWD EE BAY [Group 1-11: ]. . . . . . . 57

Task 2 – REPLACEMENT OF COUPLINGS LOCATED ABOVE FWD EE BAY [Group 12-13: ]. . . . . . 62

Task 3 – REPLACEMENT OF COUPLINGS LOCATED ABOVE FWD EE BAY [Group 14-16: ]. . . . . . 67

Task 4 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY [Group 1: ]. . . . . . . . . 72

Task 5 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY [Group 2, 12: ]. . . . . . . 83

TABLE OF CONTENTS B787-81205-SB380009-00

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Task 6 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY [Group 3, 14: ]. . . . . . . 94

Task 7 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY [Group 4, 15: ]. . . . . . 105

Task 8 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY [Group 5: ]. . . . . . . . 116

Task 9 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY [Group 6: ]. . . . . . . . 121

Task 10 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY [Group 7, 13: ]. . . . . 132

Task 11 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY [Group 16: ]. . . . . . . 143

Task 12 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY [Group 8: ]. . . . . . . 158

Task 13 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY [Group 9: ]. . . . . . . 176

Task 14 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY [Group 10: ]. . . . . . . 192

Task 15 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY [Group 11: ]. . . . . . . 206

Appendix A – 787 POTABLE WATER SHROUD INSTALLATION [Group 1-16:]. . . . . . . . . . . . . . 219

TABLE OF CONTENTS B787-81205-SB380009-00

Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

List of Illustrations

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Description

Group 1-16:

Table 1 List of Illustrations - Service Bulletin B787-81205-SB380009-00

ICN Used In

ICN-B787-A-000061-A-81205-08917-A-01-1 B787-A-38-00-0009-00A-931C-D Issue 002

ICN-B787-A-000061-A-81205-08918-A-01-1 B787-A-38-00-0009-01A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08919-A-01-1 B787-A-38-00-0009-01A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08920-A-01-1 B787-A-38-00-0009-01A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08921-A-01-1 B787-A-38-00-0009-02A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08922-A-01-1 B787-A-38-00-0009-02A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08923-A-01-1 B787-A-38-00-0009-02A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08924-A-01-1 B787-A-38-00-0009-03A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08925-A-01-1 B787-A-38-00-0009-03A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08926-A-01-1 B787-A-38-00-0009-03A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08927-A-01-1 B787-A-38-00-0009-04A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08928-A-01-1 B787-A-38-00-0009-04A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08929-A-01-1 B787-A-38-00-0009-04A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08930-A-01-1 B787-A-38-00-0009-04A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08931-A-01-1 B787-A-38-00-0009-04A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08932-A-01-1 B787-A-38-00-0009-04A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08933-A-01-1 B787-A-38-00-0009-04A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08934-A-01-1 B787-A-38-00-0009-04A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08935-A-01-1 B787-A-38-00-0009-04A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08936-A-01-1 B787-A-38-00-0009-05A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08937-A-01-1 B787-A-38-00-0009-05A-933B-D Issue 002

Applicable To: B787-A-38-00-0009-00A-00AA-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 1 List of Illustrations - Service Bulletin B787-81205-SB380009-00

ICN Used In

ICN-B787-A-000061-A-81205-08938-A-01-1 B787-A-38-00-0009-05A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08939-A-01-1 B787-A-38-00-0009-05A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08940-A-01-1 B787-A-38-00-0009-05A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08941-A-01-1 B787-A-38-00-0009-05A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08942-A-01-1 B787-A-38-00-0009-05A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08943-A-01-1 B787-A-38-00-0009-05A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08944-A-01-1 B787-A-38-00-0009-06A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08945-A-01-1 B787-A-38-00-0009-06A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08946-A-01-1 B787-A-38-00-0009-06A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08947-A-01-1 B787-A-38-00-0009-06A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08948-A-01-1 B787-A-38-00-0009-06A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08949-A-01-1 B787-A-38-00-0009-06A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08950-A-01-1 B787-A-38-00-0009-06A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08951-A-01-1 B787-A-38-00-0009-06A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08952-A-01-1 B787-A-38-00-0009-07A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08953-A-01-1 B787-A-38-00-0009-07A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08954-A-01-1 B787-A-38-00-0009-07A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08955-A-01-1 B787-A-38-00-0009-07A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08956-A-01-1 B787-A-38-00-0009-07A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08957-A-01-1 B787-A-38-00-0009-07A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08958-A-01-1 B787-A-38-00-0009-07A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08959-A-01-1 B787-A-38-00-0009-07A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08960-A-01-1 B787-A-38-00-0009-08A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08961-A-01-1 B787-A-38-00-0009-08A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08962-A-01-1 B787-A-38-00-0009-08A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08963-A-01-1 B787-A-38-00-0009-09A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08964-A-01-1 B787-A-38-00-0009-09A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08965-A-01-1 B787-A-38-00-0009-09A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08966-A-01-1 B787-A-38-00-0009-09A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08967-A-01-1 B787-A-38-00-0009-09A-933B-D Issue 002

Applicable To: B787-A-38-00-0009-00A-00AA-D

Model 787 Issue 002, 09 Dec 2015

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AIRCRAFT SERVICE BULLETIN
Table 1 List of Illustrations - Service Bulletin B787-81205-SB380009-00

ICN Used In

ICN-B787-A-000061-A-81205-08968-A-01-1 B787-A-38-00-0009-09A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08969-A-01-1 B787-A-38-00-0009-09A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08970-A-01-1 B787-A-38-00-0009-09A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08971-A-01-1 B787-A-38-00-0009-10A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08972-A-01-1 B787-A-38-00-0009-10A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08973-A-01-1 B787-A-38-00-0009-10A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08974-A-01-1 B787-A-38-00-0009-10A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08975-A-01-1 B787-A-38-00-0009-10A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08976-A-01-1 B787-A-38-00-0009-10A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08977-A-01-1 B787-A-38-00-0009-10A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08978-A-01-1 B787-A-38-00-0009-10A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08979-A-01-1 B787-A-38-00-0009-11A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08980-A-01-1 B787-A-38-00-0009-11A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08981-A-01-1 B787-A-38-00-0009-11A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08982-A-01-1 B787-A-38-00-0009-11A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08983-A-01-1 B787-A-38-00-0009-11A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08984-A-01-1 B787-A-38-00-0009-11A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08985-A-01-1 B787-A-38-00-0009-11A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08986-A-01-1 B787-A-38-00-0009-11A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08987-A-01-1 B787-A-38-00-0009-11A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08988-A-01-1 B787-A-38-00-0009-11A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08989-A-01-1 B787-A-38-00-0009-11A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08990-A-01-1 B787-A-38-00-0009-11A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08991-A-01-1 B787-A-38-00-0009-12A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08992-A-01-1 B787-A-38-00-0009-12A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08993-A-01-1 B787-A-38-00-0009-12A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08994-A-01-1 B787-A-38-00-0009-12A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08995-A-01-1 B787-A-38-00-0009-12A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08996-A-01-1 B787-A-38-00-0009-12A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08997-A-01-1 B787-A-38-00-0009-12A-933B-D Issue 002

Applicable To: B787-A-38-00-0009-00A-00AA-D

Model 787 Issue 002, 09 Dec 2015

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Table 1 List of Illustrations - Service Bulletin B787-81205-SB380009-00

ICN Used In

ICN-B787-A-000061-A-81205-08998-A-01-1 B787-A-38-00-0009-12A-933B-D Issue 002

ICN-B787-A-000061-A-81205-08999-A-01-1 B787-A-38-00-0009-12A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09000-A-01-1 B787-A-38-00-0009-12A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09001-A-01-1 B787-A-38-00-0009-12A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09002-A-01-1 B787-A-38-00-0009-12A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09003-A-01-1 B787-A-38-00-0009-12A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09004-A-01-1 B787-A-38-00-0009-12A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09005-A-01-1 B787-A-38-00-0009-12A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09006-A-01-1 B787-A-38-00-0009-13A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09007-A-01-1 B787-A-38-00-0009-13A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09008-A-01-1 B787-A-38-00-0009-13A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09009-A-01-1 B787-A-38-00-0009-13A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09010-A-01-1 B787-A-38-00-0009-13A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09011-A-01-1 B787-A-38-00-0009-13A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09012-A-01-1 B787-A-38-00-0009-13A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09013-A-01-1 B787-A-38-00-0009-13A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09014-A-01-1 B787-A-38-00-0009-13A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09015-A-01-1 B787-A-38-00-0009-13A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09016-A-02-1 B787-A-38-00-0009-13A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09017-A-02-1 B787-A-38-00-0009-13A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09018-A-01-1 B787-A-38-00-0009-13A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09019-A-01-1 B787-A-38-00-0009-14A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09020-A-01-1 B787-A-38-00-0009-14A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09021-A-01-1 B787-A-38-00-0009-14A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09022-A-01-1 B787-A-38-00-0009-14A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09023-A-01-1 B787-A-38-00-0009-14A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09024-A-01-1 B787-A-38-00-0009-14A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09025-A-01-1 B787-A-38-00-0009-14A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09026-A-01-1 B787-A-38-00-0009-14A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09027-A-01-1 B787-A-38-00-0009-14A-933B-D Issue 002

Applicable To: B787-A-38-00-0009-00A-00AA-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 1 List of Illustrations - Service Bulletin B787-81205-SB380009-00

ICN Used In

ICN-B787-A-000061-A-81205-09028-A-01-1 B787-A-38-00-0009-14A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09029-A-01-1 B787-A-38-00-0009-14A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09030-A-01-1 B787-A-38-00-0009-15A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09031-A-01-1 B787-A-38-00-0009-15A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09032-A-01-1 B787-A-38-00-0009-15A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09033-A-01-1 B787-A-38-00-0009-15A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09034-A-01-1 B787-A-38-00-0009-15A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09035-A-01-1 B787-A-38-00-0009-15A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09036-A-01-1 B787-A-38-00-0009-15A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09037-A-01-1 B787-A-38-00-0009-15A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09038-A-01-1 B787-A-38-00-0009-15A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09039-A-01-1 B787-A-38-00-0009-15A-933B-D Issue 002

ICN-B787-A-000061-A-81205-09040-A-01-1 B787-A-38-00-0009-0AA-931D-D Issue 002

ICN-B787-A-000061-A-81205-09041-A-01-1 B787-A-38-00-0009-0AA-931D-D Issue 002

ICN-B787-A-000061-A-81205-09042-A-01-1 B787-A-38-00-0009-0AA-931D-D Issue 002

ICN-B787-A-000061-A-81205-09043-A-01-1 B787-A-38-00-0009-0AA-931D-D Issue 002

ICN-B787-A-000061-A-81205-09044-A-01-1 B787-A-38-00-0009-0AA-931D-D Issue 002

ICN-B787-A-000061-A-81205-09045-A-01-1 B787-A-38-00-0009-0AA-931D-D Issue 002

ICN-B787-A-000061-A-81205-09046-A-01-1 B787-A-38-00-0009-0AA-931D-D Issue 002

ICN-B787-A-000061-A-81205-09047-A-01-1 B787-A-38-00-0009-0AA-931D-D Issue 002

ICN-B787-A-000061-A-81205-09048-A-01-1 B787-A-38-00-0009-0AA-931D-D Issue 002

ICN-B787-A-000061-A-81205-09049-A-01-1 B787-A-38-00-0009-0AA-931D-D Issue 002

Applicable To: B787-A-38-00-0009-00A-00AA-D

Model 787 End of data module Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

List of Effective Data Modules

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Description

Group 1-16:

Table 1 List of Effective Data Modules - Service Bulletin B787-81205-SB380009-00

Data Module – Information Name Issue Issue Status Issue Date

B787-A-38-00-0009-00A-00AA-D – List of Illustrations 002 Changed 2015-12-09

B787-A-38-00-0009-00A-00SA-D – List of Effective Data Modules 002 Changed 2015-12-09

B787-A-38-00-0009-00A-931B-D – Revision Transmittal Information 001 New 2015-12-09

B787-A-38-00-0009-00A-931C-D – Summary 002 Changed 2015-12-09

B787-A-38-00-0009-00A-932A-D – PLANNING INFORMATION 002 Changed 2015-12-09

B787-A-38-00-0009-00A-934A-D – MATERIAL INFORMATION 002 Changed 2015-12-09

B787-A-38-00-0009-00A-933A-D – ACCOMPLISHMENT INSTRUCTIONS 002 Changed 2015-12-09

B787-A-38-00-0009-01A-933B-D – Task 1 – REPLACEMENT OF COU- 002 Changed 2015-12-09

PLINGS LOCATED ABOVE FWD EE BAY [Group 1-11: ]

B787-A-38-00-0009-02A-933B-D – Task 2 – REPLACEMENT OF COU- 002 Changed 2015-12-09

PLINGS LOCATED ABOVE FWD EE BAY [Group 12-13: ]

B787-A-38-00-0009-03A-933B-D – Task 3 – REPLACEMENT OF COU- 002 Changed 2015-12-09

PLINGS LOCATED ABOVE FWD EE BAY [Group 14-16: ]

B787-A-38-00-0009-04A-933B-D – Task 4 – REPLACEMENT OF COU- 002 Changed 2015-12-09

PLINGS LOCATED ABOVE AFT EE BAY [Group 1: ]

B787-A-38-00-0009-05A-933B-D – Task 5 – REPLACEMENT OF COU- 002 Changed 2015-12-09

PLINGS LOCATED ABOVE AFT EE BAY [Group 2, 12: ]

B787-A-38-00-0009-06A-933B-D – Task 6 – REPLACEMENT OF COU- 002 Changed 2015-12-09

PLINGS LOCATED ABOVE AFT EE BAY [Group 3, 14: ]

B787-A-38-00-0009-07A-933B-D – Task 7 – REPLACEMENT OF COU- 002 Changed 2015-12-09

PLINGS LOCATED ABOVE AFT EE BAY [Group 4, 15: ]

B787-A-38-00-0009-08A-933B-D – Task 8 – REPLACEMENT OF COU- 002 Changed 2015-12-09

PLINGS LOCATED ABOVE AFT EE BAY [Group 5: ]

B787-A-38-00-0009-09A-933B-D – Task 9 – REPLACEMENT OF COU- 002 Changed 2015-12-09

PLINGS LOCATED ABOVE AFT EE BAY [Group 6: ]

Applicable To: B787-A-38-00-0009-00A-00SA-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 1 List of Effective Data Modules - Service Bulletin B787-81205-SB380009-00

Data Module – Information Name Issue Issue Status Issue Date

B787-A-38-00-0009-10A-933B-D – Task 10 – REPLACEMENT OF COU- 002 Changed 2015-12-09

PLINGS LOCATED ABOVE AFT EE BAY [Group 7, 13: ]

B787-A-38-00-0009-11A-933B-D – Task 11 – REPLACEMENT OF COU- 002 Changed 2015-12-09

PLINGS LOCATED ABOVE AFT EE BAY [Group 16: ]

B787-A-38-00-0009-12A-933B-D – Task 12 – REPLACEMENT OF COU- 002 Changed 2015-12-09

PLINGS LOCATED ABOVE AFT EE BAY [Group 8: ]

B787-A-38-00-0009-13A-933B-D – Task 13 – REPLACEMENT OF COU- 002 Changed 2015-12-09

PLINGS LOCATED ABOVE AFT EE BAY [Group 9: ]

B787-A-38-00-0009-14A-933B-D – Task 14 – REPLACEMENT OF COU- 002 Changed 2015-12-09

PLINGS LOCATED ABOVE AFT EE BAY [Group 10: ]

B787-A-38-00-0009-15A-933B-D – Task 15 – REPLACEMENT OF COU- 002 Changed 2015-12-09

PLINGS LOCATED ABOVE AFT EE BAY [Group 11: ]

B787-A-38-00-0009-0AA-931D-D – Appendix A – 787 POTABLE WATER 002 Changed 2015-12-09

SHROUD INSTALLATION [Group 1-16:]

Applicable To: B787-A-38-00-0009-00A-00SA-D

Model 787 End of data module Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

Revision Transmittal Information

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

References

Reference Title

Service Bulletin

B787-81205-SB380009-00 – Summary

SB B787-A-38-00-0009-00A-931C-D Issue 002

SB B787-A-38-00-0009-00A-932A-D Issue 002, Reason

Paragraph 3.

SB B787-A-38-00-0009-00A-932A-D Issue 002, Publications Affected

Paragraph 11.

Service Bulletin B787-81205-SB380009-00 – Task

13 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE AFT EE BAY [Group 9: ]

SB B787-A-38-00-0009-13A-933B-D Issue 002

SB B787-A-38-00-0009-00A-933A-D Issue 002, Step 2. Work Instructions

SB B787-A-38-00-0009-00A-932A-D Issue 002, Airplanes

Paragraph 1.A.

Description

Group 1-16:

This revision includes all pages of the service bulletin.

1. COMPLIANCE INFORMATION RELATED TO THIS REVISION

Effects of this revision on Airplanes on which Issue 001 was previously done:

None

2. REASON FOR REVISION

As a part of a service bulletin validation program, this change was completed on airplane ZA182 by Service

Bulletin B787-81205-SB38-0009-00 Issue 001 before the release of Issue 002 of this service bulletin. The

change completed on airplane ZA182 by Service Bulletin B787-81205-SB38-0009-00 Issue 001 is equivalent

to the release of Issue 2 of this service bulletin. Airplane ZA182 has the configuration of a Group 9 airplane.

The Issue 002 is sent to add notes in the Background, Reason, Work Instructions, revise the waiting time

in the leak test, and correct the STA number in Figure 11 and Figure 12.

These sections were changed:

Applicable To: B787-A-38-00-0009-00A-931B-D

Model 787 Issue 001, 09 Dec 2015

See Applicability of this data module

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
1. In Data Module Summary, SB B787-A-38-00-0009-00A-931C-D, Paragraph 2., Background - Added a

note.

2. In Data Module SB B787-A-38-00-0009-00A-932A-D, Paragraph 3., Reason - Added a note.

3. In Data Module SB B787-A-38-00-0009-00A-932A-D, Paragraph 11., Publications Affected

4. In Data Module Task 13, SB B787-A-38-00-0009-13A-933B-D - Revised STA number in Figure 11 and

Figure 12.

5. In Data Module SB B787-A-38-00-0009-00A-933A-D, Step 2., Work Instructions - Added a note in

Paragraph 2.A.(5) and 2.B.(6)

6. In Data Module SB B787-A-38-00-0009-00A-933A-D, Step 2., Work Instructions - Added AMM references

in Paragraph 2.B.(4) and 2.B(7)

Change marks are added, except in Data Module SB B787-A-38-00-0009-00A-932A-D, Paragraph 1.A.,

Airplanes and format changes, to show the location of all content changes.

3. REVISION HISTORY

Table 1 

Issue 1: March 26, 2015

Issue 2: December 09, 2015

Applicable To: B787-A-38-00-0009-00A-931B-D

Model 787 End of data module Issue 001, 09 Dec 2015

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

Summary

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

References

Reference Title

SB B787-A-38-00-0009-00A-932A-D Issue 002, Spares Affected

Paragraph 1.B.

SB B787-A-38-00-0009-00A-932A-D Issue 002, Compliance

Paragraph 5.

SB B787-A-38-00-0009-00A-932A-D Issue 002, Weight and Balance Changes

Paragraph 8.

SB B787-A-38-00-0009-00A-932A-D Issue 002, Electrical Load Data

Paragraph 9.

SB B787-A-38-00-0009-00A-932A-D Issue 002, Publications Affected

Paragraph 11.

SB B787-A-38-00-0009-00A-934A-D Issue 002, Kits/Parts

Paragraph 3.A.

SB B787-A-38-00-0009-00A-934A-D Issue 002, Parts and Materials Supplied by the Operator

Paragraph 3.B.

SB B787-A-38-00-0009-00A-934A-D Issue 002, Special Tooling Necessary to do this Service Bulletin

Paragraph 6.

SB B787-A-38-00-0009-00A-932A-D Issue 002, Effectivity

Paragraph 1.

SB B787-A-38-00-0009-00A-934A-D Issue 002, Industry Support Information

Paragraph 2.

SB B787-A-38-00-0009-00A-932A-D Issue 002, Manpower

Paragraph 7.

SB B787-A-38-00-0009-00A-934A-D Issue 002, Material - Price and Availability

Paragraph 1.

Applicable To: B787-A-38-00-0009-00A-931C-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Description

Group 1-16:

1. CONCURRENT REQUIREMENTS

None.

2. BACKGROUND

This service bulletin gives instructions to replace the existing potable water line couplings below the passenger

compartment floor above the FORWARD (FWD) Electrical Electronic (EE) bay in Section 41 and above the

AFT EE bay in Section 46. The new coupling has a strap that will ensure its latches are secure, facilitate a

more rapid visual inspection of the strap engaged over the pawl and reduce the potential to inadvertently

unlatch the coupling after the installation of shrouds over the tubes. If this service bulletin is not incorporated,

water leaking onto equipment in the EE bays could result in an electrical short and potential loss of system

functions.

There have been in-service reports of water leakage in the potable water system due to potable water line

couplings not being installed properly, resulting in delays and replacement of equipment in the EE bays. In

six cases, the cause of the water leakage was due to improper installation of the potable waterline couplings.

Incorporation of this service bulletin will ensure the coupling latches are secure and that after inspection,

reinstallation of the shroud does not accidentally loosen the coupling.

NOTE: Due to common access requirements, operators should consider incorporation of B787-81205-

SB530029 and B787-81205-SB530031 at the same time as this service bulletin is incorporated. 

Boeing Service Related Problem (SRP) 787 SRP-38-0065 is related to this service bulletin.

Boeing Fleet Team Digest (FTD) 787-FTD-38-13006 is related to this service bulletin.

This table is provided to operators for planning purposes only. Refer to the applicable sections for more information.

Table 1 

Planning Data Affected Data Module Reference

Data Module SB B787-A-38-00-0009-00A-932AD, Paragraph 1.B., Spares AffectedSpares Affected No

Data Module SB B787-A-38-00-0009-00A-932AD, Paragraph 5., ComplianceAD Related Yes

Data Module SB B787-A-38-00-0009-00A-932AD, Paragraph 8., Weight and Balance ChangesWeight and Balance Changed No

Data Module SB B787-A-38-00-0009-00A-932AD, Paragraph 9., Electrical Load DataElectrical Load Changed No

Data Module SB B787-A-38-00-0009-00A-932AD, Paragraph 11., Publications AffectedPublications Affected Yes

Data Module SB B787-A-38-00-0009-00A-932AD, Paragraph 11., Publications AffectedAirplane Flight Operations Affected (Flight Crew No

Operations Manual and/or FAA Approved Airplane Flight Manual)

Applicable To: B787-A-38-00-0009-00A-931C-D

Model 787 Issue 002, 09 Dec 2015

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AIRCRAFT SERVICE BULLETIN
Table 1 

Planning Data Affected Data Module Reference

Data Module SB B787-A-38-00-0009-00A-934AD, Paragraph 3.A., Kits/PartsKits/Parts Required Yes

Data Module SB B787-A-38-00-0009-00A-934AD, Paragraph 3.B., Parts and Materials Supplied

by the Operator

Operator Supplied Parts/Material Yes

Data Module SB B787-A-38-00-0009-00A-934AD, Paragraph 6., Special Tooling Necessary to

do this Service Bulletin

Special Tooling Required No

As a part of a service bulletin validation program, this change was completed on airplane ZA182 by Service

Bulletin B787-81205-SB38-0009-00 Issue 001 before the release of Issue 002 of this service bulletin. The

change completed on airplane ZA182 by Service Bulletin B787-81205-SB38-0009-00 Issue 001 is equivalent

to the release of Issue 2 of this service bulletin. Airplane ZA182 has the configuration of a Group 9 airplane.

3. ACTION

(CN-AC45386A)

1. WORK PACKAGE 1

- Drain the potable water system

- Get access to FWD EE bay

- Remove the existing potable waterline couplings

- Install new potable waterline couplings

- Do the Potable Water System - Leak Test

- Close access

2. WORK PACKAGE 2

- Drain the potable water system

- Get access to AFT EE bay

Group 7-11, 13, 16:

- Remove door 3 centerline lavatories and floor super panels under lavatory if necessary to access the

couplings.

Group 1-16:

- Remove the existing potable waterline couplings

- Install new potable waterline couplings

- Do the Potable Water System - Leak Test

Group 7-11, 13, 16:

- Restore door 3 centerline lavatories and floor super panels under lavatory if removed.

Applicable To: B787-A-38-00-0009-00A-931C-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Group 1-16:

- Close access

4. EFFECTIVITY

787-8 Airplanes. Refer to Data Module SB B787-A-38-00-0009-00A-932A-D, Paragraph 1., Effectivity for

the list of affected airplanes.

5. COMPLIANCE

The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to this

service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service

bulletin mandatory.

Refer to Data Module SB B787-A-38-00-0009-00A-932A-D, Paragraph 5., Compliance.

6. INDUSTRY SUPPORT INFORMATION

Refer to Data Module SB B787-A-38-00-0009-00A-934A-D, Paragraph 2., Industry Support Information.

7. MANPOWER

Refer to Data Module SB B787-A-38-00-0009-00A-932A-D, Paragraph 7., Manpower.

8. MATERIAL INFORMATION

Boeing Supplied Kits/Parts.

Refer to Data Module SB B787-A-38-00-0009-00A-934A-D, Paragraph 1., Material - Price and Availability.

Applicable To: B787-A-38-00-0009-00A-931C-D

Model 787 Issue 002, 09 Dec 2015

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AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08917-A-01-1

Figure 1 

Applicable To: B787-A-38-00-0009-00A-931C-D

Model 787 End of data module Issue 002, 09 Dec 2015

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

PLANNING INFORMATION

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

References

Reference Title

SB B787-A-38-00-0009-00A-934A-D Issue 002, Parts Necessary for Each Airplane

Paragraph 3.

SOPM 20-50-01 BOLT AND NUT INSTALLATION

SWPM 20-10-11 Standard Wiring Practices Manual

SWPM 20-10-12 Standard Wiring Practices Manual

787 AMM 06-47-00 INTERIOR ACCESS DOORS AND PANELS

787 AMM 12-14-01 POTABLE WATER SYSTEM MAINTENANCE

787 AMM 24-00-02 CIRCUIT BREAKER INDICATION AND CONTROL

787 AMM 25-24-10 CLOSETS

787 AMM 25-24-20 PARTITION

787 AMM 25-24-22 CLASS DIVIDER

787 AMM 25-25-01 PASSENGER SEAT AND COMPONENTS

787 AMM 25-25-02 PASSENGER SEAT TRACK COVER

787 AMM 25-27-01 CARPET

787 AMM 25-27-02 FLOOR MAT

787 AMM 25-28-05 FLOOR MOUNTED STOWAGE BOX

787 AMM 25-31 GALLEY

787 AMM 25-41 LAVATORY

787 AMM 25-41-00 LAVATORY

787 AMM 38-10-00 POTABLE WATER SYSTEM

787 AMM 53-01-01 FLOOR PANEL

Applicable To: B787-A-38-00-0009-00A-932A-D

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AIRCRAFT SERVICE BULLETIN
Description

Group 1-16:

1. Effectivity

A. Airplanes

This service bulletin is applicable to 787-8 Airplanes, line numbers 6-9, 20-21, 23-125, 127-132, 134-

145, 147-168, 170-180, 182-201, and 203-210 in 16 Group(s). The Variable Numbers and Group information for the applicable airplanes is given below. An equivalent change is on subsequent production

airplanes. Refer to CN-AC45386A for data about this change.

Table 1 

GROUP CONFIGURATION DESCRIPTION

1 - Has different shroud and coupling configuration

2 - Has different shroud and coupling configuration

3 - Has different shroud and coupling configuration

4 - Has different shroud and coupling configuration

5 - Has different shroud and coupling configuration

6 - Has different shroud and coupling configuration

7 - Has different shroud and coupling configuration

8 - Has different shroud and coupling configuration

9 - Has different shroud and coupling configuration

10 - Has different shroud and coupling configuration

11 - Has different shroud and coupling configuration

12 - Has different shroud and coupling configuration

13 - Has different shroud and coupling configuration

14 - Has different shroud and coupling configuration

15 - Has different shroud and coupling configuration

16 - Has different shroud and coupling configuration

Airplane Models: 787-8

Table 2 

Variable Number Group

ZA006 5

ZA100-ZA105 1

ZA116-ZA124 10

ZA135-ZA139 1

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Table 2 

Variable Number Group

ZA175-ZA189 9

ZA215-ZA221 2

ZA230-ZA246 11

ZA260-ZA268 2

ZA270-ZA275 3

ZA285-ZA295 15

ZA317-ZA322 13

ZA327 13

ZA334 13

ZA380-ZA389 8

ZA430-ZA437 3

ZA445-ZA448 4

ZA450-ZA457 6

ZA460-ZA475 16

ZA506-ZA516 7

ZA536-ZA544 3

ZA560 1

ZA561-ZA565 3

ZA576-ZA580 14

ZA586 5

ZA588-ZA589 3

ZA610-ZA612 12

ZA650-ZA651 14

ZA655-ZA658 3

ZA680 3

ZA695 8

ZA778-ZA779 5

B. Spares Affected

None.

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2. Concurrent Requirements

None.

3. Reason

This service bulletin gives instructions to replace the existing potable water line couplings below the passenger compartment floor above the FORWARD (FWD) Electrical Electronic (EE) bay in Section 41 and

above the AFT EE bay in Section 46. The new coupling has a strap that will ensure its latches are secure,

facilitate a more rapid visual inspection of the strap engaged over the pawl and reduce the potential to inadvertently unlatch the coupling after the installation of shrouds over the tubes. If this service bulletin is

not incorporated, water leaking onto equipment in the EE bays could result in an electrical short and potential

loss of system functions.

There have been in-service reports of water leakage in the potable water system due to potable water line

couplings not being installed properly, resulting in delays and replacement of equipment in the EE bays.

In six cases, the cause of the water leakage was due to improper installation of the potable waterline couplings.

Incorporation of this service bulletin will ensure the coupling latches are secure and that after inspection,

reinstallation of the shroud does not accidentally loosen the coupling.

NOTE: Due to common access requirements, operators should consider incorporation of B787-81205-

SB530029 and B787-81205-SB530031 at the same time as this service bulletin is incorporated. 

Boeing Service Related Problem (SRP) 787 SRP-38-0065 is related to this service bulletin.

Boeing Fleet Team Digest (FTD) 787-FTD-38-13006 is related to this service bulletin.

As a part of a service bulletin validation program, this change was completed on airplane ZA182 by Service

Bulletin B787-81205-SB38-0009-00 Issue 001 before the release of Issue 002 of this service bulletin. The

change completed on airplane ZA182 by Service Bulletin B787-81205-SB38-0009-00 Issue 001 is equivalent

to the release of Issue 2 of this service bulletin. Airplane ZA182 has the configuration of a Group 9 airplane.

4. Description

1. WORK PACKAGE 1

- Drain the potable water system

- Get access to FWD EE bay

- Remove the existing potable waterline couplings

- Install new potable waterline couplings

- Do the Potable Water System - Leak Test

- Close access

2. WORK PACKAGE 2

- Drain the potable water system

- Get access to AFT EE bay

Applicable To: B787-A-38-00-0009-00A-932A-D

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Group 7-11, 13, 16:

- Remove door 3 centerline lavatories and floor super panels under lavatory if necessary to access the

couplings.

Group 1-16:

- Remove the existing potable waterline couplings

- Install new potable waterline couplings

- Do the Potable Water System - Leak Test

Group 7-11, 13, 16:

- Restore door 3 centerline lavatories and floor super panels under lavatory if removed.

Group 1-16:

- Close access

The work in this service bulletin is done in the maintenance zone(s) given below.

Table 3 

Affected Maintenance Zones

Model Zone

787-8 117, 118, 145, 146, 251, 252

5. Compliance

The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to this

service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service

bulletin mandatory.

Boeing recommends that the change given in this service bulletin be done within 24 months after the Issue

001 date of this service bulletin.

6. Approval

This service bulletin was examined by the Federal Aviation Administration (FAA). The changes specified

in this service bulletin comply with the applicable regulations and are FAA approved, as well as European

Aviation Safety Agency (EASA)/Joint Aviation Authorities (JAA) approved for all EASA/JAA approved airplanes listed in the service bulletin effectivity. This service bulletin and its approval were based on the airplane

in its original Boeing delivery configuration or as modified by other approved Boeing changes.

If an airplane has a non-Boeing modification or repair that affects a component or system also affected by

this service bulletin, the operator is responsible for obtaining appropriate regulatory agency approval before

incorporating this service bulletin.

7. Manpower

The table below shows an estimate of the task hours necessary to do this change for each airplane. This

estimate is for direct labor only, done by an experienced crew. Adjust the estimate with operator task hour

data if necessary. The estimate does not include lost time. These are some examples of lost time:

– Time to adjust to the workplace

– Time to schedule the work

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– Time to inspect the work

– Time to cure the materials

– Time to make the parts

– Time to find the tools

Group 1-11:

Table 4 Work Package 1 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE FWD EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Potable Water 1 2.50 2.50

Drain

Open Access to 1 0.75 0.75

FWD EE bay

Task 1 1 1.50 1.50

Leak Test 2 7.30 3.65

Close Access 1 0.75 0.75

TOTAL FOR EACH AIRPLANE 12.80 9.15

Group 12-13:

Table 5 Work Package 1 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE FWD EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Potable Water 1 2.50 2.50

Drain

Open Access to 1 0.75 0.75

FWD EE bay

Task 2 1 1.50 1.50

Leak Test 2 7.30 3.65

Close Access 1 0.75 0.75

TOTAL FOR EACH AIRPLANE 12.80 9.15

Applicable To: B787-A-38-00-0009-00A-932A-D

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Group 14-16:

Table 6 Work Package 1 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE FWD EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Potable Water 1 2.50 2.50

Drain

Open Access to 1 0.75 0.75

FWD EE bay

Task 3 1 1.50 1.50

Leak Test 2 7.30 3.65

Close Access 1 0.75 0.75

TOTAL FOR EACH AIRPLANE 12.80 9.15

Group 1:

Table 7 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Potable Water

Drain *[1]

Open Access to 1 0.75 0.75

AFT EE bay

Task 4 2 6.50 3.25

Leak Test *[1]

Close Access 1 0.75 0.75

TOTAL FOR EACH AIRPLANE 8.00 4.75

*[1] Hours provided in the Work Package 1.

Group 2, 12:

Table 8 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Potable Water

Drain *[1]

Open Access to 1 0.75 0.75

AFT EE bay

Task 5 2 5.50 2.75

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Table 8 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Leak Test *[1]

Close Access 1 0.75 0.75

TOTAL FOR EACH AIRPLANE 7.00 4.25

*[1] Hours provided in the Work Package 1.

Group 3, 14:

Table 9 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Potable Water

Drain *[1]

Open Access to 1 0.75 0.75

AFT EE bay

Task 6 2 7.20 3.60

Leak Test *[1]

Close Access 1 0.75 0.75

TOTAL FOR EACH AIRPLANE 8.70 5.10

*[1] Hours provided in the Work Package 1.

Group 4, 15:

Table 10 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Potable Water

Drain *[1]

Open Access to 1 0.75 0.75

AFT EE bay

Task 7 2 5.50 2.75

Leak Test *[1]

Close Access 1 0.75 0.75

TOTAL FOR EACH AIRPLANE 7.00 4.25

*[1] Hours provided in the Work Package 1.

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Group 5:

Table 11 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Potable Water

Drain *[1]

Open Access to 1 0.75 0.75

AFT EE bay

Task 8 1 2.00 2.00

Leak Test *[1]

Close Access 1 0.75 0.75

TOTAL FOR EACH AIRPLANE 3.50 3.50

*[1] Hours provided in the Work Package 1.

Group 6:

Table 12 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Potable Water

Drain *[1]

Open Access to 1 0.75 0.75

AFT EE bay

Task 9 2 6.30 3.15

Leak Test *[1]

Close Access 1 0.75 0.75

TOTAL FOR EACH AIRPLANE 7.80 4.65

*[1] Hours provided in the Work Package 1.

Group 7, 13:

Table 13 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Potable Water

Drain *[1]

Open Access to 1 0.75 0.75

AFT EE bay

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Table 13 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Lavatories and 2 4.50 2.25

Floor Removal By

door 3

Task 10 2 7.30 3.65

Leak Test *[1]

Restore the re- 2 6.50 3.25

moved Lavatories

and Floor By door

3

Close Access 1 0.75 0.75

TOTAL FOR EACH AIRPLANE 19.80 10.65

*[1] Hours provided in the Work Package 1.

Group 16:

Table 14 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Potable Water

Drain *[1]

Open Access to 1 0.75 0.75

AFT EE bay

Lavatories and 2 4.50 2.25

Floor Removal By

door 3

Task 11 2 8.83 4.15

Leak Test *[1]

Restore the re- 2 6.50 3.25

moved Lavatories

and Floor By door

3

Close Access 1 0.75 0.75

TOTAL FOR EACH AIRPLANE 20.80 11.15

*[1] Hours provided in the Work Package 1.

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Group 8:

Table 15 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Potable Water

Drain *[1]

Open Access to 1 0.75 0.75

AFT EE bay

Lavatories and 2 4.50 2.25

Floor Removal By

door 3

Task 12 2 11.20 5.60

Leak Test *[1]

Restore the re- 2 6.50 3.25

moved Lavatories

and Floor By door

3

Close Access 1 0.75 0.75

TOTAL FOR EACH AIRPLANE 23.70 12.60

*[1] Hours provided in the Work Package 1.

Group 9:

Table 16 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Potable Water

Drain *[1]

Open Access to 1 0.75 0.75

AFT EE bay

Lavatories and 2 4.50 2.25

Floor Removal By

door 3

Task 13 2 11.00 5.50

Leak Test *[1]

Restore the re- 2 6.50 3.25

moved Lavatories

and Floor By door

3

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Table 16 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Close Access 1 0.75 0.75

TOTAL FOR EACH AIRPLANE 23.50 12.50

*[1] Hours provided in the Work Package 1.

Group 10:

Table 17 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Potable Water

Drain *[1]

Open Access to 1 0.75 0.75

AFT EE bay

Lavatories and 2 4.50 2.25

Floor Removal By

door 3

Task 14 2 7.50 3.75

Leak Test *[1]

Restore the re- 2 6.50 3.25

moved Lavatories

and Floor By door

3

Close Access 1 0.75 0.75

TOTAL FOR EACH AIRPLANE 20.00 10.75

*[1] Hours provided in the Work Package 1.

Group 11:

Table 18 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Potable Water

Drain *[1]

Open Access to 1 0.75 0.75

AFT EE bay

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Table 18 Work Package 2 - REPLACEMENT OF POTABLE WATERLINE 

COUPLINGS LOCATED ABOVE THE AFT EE BAY

Number of Per- Task Hours Elapsed Hours

sons

Task

Lavatories and 2 4.50 2.25

Floor Removal By

door 3

Task 15 2 7.00 3.50

Leak Test *[1]

Restore the re- 2 6.50 3.25

moved Lavatories

and Floor By door

3

Close Access 1 0.75 0.75

TOTAL FOR EACH AIRPLANE 19.50 10.50

*[1] Hours provided in the Work Package 1.

Group 1-16:

Work Package 1 can be done at the same time as Work Package 2.

8. Weight and Balance Changes

None.

9. Electrical Load Data

None.

10. References

A. Existing Data:

1. Change Notice CN-AA45386F, CN-AC45386A

2. Aircraft Maintenance Manual (AMM) 787 AMM 06-47-00, 787 AMM 12-14-01, 787 AMM 24-00-

02, 787 AMM 25-24-10, 787 AMM 25-24-20, 787 AMM 25-24-22, 787 AMM 25-25-01, 787 AMM

25-25-02, 787 AMM 25-27-01, 787 AMM 25-27-02, 787 AMM 25-28-05, 787 AMM 25-31, 787

AMM 25-41, 787 AMM 25-41-00, 787 AMM 38-10-00, 787 AMM 53-01-01

3. Boeing Service Related Problem (SRP) 787 SRP-38-0065

4. Standard Overhaul Practices Manual (SOPM) SOPM 20-50-01

5. Standard Wiring Practices Manual (SWPM) SWPM 20-10-11, SWPM 20-10-12

6. Boeing Fleet Team Digest (FTD) 787-FTD-38-13006

7. Multi Operators Message (MOM) MOM-MOM-14-0542-01B

Applicable To: B787-A-38-00-0009-00A-932A-D

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AIRCRAFT SERVICE BULLETIN
B. Data Supplied with this Service Bulletin:

None.

C. Installation Requirement Modules Used in the Preparation of this Service Bulletin:

Table 19 

Title Requirement Mod- *[1]

ule

824Z1102 PWS DR1 LAV1F-1L BRANCHLINE INSTL

824Z1101 PWS SUPPLY IRM

824Z1802 PWS DOOR1 CAPPING INSTL

824Z1600 POTABLE WATER SYSTEM - DOOR 3 - TRUNK-RUN INSTL

824Z1601 POTABLE WATER SYSTEM - DOOR 3 BRANCH LINE INSTL

824Z1501 WATER SYSTEM IRM

*[1] Acronyms Definition: Potable Water System (PWS), Door 1 (DR1), Lavatory (LAV), Installation (INSTL), Installation requirement Model (IRM)

The Requirements Modules above were used to prepare this service bulletin. The Requirements

Modules are not necessary to make the specified changes, and are not supplied with this service bulletin.

The Requirements Modules may not be applicable to all airplane configurations or operators..

11. Publications Affected

Table 20 

Publication Chapter-Section

787 Illustrated Parts Data (IPD) 38-00, 38-10

Damage Tolerance Based Structural Inspections:

Boeing has evaluated the repairs and/or changes in this service bulletin for effects on Fatigue Critical

Structure (FCS) and for changes to Damage Tolerance Inspections (DTI) required in the Maintenance

Program. This service bulletin does not affect FCS, therefore DTIs are not necessary.

12. Interchangeability and Intermixability of Parts

Refer to Data Module SB B787-A-38-00-0009-00A-934A-D, Paragraph 3., Parts Necessary for Each Airplane,

for interchangeability and intermixability information.

13. Software Accomplishment Summary

Not Affected.

Applicable To: B787-A-38-00-0009-00A-932A-D

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Service Bulletin B787-81205-SB380009-00

MATERIAL INFORMATION

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

References

Reference Title

Service Bulletin

B787-81205-SB380009-00 – Appendix A – 787

SB B787-A-38-00-0009-0AA-931D-D Issue 002

POTABLE WATER SHROUD INSTALLATION [Group

1-16:]

SB B787-A-38-00-0009-00A-932A-D Issue 002, References

Paragraph 10.

Description

Group 1-16:

1. Material - Price and Availability

Boeing can supply the kits shown in Paragraph 3., Parts Necessary for Each Airplane. Operators are encouraged to share schedule requirements with Boeing for incorporation of the service bulletin. The kits are

subject to the terms and conditions of the Boeing standard purchase order acknowledgment. Prices are in

United States Dollars. Terms: Net 30 days.

Reference this service bulletin and submit your purchase order by one of these methods:

1. Order on-line via ATA Spec 2000 or The Boeing PART Page

2. Fax to (206) 662-7145

REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER

AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION.

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Group 1:

Table 1 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 12 139 $2127.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-1

Group 2:

Table 2 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 16 139 $2008.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-2

Group 3:

Table 3 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 1 139 $2245.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-3

Applicable To: B787-A-38-00-0009-00A-934A-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 33 of 227

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Group 4:

Table 4 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 34 139 $2008.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-4

Group 5:

Table 5 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 4 139 $1415.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-5

Group 6:

Table 6 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 4 139 $2127.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-6

Applicable To: B787-A-38-00-0009-00A-934A-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 34 of 227

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Group 7:

Table 7 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 11 139 $2008.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-7

Group 8:

Table 8 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 11 139 $3195.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-8

Group 9:

Table 9 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 15 139 $2839.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-9

Applicable To: B787-A-38-00-0009-00A-934A-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 35 of 227

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Group 10:

Table 10 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 9 139 $2364.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-10

Group 11:

Table 11 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 17 139 $2245.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-11

Group 12:

Table 12 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 3 139 $2008.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-12

Applicable To: B787-A-38-00-0009-00A-934A-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 36 of 227

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Group 13:

Table 13 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 8 139 $2008.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-13

Group 14:

Table 14 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 7 139 $2248.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-14

Group 15:

Table 15 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 11 139 $2011.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-15

Applicable To: B787-A-38-00-0009-00A-934A-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 37 of 227

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Group 16:

Table 16 

Unit Price as of the

Issue 1 date of this

Service Bulletin

(US Dollars)

ROLT as of the Issue 1 date of this

Service Bulletin

(Calendar Days)

Kit Number Name Date QTY

SERVICE BUL- November 19, 2014 16 139 $2604.00

LETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-16

Group 1-16:

2. Industry Support Information

Boeing warranty remedies are available for 787 airplanes in warranty as of August 23, 2013. For labor task

hour reimbursement for airplanes in warranty as of that date, send a warranty claim to Boeing Fleet Support

Contracts - Warranty. The kits for airplanes in warranty as of that date will be supplied at no charge. Send

a purchase order for the kits to Boeing Material Management. Please refer to this service bulletin number

and reference the airplane variable number(s) in your purchase order. The warranty remedies will expire

eight years from the original release date of this service bulletin.

3. Parts Necessary for Each Airplane

A. Kits/Parts:

To get the kits/parts shown below, refer to Paragraph 1., Material - Price and Availability.

NOTE: One top kit and the items shown in Paragraph 3.B., Parts and Materials Supplied by the Operator, are necessary for each airplane. 

Table 17 

Kit 036Z0203

Existing Part Notes

Number

New Part Number QTY Name

-1 -2 -3 -4 -5 -6

SERVICE BULLETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-1 - . . . . .

SERVICE BULLETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-2 . - . . . .

Applicable To: B787-A-38-00-0009-00A-934A-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 38 of 227

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 17 

Kit 036Z0203

Existing Part Notes

Number

New Part Number QTY Name

-1 -2 -3 -4 -5 -6

SERVICE BULLETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-3 . . - . . .

SERVICE BULLETIN TOP KITCLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-4 . . . - . .

SERVICE BULLETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-5 . . . . - .

SERVICE BULLETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-6 . . . . . -

POTABLE WATER

SYSTEM - DOOR

1 COUPLING

RETROFIT INSTL

824Z1810-128 1 1 1 1 1 1

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-131 1 . . . . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-132 . 1 . . . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-133 . . 1 . . .

Applicable To: B787-A-38-00-0009-00A-934A-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 39 of 227

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 17 

Kit 036Z0203

Existing Part Notes

Number

New Part Number QTY Name

-1 -2 -3 -4 -5 -6

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-134 . . . 1 . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-135 . . . . 1 .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-136 . . . . . 1

POTABLE WATER

SYSTEM - COUPLING RETROFIT

KIT - TIE STRAP

INSTL

824Z1810-145 1 1 1 1 1 1

Table 18 

Kit 036Z0203

Existing Part Notes

Number

New Part Number QTY Name

-7 -8 -9 -10 -11 -12

SERVICE BULLETIN TOP KITCLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-7 - . . . . .

SERVICE BULLETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-8 . - . . . .

SERVICE BULLETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-9 . . - . . .

Applicable To: B787-A-38-00-0009-00A-934A-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 40 of 227

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 18 

Kit 036Z0203

Existing Part Notes

Number

New Part Number QTY Name

-7 -8 -9 -10 -11 -12

SERVICE BULLETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-10 . . . - . .

SERVICE BULLETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-11 . . . . - .

SERVICE BULLETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-12 . . . . . -

POTABLE WATER

SYSTEM - DOOR

1 COUPLING

RETROFIT INSTL

824Z1810-128 1 1 1 1 1 .

POTABLE WATER

SYSTEM - DOOR

1 COUPLING

RETROFIT INSTL

824Z1810-129 . . . . . 1

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-132 . . . . . 1

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-137 1 . . . . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-139 . 1 . . . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-140 . . 1 . . .

Applicable To: B787-A-38-00-0009-00A-934A-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 41 of 227

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 18 

Kit 036Z0203

Existing Part Notes

Number

New Part Number QTY Name

-7 -8 -9 -10 -11 -12

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-141 . . . 1 . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-142 . . . . 1 .

POTABLE WATER

SYSTEM - COUPLING RETROFIT

KIT - TIE STRAP

INSTL

824Z1810-145 1 1 1 1 1 1

Table 19 

Kit 036Z0203

Existing Part Notes

Number

New Part Number QTY Name

-13 -14 -15 -16

SERVICE BULLETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-13 - . . .

SERVICE BULLETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-14 . - . .

SERVICE BULLETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-15 . . - .

SERVICE BULLETIN TOP KIT -

CLAMSHELL

COUPLINGS REPLACEMENT

036Z0203-16 . . . -

Applicable To: B787-A-38-00-0009-00A-934A-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 42 of 227

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 19 

Kit 036Z0203

Existing Part Notes

Number

New Part Number QTY Name

-13 -14 -15 -16

POTABLE WATER

SYSTEM - DOOR

1 COUPLING

RETROFIT INSTL

824Z1810-129 1 . . .

POTABLE WATER

SYSTEM - DOOR

1 COUPLING

RETROFIT INSTL

824Z1810-130 . 1 1 1

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-133 . 1 . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-134 . . 1 .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-137 1 . . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-138 . . . 1

POTABLE WATER

SYSTEM - COUPLING RETROFIT

KIT - TIE STRAP

INSTL

824Z1810-145 1 1 1 1

Applicable To: B787-A-38-00-0009-00A-934A-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 43 of 227

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 20 

Kit 824Z1810

Existing Part Notes

Number

New Part Number QTY Name

-128 -129 -130 -131 -132 -133

POTABLE WATER

SYSTEM - DOOR

1 COUPLING

RETROFIT INSTL

824Z1810-128 - . . . . .

POTABLE WATER

SYSTEM - DOOR

1 COUPLING

RETROFIT INSTL

824Z1810-129 . - . . . .

POTABLE WATER

SYSTEM - DOOR

1 COUPLING

RETROFIT INSTL

824Z1810-130 . . - . . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-131 . . . - . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-132 . . . . - .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-133 . . . . . -

*[1] *[2]

*[3]

COUPLING AS1655C08

BODY, THREADLESS - FLEXIBLE,

FIXED CAVITY,

SELF-BONDING

14C34-08C 4 4 4 6 5 7

*[1] *[2]

*[3]

COUPLING AS1655C12

BODY, THREADLESS - FLEXIBLE,

FIXED CAVITY,

SELF-BONDING

14C34-12C . . . 6 6 6

*[1] Discard the existing part.

*[2] This part is used in production.

*[3] You cannot use the existing part to replace the new or changed part.

Applicable To: B787-A-38-00-0009-00A-934A-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 44 of 227

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 21 

Kit 824Z1810

Existing Part Notes

Number

New Part Number QTY Name

-134 -135 -136 -137 -138 -139

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-134 - . . . . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-135 . - . . . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-136 . . - . . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-137 . . . - . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-138 . . . . - .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-139 . . . . . -

*[1] *[2]

*[3]

COUPLING AS1655C08

BODY, THREADLESS - FLEXIBLE,

FIXED CAVITY,

SELF-BONDING

14C34-08C 5 . 6 5 10 15

*[1] *[2]

*[3]

COUPLING AS1655C12

BODY, THREADLESS - FLEXIBLE,

FIXED CAVITY,

SELF-BONDING

14C34-12C 6 5 6 6 6 6

*[1] Discard the existing part.

*[2] This part is used in production.

*[3] You cannot use the existing part to replace the new or changed part.

Applicable To: B787-A-38-00-0009-00A-934A-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 45 of 227

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 22 

Kit 824Z1810

Existing Part Notes

Number

New Part Number QTY Name

-140 -141 -142 -145

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-140 - . . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-141 . - . .

POTABLE WATER

SYSTEM - DOOR

3 COUPLING

RETROFIT INSTL

824Z1810-142 . . - .

POTABLE WATER

SYSTEM - COUPLING RETROFIT

KIT - TIE STRAP

INSTL

824Z1810-145 . . . -

*[1] *[2]

*[3]

COUPLING AS1655C08

BODY, THREADLESS - FLEXIBLE,

FIXED CAVITY,

SELF-BONDING

14C34-08C 12 8 7 .

*[1] *[2]

*[3]

COUPLING AS1655C12

BODY, THREADLESS - FLEXIBLE,

FIXED CAVITY,

SELF-BONDING

14C34-12C 6 6 6 .

STRAP, PLASTIC, *[4]

ADJUSTABLE,

SELF-LOCKING

BACS38K1 . . . 150

*[1] Discard the existing part.

*[2] This part is used in production.

*[3] You cannot use the existing part to replace the new or changed part.

*[4] There are more parts than are necessary.

Applicable To: B787-A-38-00-0009-00A-934A-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

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AIRCRAFT SERVICE BULLETIN
B. Parts and Materials Supplied by the Operator:

Table 23 

Part Number / QTY Name Notes

Specification

Permacel P-29 1 Roll TAPE

Self-bonding silicone rubber, high temperature;

rectangular cross-section,

0.012 inch thick, 1 inch

wide. *[1]

Scotch 70 / A-A- 1 Roll TAPE

59163

White. BMS13-54 1 Roll LACING TAPE *[1]

*[1] See Data Module Appendix A, SB B787-A-38-00-0009-0AA-931D-D, Note 5.

C. Parts Modified and Reidentified:

None.

D. Parts Removed and Not Replaced:

None.

4. Parts Necessary to Change Spares

None.

5. Special Tooling - Price and Availability

None.

6. Special Tooling Necessary to do this Service Bulletin

No special tools or equipment are necessary to do the change in this service bulletin. But, maintenance and

overhaul tools in the manuals given in Data Module SB B787-A-38-00-0009-00A-932A-D, Paragraph 10.,

References, can be necessary. Examine operator tool supply to make sure all necessary tools are available.

Applicable To: B787-A-38-00-0009-00A-934A-D

Model 787 End of data module Issue 002, 09 Dec 2015

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

ACCOMPLISHMENT INSTRUCTIONS

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

References

Reference Title

SB B787-A-38-00-0009-00A-932A-D Issue 002, References

Paragraph 10.

SB B787-A-38-00-0009-00A-932A-D Issue 002, Manpower

Paragraph 7.

SB B787-A-38-00-0009-00A-932A-D Issue 002, Compliance

Paragraph 5.

Service Bulletin B787-81205-SB380009-00 – Task

1 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE FWD EE BAY [Group 1-11: ]

SB B787-A-38-00-0009-01A-933B-D Issue 002

Service Bulletin B787-81205-SB380009-00 – Task

2 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE FWD EE BAY [Group 12-13: ]

SB B787-A-38-00-0009-02A-933B-D Issue 002

Service Bulletin B787-81205-SB380009-00 – Task

3 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE FWD EE BAY [Group 14-16: ]

SB B787-A-38-00-0009-03A-933B-D Issue 002

Service Bulletin B787-81205-SB380009-00 – Task

4 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE AFT EE BAY [Group 1: ]

SB B787-A-38-00-0009-04A-933B-D Issue 002

Service Bulletin B787-81205-SB380009-00 – Task

5 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE AFT EE BAY [Group 2, 12: ]

SB B787-A-38-00-0009-05A-933B-D Issue 002

Service Bulletin B787-81205-SB380009-00 – Task

6 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE AFT EE BAY [Group 3, 14: ]

SB B787-A-38-00-0009-06A-933B-D Issue 002

Service Bulletin B787-81205-SB380009-00 – Task

7 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE AFT EE BAY [Group 4, 15: ]

SB B787-A-38-00-0009-07A-933B-D Issue 002

Applicable To: B787-A-38-00-0009-00A-933A-D

Model 787 Issue 002, 09 Dec 2015

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AIRCRAFT SERVICE BULLETIN
Reference Title

Service Bulletin B787-81205-SB380009-00 – Task

8 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE AFT EE BAY [Group 5: ]

SB B787-A-38-00-0009-08A-933B-D Issue 002

Service Bulletin B787-81205-SB380009-00 – Task

9 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE AFT EE BAY [Group 6: ]

SB B787-A-38-00-0009-09A-933B-D Issue 002

Service Bulletin B787-81205-SB380009-00 – Task

10 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE AFT EE BAY [Group 7, 13: ]

SB B787-A-38-00-0009-10A-933B-D Issue 002

Service Bulletin B787-81205-SB380009-00 – Task

11 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE AFT EE BAY [Group 16: ]

SB B787-A-38-00-0009-11A-933B-D Issue 002

Service Bulletin B787-81205-SB380009-00 – Task

12 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE AFT EE BAY [Group 8: ]

SB B787-A-38-00-0009-12A-933B-D Issue 002

Service Bulletin B787-81205-SB380009-00 – Task

13 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE AFT EE BAY [Group 9: ]

SB B787-A-38-00-0009-13A-933B-D Issue 002

Service Bulletin B787-81205-SB380009-00 – Task

14 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE AFT EE BAY [Group 10: ]

SB B787-A-38-00-0009-14A-933B-D Issue 002

Service Bulletin B787-81205-SB380009-00 – Task

15 – REPLACEMENT OF COUPLINGS LOCATED

ABOVE AFT EE BAY [Group 11: ]

SB B787-A-38-00-0009-15A-933B-D Issue 002

SWPM 20-10-12 Standard Wiring Practices Manual

SOPM 20-50-01 BOLT AND NUT INSTALLATION

SOPM 20-44-02 TEMPORARY PROTECTIVE COATINGS

787 AMM 12-14-01 POTABLE WATER SYSTEM MAINTENANCE

787 AMM 24-00-02 CIRCUIT BREAKER INDICATION AND CONTROL

787 AMM 38-10-00 POTABLE WATER SYSTEM

787 AMM 25-41-00 LAVATORY

787 AMM 53-01-01 FLOOR PANEL

787 AMM 06-47-00 INTERIOR ACCESS DOORS AND PANELS

787 AMM 25-25-01 PASSENGER SEAT AND COMPONENTS

787 AMM 25-27-01 CARPET

Applicable To: B787-A-38-00-0009-00A-933A-D

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Reference Title

787 AMM 25-27-02 FLOOR MAT

787 AMM 25-28-05 FLOOR MOUNTED STOWAGE BOX

787 AMM 25-24-10 CLOSETS

787 AMM 25-24-20 PARTITION

787 AMM 25-24-22 CLASS DIVIDER

787 AMM 25-25-02 PASSENGER SEAT TRACK COVER

787 AMM 25-31 GALLEY

787 AMM 25-41 LAVATORY

Procedure

Group 1-16:

1. GENERAL INFORMATION

CAUTION: KEEP THE WORK AREA, WIRES AND ELECTRICAL BUNDLES CLEAN OF METAL PARTICLES OR CONTAMINATION WHEN YOU USE TOOLS. UNWANTED MATERIAL, METAL

PARTICLES OR CONTAMINATION CAUGHT IN WIRE BUNDLES CAN CAUSE DAMAGE

TO THE BUNDLES. DAMAGED WIRE BUNDLES CAN CAUSE SPARKS OR OTHER

ELECTRICAL DAMAGE.

NOTE: 1. Manual titles are referred to by acronyms. Refer to Data Module SB B787-A-38-00-0009-00A932A-D, Paragraph 10., References, for definition of the acronyms.

2. Obey all of the warnings and cautions given in the specified manual sections.

3. The work instructions are divided into work packages. Task Hours and Elapsed Hours for each

package are given in Data Module SB B787-A-38-00-0009-00A-932A-D, Paragraph 7., Manpower.

You can do each work package independently.

4. Unless shown differently, these dimensions and tolerances are used:

– Linear dimensions are in inches

– Tolerance on linear dimensions, other than rivet and bolt edge margins, is plus or minus

0.03 inch

– Tolerance on rivet and bolt edge margin is plus or minus 0.05 inch

– Angular tolerance is plus or minus 2 degrees

– Hole dimensions for standard solid rivets and fasteners are in SRM Chapter 51

– Torque Values:

– Values for structural fasteners are given in 787 Structural Repair Manual, Chapter 51.

– Values for airframe maintenance tasks are included in Chapter 20 of 787 Aircraft Maintenance Manual (AMM).

– Values for electrical maintenance tasks are included in Chapter 20 of Standard Wiring

Practices Manual (SWPM).

Applicable To: B787-A-38-00-0009-00A-933A-D

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– Values for engine maintenance tasks are included in Chapter 70 of 787 Aircraft Maintenance Manual (AMM).

– Non-standard torque values for maintenance tasks are included in the applicable installation step.

5. Use the approved fastener, process and material substitutions in accordance with SRM Chapter

51.

6. The necessary conditions for selection of clamp type and size are included in SWPM 20-10-12.

If any wire bundle support clamp specified in this service bulletin does not make a correct fit on

the wire bundle, refer to SWPM 20-10-12 as an accepted procedure to select a clamp that fits

correctly.

7. If the length of any fastener specified in this service bulletin does not meet the installation

standards in SRM Chapter 51, then a fastener of the same specification, or an approved substitute, with a length which meets the installation standards in SRM Chapter 51 may be used. In

addition, washers may be installed for fastener grip length in accordance with SRM Chapter 51.

Refer to SOPM 20-50-01 for alternate full threaded fasteners (screws) needed for installation

in this service bulletin.

8. These work instructions refer to procedures included in other Boeing documents. When the

words "refer to" are used and the operator has an accepted alternative procedure, the accepted

alternative procedure can be used. When the words "in accordance with" are included in the

instruction, the procedure in the Boeing document must be used.

9. Refer to Appendix A for the re-installation of the removed shrouds.

10. If it is necessary to remove more parts for access, you can remove those parts. If you can get

access without removing identified parts, it is not necessary to remove all of the identified parts.

Jacking and shoring limitations must be observed.

11. Where the work instructions include installation of a kept part, a new or serviceable part with

the same part number can be installed as an alternative to the kept part.

12. Use of colors in Tasks is based on guidance from the S1000D International specification for

technical publications.

13. The compliance times for the actions in Step 2., Work Instructions are in Data Module SB B787-

A-38-00-0009-00A-932A-D, Paragraph 5., Compliance.

14. Some steps in the Work Instructions are identified as Required for Compliance (RC). If this

service bulletin is mandated by an Airworthiness Directive (AD), then the steps identified as RC

must be done to comply with the AD. Alternative procedures for steps not identified with RC can

be used if the RC steps can still be done as specified, and the airplane can be put back in a

serviceable condition. An Alternative Method of Compliance (AMOC) is not necessary for deviations to steps that are not identified as RC.

2. WORK INSTRUCTIONS

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AIRCRAFT SERVICE BULLETIN
A. WORK PACKAGE 1 - REPLACEMENT OF POTABLE WATERLINE COUPLINGS LOCATED ABOVE

THE FORWARD (FWD) ELECTRICAL ELECTRONIC (EE) BAY

(1) Drain the Potable Water System. Refer to 787 AMM 12-14-01, "Potable Water System - Drain Liquid",

as an accepted procedure.

NOTE: Potable water system drain is needed to be done only one time if both Work Package 1

and Work Package 2 are being accomplished during the same maintenance visit. 

(2) Open these circuit breakers and lock with DO NOT CLOSE tags. Refer to 787 AMM 24-00-02 as an

accepted procedure.

Table 1 

Designation CB

POTABLE WATER PUMP - L CE3815411

POTABLE WATER PUMP - R CE3815412

WATER SERVICE PNL CE3814821

(3) Get access to the FWD EE Bay.

(4) (RC) Do replacement of potable waterline couplings located above the FWD EE Bay, applicable to

your airplane group:

NOTE: Do not re-install the shrouds until successful completion of Potable Water System - Leak

Test in Step 5 of Work Package 1. 

Group 1-11:

(a) Replace the potable waterline couplings in accordance with Data Module Task 1, SB B787-A38-00-0009-01A-933B-D

Group 12-13:

(b) Replace the potable waterline couplings in accordance with Data Module Task 2, SB B787-A38-00-0009-02A-933B-D

Group 14-16:

(c) Replace the potable waterline couplings in accordance with Data Module Task 3, SB B787-A38-00-0009-03A-933B-D

Group 1-16:

(5) Do the Potable Water System - Leak Test. After making sure that the pressure does not decrease

more than 2 psig (14 kPa) for a minimum of 20 minutes, it is only necessary to make sure there are

no air or water leaks at the locations where the water system was worked on. Refer to 787 AMM 38-

10-00 as an accepted procedure.

NOTE: – Potable Water System - Leak Test, is needed to be done only one time if both Work

Package 1 and Work Package 2 are being accomplished during the same maintenance

visit.

– Re-install the shrouds after successful completion of the Potable Water System - Leak

Test in Step 5 of Work Package 1.

Applicable To: B787-A-38-00-0009-00A-933A-D

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– If any lavatories are removed, the potable water hoses will need to be capped. Cap part

number LC200-08C can be used to cap the open lavatory hose. The NAS1611-015A

O-ring and AC1655A08, or 14C33-08 or 14C34-08 coupling can be used to secure the

cap.

– Usage of an equivalent tool to the K38003-1 tool as specified in 787 AMM 38-10-00 is

acceptable.

(6) Close circuit breakers and remove the DO NOT CLOSE tags:

Table 2 

Designation CB

POTABLE WATER PUMP - L CE3815411

POTABLE WATER PUMP - R CE3815412

WATER SERVICE PNL CE3814821

(7) Put the airplane back to a serviceable condition.

B. WORK PACKAGE 2 - REPLACEMENT OF POTABLE WATERLINE COUPLINGS LOCATED ABOVE

THE AFT EE BAY

(1) Drain the Potable Water System. Refer to 787 AMM 12-14-01, "Potable Water System - Drain Liquid",

as an accepted procedure.

NOTE: Potable water system drain is needed to be done only one time if both Work Package 1

and Work Package 2 are being accomplished during the same maintenance visit. 

(2) Open these circuit breakers and lock with DO NOT CLOSE tags. Refer to 787 AMM 24-00-02 as an

accepted procedure.

Table 3 

Designation CB

POTABLE WATER PUMP - L CE3815411

POTABLE WATER PUMP - R CE3815412

WATER SERVICE PNL CE3814821

(3) Get access to the AFT EE bay.

Group 7-11, 13, 16:

(4) Remove door 3 centerline galleys and lavatories and floor super panels under those lavatories if

necessary to gain access to potable waterline couplings AFT of STA 1281. To remove lavatories,

refer to 787 AMM 25-41-00 and to remove panels, refer to 787 AMM 53-01-01 as an accepted procedure. This is necessary, as access to the potable waterline couplings is difficult from the AFT EE

Bay.

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NOTE: TEMPORARY PROTECTION IS REQUIRED DURING HANDLING, TRANSPORTATION

AND STOWAGE OF INTERIOR EQUIPMENT. REFER TO SOPM 20-44-02 AS AN ACCEPTED PROCEDURE. 

The following list is not specific to each interior configuration. Do the following tasks as applicable

to your interior configuration. Retain all removed interior equipments for reinstallation.

– To identify floor panels, refer to 787 AMM 06-47-00 as an accepted procedure.

– To remove passenger seats, refer to 787 AMM 25-25-01 as an accepted procedure.

– To remove carpet, refer to 787 AMM 25-27-01 as an accepted procedure.

– To remove mats, refer to 787 AMM 25-27-02 as an accepted procedure.

– To remove floor mounted stowage boxes, refer to 787 AMM 25-28-05 as an accepted procedure.

NOTE: IT IS ONLY NECESSARY TO REMOVE THE FLOOR MOUNTED STOWAGE BOX

ASSEMBLY. DO NOT REMOVE THE FITTINGS THAT ATTACH THE FLOOR

MOUNTED STORAGE BOXES TO THE SEAT TRACKS. 

– To remove closets, refer to 787 AMM 25-24-10 as an accepted procedure.

– To remove partitions, refer to 787 AMM 25-24-20 as an accepted procedure.

– To remove class dividers, refer to 787 AMM 25-24-22 as an accepted procedure.

– To remove seat track covers, refer to 787 AMM 25-25-02 as an accepted procedure.

– To Remove galleys, refer to 787 AMM 25-31 as an accepted procedure.

Group 1-16:

(5) (RC) Do replacement of potable waterline couplings located above the AFT EE Bay, as applicable

to your airplane group:

NOTE: Do not re-install the shrouds until successful completion of Potable Water System - Leak

Test in Step 6 of Work Package 2 

Group 1:

(a) Replace the potable waterline couplings in accordance with Data Module Task 4, SB B787-A38-00-0009-04A-933B-D.

Group 2, 12:

(b) Replace the potable waterline couplings in accordance with Data Module Task 5, SB B787-A38-00-0009-05A-933B-D.

Group 3, 14:

(c) Replace the potable waterline couplings in accordance with Data Module Task 6, SB B787-A38-00-0009-06A-933B-D.

Group 4, 15:

(d) Replace the potable waterline couplings in accordance with Data Module Task 7, SB B787-A38-00-0009-07A-933B-D.

Applicable To: B787-A-38-00-0009-00A-933A-D

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Group 5:

(e) Replace the potable waterline couplings in accordance with Data Module Task 8, SB B787-A38-00-0009-08A-933B-D.

Group 6:

(f) Replace the potable waterline couplings in accordance with Data Module Task 9, SB B787-A38-00-0009-09A-933B-D.

Group 7, 13:

(g) Replace the potable waterline couplings in accordance with Data Module Task 10, SB B787-A38-00-0009-10A-933B-D.

Group 16:

(h) Replace the potable waterline couplings in accordance with Data Module Task 11, SB B787-A38-00-0009-11A-933B-D.

Group 8:

(i) Replace the potable waterline couplings in accordance with Data Module Task 12, SB B787-A38-00-0009-12A-933B-D.

Group 9:

(j) Replace the potable waterline couplings in accordance with Data Module Task 13, SB B787-A38-00-0009-13A-933B-D.

Group 10:

(k) Replace the potable waterline couplings in accordance with Data Module Task 14, SB B787-A38-00-0009-14A-933B-D.

Group 11:

(l) Replace the potable waterline couplings in accordance with Data Module Task 15, SB B787-A38-00-0009-15A-933B-D.

Group 1-16:

(6) Do the Potable Water System - Leak Test. After making sure that the pressure does not decrease

more than 2 psig (14 kPa) for a minimum of 20 minutes, it is only necessary to make sure there are

no air or water leaks at the locations where the water system was worked on. Refer to 787 AMM 38-

10-00 as an accepted procedure.

NOTE: – Potable Water System - Leak Test, is needed to be done only one time if both Work

Package 1 and Work Package 2 are being accomplished during the same maintenance

visit.

– Re-install the shrouds after successful completion of the Potable Water System - Leak

Test in Step 6 of Work Package 2.

– If any lavatories are removed, the potable water hoses will need to be capped. Cap part

number LC200-08C can be used to cap the open lavatory hose. The NAS1611-015A

O-ring and AC1655A08, or 14C33-08 or 14C34-08 coupling can be used to secure the

cap.

Applicable To: B787-A-38-00-0009-00A-933A-D

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– Usage of an equivalent tool to the K38003-1 tool as specified in 787 AMM 38-10-00 is

acceptable.

Group 7-11, 13, 16:

(7) Restore the removed centerline lavatories by door 3 and the floor super panels if removed.

The following list is not specific to each interior configuration. Do the following tasks as applicable

to your interior configuration.

– To install floor panels, refer to 787 AMM 53-01-01 as an accepted procedure.

– To install galleys, refer to 787 AMM 25-31 as an accepted procedure.

– To install lavatories, refer to , 787 AMM 25-41 as an accepted procedure.

– To install seat track covers, refer to 787 AMM 25-25-02 as an accepted procedure.

– To install class dividers, refer to 787 AMM 25-24-22 as an accepted procedure.

– To install partitions, refer to 787 AMM 25-24-20 as an accepted procedure.

– To install closets, refer to 787 AMM 25-24-10 as an accepted procedure.

– To install floor mounted stowage boxes, refer to 787 AMM 25-28-05 as an accepted procedure.

– To install mats, refer to 787 AMM 25-27-02 as an accepted procedure.

– To install carpet, refer to 787 AMM 25-27-01 as an accepted procedure.

– To install passenger seats, refer to 787 AMM 25-25-01 as an accepted procedure.

Group 1-16:

(8) Close circuit breakers and remove the DO NOT CLOSE tags.

Table 4 

Designation CB

POTABLE WATER PUMP - L CE3815411

POTABLE WATER PUMP - R CE3815412

WATER SERVICE PNL CE3814821

(9) Put the airplane back to a serviceable condition.

Applicable To: B787-A-38-00-0009-00A-933A-D

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Service Bulletin B787-81205-SB380009-00

Task 1 – REPLACEMENT OF COUPLINGS LOCATED ABOVE FWD EE BAY

[Group 1-11: ]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Preliminary Requirements

Required Conditions

Action/Condition Data Module/Technical Publication

Service Bulletin B787-81205-SB380009-00 - B787-A-38-00-0009-00A-933A-D Issue 002

ACCOMPLISHMENT INSTRUCTIONS

Applicable To: B787-A-38-00-0009-01A-933B-D

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Procedure

This Task applies to Group 1-11:

ICN-B787-A-000061-A-81205-08918-A-01-1

Figure 1 

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ICN-B787-A-000061-A-81205-08919-A-01-1

Figure 2 

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ICN-B787-A-000061-A-81205-08920-A-01-1

Figure 3 

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1. The step numbers shown below agree with the numbers shown in the circle symbols in the Task. The QTY

numbers shown below are the number of parts necessary for this Task.

Table 1 

Step Action Name Identification Qty More Data

1 Remove TAPE PERMACEL P-29 1

Remove / Keep TEE SHROUD 77000-912-004 1

2 Remove TIE STRAP BACS38K1 3 *[1]

Remove / Keep SPLIT SHROUD 77000-910-() 3

3 Remove COUPLING AS1655C08 4

COUPLING BODY, 14C34-08C 4 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

4 Install (New)

5 Install (Kept) TEE SHROUD 77000-912-004 1 *[3] *[4]

6 Install (Kept) SPLIT SHROUD 77000-910-() 3 *[3] *[4]

7 Install (New) TAPE PERMACEL P-29 1 *[3] *[4]

STRAP, PLASTIC, AD- BACS38K1 3 *[3] *[4]

JUSTABLE, SELFLOCKING

8 Install (New)

*[1] Remove tie straps as needed to locally peel back split shrouds to get access to the couplings inside the split shrouds.

*[2] Install the clamshell body over the sleeve (or female ferrule), enclosing both end flanges and snap shut the latch pawls. Make sure

that the clamshell body is completely engaged. Engage the safety strap onto the pawl. Make sure that the latches and safety strap

are fully secured and the latches are fully engaged.

*[3] Do not install the kept shroud and new tie straps until successful completion of the Potable Water System - Leak Test in Step 5 of

Work Package 1 in the Work Instructions.

*[4] Refer to Appendix A to re-install the shrouds as an accepted procedure.

Applicable To: B787-A-38-00-0009-01A-933B-D

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Service Bulletin B787-81205-SB380009-00

Task 2 – REPLACEMENT OF COUPLINGS LOCATED ABOVE FWD EE BAY

[Group 12-13: ]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Preliminary Requirements

Required Conditions

Action/Condition Data Module/Technical Publication

Service Bulletin B787-81205-SB380009-00 - B787-A-38-00-0009-00A-933A-D Issue 002

ACCOMPLISHMENT INSTRUCTIONS

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Procedure

This Task applies to Group 12-13:

ICN-B787-A-000061-A-81205-08921-A-01-1

Figure 1 

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08922-A-01-1

Figure 2 

Applicable To: B787-A-38-00-0009-02A-933B-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

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AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08923-A-01-1

Figure 3 

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Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
1. The step numbers shown below agree with the numbers shown in the circle symbols in the Task. The QTY

numbers shown below are the number of parts necessary for this Task.

Table 1 

Step Action Name Identification Qty More Data

1 Remove TAPE PERMACEL P-29 1

Remove / Keep TEE SHROUD 77000-912-004 1

2 Remove TIE STRAP BACS38K1 3 *[1]

Remove / Keep SPLIT SHROUD 77000-910-() 3

3 Remove COUPLING AS1655C08 4

COUPLING BODY, 14C34-08C 4 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

4 Install (New)

5 Install (Kept) TEE SHROUD 77000-912-004 1 *[3] *[4]

6 Install (Kept) SPLIT SHROUD 77000-910-() 3 *[3] *[4]

7 Install (New) TAPE PERMACEL P-29 1 *[3] *[4]

STRAP, PLASTIC, AD- BACS38K1 3 *[3] *[4]

JUSTABLE, SELFLOCKING

8 Install (New)

*[1] Remove tie straps as needed to locally peel back split shrouds to get access to the couplings inside the split shrouds.

*[2] Install the clamshell body over the sleeve (or female ferrule), enclosing both end flanges and snap shut the latch pawls. Make sure

that the clamshell body is completely engaged. Engage the safety strap onto the pawl. Make sure that the latches and safety strap

are fully secured and the latches are fully engaged.

*[3] Do not install the kept shrouds and new tie straps until successful completion of the Potable Water System - Leak Test in Step 5 of

the Work Package 1 in the Work Instructions.

*[4] Refer to Appendix A to re-install the shrouds as an accepted procedure.

Applicable To: B787-A-38-00-0009-02A-933B-D

Model 787 End of data module Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

Task 3 – REPLACEMENT OF COUPLINGS LOCATED ABOVE FWD EE BAY

[Group 14-16: ]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Preliminary Requirements

Required Conditions

Action/Condition Data Module/Technical Publication

Service Bulletin B787-81205-SB380009-00 - B787-A-38-00-0009-00A-933A-D Issue 002

ACCOMPLISHMENT INSTRUCTIONS

Applicable To: B787-A-38-00-0009-03A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Procedure

This Task applies to Group 14-16:

ICN-B787-A-000061-A-81205-08924-A-01-1

Figure 1 

Applicable To: B787-A-38-00-0009-03A-933B-D

Model 787 Issue 002, 09 Dec 2015

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08925-A-01-1

Figure 2 

Applicable To: B787-A-38-00-0009-03A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08926-A-01-1

Figure 3 

Applicable To: B787-A-38-00-0009-03A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
1. The step numbers shown below agree with the numbers shown in the circle symbols in the Task. The QTY

numbers shown below are the number of parts necessary for this Task.

Table 1 

Step Action Name Identification Qty More Data

1 Remove TAPE PERMACEL P-29 1

Remove / Keep TEE SHROUD 77000-912-004 1

2 Remove TIE STRAP BACS38K1 2 *[1]

Remove / Keep SPLIT SHROUD 77000-910-() 2 *[1]

3 Remove COUPLING AS1655C08 4

COUPLING BODY, 14C34-08C 4 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

4 Install (New)

5 Install (Kept) TEE SHROUD 77000-912-004 1 *[3] *[4]

6 Install (Kept) SPLIT SHROUD 77000-910-() 2 *[3] *[4]

7 Install (New) TAPE PERMACEL P-29 1 *[3] *[4]

STRAP, PLASTIC, AD- BACS38K1 2 *[3] *[4]

JUSTABLE, SELFLOCKING

8 Install (New)

*[1] Remove tie straps as needed to locally peel back split shrouds to get access to the couplings inside the split shrouds.

*[2] Install the clamshell body over the sleeve (or female ferrule), enclosing both end flanges and snap shut the latch pawls. Make sure

that the clamshell body is completely engaged. Engage the safety strap onto the pawl. Make sure that the latches and safety strap

are fully secured and the latches are fully engaged.

*[3] Do not install the kept shrouds and new tie straps until successful completion of the Potable Water System - Leak Test in Step 5 of

the Work Package 1 in the Work Instructions.

*[4] Refer to Appendix A to re-install the shrouds as an accepted procedure.

Applicable To: B787-A-38-00-0009-03A-933B-D

Model 787 End of data module Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

Task 4 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY

[Group 1: ]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Preliminary Requirements

Required Conditions

Action/Condition Data Module/Technical Publication

Service Bulletin B787-81205-SB380009-00 - B787-A-38-00-0009-00A-933A-D Issue 002

ACCOMPLISHMENT INSTRUCTIONS

Applicable To: B787-A-38-00-0009-04A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Procedure

This Task applies to Group 1:

ICN-B787-A-000061-A-81205-08927-A-01-1

Figure 1 

Applicable To: B787-A-38-00-0009-04A-933B-D

Model 787 Issue 002, 09 Dec 2015

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08928-A-01-1

Figure 2 

Applicable To: B787-A-38-00-0009-04A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08929-A-01-1

Figure 3 

Applicable To: B787-A-38-00-0009-04A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08930-A-01-1

Figure 4 

Applicable To: B787-A-38-00-0009-04A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08931-A-01-1

Figure 5 

Applicable To: B787-A-38-00-0009-04A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08932-A-01-1

Figure 6 

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Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08933-A-01-1

Figure 7 

Applicable To: B787-A-38-00-0009-04A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08934-A-01-1

Figure 8 

Applicable To: B787-A-38-00-0009-04A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08935-A-01-1

Figure 9 

Applicable To: B787-A-38-00-0009-04A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
1. The step numbers shown below agree with the numbers shown in the circle symbols in the Task. The QTY

numbers shown below are the number of parts necessary for this Task.

Table 1 

Step Action Name Identification Qty More Data

1 Remove TIE STRAP BACS38K1 27 *[1]

2 Remove / Keep SPLIT SHROUD 77000-910-() 10 *[1]

3 Remove / Keep TEE SHROUD 77000-912-003 1

4 Remove COUPLING AS1655C12 6

COUPLING BODY, 14C34-12C 6 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

5 Install (New)

6 Remove TAPE PERMACEL P-29 1

7 Remove / Keep WYE SHROUD 77000-912-() 2

8 Remove / Keep UPPER TEE SHROUD 77000-912-002 2

Remove / Keep LOWER TEE SHROUD 77000-912-002 2

9 Remove COUPLING AS1655C08 6

COUPLING BODY, 14C34-08C 6 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

10 Install (New)

11 Install (Kept) UPPER TEE SHROUD 77000-912-002 2 *[3] *[4]

Install (Kept) LOWER TEE SHROUD 77000-912-002 2

12 Install (Kept) WYE SHROUD 77000-912-001 2 *[3] *[4]

13 Install (New) TAPE PERMACEL P-29 1 *[3] *[4]

14 Install (Kept) SPLIT SHROUD 77000-910-() 10 *[3] *[4]

15 Install (Kept) TEE SHROUD 77000-912-003 1 *[3] *[4]

16 Install (New) TIE STRAP BACS38K1 27 *[3] *[4]

*[1] Remove tie straps as needed to locally peel back split shrouds to get access to the couplings inside the split shrouds.

*[2] Install the clamshell body over the sleeve (or female ferrule), enclosing both end flanges and snap shut the latch pawls. Make sure

that the clamshell body is completely engaged. Engage the safety strap onto the pawl. Make sure that the latches and safety strap

are fully secured and the latches are fully engaged.

*[3] Do not install the kept shrouds and new tie straps until successful completion of the Potable Water System - Leak Test in Step 6 of

the Work Package 2 in the Work Instructions.

*[4] Refer to Appendix A to re-install the shrouds as an accepted procedure.

Applicable To: B787-A-38-00-0009-04A-933B-D

Model 787 End of data module Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

Task 5 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY

[Group 2, 12: ]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Preliminary Requirements

Required Conditions

Action/Condition Data Module/Technical Publication

Service Bulletin B787-81205-SB380009-00 - B787-A-38-00-0009-00A-933A-D Issue 002

ACCOMPLISHMENT INSTRUCTIONS

Applicable To: B787-A-38-00-0009-05A-933B-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Procedure

This Task applies to Group 2, 12:

ICN-B787-A-000061-A-81205-08936-A-01-1

Figure 1 

Applicable To: B787-A-38-00-0009-05A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08937-A-01-1

Figure 2 

Applicable To: B787-A-38-00-0009-05A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08938-A-01-1

Figure 3 

Applicable To: B787-A-38-00-0009-05A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08939-A-01-1

Figure 4 

Applicable To: B787-A-38-00-0009-05A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08940-A-01-1

Figure 5 

Applicable To: B787-A-38-00-0009-05A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08941-A-01-1

Figure 6 

Applicable To: B787-A-38-00-0009-05A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08942-A-01-1

Figure 7 

Applicable To: B787-A-38-00-0009-05A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08943-A-01-1

Figure 8 

Applicable To: B787-A-38-00-0009-05A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
1. The step numbers shown below agree with the numbers shown in the circle symbols in the Task. The QTY

numbers shown below are the number of parts necessary for this Task.

Table 1 

Step Action Name Identification Qty More Data

1 Remove TIE STRAP BACS38K1 23 *[1]

2 Remove / Keep SPLIT SHROUD 77000-910-() 10 *[1]

3 Remove / Keep TEE SHROUD 77000-912-003 1

4 Remove COUPLING AS1655C12 6

COUPLING BODY, 14C34-12C 6 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

5 Install (New)

6 Remove TAPE PERMACEL P-29 1

7 Remove / Keep WYE SHROUD 77000-912-() 1

8 Remove / Keep UPPER TEE SHROUD 77000-912-002 1

Remove / Keep LOWER TEE SHROUD 77000-912-002 1

9 Remove COUPLING AS1655C08 5

COUPLING BODY, 14C34-08C 5 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

10 Install (New)

11 Install (Kept) UPPER TEE SHROUD 77000-912-002 1 *[3] *[4]

Install (Kept) LOWER TEE SHROUD 77000-912-002 1

12 Install (Kept) WYE SHROUD 77000-912-001 1 *[3] *[4]

13 Install (New) TAPE PERMACEL P-29 1 *[3] *[4]

14 Install (Kept) SPLIT SHROUD 77000-910-() 10 *[3] *[4]

15 Install (Kept) TEE SHROUD 77000-912-003 1 *[3] *[4]

STRAP, PLASTIC, AD- BACS38K1 23 *[3] *[4]

JUSTABLE, SELFLOCKING

16 Install (New)

*[1] Remove tie straps as needed to locally peel back split shrouds to get access to the couplings inside the split shrouds.

*[2] Install the clamshell body over the sleeve (or female ferrule), enclosing both end flanges and snap shut the latch pawls. Make sure

that the clamshell body is completely engaged. Engage the safety strap onto the pawl. Make sure that the latches and safety strap

are fully secured and the latches are fully engaged.

Applicable To: B787-A-38-00-0009-05A-933B-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 1 

Step Action Name Identification Qty More Data

*[3] Do not install the kept shrouds and new tie straps until successful completion of the Potable Water System - Leak Test in Step 6 of

the Work Package 2 in the Work Instructions.

*[4] Refer to Appendix A to re-install the shrouds as an accepted procedure.

Applicable To: B787-A-38-00-0009-05A-933B-D

Model 787 End of data module Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

Task 6 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY

[Group 3, 14: ]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Preliminary Requirements

Required Conditions

Action/Condition Data Module/Technical Publication

Service Bulletin B787-81205-SB380009-00 - B787-A-38-00-0009-00A-933A-D Issue 002

ACCOMPLISHMENT INSTRUCTIONS

Applicable To: B787-A-38-00-0009-06A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Procedure

This Task applies to Group 3, 14:

ICN-B787-A-000061-A-81205-08944-A-01-1

Figure 1 

Applicable To: B787-A-38-00-0009-06A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08945-A-01-1

Figure 2 

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Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08946-A-01-1

Figure 3 

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Model 787 Issue 002, 09 Dec 2015

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AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08947-A-01-1

Figure 4 

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Model 787 Issue 002, 09 Dec 2015

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AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08948-A-01-1

Figure 5 

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Model 787 Issue 002, 09 Dec 2015

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08949-A-01-1

Figure 6 

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Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08950-A-01-1

Figure 7 

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Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08951-A-01-1

Figure 8 

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Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
1. The step numbers shown below agree with the numbers shown in the circle symbols in the Task. The QTY

numbers shown below are the number of parts necessary for this Task.

Table 1 

Step Action Name Identification Qty More Data

1 Remove TIE STRAP BACS38K1 25 *[1]

2 Remove / Keep SPLIT SHROUD 77000-910-() 14 *[1]

3 Remove / Keep TEE SHROUD 77000-912-003 1

4 Remove COUPLING AS1655C12 6

COUPLING BODY, 14C34-12C 6 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

5 Install (New)

6 Remove TAPE PERMACEL P-29 1

7 Remove / Keep WYE SHROUD 77000-912-() 1

8 Remove / Keep UPPER TEE SHROUD 77000-912-002 3

Remove / Keep LOWER TEE SHROUD 77000-912-002 3

9 Remove COUPLING AS1655C08 7

COUPLING BODY, 14C34-08C 7 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

10 Install (New)

11 Install (Kept) UPPER TEE SHROUD 77000-912-002 3 *[3] *[4]

Install (Kept) LOWER TEE SHROUD 77000-912-002 3

12 Install (Kept) WYE SHROUD 77000-912-001 1 *[3] *[4]

13 Install (New) TAPE PERMACEL P-29 1 *[3] *[4]

14 Install (Kept) SPLIT SHROUD 77000-910-() 14 *[3] *[4]

15 Install (Kept) TEE SHROUD 77000-912-003 1 *[3] *[4]

STRAP, PLASTIC, AD- BACS38K1 25 *[3] *[4]

JUSTABLE, SELFLOCKING

16 Install (New)

*[1] Remove tie straps as needed to locally peel back split shrouds to get access to the couplings inside the split shrouds.

*[2] Install the clamshell body over the sleeve (or female ferrule), enclosing both end flanges and snap shut the latch pawls. Make sure

that the clamshell body is completely engaged. Engage the safety strap onto the pawl. Make sure that the latches and safety strap

are fully secured and the latches are fully engaged.

Applicable To: B787-A-38-00-0009-06A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 1 

Step Action Name Identification Qty More Data

*[3] Do not install the kept shrouds and new tie straps until successful completion of the Potable Water System - Leak Test in Step 6 of

the Work Package 2 in the Work Instructions.

*[4] Refer to Appendix A to re-install the shrouds as an accepted procedure.

Applicable To: B787-A-38-00-0009-06A-933B-D

Model 787 End of data module Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

Task 7 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY

[Group 4, 15: ]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Preliminary Requirements

Required Conditions

Action/Condition Data Module/Technical Publication

Service Bulletin B787-81205-SB380009-00 - B787-A-38-00-0009-00A-933A-D Issue 002

ACCOMPLISHMENT INSTRUCTIONS

Applicable To: B787-A-38-00-0009-07A-933B-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Procedure

This Task applies to Group 4, 15:

ICN-B787-A-000061-A-81205-08952-A-01-1

Figure 1 

Applicable To: B787-A-38-00-0009-07A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08953-A-01-1

Figure 2 

Applicable To: B787-A-38-00-0009-07A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08954-A-01-1

Figure 3 

Applicable To: B787-A-38-00-0009-07A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08955-A-01-1

Figure 4 

Applicable To: B787-A-38-00-0009-07A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08956-A-01-1

Figure 5 

Applicable To: B787-A-38-00-0009-07A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08957-A-01-1

Figure 6 

Applicable To: B787-A-38-00-0009-07A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08958-A-01-1

Figure 7 

Applicable To: B787-A-38-00-0009-07A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08959-A-01-1

Figure 8 

Applicable To: B787-A-38-00-0009-07A-933B-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
1. The step numbers shown below agree with the numbers shown in the circle symbols in the Task. The QTY

numbers shown below are the number of parts necessary for this Task.

Table 1 

Step Action Name Identification Qty More Data

1 Remove TIE STRAP BACS38K1 23 *[1]

2 Remove / Keep SPLIT SHROUD 77000-910-() 10 *[1]

3 Remove / Keep TEE SHROUD 77000-912-003 1

4 Remove COUPLING AS1655C12 6

COUPLING BODY, 14C34-12C 6 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

5 Install (New)

6 Remove TAPE PERMACEL P-29 1

7 Remove / Keep WYE SHROUD 77000-912-() 1

8 Remove / Keep UPPER TEE SHROUD 77000-912-002 1

Remove / Keep LOWER TEE SHROUD 77000-912-002 1

9 Remove COUPLING AS1655C08 5

COUPLING BODY, 14C34-08C 5 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

10 Install (New)

11 Install (Kept) UPPER TEE SHROUD 77000-912-002 1 *[3] *[4]

Install (Kept) LOWER TEE SHROUD 77000-912-002 1 *[3] *[4]

12 Install (Kept) WYE SHROUD 77000-912-001 1 *[3] *[4]

13 Install (New) TAPE PERMACEL P-29 1 *[3] *[4]

14 Install (Kept) SPLIT SHROUD 77000-910-() 10 *[3] *[4]

15 Install (Kept) TEE SHROUD 77000-912-003 1 *[3] *[4]

STRAP, PLASTIC, AD- BACS38K1 23 *[3] *[4]

JUSTABLE, SELFLOCKING

16 Install (New)

*[1] Remove tie straps as needed to locally peel back split shrouds to get access to the couplings inside the split shrouds.

*[2] Install the clamshell body over the sleeve (or female ferrule), enclosing both end flanges and snap shut the latch pawls. Make sure

that the clamshell body is completely engaged. Engage the safety strap onto the pawl. Make sure that the latches and safety strap

are fully secured and the latches are fully engaged.

Applicable To: B787-A-38-00-0009-07A-933B-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 1 

Step Action Name Identification Qty More Data

*[3] Do not install the kept shrouds and new tie straps until successful completion of the Potable Water System - Leak Test in Step 6 of

the Work Package 2 in the Work Instructions.

*[4] Refer to Appendix A to re-install the shrouds as an accepted procedure.

Applicable To: B787-A-38-00-0009-07A-933B-D

Model 787 End of data module Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

Task 8 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY

[Group 5: ]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Preliminary Requirements

Required Conditions

Action/Condition Data Module/Technical Publication

Service Bulletin B787-81205-SB380009-00 - B787-A-38-00-0009-00A-933A-D Issue 002

ACCOMPLISHMENT INSTRUCTIONS

Applicable To: B787-A-38-00-0009-08A-933B-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 116 of 227

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Procedure

This Task applies to Group 5:

ICN-B787-A-000061-A-81205-08960-A-01-1

Figure 1 

Applicable To: B787-A-38-00-0009-08A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08961-A-01-1

Figure 2 

Applicable To: B787-A-38-00-0009-08A-933B-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08962-A-01-1

Figure 3 

Applicable To: B787-A-38-00-0009-08A-933B-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 119 of 227

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
1. The step numbers shown below agree with the numbers shown in the circle symbols in the Task. The QTY

numbers shown below are the number of parts necessary for this Task.

Table 1 

Step Action Name Identification Qty More Data

1 Remove TIE STRAP BACS38K1 7 *[1]

2 Remove / Keep SPLIT SHROUD 77000-910-() 4 *[1]

3 Remove / Keep TEE SHROUD 77000-912-003 1

4 Remove COUPLING AS1655C12 5

COUPLING BODY, 14C34-12C 5 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

5 Install (New)

6 Install (Kept) SPLIT SHROUD 77000-910-() 4 *[3] *[4]

7 Install (Kept) TEE SHROUD 77000-912-003 1 *[3] *[4]

STRAP, PLASTIC, AD- BACS38K1 7 *[3] *[4]

JUSTABLE, SELFLOCKING

8 Install (New)

*[1] Remove tie straps as needed to locally peel back split shrouds to get access to the couplings inside the split shrouds.

*[2] Install the clamshell body over the sleeve (or female ferrule), enclosing both end flanges and snap shut the latch pawls. Make sure

that the clamshell body is completely engaged. Engage the safety strap onto the pawl. Make sure that the latches and safety strap

are fully secured and the latches are fully engaged.

*[3] Do not install the kept shrouds and new tie straps until successful completion of the Potable Water System - Leak Test in Step 6 of

the Work Package 2 in the Work Instructions.

*[4] Refer to Appendix A to re-install the shrouds as an accepted procedure.

Applicable To: B787-A-38-00-0009-08A-933B-D

Model 787 End of data module Issue 002, 09 Dec 2015

See Applicability of this data module

Page 120 of 227

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

Task 9 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY

[Group 6: ]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Preliminary Requirements

Required Conditions

Action/Condition Data Module/Technical Publication

Service Bulletin B787-81205-SB380009-00 - B787-A-38-00-0009-00A-933A-D Issue 002

ACCOMPLISHMENT INSTRUCTIONS

Applicable To: B787-A-38-00-0009-09A-933B-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 121 of 227

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Procedure

This Task applies to Group 6:

ICN-B787-A-000061-A-81205-08963-A-01-1

Figure 1 

Applicable To: B787-A-38-00-0009-09A-933B-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08964-A-01-1

Figure 2 

Applicable To: B787-A-38-00-0009-09A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08965-A-01-1

Figure 3 

Applicable To: B787-A-38-00-0009-09A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08966-A-01-1

Figure 4 

Applicable To: B787-A-38-00-0009-09A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08967-A-01-1

Figure 5 

Applicable To: B787-A-38-00-0009-09A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08968-A-01-1

Figure 6 

Applicable To: B787-A-38-00-0009-09A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08969-A-01-1

Figure 7 

Applicable To: B787-A-38-00-0009-09A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08970-A-01-1

Figure 8 

Applicable To: B787-A-38-00-0009-09A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
1. The step numbers shown below agree with the numbers shown in the circle symbols in the Task. The QTY

numbers shown below are the number of parts necessary for this Task.

Table 1 

Step Action Name Identification Qty More Data

1 Remove TIE STRAP BACS38K1 24 *[1]

2 Remove / Keep SPLIT SHROUD 77000-910-() 12 *[1]

3 Remove / Keep TEE SHROUD 77000-912-003 1

4 Remove COUPLING AS1655C12 6

COUPLING BODY, 14C34-12C 6 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

5 Install (New)

6 Remove TAPE PERMACEL P-29 1

7 Remove / Keep WYE SHROUD 77000-912-() 1

8 Remove / Keep UPPER TEE SHROUD 77000-912-002 2

Remove / Keep LOWER TEE SHROUD 77000-912-002 2

9 Remove COUPLING AS1655C08 6

COUPLING BODY, 14C34-08C 6 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

10 Install (New)

11 Install (Kept) UPPER TEE SHROUD 77000-912-002 2 *[3] *[4]

Install (Kept) LOWER TEE SHROUD 77000-912-002 2

12 Install (Kept) WYE SHROUD 77000-912-001 1 *[3] *[4]

13 Install (New) TAPE PERMACEL P-29 1 *[3] *[4]

14 Install (Kept) SPLIT SHROUD 77000-910-() 12 *[3] *[4]

15 Install (Kept) TEE SHROUD 77000-912-003 1 *[3] *[4]

STRAP, PLASTIC, AD- BACS38K1 24 *[3] *[4]

JUSTABLE, SELFLOCKING

16 Install (New)

*[1] Remove tie straps as needed to locally peel back split shrouds to get access to the couplings inside the split shrouds.

*[2] Install the clamshell body over the sleeve (or female ferrule), enclosing both end flanges and snap shut the latch pawls. Make sure

that the clamshell body is completely engaged. Engage the safety strap onto the pawl. Make sure that the latches and safety strap

are fully secured and the latches are fully engaged.

Applicable To: B787-A-38-00-0009-09A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 1 

Step Action Name Identification Qty More Data

*[3] Do not install the kept shrouds and new tie straps until successful completion of the Potable Water System - Leak Test in Step 6 of

the Work Package 2 in the Work Instructions.

*[4] Refer to Appendix A to re-install the shrouds as an accepted procedure.

Applicable To: B787-A-38-00-0009-09A-933B-D

Model 787 End of data module Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

Task 10 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY

[Group 7, 13: ]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Preliminary Requirements

Required Conditions

Action/Condition Data Module/Technical Publication

Service Bulletin B787-81205-SB380009-00 - B787-A-38-00-0009-00A-933A-D Issue 002

ACCOMPLISHMENT INSTRUCTIONS

Applicable To: B787-A-38-00-0009-10A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Procedure

This Task applies to Group 7, 13:

ICN-B787-A-000061-A-81205-08971-A-01-1

Figure 1 

Applicable To: B787-A-38-00-0009-10A-933B-D

Model 787 Issue 002, 09 Dec 2015

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08972-A-01-1

Figure 2 

Applicable To: B787-A-38-00-0009-10A-933B-D

Model 787 Issue 002, 09 Dec 2015

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AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08973-A-01-1

Figure 3 

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Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

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ICN-B787-A-000061-A-81205-08974-A-01-1

Figure 4 

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Model 787 Issue 002, 09 Dec 2015

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AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08975-A-01-1

Figure 5 

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Model 787 Issue 002, 09 Dec 2015

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AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08976-A-01-1

Figure 6 

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Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08977-A-01-1

Figure 7 

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Model 787 Issue 002, 09 Dec 2015

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AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08978-A-01-1

Figure 8 

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Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
1. The step numbers shown below agree with the numbers shown in the circle symbols in the Task. The QTY

numbers shown below are the number of parts necessary for this Task.

Table 1 

Step Action Name Identification Qty More Data

1 Remove TIE STRAP BACS38K1 24 *[1]

2 Remove / Keep SPLIT SHROUD 77000-910-() 10 *[1]

3 Remove / Keep TEE SHROUD 77000-912-003 1

4 Remove COUPLING AS1655C12 6

COUPLING BODY, 14C34-12C 6 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

5 Install (New)

6 Remove TAPE PERMACEL P-29 1

7 Remove / Keep WYE SHROUD 77000-912-() 1

8 Remove / Keep UPPER TEE SHROUD 77000-912-002 1

Remove / Keep LOWER TEE SHROUD 77000-912-002 1

9 Remove COUPLING AS1655C08 5

COUPLING BODY, 14C34-08C 5 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

10 Install (New)

11 Install (Kept) UPPER TEE SHROUD 77000-912-002 1 *[3] *[4]

Install (Kept) LOWER TEE SHROUD 77000-912-002 1

12 Install (Kept) WYE SHROUD 77000-912-001 1 *[3] *[4]

13 Install (New) TAPE PERMACEL P-29 1 *[3] *[4]

14 Install (Kept) SPLIT SHROUD 77000-910-() 10 *[3] *[4]

15 Install (Kept) TEE SHROUD 77000-912-003 1 *[3] *[4]

STRAP, PLASTIC, AD- BACS38K1 24 *[3] *[4]

JUSTABLE, SELFLOCKING

16 Install (New)

*[1] Remove tie straps as needed to locally peel back split shrouds to get access to the couplings inside the split shrouds.

*[2] Install the clamshell body over the sleeve (or female ferrule), enclosing both end flanges and snap shut the latch pawls. Make sure

that the clamshell body is completely engaged. Engage the safety strap onto the pawl. Make sure that the latches and safety strap

are fully secured and the latches are fully engaged.

Applicable To: B787-A-38-00-0009-10A-933B-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

Page 141 of 227

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 1 

Step Action Name Identification Qty More Data

*[3] Do not install the kept shrouds and new tie straps until successful completion of the Potable Water System - Leak Test in Step 6 of

the Work Package 2 in the Work Instructions.

*[4] Refer to Appendix A to re-install the shrouds as an accepted procedure.

Applicable To: B787-A-38-00-0009-10A-933B-D

Model 787 End of data module Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

Task 11 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY

[Group 16: ]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Preliminary Requirements

Required Conditions

Action/Condition Data Module/Technical Publication

Service Bulletin B787-81205-SB380009-00 - B787-A-38-00-0009-00A-933A-D Issue 002

ACCOMPLISHMENT INSTRUCTIONS

Applicable To: B787-A-38-00-0009-11A-933B-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Procedure

This Task applies to Group 16:

ICN-B787-A-000061-A-81205-08979-A-01-1

Figure 1 

Applicable To: B787-A-38-00-0009-11A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08980-A-01-1

Figure 2 

Applicable To: B787-A-38-00-0009-11A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08981-A-01-1

Figure 3 

Applicable To: B787-A-38-00-0009-11A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08982-A-01-1

Figure 4 

Applicable To: B787-A-38-00-0009-11A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08983-A-01-1

Figure 5 

Applicable To: B787-A-38-00-0009-11A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08984-A-01-1

Figure 6 

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Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

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AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08985-A-01-1

Figure 7 

Applicable To: B787-A-38-00-0009-11A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08986-A-01-1

Figure 8 

Applicable To: B787-A-38-00-0009-11A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08987-A-01-1

Figure 9 

Applicable To: B787-A-38-00-0009-11A-933B-D

Model 787 Issue 002, 09 Dec 2015

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08988-A-01-1

Figure 10 

Applicable To: B787-A-38-00-0009-11A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08989-A-01-1

Figure 11 

Applicable To: B787-A-38-00-0009-11A-933B-D

Model 787 Issue 002, 09 Dec 2015

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08990-A-01-1

Figure 12 

Applicable To: B787-A-38-00-0009-11A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
1. The step numbers shown below agree with the numbers shown in the circle symbols in the Task. The QTY

numbers shown below are the number of parts necessary for this Task.

Table 1 

Step Action Name Identification Qty More Data

1 Remove TIE STRAP BACS38K1 36 *[1]

2 Remove / Keep SPLIT SHROUD 77000-910-() 15 *[1]

3 Remove / Keep TEE SHROUD 77000-912-003 1

4 Remove COUPLING AS1655C12 6

COUPLING BODY, 14C34-12C 6 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

5 Install (New)

6 Remove TAPE PERMACEL P-29 1

7 Remove / Keep WYE SHROUD 77000-912-() 2

8 Remove / Keep UPPER TEE SHROUD 77000-912-002 2

Remove / Keep LOWER TEE SHROUD 77000-912-002 2

9 Remove COUPLING AS1655C08 10

COUPLING BODY, 14C34-08C 10 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

10 Install (New)

11 Install (Kept) UPPER TEE SHROUD 77000-912-002 2 *[3] *[4]

Install (Kept) LOWER TEE SHROUD 77000-912-002 2

12 Install (Kept) WYE SHROUD 77000-912-001 2 *[3] *[4]

13 Install (New) TAPE PERMACEL P-29 1 *[3] *[4]

14 Install (Kept) SPLIT SHROUD 77000-910-() 15 *[3] *[4]

15 Install (Kept) TEE SHROUD 77000-912-003 1 *[3] *[4]

STRAP, PLASTIC, AD- BACS38K1 36 *[3] *[4]

JUSTABLE, SELFLOCKING

16 Install (New)

*[1] Remove tie straps as needed to locally peel back split shrouds to get access to the couplings inside the split shrouds.

*[2] Install the clamshell body over the sleeve (or female ferrule), enclosing both end flanges and snap shut the latch pawls. Make sure

that the clamshell body is completely engaged. Engage the safety strap onto the pawl. Make sure that the latches and safety strap

are fully secured and the latches are fully engaged.

Applicable To: B787-A-38-00-0009-11A-933B-D

Model 787 Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 1 

Step Action Name Identification Qty More Data

*[3] Do not install the kept shrouds and new tie straps until successful completion of the Potable Water System - Leak Test in Step 6 of

the Work Package 2 in the Work Instructions.

*[4] Refer to Appendix A to re-install the shrouds as an accepted procedure.

Applicable To: B787-A-38-00-0009-11A-933B-D

Model 787 End of data module Issue 002, 09 Dec 2015

See Applicability of this data module

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

Task 12 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY

[Group 8: ]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Preliminary Requirements

Required Conditions

Action/Condition Data Module/Technical Publication

Service Bulletin B787-81205-SB380009-00 - B787-A-38-00-0009-00A-933A-D Issue 002

ACCOMPLISHMENT INSTRUCTIONS

Applicable To: B787-A-38-00-0009-12A-933B-D

Model 787 Issue 002, 09 Dec 2015

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Procedure

This Task applies to Group 8:

ICN-B787-A-000061-A-81205-08991-A-01-1

Figure 1 

Applicable To: B787-A-38-00-0009-12A-933B-D

Model 787 Issue 002, 09 Dec 2015

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ICN-B787-A-000061-A-81205-08992-A-01-1

Figure 2 

Applicable To: B787-A-38-00-0009-12A-933B-D

Model 787 Issue 002, 09 Dec 2015

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ICN-B787-A-000061-A-81205-08993-A-01-1

Figure 3 

Applicable To: B787-A-38-00-0009-12A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

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AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08994-A-01-1

Figure 4 

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AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-08995-A-01-1

Figure 5 

Applicable To: B787-A-38-00-0009-12A-933B-D

Model 787 Issue 002, 09 Dec 2015

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ICN-B787-A-000061-A-81205-08996-A-01-1

Figure 6 

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ICN-B787-A-000061-A-81205-08997-A-01-1

Figure 7 

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ICN-B787-A-000061-A-81205-08998-A-01-1

Figure 8 

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ICN-B787-A-000061-A-81205-08999-A-01-1

Figure 9 

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-09000-A-01-1

Figure 10 

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ICN-B787-A-000061-A-81205-09001-A-01-1

Figure 11 

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ICN-B787-A-000061-A-81205-09002-A-01-1

Figure 12 

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ICN-B787-A-000061-A-81205-09003-A-01-1

Figure 13 

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ICN-B787-A-000061-A-81205-09004-A-01-1

Figure 14 

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ICN-B787-A-000061-A-81205-09005-A-01-1

Figure 15 

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
1. The step numbers shown below agree with the numbers shown in the circle symbols in the Task. The QTY

numbers shown below are the number of parts necessary for this Task.

Table 1 

Step Action Name Identification Qty More Data

1 Remove TIE STRAP BACS38K1 50 *[1]

2 Remove / Keep SPLIT SHROUD 77000-910-() 19 *[1]

3 Remove / Keep TEE SHROUD 77000-912-003 1

4 Remove COUPLING AS1655C12 6

COUPLING BODY, 14C34-12C 6 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

5 Install (New)

6 Remove TAPE PERMACEL P-29 1

7 Remove / Keep WYE SHROUD 77000-912-() 3

8 Remove / Keep UPPER TEE SHROUD 77000-912-002 3

Remove / Keep LOWER TEE SHROUD 77000-912-002 3

9 Remove COUPLING AS1655C08 15

COUPLING BODY, 14C34-08C 15 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

10 Install (New)

11 Install (Kept) UPPER TEE SHROUD 77000-912-002 3 *[3] *[4]

Install (Kept) LOWER TEE SHROUD 77000-912-002 3

12 Install (Kept) WYE SHROUD 77000-912-001 3 *[3] *[4]

13 Install (New) TAPE PERMACEL P-29 1 *[3] *[4]

14 Install (Kept) SPLIT SHROUD 77000-910-() 19 *[3] *[4]

15 Install (Kept) TEE SHROUD 77000-912-003 1 *[3] *[4]

STRAP, PLASTIC, AD- BACS38K1 50 *[3] *[4]

JUSTABLE, SELFLOCKING

16 Install (New)

*[1] Remove tie straps as needed to locally peel back split shrouds to get access to the couplings inside the split shrouds.

*[2] Install the clamshell body over the sleeve (or female ferrule), enclosing both end flanges and snap shut the latch pawls. Make sure

that the clamshell body is completely engaged. Engage the safety strap onto the pawl. Make sure that the latches and safety strap

are fully secured and the latches are fully engaged.

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Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 1 

Step Action Name Identification Qty More Data

*[3] Do not install the kept shrouds and new tie straps until successful completion of the Potable Water System - Leak Test in Step 6 of

the Work Package 2 in the Work Instructions.

*[4] Refer to Appendix A to re-install the shrouds as an accepted procedure.

Applicable To: B787-A-38-00-0009-12A-933B-D

Model 787 End of data module Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

Task 13 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY

[Group 9: ]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Preliminary Requirements

Required Conditions

Action/Condition Data Module/Technical Publication

Service Bulletin B787-81205-SB380009-00 - B787-A-38-00-0009-00A-933A-D Issue 002

ACCOMPLISHMENT INSTRUCTIONS

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AIRCRAFT SERVICE BULLETIN
Procedure

This Task applies to Group 9:

ICN-B787-A-000061-A-81205-09006-A-01-1

Figure 1 

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ICN-B787-A-000061-A-81205-09007-A-01-1

Figure 2 

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ICN-B787-A-000061-A-81205-09008-A-01-1

Figure 3 

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ICN-B787-A-000061-A-81205-09009-A-01-1

Figure 4 

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ICN-B787-A-000061-A-81205-09010-A-01-1

Figure 5 

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ICN-B787-A-000061-A-81205-09011-A-01-1

Figure 6 

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ICN-B787-A-000061-A-81205-09012-A-01-1

Figure 7 

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ICN-B787-A-000061-A-81205-09013-A-01-1

Figure 8 

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ICN-B787-A-000061-A-81205-09014-A-01-1

Figure 9 

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ICN-B787-A-000061-A-81205-09015-A-01-1

Figure 10 

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ICN-B787-A-000061-A-81205-09016-A-02-1

Figure 11 

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ICN-B787-A-000061-A-81205-09017-A-02-1

Figure 12 

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ICN-B787-A-000061-A-81205-09018-A-01-1

Figure 13 

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
1. The step numbers shown below agree with the numbers shown in the circle symbols in the Task. The QTY

numbers shown below are the number of parts necessary for this Task.

Table 1 

Step Action Name Identification Qty More Data

1 Remove TIE STRAP BACS38K1 44 *[1]

2 Remove / Keep SPLIT SHROUD 77000-910-() 20 *[1]

3 Remove / Keep TEE SHROUD 77000-912-003 1

4 Remove COUPLING AS1655C12 6

COUPLING BODY, 14C34-12C 6 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

5 Install (New)

6 Remove TAPE PERMACEL P-29 1

7 Remove / Keep WYE SHROUD 77000-912-() 2

8 Remove / Keep UPPER TEE SHROUD 77000-912-002 4

Remove / Keep LOWER TEE SHROUD 77000-912-002 4

9 Remove COUPLING AS1655C08 12

COUPLING BODY, 14C34-08C 12 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

10 Install (New)

11 Install (Kept) UPPER TEE SHROUD 77000-912-002 4 *[3] *[4]

Install (Kept) LOWER TEE SHROUD 77000-912-002 4

12 Install (Kept) WYE SHROUD 77000-912-001 2 *[3] *[4]

13 Install (New) TAPE PERMACEL P-29 1 *[3] *[4]

14 Install (Kept) SPLIT SHROUD 77000-910-() 20 *[3] *[4]

15 Install (Kept) TEE SHROUD 77000-912-003 1 *[3] *[4]

STRAP, PLASTIC, AD- BACS38K1 44 *[3] *[4]

JUSTABLE, SELFLOCKING

16 Install (New)

*[1] Remove tie straps as needed to locally peel back split shrouds to get access to the couplings inside the split shrouds.

*[2] Install the clamshell body over the sleeve (or female ferrule), enclosing both end flanges and snap shut the latch pawls. Make sure

that the clamshell body is completely engaged. Engage the safety strap onto the pawl. Make sure that the latches and safety strap

are fully secured and the latches are fully engaged.

Applicable To: B787-A-38-00-0009-13A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Table 1 

Step Action Name Identification Qty More Data

*[3] Do not install the kept shrouds and new tie straps until successful completion of the Potable Water System - Leak Test in Step 6 of

the Work Package 2 in the Work Instructions.

*[4] Refer to Appendix A to re-install the shrouds as an accepted procedure.

Applicable To: B787-A-38-00-0009-13A-933B-D

Model 787 End of data module Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB380009-00

Task 14 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY

[Group 10: ]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Preliminary Requirements

Required Conditions

Action/Condition Data Module/Technical Publication

Service Bulletin B787-81205-SB380009-00 - B787-A-38-00-0009-00A-933A-D Issue 002

ACCOMPLISHMENT INSTRUCTIONS

Applicable To: B787-A-38-00-0009-14A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
Procedure

This Task applies to Group 10:

ICN-B787-A-000061-A-81205-09019-A-01-1

Figure 1 

Applicable To: B787-A-38-00-0009-14A-933B-D

Model 787 Issue 002, 09 Dec 2015

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ICN-B787-A-000061-A-81205-09020-A-01-1

Figure 2 

Applicable To: B787-A-38-00-0009-14A-933B-D

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ICN-B787-A-000061-A-81205-09021-A-01-1

Figure 3 

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ICN-B787-A-000061-A-81205-09022-A-01-1

Figure 4 

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AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-09023-A-01-1

Figure 5 

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ICN-B787-A-000061-A-81205-09024-A-01-1

Figure 6 

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ICN-B787-A-000061-A-81205-09025-A-01-1

Figure 7 

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ICN-B787-A-000061-A-81205-09026-A-01-1

Figure 8 

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ICN-B787-A-000061-A-81205-09027-A-01-1

Figure 9 

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ICN-B787-A-000061-A-81205-09028-A-01-1

Figure 10 

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Model 787 Issue 002, 09 Dec 2015

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AIRCRAFT SERVICE BULLETIN
ICN-B787-A-000061-A-81205-09029-A-01-1

Figure 11 

Applicable To: B787-A-38-00-0009-14A-933B-D

Model 787 Issue 002, 09 Dec 2015

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B787-81205-SB380009-00

Issue 002, 09 Dec 2015

AIRCRAFT SERVICE BULLETIN
1. The step numbers shown below agree with the numbers shown in the circle symbols in the Task. The QTY

numbers shown below are the number of parts necessary for this Task.

Table 1 

Step Action Name Identification Qty More Data

1 Remove TIE STRAP BACS38K1 31 *[1]

2 Remove / Keep SPLIT SHROUD 77000-910-() 13 *[1]

3 Remove / Keep TEE SHROUD 77000-912-003 1

4 Remove COUPLING AS1655C12 6

COUPLING BODY, 14C34-12C 6 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

5 Install (New)

6 Remove TAPE PERMACEL P-29 1

7 Remove / Keep WYE SHROUD 77000-912-() 2

8 Remove / Keep UPPER TEE SHROUD 77000-912-002 2

Remove / Keep LOWER TEE SHROUD 77000-912-002 2

9 Remove COUPLING AS1655C08 8

COUPLING BODY, 14C34-08C 8 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

10 Install (New)

11 Install (Kept) UPPER TEE SHROUD 77000-912-002 2 *[3] *[4]

Install (Kept) LOWER TEE SHROUD 77000-912-002 2

12 Install (Kept) WYE SHROUD 77000-912-001 2 *[3] *[4]

13 Install (New) TAPE PERMACEL P-29 1 *[3] *[4]

14 Install (Kept) SPLIT SHROUD 77000-910-() 13 *[3] *[4]

15 Install (Kept) TEE SHROUD 77000-912-003 1 *[3] *[4]

STRAP, PLASTIC, AD- BACS38K1 31 *[3] *[4]

JUSTABLE, SELFLOCKING

16 Install (New)

*[1] Remove tie straps as needed to locally peel back split shrouds to get access to the couplings inside the split shrouds.

*[2] Install the clamshell body over the sleeve (or female ferrule), enclosing both end flanges and snap shut the latch pawls. Make sure

that the clamshell body is completely engaged. Engage the safety strap onto the pawl. Make sure that the latches and safety strap

are fully secured and the latches are fully engaged.

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Table 1 

Step Action Name Identification Qty More Data

*[3] Do not install the kept shrouds and new tie straps until successful completion of the Potable Water System - Leak Test in Step 6 of

the Work Package 2 in the Work Instructions.

*[4] Refer to Appendix A to re-install the shrouds as an accepted procedure.

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Service Bulletin B787-81205-SB380009-00

Task 15 – REPLACEMENT OF COUPLINGS LOCATED ABOVE AFT EE BAY

[Group 11: ]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

Preliminary Requirements

Required Conditions

Action/Condition Data Module/Technical Publication

Service Bulletin B787-81205-SB380009-00 - B787-A-38-00-0009-00A-933A-D Issue 002

ACCOMPLISHMENT INSTRUCTIONS

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Procedure

This Task applies to Group 11:

ICN-B787-A-000061-A-81205-09030-A-01-1

Figure 1 

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ICN-B787-A-000061-A-81205-09031-A-01-1

Figure 2 

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ICN-B787-A-000061-A-81205-09032-A-01-1

Figure 3 

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ICN-B787-A-000061-A-81205-09033-A-01-1

Figure 4 

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ICN-B787-A-000061-A-81205-09034-A-01-1

Figure 5 

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ICN-B787-A-000061-A-81205-09035-A-01-1

Figure 6 

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ICN-B787-A-000061-A-81205-09036-A-01-1

Figure 7 

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ICN-B787-A-000061-A-81205-09037-A-01-1

Figure 8 

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ICN-B787-A-000061-A-81205-09038-A-01-1

Figure 9 

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ICN-B787-A-000061-A-81205-09039-A-01-1

Figure 10 

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1. The step numbers shown below agree with the numbers shown in the circle symbols in the Task. The QTY

numbers shown below are the number of parts necessary for this Task.

Table 1 

Step Action Name Identification Qty More Data

1 Remove TIE STRAP BACS38K1 28 *[1]

2 Remove / Keep SPLIT SHROUD 77000-910-() 12 *[1]

3 Remove / Keep TEE SHROUD 77000-912-003 1

4 Remove COUPLING AS1655C12 6

COUPLING BODY, 14C34-12C 6 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

5 Install (New)

6 Remove TAPE PERMACEL P-29 1

7 Remove / Keep WYE SHROUD 77000-912-() 2

8 Remove / Keep UPPER TEE SHROUD 77000-912-002 2

Remove / Keep LOWER TEE SHROUD 77000-912-002 2

9 Remove COUPLING AS1655C08 7

COUPLING BODY, 14C34-08C 7 *[2]

THREADLESS -

FLEXIBLE, FIXED

CAVITY, SELF-BONDING

10 Install (New)

11 Install (Kept) UPPER TEE SHROUD 77000-912-002 2 *[3] *[4]

Install (Kept) LOWER TEE SHROUD 77000-912-002 2

12 Install (Kept) WYE SHROUD 77000-912-001 2 *[3] *[4]

13 Install (New) TAPE PERMACEL P-29 1 *[3] *[4]

14 Install (Kept) SPLIT SHROUD 77000-910-() 12 *[3] *[4]

15 Install (Kept) TEE SHROUD 77000-912-003 1 *[3] *[4]

STRAP, PLASTIC, AD- BACS38K1 28 *[3] *[4]

JUSTABLE, SELFLOCKING

16 Install (New)

*[1] Remove tie straps as needed to locally peel back split shrouds to get access to the couplings inside the split shrouds.

*[2] Install the clamshell body over the sleeve (or female ferrule), enclosing both end flanges and snap shut the latch pawls. Make sure

that the clamshell body is completely engaged. Engage the safety strap onto the pawl. Make sure that the latches and safety strap

are fully secured and the latches are fully engaged.

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Table 1 

Step Action Name Identification Qty More Data

*[3] Do not install the kept shrouds and new tie straps until successful completion of the Potable Water System - Leak Test in Step 6 of

the Work Package 2 in the Work Instructions.

*[4] Refer to Appendix A to re-install the shrouds as an accepted procedure.

Applicable To: B787-A-38-00-0009-15A-933B-D

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Service Bulletin B787-81205-SB380009-00

Appendix A – 787 POTABLE WATER SHROUD INSTALLATION [Group

1-16:]

This is a standard issue of Alert Service Bulletin B787-81205-SB380009-00. While the information

revised in this issue is standard, the service bulletin is alert and requires the urgent attention of

affected operators.

Alert:

References

Reference Title

SWPM 20-10-11 Standard Wiring Practices Manual

Procedure

Group 1-16:

1. GENERAL SHROUD INSTALLATION REQUIREMENTS

Install shrouds using the -shingle principle-, working your way down so that the upper shroud feeds into the

lower shroud.

Ensure there are no valleys or buckling along the shroud that would prevent water flow.

The shroud shall be installed to completely cover the intended hose / tube and couplings.

In trunk runs and in areas where clamps are installed over split shrouds, install the shroud with the seam

facing up. In areas where support clamps are clamped to the tube or hose inside the shroud, orient the

overlap so that the upper seam feeds inside the lower seam.

Ensure that the clamps and/or tie straps do not collapse the shroud.

Figure 1 shows the split shroud overlap orientation. In trunk runs or on Door 1 branch lines where the clamps

are installed over the shroud, install shroud with seam facing up and maintaining a minimum 0.25 inch

overlap. In areas where support clamps are clamped to the tube or hose inside the shroud and the clamp

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locations prohibit the seam from being on top of the shroud, orient the overlap so that the upper seam feeds

inside the lower seam.

ICN-B787-A-000061-A-81205-09040-A-01-1

Figure 1 TYPICAL SPLIT SHROUD OVERLAP ORIENTATION

Figure 2 shows the split shroud supported by a clamp. At door 1, the clamps are installed over the shroud,

so install the split shroud with the seam facing up as shown

ICN-B787-A-000061-A-81205-09041-A-01-1

Figure 2 TYPICAL SPLIT SHROUDS INSIDE A CLAMP SUPPORT

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Figure 3 shows the tee shroud in the potable water line near the forward monuments in a typical configuration

when there is a lavatory on the left side and a galley on the right hand side.

ICN-B787-A-000061-A-81205-09042-A-01-1

Figure 3 TEE SHROUD WITH HEATED HOSE CONNECTIONS (DOOR 1)

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Figure 4 shows the tee shroud in the potable water line near the forward monuments in a configuration when

there is not a lavatory on the left side and a galley on the right hand side.

ICN-B787-A-000061-A-81205-09043-A-01-1

Figure 4 TEE SHROUD WITH NO LEFT HAND LAVATORY (DOOR 1)

Figure 5 shows the typical Door 3 trunk run split shroud as it goes around tube supports and couplings

(shroud is shown transparent in the detail so the supports and couplings can be seen). Install the split shroud

with the seam facing up as shown.

ICN-B787-A-000061-A-81205-09044-A-01-1

Figure 5 TRUNK RUN SPLIT SHROUDS AROUND SUPPORTS (DOOR 3)

Figure 6 shows the shrouds in the connections where the potable water line transitions from a trunk run into

the branch lines. In this Figure there are branch lines going in both directions. The molded wye and tee

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shrouds get installed over the trunk run pullout tube and tee, and then the trunk run split shroud gets installed

over the molded wye shroud and secured with tie straps.

ICN-B787-A-000061-A-81205-09045-A-01-1

Figure 6 WYE SHROUD AND TEE SHROUD WITH LINES GO TWO WAYS LEFT AND RIGHT (DOOR 3)

Figure 7 shows the shrouds in the connections where the potable water line transitions from a trunk run into

a branch line. In this Figure there is a branch line going in only one direction, so the unused side of the

molded tee shroud needs to be taped over to prevent water spray in the event of a leak. The molded wye

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and tee shrouds get installed over the trunk run pullout tube and elbow, and then the trunk run split shroud

gets installed over the molded wye shroud and secured with tie straps.

ICN-B787-A-000061-A-81205-09046-A-01-1

Figure 7 WYE SHROUD AND TEE SHROUD WITH LINE GO ONE WAY (DOOR 3)

Figure 8 and 9 shows the situation when there is a branch line that has a tee installed in the middle. In this

situation, a molded shroud is placed over the tee and then the split shrouds on each side get taped to the

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molded shroud. Also see Figure 9, View A, where another view of this area is provided where the split shroud

overlap detail can be seen for clarification.

ICN-B787-A-000061-A-81205-09047-A-01-1

Figure 8 TEE SHROUD IN BRANCH LINE CONNECTION (DOOR 3)

ICN-B787-A-000061-A-81205-09048-A-01-1

Figure 9 TEE SHROUD IN BRANCH LINE CONNECTION - VIEW A (DOOR 3)

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Figure 10 shows the typical Door 3 branch line split shroud. At door 3, the support clamps are clamped to

the tube or hose inside the shroud, so orient the overlap of the split shroud so that the upper seam feeds

inside the lower seam.

ICN-B787-A-000061-A-81205-09049-A-01-1

Figure 10 SPLIT SHROUD IN BRANCH LINE WITH SUPPORTS (DOOR 3)

Table 1 

NOTE NUMBER DESCRIPTION

Locate BACS38K1 tie straps approximately as shown, 8 inch

maximum spacing, plus extra on either side of tube supports,

where other shrouds protrude, and in corner areas to ensure

shroud remains closed. Loosely install BACS38K1 tie straps

around the shroud until just snug. DO NOT COLLAPSE SHROUD.

1

Seal joint between shrouds with a minimum of 2 layers of P-29

Permacel tape and ensure a minimum 0.50 inches overlap on

each shroud.

2

Install BACS38K1 tie straps. In these indicated locations, tension

tie straps with panduit tool to secure split shroud to molded tee

shroud.

3

Seal joint between shrouds with a minimum of 2 layers of P-29

Permacel tape and ensure a minimum 0.50 inches overlap on

each shroud. Seal seam of vertical branch of tee shroud with 2

wraps of tape with 0.25 inch minimum tape overlap. Seal around

wires protruding through vertical seam.

4

If removed, wrap pigtail wire with A-A-59163 buildup tape. Secure

to shroud with BMS13-54 lacing tape. Apply as required to secure

pigtail. Refer to SWPM 20-10-11 as an accepted procedure.

5

Apply minimum 2 layers of P-29 Permacel tape to shroud end to

cover opening. Secure by applying minimum 2 wraps of P-29

Permacel tape around shroud

6

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Table 1 

NOTE NUMBER DESCRIPTION

If removed, loosely install BACS38K1 tie strap in the clamp as

shown until just snug. Do not close clamp ends together or shroud

may collapse or be damaged. Do not collapse shroud.

7

Orient the overlap so that the upper seam feeds inside the lower

seam.

8

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