Service Bulletin B787-81205-SB270023-00 FLIGHT CONTROLS - Primary

Flight Control Function - Flight Control Electronics Block Point 4 Software

Change

Publication: B787-81205-SB270023-00 Issue 001, 24 Jul 2014

BOEING PROPRIETARY, CONFIDENTIAL AND/OR TRADE SECRET

Copyright © 2014 Boeing. Unpublished Work. All rights reserved.

Treatment of this data module and its content is governed by contract with Boeing. Rights to use this data module are licensed on a per

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ECCN: 9E991

The applicability information below is referenced at the lower left of each page to indicate the page applicability.

These references are valid for this print copy only.

PM Applicability (Publication Module applicability)

787-8 Airplanes. Refer to Data Module SB B787-A-27-00-0023-00A-932A-D, Paragraph 1., Effectivity for the

list of affected airplanes.

TITLE PAGE B787-81205-SB270023-00

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2.0

B787-81205-SB270023-00

Issue 001, 24 Jul 2014

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB270023-00

Table of Contents

Page

Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4

PLANNING INFORMATION ..........................................7

1. Effectivity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7

A. Airplanes ............................................7

B. Spares Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

2. Concurrent Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

3. Reason . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

4. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

5. Compliance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

6. Approval . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

7. Manpower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

8. Weight and Balance Changes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

9. Electrical Load Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

10. References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

A. Existing Data: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

B. Data Supplied with this Service Bulletin: . . . . . . . . . . . . . . . . . . . . . . . . . . 14

C. Installation Requirement Modules Used in the Preparation of this Service Bulletin: . . . 14

11. Publications Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14

12. Interchangeability and Intermixability of Parts . . . . . . . . . . . . . . . . . . . . . . . . . 14

13. Software Accomplishment Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14

MATERIAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

1. Material - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

2. Industry Support Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

3. Parts Necessary for Each Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

A. Kits/Parts: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

B. Parts and Materials Supplied by the Operator: . . . . . . . . . . . . . . . . . . . . . . . 15

C. Parts Modified and Reidentified: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

D. Parts Removed and Not Replaced: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19

4. Parts Necessary to Change Spares . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

5. Special Tooling - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20

6. Special Tooling Necessary to do this Service Bulletin . . . . . . . . . . . . . . . . . . . . . 20

ACCOMPLISHMENT INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

1. GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

2. WORK INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22

TABLE OF CONTENTS B787-81205-SB270023-00

Issue 001, 24 Jul 2014

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B787-81205-SB270023-00

Issue 001, 24 Jul 2014

AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB270023-00

List of Effective Data Modules

Description

Group 1-2:

Table 1 List of Effective Data Modules - Service Bulletin B787-81205-SB270023-00

Data Module – Information Name Issue Issue Status Issue Date

B787-A-27-00-0023-00A-00SA-D – List of Effective Data Modules 001 New 2014-07-24

B787-A-27-00-0023-00A-931C-D – Summary 001 New 2014-07-24

B787-A-27-00-0023-00A-932A-D – PLANNING INFORMATION 001 New 2014-07-24

B787-A-27-00-0023-00A-934A-D – MATERIAL INFORMATION 001 New 2014-07-24

B787-A-27-00-0023-00A-933A-D – ACCOMPLISHMENT INSTRUCTIONS 001 New 2014-07-24

Applicable To: B787-A-27-00-0023-00A-00SA-D

Model 787 End of data module Issue 001, 24 Jul 2014

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B787-81205-SB270023-00

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AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB270023-00

Summary

References

Reference Title

SB B787-A-27-00-0023-00A-932A-D Issue 001, Concurrent Requirements

Paragraph 2.

SB B787-A-27-00-0023-00A-932A-D Issue 001, Spares Affected

Paragraph 1.B.

SB B787-A-27-00-0023-00A-932A-D Issue 001, Compliance

Paragraph 5.

SB B787-A-27-00-0023-00A-932A-D Issue 001, Weight and Balance Changes

Paragraph 8.

SB B787-A-27-00-0023-00A-932A-D Issue 001, Electrical Load Data

Paragraph 9.

SB B787-A-27-00-0023-00A-932A-D Issue 001, Publications Affected

Paragraph 11.

SB B787-A-27-00-0023-00A-934A-D Issue 001, Kits/Parts

Paragraph 3.A.

SB B787-A-27-00-0023-00A-934A-D Issue 001, Parts and Materials Supplied by the Operator

Paragraph 3.B.

SB B787-A-27-00-0023-00A-934A-D Issue 001, Special Tooling Necessary to do this Service Bulletin

Paragraph 6.

SB B787-A-27-00-0023-00A-932A-D Issue 001, Effectivity

Paragraph 1.

SB B787-A-27-00-0023-00A-934A-D Issue 001, Industry Support Information

Paragraph 2.

SB B787-A-27-00-0023-00A-932A-D Issue 001, Manpower

Paragraph 7.

SB B787-A-27-00-0023-00A-934A-D Issue 001, Material - Price and Availability

Paragraph 1.

Applicable To: B787-A-27-00-0023-00A-931C-D

Model 787 Issue 001, 24 Jul 2014

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B787-81205-SB270023-00

Issue 001, 24 Jul 2014

AIRCRAFT SERVICE BULLETIN
Description

Group 1-2:

1. CONCURRENT REQUIREMENTS

Refer to Data Module SB B787-A-27-00-0023-00A-932A-D, Paragraph 2., Concurrent Requirements.

2. BACKGROUND

This service bulletin gives instructions to install Flight Control Module (FCM) Operational Program Software

(OPS), FCM Loadable Diagnostic Information (LDI) Database (DB), FCM Air Data Reference Function

(ADRF) DB, and Central Maintenance Computer Function (CMCF) LDI DB software to correct deficiencies

in the following areas:

– Nuisance unwanted post flight or initiated test failures under unusual operating conditions or with some

pre-existing failures

– Fixes for difficulties gathering fault data, or doing detailed troubleshooting with initiated test capabilities

on airplanes in service

– Misleading, extra, or missing fault reports that can lead to the mechanic not being given satisfactory

data on what components to change

– Address when initiated tests either cannot be run, or require time consuming procedures when some

pre-existing failures are present

– Nuisance advisory Engine-Indicating and Crew-Alerting System (EICAS) messages requiring inspections

and system tests before further airplane dispatch

– Correct nuisance issues in the Air Data Reference Function (ADRF)

– Nuisance disconnect of the Autopilot Column Backdrive

– Nuisance indications of NO LAND 3, NO AUTOLAND, and AUTOFLIGHT FUNCTION status and advisory messages.

If the changes in this service bulletin are not done, the FCE software may not function as originally intended,

which could result in deficiencies in the control law and maintenance areas which could result in nuisance

EICAS and Maintenance messages, and could cause intermittent indications in the flight deck.

Boeing Service Related Problem (SRP) 787 SRP-27-0249 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-27-00-0023-00A-932AD, Paragraph 1.B., Spares AffectedSpares Affected No

Data Module SB B787-A-27-00-0023-00A-932AD, Paragraph 5., ComplianceAD Related No

Data Module SB B787-A-27-00-0023-00A-932AD, Paragraph 8., Weight and Balance ChangesWeight and Balance Changed No

Data Module SB B787-A-27-00-0023-00A-932AD, Paragraph 9., Electrical Load DataElectrical Load Changed No

Applicable To: B787-A-27-00-0023-00A-931C-D

Model 787 Issue 001, 24 Jul 2014

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AIRCRAFT SERVICE BULLETIN
Table 1

Planning Data Affected Data Module Reference

Data Module SB B787-A-27-00-0023-00A-932AD, Paragraph 11., Publications AffectedPublications Affected Yes

Data Module SB B787-A-27-00-0023-00A-932AD, Paragraph 11., Publications AffectedAirplane Flight Operations Affected (Flight Crew No

Operations Manual and/or FAA Approved Airplane Flight Manual)

Data Module SB B787-A-27-00-0023-00A-934AD, Paragraph 3.A., Kits/PartsKits/Parts Required No

Data Module SB B787-A-27-00-0023-00A-934AD, Paragraph 3.B., Parts and Materials Supplied

by the Operator

Operator Supplied Parts/Material Yes

Data Module SB B787-A-27-00-0023-00A-934AD, Paragraph 6., Special Tooling Necessary to

do this Service Bulletin

Special Tooling Required No

3. ACTION

(CN-AA45979B)

Use the Onboard Data Load Function (ODLF) to install Flight Control Module (FCM) Operational Program

Software (OPS), FCM Loadable Diagnostic Information (LDI) Database (DB), FCM Air Data Reference

Function (ADRF) DB, and Central Maintenance Computer Function (CMCF) LDI DB software, and do a

software configuration check.

4. EFFECTIVITY

787-8 Airplanes. Refer to Data Module SB B787-A-27-00-0023-00A-932A-D, Paragraph 1., Effectivity for

the list of affected airplanes.

5. COMPLIANCE

Refer to Data Module SB B787-A-27-00-0023-00A-932A-D, Paragraph 5., Compliance.

6. INDUSTRY SUPPORT INFORMATION

Boeing warranty remedies are available for airplanes in warranty as of February 13th, 2014. Please refer

to Data Module SB B787-A-27-00-0023-00A-934A-D, Paragraph 2., Industry Support Information. The

warranty remedies will expire eight years from the original release date of this service bulletin.

7. MANPOWER

Refer to Data Module SB B787-A-27-00-0023-00A-932A-D, Paragraph 7., Manpower.

8. MATERIAL INFORMATION

Operator Supplied Parts/Materials.

Refer to Data Module SB B787-A-27-00-0023-00A-934A-D, Paragraph 1., Material - Price and Availability.

Applicable To: B787-A-27-00-0023-00A-931C-D

Model 787 End of data module Issue 001, 24 Jul 2014

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B787-81205-SB270023-00

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AIRCRAFT SERVICE BULLETIN
Service Bulletin B787-81205-SB270023-00

PLANNING INFORMATION

References

Reference Title

SB B787-A-27-00-0023-00A-934A-D Issue 001, Parts Necessary for Each Airplane

Paragraph 3.

INDICATING/RECORDING SYSTEMS - Primary

Display System - Displays and Crew Alerting

SB B787-81205-SB310008-00

Operational Program Software Block Point 3.5

Installation

787 AMM 24-22-00 AC GENERATION AND BUS CONTROL

CENTRAL MAINTENANCE COMPUTING

FUNCTION

787 AMM 45-11-00

787 AMM 45-13-00 ONBOARD DATA LOAD FUNCTION

ONBOARD BOEING ELECTRONIC DISTRIBUTION

SYSTEM

787 AMM 46-13-00

787 FIM 27-00 FLIGHT CONTROLS

Description

Group 1-2:

1. Effectivity

A. Airplanes

This service bulletin is applicable to 787-8 Airplanes equipped with General Engine engines, line

numbers 6-6, 11-11, 20-21, 23-23, 25-30, 32-39, 43-46, 49-50, 52-55, 57-58, 60-60, 62-62, 64-65, 70-

73, 75-77, 79-79, 81-82, 84-85, 89-96, 98-100, 103-106, 109-109, 115-117, 119-119, 122-125, 127-

127, 129-129, 131-131, 134-135, 137-138, 141-145, 150-152, 154-155, 157-160, 162-164, 167-168,

170-172, 174-176, 180-180, 182-182, 184-184, 186-186, 188-189, 191-192, 194-194, and 198 and

Rolls Royce Engines, line numbers 7-9, 24-24, 31-31, 40-42, 47-48, 51-51, 56-56, 59-59, 61-61, 63-

63, 66-69, 74-74, 78-78, 80-80, 83-83, 86-88, 97-97, 101-102, 107-108, 110-114, 118-118, 120-121,

128-128, 130-130, 132-132, 136-136, 140-140, 147-149, 153-153, 156-156, 161-161, 165-166, 173-

173, 177-179, 183-183, 185-185, 187-187, 190-190, 193-193, 195-195, 197-197 and 199 in 2 Groups.

The Variable Numbers and Group information for the applicable airplanes is given below. An equivalent

change is on subsequent production airplanes. Refer to CN-AA45979 for data about this change.

Applicable To: B787-A-27-00-0023-00A-932A-D

Model 787 Issue 001, 24 Jul 2014

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B787-81205-SB270023-00

Issue 001, 24 Jul 2014

AIRCRAFT SERVICE BULLETIN
Table 1

GROUP CONFIGURATION DESCRIPTION

1 - 787-8 Airplanes with General Electric engines

787-8 Airplanes with General Electric engines that must accomplish

Service Bulletin SB B787-81205-SB310008-00, are affected by Service

Bulletin SB B787-81205-SB240039-00, and have accomplished Service

Bulletin SB B787-81205-SB240039-00.

1

787-8 Airplanes with General Electric engines that must accomplish

Service Bulletin SB B787-81205-SB310008-00, are affected by Service

Bulletin SB B787-81205-SB240039-00, and have not accomplished

Service Bulletin SB B787-81205-SB240039-00.

2

787-8 Airplanes with General Electric engines that are not affected

by Service Bulletin SB B787-81205-SB310008-00, are affected by

Service Bulletin SB B787-81205-SB240039-00, and have accomplished

Service Bulletin SB B787-81205-SB240039-00.

3

787-8 Airplanes with General Electric engines that are not affected

by Service Bulletin SB B787-81205-SB310008-00, are affected by

Service Bulletin SB B787-81205-SB240039-00, and have not accomplished Service Bulletin SB B787-81205-SB240039-00.

4

787-8 Airplanes with General Electric engines that are not affected

by Service Bulletin SB B787-81205-SB310008-00, and are not affected

by Service Bulletin SB B787-81205-SB240039-00.

5

Applicable To: B787-A-27-00-0023-00A-932A-D

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B787-81205-SB270023-00

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AIRCRAFT SERVICE BULLETIN
Table 1

GROUP CONFIGURATION DESCRIPTION

2 - 787-8 Airplanes with Rolls Royce engines

787-8 Airplanes with Rolls Royce engines that must accomplish Service

Bulletin SB B787-81205-SB310008-00, and must accomplish Service

Bulletin SB B787-81250-730017-00, are affected by Service Bulletin

SB B787-81205-SB240039-00, and have accomplished Service Bulletin

SB B787-81205-SB240039-00.

1

787-8 Airplanes with Rolls Royce engines that must accomplish Service

Bulletin SB B787-81205-SB310008-00, and must accomplish Service

Bulletin SB B787-81250-730017-00, are affected by Service Bulletin

SB B787-81205-SB240039-00, and have not accomplished Service

Bulletin SB B787-81205-SB240039-00.

2

787-8 Airplanes with Rolls Royce engines that must accomplish Service

Bulletin SB B787-81250-730017-00, are not affected by Service Bulletin

SB B787-81205-SB310008-00, are affected by Service Bulletin SB

B787-81205-SB240039-00, and have accomplished Service Bulletin

SB B787-81205-SB240039-00.

3

787-8 Airplanes with Rolls Royce engines that must accomplish Service

Bulletin SB B787-81250-730017-00, are not affected by Service Bulletin

SB B787-81205-SB310008-00, are affected by Service Bulletin SB

B787-81205-SB240039-00, and have not accomplished Service Bulletin SB B787-81205-SB240039-00.

4

787-8 Airplanes with Rolls Royce engines that must accomplish Service

Bulletin SB B787-81250-730017-00, are not affected by Service Bulletin

SB B787-81205-SB310008-00, and are not affected by Service Bulletin

SB B787-81205-SB240039-00.

5

787-8 Airplanes with Rolls Royce engines that are not affected by

Service Bulletin SB B787-81205-SB310008-00, are not affected by

Service Bulletin SB B787-81205-SB240039-00, and are not affected

by Service Bulletin SB B787-81250-730017-00.

6

Airplane Models: 787-8

Table 2

Variable Number Group

ZA006 1

ZA100-ZA105 2

ZA116-ZA124 2

ZA135-ZA137 2

ZA175-ZA189 1

ZA215-ZA220 1

Applicable To: B787-A-27-00-0023-00A-932A-D

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AIRCRAFT SERVICE BULLETIN
Table 2

Variable Number Group

ZA230-ZA245 1

ZA260-ZA267 1

ZA270-ZA275 2

ZA285-ZA295 1

ZA317-ZA322 1

ZA327 1

ZA334 1

ZA380-ZA389 1

ZA430-ZA437 1

ZA445-ZA448 2

ZA450-ZA457 2

ZA460-ZA474 1

ZA506-ZA516 2

ZA536-ZA542 2

ZA560-ZA565 1

ZA576-ZA580 2

ZA586 1

ZA588 2

ZA610-ZA612 1

ZA650-ZA651 2

ZA655-ZA657 1

ZA695 1

ZA778-ZA779 2

ZA841 1

B. Spares Affected

None.

2. Concurrent Requirements

Group 1, Configuration 1-2:

The service bulletin listed below must be done before this service bulletin.

Applicable To: B787-A-27-00-0023-00A-932A-D

Model 787 Issue 001, 24 Jul 2014

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B787-81205-SB270023-00

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AIRCRAFT SERVICE BULLETIN
Group 1, Configuration 1-2:

Table 3

Company Service Bulletin Description

INDICATING/RECORDING SYSTEMS -

Primary Display System - Displays and Crew

Alerting Operational Program Software Block

Point 3.5 Installation

Service Bulletin SB B787-81205-SB310008-

00 Issue 001

Boeing

Group 2, Configuration 1-2:

The service bulletins listed below must be done before this service bulletin.

Group 2, Configuration 1-2:

Table 4

Company Service Bulletin Description

INDICATING/RECORDING SYSTEMS -

Primary Display System - Displays and Crew

Alerting Operational Program Software Block

Point 3.5 Installation

Service Bulletin SB B787-81205-SB310008-

00 Issue 001

Boeing

ENGINE FUEL AND CONTROL - RollsRoyce Trent 1000, Electronic Engine Control

(EEC), Version MB6.12.1 Software Change

Service Bulletin SB B787-81205-SB730017-

00 Issue 00

Boeing

Group 2, Configuration 3-5:

The service bulletin listed below must be done before this service bulletin.

Group 2, Configuration 3-5:

Table 5

Company Service Bulletin Description

ENGINE FUEL AND CONTROL - RollsRoyce Trent 1000, Electronic Engine Control

(EEC), Version MB6.12.1 Software Change

Service Bulletin SB B787-81205-SB730017-

00 Issue 001

Boeing

Group 1, Configuration 3-5; Group 2, Configuration 6:

None.

Group 1-2:

3. Reason

This service bulletin gives instructions to install Flight Control Module (FCM) Operational Program Software

(OPS), FCM Loadable Diagnostic Information (LDI) Database (DB), FCM Air Data Reference Function

(ADRF) DB, and Central Maintenance Computer Function (CMCF) LDI DB software to correct deficiencies

in the following areas:

– Nuisance unwanted post flight or initiated test failures under unusual operating conditions or with some

pre-existing failures

– Fixes for difficulties gathering fault data, or doing detailed troubleshooting with initiated test capabilities

on airplanes in service

Applicable To: B787-A-27-00-0023-00A-932A-D

Model 787 Issue 001, 24 Jul 2014

See Applicability of this data module

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B787-81205-SB270023-00

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AIRCRAFT SERVICE BULLETIN
– Misleading, extra, or missing fault reports that can lead to the mechanic not being given satisfactory

data on what components to change

– Address when initiated tests either cannot be run, or require time consuming procedures when some

pre-existing failures are present

– Nuisance advisory Engine-Indicating and Crew-Alerting System (EICAS) messages requiring inspections

and system tests before further airplane dispatch

– Correct nuisance issues in the Air Data Reference Function (ADRF)

– Nuisance disconnect of the Autopilot Column Backdrive

– Nuisance indications of NO LAND 3, NO AUTOLAND, and AUTOFLIGHT FUNCTION status and advisory messages.

If the changes in this service bulletin are not done, the FCE software may not function as originally intended,

which could result in deficiencies in the control law and maintenance areas which could result in nuisance

EICAS and Maintenance messages, and could cause intermittent indications in the flight deck.

Boeing Service Related Problem (SRP) 787 SRP-27-0249 is related to this service bulletin.

4. Description

Use the Onboard Data Load Function (ODLF) to install Flight Control Module (FCM) Operational Program

Software (OPS), FCM Loadable Diagnostic Information (LDI) Database (DB), FCM Air Data Reference

Function (ADRF) DB, and Central Maintenance Computer Function (CMCF) LDI DB software, and do a

software configuration check.

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

Table 6

Affected Maintenance Zones

Model Zone

787-8 117, 145, 211, 222

5. Compliance

Boeing recommends that the change given in this service bulletin be done within 12 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.

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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

– Time to inspect the work

– Time to cure the materials

– Time to make the parts

– Time to find the tools

This estimate gives general service bulletin incorporation time. The specific software data transfer times

can change the estimate given in the table.

This estimate does not include the task hour data given in the service bulletins in Paragraph 2., Concurrent

Requirements.

Table 7

Number of Per- Task Hours Elapsed Hours

sons

Task

Install and Check 1 2.00 2.00

Software

TOTAL FOR EACH AIRPLANE 2.00 2.00

8. Weight and Balance Changes

None.

9. Electrical Load Data

Not changed.

10. References

A. Existing Data:

Group 1:

1. Change Notice CN-AA45979B

2. Aircraft Maintenance Manual (AMM) 787 AMM 24-22-00, 787 AMM 45-11-00, 787 AMM 45-13-

00, 787 AMM 46-13-00

3. Boeing Service Bulletin (SB) SB B787-81205-SB240039-00, SB B787-81205-SB310008-00

4. Boeing Service Related Problem (SRP) 787 SRP-27-0249

5. Fault Isolation Manual (FIM) 787 FIM 27-00

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Group 2:

1. Change Notice CN-AA45979B

2. Aircraft Maintenance Manual (AMM) 787 AMM 24-22-00, 787 AMM 45-11-00, 787 AMM 45-13-

00, 787 AMM 46-13-00

3. Boeing Service Bulletin (SB) SB B787-81205-SB240039-00, SB B787-81205-SB310008-00, SB

B787-81205-SB730017-00

4. Boeing Service Related Problem (SRP) 787 SRP-27-0249

5. Fault Isolation Manual (FIM) 787 FIM 27-00

Group 1-2:

B. Data Supplied with this Service Bulletin:

None.

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

None.

11. Publications Affected

Table 8

Publication Chapter-Section

787 Fault Isolation Manual 787 FIM 27-00

787 Illustrated Parts Data IPD ZA9-09

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-27-00-0023-00A-934A-D, Paragraph 3., Parts Necessary for Each Airplane,

for interchangeability and intermixability information.

13. Software Accomplishment Summary

1. System affected by this change: Flight Controls

2. Software changes which affect operational procedures: None.

3. Other software improvements: Elimination of in-service findings associated to Flight Control Electronics(FCE) software change.

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Service Bulletin B787-81205-SB270023-00

MATERIAL INFORMATION

References

Reference Title

SB B787-A-27-00-0023-00A-932A-D Issue 001, References

Paragraph 10.

Description

Group 1-2:

1. Material - Price and Availability

The operator can supply the parts and materials shown in Paragraph 3., Parts Necessary for Each Airplane.

1. For Boeing provided Loadable Software (LSW) part numbers, order the LSW part number as follows:

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

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

B. 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.

2. For Supplier provided Loadable Software (LSW) part numbers, order the LSW part number from the

supplier.

Operators must order each instance of the Loadable Software (LSW) part numbers in Table 2 - Loadable

Software Attributes as shown in Paragraph 3.B., Parts and Materials Supplied by the Operator. The LSW

provider information is available in the Notes column of the Loadable Software Attributes Table.

2. Industry Support Information

Boeing warranty remedies are available for 787 airplanes in warranty as of February 13th, 2014. For task

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

Fleet Support Contracts - Warranty. 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:

None.

B. Parts and Materials Supplied by the Operator:

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

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Group 1, Configuration 2, 4; Group 2, Configuration 2, 4:

Table 1 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification (SLID)

Data Load DestinationPart Number

HNP5D-AL01- FCM-R LS1071950 FCM OPS 27 FCM OPS *[1] *[2] *[3] *[4]

5013

CIS MS FSM LS1185146 FCM OPS 27 FCM OPS *[1] *[2] *[3] *[4]

MSD-1

HNP5D-AL01-

5013

HNP5D-AL01- FCM-C LS1521993 FCM OPS 27 FCM OPS *[1] *[2] *[3] *[4]

5013

HNP5D-AL01- FCM-L LS1731825 FCM OPS 27 FCM OPS *[1] *[2] *[3] *[4]

5013

CIS MS FSM LS1765187 FCM OPS 27 FCM OPS *[1] *[2] *[3] *[4] *[5]

MSD-2

HNP5D-AL01-

5013

FCM LDI 27 FCM LDI DB *[1] *[2] *[4]

DATABASE

HNP5C-AD09- FCM-R LS1071950

5012

FCM LDI 27 FCM LDI DB *[1] *[2] *[4] *[6]

DATABASE

CIS MS FSM LS1185146

MSD-1

HNP5C-AD09-

5012

FCM LDI 27 FCM LDI DB *[1] *[2] *[4] *[6]

DATABASE

HNP5C-AD09- FCM-C LS1521993

5012

FCM LDI 27 FCM LDI DB *[1] *[2] *[4] *[6]

DATABASE

HNP5C-AD09- FCM-L LS1731825

5012

FCM LDI 27 FCM LDI DB *[1] *[2] *[4] *[6] *[5]

DATABASE

CIS MS FSM LS1765187

MSD-2

HNP5C-AD09-

5012

27 FCM ADRF *[1] *[2] *[7] *[8]

DB

FCM ADRF

DATABASE

HNP22-AD0E- FCM-R LS1071950

5001

27 FCM ADRF *[1] *[2] *[7] *[8]

DB

FCM ADRF

DATABASE

CIS MS FSM LS1185146

MSD-1

HNP22-AD0E5001

27 FCM ADRF *[1] *[2] *[7] *[8]

DB

FCM ADRF

DATABASE

HNP22-AD0E- FCM-C LS1521993

5001

27 FCM ADRF *[1] *[2] *[7] *[8]

DB

FCM ADRF

DATABASE

HNP22-AD0E- FCM-L LS1731825

5001

27 FCM ADRF *[1] *[2] *[7] *[5] *[8]

DB

FCM ADRF

DATABASE

CIS MS FSM LS1765187

MSD-2

HNP22-AD0E5001

CENTRAL 45 LDI DB *[1] *[2] *[9]

MAINTENANCE

COMPUTER

FUNCTION

BCG44-45LD- CCR GPM-L7 LS1696327

0029

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Table 1 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification (SLID)

Data Load DestinationPart Number

CENTRAL 45 LDI DB *[1] *[2] *[9]

MAINTENANCE

COMPUTER

FUNCTION

BCG44-45LD- CCR GPM-R7 LS1267201

0029

CENTRAL 45 LDI DB *[1] *[2] *[9]

MAINTENANCE

COMPUTER

FUNCTION

CIS MS FSM LS1185146

MSD-1

BCG44-45LD0029

CENTRAL 45 LDI DB *[1] *[2] *[5] *[9]

MAINTENANCE

COMPUTER

FUNCTION

CIS MS FSM LS1765187

MSD-2

BCG44-45LD0029

CENTRAL 45 LDI DB *[1] *[2] *[9]

MAINTENANCE

COMPUTER

FUNCTION

BCG44-45LD- CIS MS FSM-1 LS1205130

0029

CENTRAL 45 LDI DB *[1] *[2] *[9] *[5]

MAINTENANCE

COMPUTER

FUNCTION

BCG44-45LD- CIS MS FSM-2 LS1455153

0029

*[1] This software part number is used in production.

*[2] Boeing provided loadable software.

*[3] Reference part number HNP5DAL01-5013 for ordering purposes.

*[4] Loading of 27 FCM OPS HNP5-DAL01-5013 and 27 FCM LDI DB HNP5C-AD09-5012 in Loadable Software (LSW) part numbers in

Table 1 - Loadable Software Attributes requires the reload of 27 FCM ADRF DB HNP22-AD0E-5001, which is available in LS1185146

(CIS MS FSM MSD-1) or LS1765187 (CIS MS FSM MSD-2), if the FSM-2 is installed on the airplane.

*[5] If the FSM-2 is installed on the airplane.

*[6] Reference part number HNP5CAD09-5012 for ordering purposes.

*[7] Software is required to be reloaded on the load of 27 FCM OPS HNP5-DAL01-5013 and 27 FCM LDI DB HNP5C-AD09-5012. Refer

to Loadable Software (LSW) part numbers in Table 1 - Loadable Software Attributes.

*[8] Reference part number BHNP22AD0E5001 for ordering purposes.

*[9] Reference part number BCG44-45LD0029 for ordering purposes.

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Group 1, Configuration 1, 3, 5; Group 2, Configuration 1, 3, 5-6:

Table 2 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification (SLID)

Data Load DestinationPart Number

HNP5D-AL01- FCM-R LS1071950 FCM OPS 27 FCM OPS *[1] *[2] *[3] *[4]

5013

CIS MS FSM LS1185146 FCM OPS 27 FCM OPS *[1] *[2] *[3] *[4]

MSD-1

HNP5D-AL01-

5013

HNP5D-AL01- FCM-C LS1521993 FCM OPS 27 FCM OPS *[1] *[2] *[3] *[4]

5013

HNP5D-AL01- FCM-L LS1731825 FCM OPS 27 FCM OPS *[1] *[2] *[3] *[4]

5013

CIS MS FSM LS1765187 FCM OPS 27 FCM OPS *[1] *[2] *[3] *[4] *[5]

MSD-2

HNP5D-AL01-

5013

FCM LDI 27 FCM LDI DB *[1] *[2] *[4]

DATABASE

HNP5C-AD09- FCM-R LS1071950

5012

FCM LDI 27 FCM LDI DB *[1] *[2] *[4] *[6]

DATABASE

CIS MS FSM LS1185146

MSD-1

HNP5C-AD09-

5012

FCM LDI 27 FCM LDI DB *[1] *[2] *[4] *[6]

DATABASE

HNP5C-AD09- FCM-C LS1521993

5012

FCM LDI 27 FCM LDI DB *[1] *[2] *[4] *[6]

DATABASE

HNP5C-AD09- FCM-L LS1731825

5012

FCM LDI 27 FCM LDI DB *[1] *[2] *[4] *[6] *[5]

DATABASE

CIS MS FSM LS1765187

MSD-2

HNP5C-AD09-

5012

27 FCM ADRF *[1] *[2] *[7] *[8]

DB

FCM ADRF

DATABASE

HNP22-AD0E- FCM-R LS1071950

5001

27 FCM ADRF *[1] *[2] *[7] *[8]

DB

FCM ADRF

DATABASE

CIS MS FSM LS1185146

MSD-1

HNP22-AD0E5001

27 FCM ADRF *[1] *[2] *[7] *[8]

DB

FCM ADRF

DATABASE

HNP22-AD0E- FCM-C LS1521993

5001

27 FCM ADRF *[1] *[2] *[7] *[8]

DB

FCM ADRF

DATABASE

HNP22-AD0E- FCM-L LS1731825

5001

27 FCM ADRF *[1] *[2] *[7] *[5] *[8]

DB

FCM ADRF

DATABASE

CIS MS FSM LS1765187

MSD-2

HNP22-AD0E5001

CENTRAL 45 LDI DB *[1] *[2] *[9]

MAINTENANCE

COMPUTER

FUNCTION

BCG45-45LD- CCR GPM-L7 LS1696327

0028

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Table 2 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification (SLID)

Data Load DestinationPart Number

CENTRAL 45 LDI DB *[1] *[2] *[9]

MAINTENANCE

COMPUTER

FUNCTION

BCG45-45LD- CCR GPM-R7 LS1267201

0028

CENTRAL 45 LDI DB *[1] *[2] *[9]

MAINTENANCE

COMPUTER

FUNCTION

CIS MS FSM LS1185146

MSD-1

BCG45-45LD0028

CENTRAL 45 LDI DB *[1] *[2] *[5] *[9]

MAINTENANCE

COMPUTER

FUNCTION

CIS MS FSM LS1765187

MSD-2

BCG45-45LD0028

CENTRAL 45 LDI DB *[1] *[2] *[9]

MAINTENANCE

COMPUTER

FUNCTION

BCG45-45LD- CIS MS FSM-1 LS1205130

0028

CENTRAL 45 LDI DB *[1] *[2] *[9] *[5]

MAINTENANCE

COMPUTER

FUNCTION

BCG45-45LD- CIS MS FSM-2 LS1455153

0028

*[1] This software part number is used in production.

*[2] Boeing provided loadable software.

*[3] Reference part number HNP5DAL01-5013 for ordering purposes.

*[4] Loading of 27 FCM OPS HNP5-DAL01-5013 and 27 FCM LDI DB HNP5C-AD09-5012 in Loadable Software (LSW) part numbers in

Table 1 - Loadable Software Attributes requires the reload of 27 FCM ADRF DB HNP22-AD0E-5001, which is available in LS1185146

(CIS MS FSM MSD-1) or LS1765187 (CIS MS FSM MSD-2), if the FSM-2 is installed on the airplane.

*[5] If the FSM-2 is installed on the airplane.

*[6] Reference part number HNP5CAD09-5012 for ordering purposes.

*[7] Software is required to be reloaded on the load of 27 FCM OPS HNP5-DAL01-5013 and 27 FCM LDI DB HNP5C-AD09-5012. Refer

to Loadable Software (LSW) part numbers in Table 1 - Loadable Software Attributes.

*[8] Reference part number BHNP22AD0E5001 for ordering purposes.

*[9] Reference part number BCG45-45LD0028 for ordering purposes.

Group 1-2:

C. Parts Modified and Reidentified:

None.

D. Parts Removed and Not Replaced:

None.

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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-27-00-0023-00A-932A-D, Paragraph 10.,

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

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Service Bulletin B787-81205-SB270023-00

ACCOMPLISHMENT INSTRUCTIONS

References

Reference Title

SB B787-A-27-00-0023-00A-932A-D Issue 001, References

Paragraph 10.

SB B787-A-27-00-0023-00A-932A-D Issue 001, Concurrent Requirements

Paragraph 2.

787 AMM 45-13-00 ONBOARD DATA LOAD FUNCTION

ONBOARD BOEING ELECTRONIC DISTRIBUTION

SYSTEM

787 AMM 46-13-00

787 AMM 24-22-00 AC GENERATION AND BUS CONTROL

CENTRAL MAINTENANCE COMPUTING

FUNCTION

787 AMM 45-11-00

Procedure

Group 1-2:

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-27-00-0023-00A932A-D, Paragraph 10., References, for definition of the acronyms.

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

3. 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.

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– 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).

– 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.

4. 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.

5. Refer to 787 AMM 45-13-00 as an accepted procedure for the Onboard Data Load Function

(ODLF) and the software check.

6. Refer to 787 AMM 46-13-00 as an accepted procedure to stage software on a Mass Storage

Device (MSD).

7. The instructions in Step 2., Work Instructions and the Tasks can include operation of tools or

test equipment. Boeing Engineering Tool Drawings, the Illustrated Tool and Equipment Manual,

and the Special Tool and Ground Handling Drawing Index contain data on versions of the tools

or test equipment that you can use. It is permitted to use replaced tools. It is not permitted to

use superseded tools.

8. 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.

2. WORK INSTRUCTIONS

A. Make sure that the service bulletin(s) given in Data Module SB B787-A-27-00-0023-00A-932A-D, Paragraph 2., Concurrent Requirements has/have been accomplished.

B. Supply electrical power to the airplane. Refer to 787 AMM 24-22-00 as an accepted procedure.

C. Install each instance of the software listed in the Loadable Software Attributes, as applicable, and do a

software check. Refer to 787 AMM 45-13-00 and 787 AMM 46-13-00 as an accepted procedure.

NOTE: The procedure for staging software on a Mass Storage Device (MSD) is provided for reference

only. The operators can use their own procedure to stage the software on the MSD(s). Boeing

recommends that operators maintain the latest software on the MSD(s) so that it is available if

the software should become necessary, such as due to an unplanned component change. Refer

to Boeing Service Letter 787 SL-00-003 for more information. 

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(1) Load 27 FCM OPS and 27 FCM LDI DB to CIS MS FSM MSD-1 and CIS MS FSM MSD-2. Refer

to 787 AMM 46-13-00 as accepted procedure.

Table 1 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification

Data Load DestinationPart Number

CIS MS FSM LS1185146 FCM OPS 27 FCM OPS *[1] *[2] *[3]

MSD-1

HNP5D-AL01-

5013

CIS MS FSM LS1765187 FCM OPS 27 FCM OPS *[1] *[2] *[3] *[4]

MSD-2

HNP5D-AL01-

5013

FCM LDI 27 FCM LDI DB *[1] *[2] *[3]

DATABASE

CIS MS FSM LS1185146

MSD-1

HNP5C-AD09-

5012

FCM LDI 27 FCM LDI DB *[1] *[2] *[3] *[4]

DATABASE

CIS MS FSM LS1765187

MSD-2

HNP5C-AD09-

5012

*[1] This software part number is used in production.

*[2] Do not install previous versions of this software after installation of the new software.

*[3] Boeing provided loadable software.

*[4] If the MSD-2 is installed on the airplane, the software is loaded to MSD-2 automatically the next time the airplane is in air mode.

(2) Load 27 FCM OPS, 27 FCM LDI DB, and 27 FCM ADRF DB concurrently to the left FCM on the

airplane using the ODLF. Refer to 787 AMM 45-13-00 as an accepted procedure.

NOTE: One FCM needs to stay out of loader mode in order to provide the interlocks necessary

for the On Board Data Loading system to stay in loading mode. 

Table 2 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification

Data Load DestinationPart Number

HNP5D-AL01- FCM-L LS1731825 FCM OPS 27 FCM OPS *[1] *[2] *[3] *[4]

5013

FCM LDI 27 FCM LDI DB *[1] *[2] *[3] *[4]

DATABASE

HNP5C-AD09- FCM-L LS1731825

5012

27 FCM ADRF *[1] *[2] *[3] *[5]

DB

FCM ADRF

DATABASE

HNP22-AD0E- FCM-L LS1731825

5001

*[1] This software part number is used in production.

*[2] Do not install previous versions of this software after installation of the new software.

*[3] Boeing provided loadable software.

*[4] Loading of 27 FCM OPS HNP5D-AL01-5013 and 27 FCM LDI DB HNP5C-AD09-5012 requires reload of 27 FCM ADRF part number

HNP22-AD0E-5001, which is available in LS1185146 (CIS MS FSM MSD-1) or LS1765187 (CIS MS FSM MSD-2), if the MSD-2 is

installed on the airplane.

*[5] Software is required to be reloaded on the loading of 27 FCM OPS HNP5D-AL01-5013 and 27 FCM LDI DB HNP5C-AD09-5012

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(3) Once the data load on the left FCM completes, load 27 FCM OPS, 27 FCM LDI DB, and 27 FCM

ADRF DB to the right and center FCMs on the airplane using the ODLF. Refer to 787 AMM 45-13-

00 as an accepted procedure.

Table 3 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification

Data Load DestinationPart Number

HNP5D-AL01- FCM-R LS1071950 FCM OPS 27 FCM OPS *[1] *[2] *[3] *[4]

5013

FCM LDI 27 FCM LDI DB *[1] *[2] *[3] *[4]

DATABASE

HNP5C-AD09- FCM-R LS1071950

5012

27 FCM ADRF *[1] *[2] *[3] *[5]

DB

FCM ADRF

DATABASE

HNP22-AD0E- FCM-R LS1071950

5001

HNP5D-AL01- FCM-C LS1521993 FCM OPS 27 FCM OPS *[1] *[2] *[3] *[4]

5013

FCM LDI 27 FCM LDI DB *[1] *[2] *[3] *[4]

DATABASE

HNP5C-AD09- FCM-C LS1521993

5012

27 FCM ADRF *[1] *[2] *[3] *[5]

DB

FCM ADRF

DATABASE

HNP22-AD0E- FCM-C LS1521993

5001

*[1] This software part number is used in production.

*[2] Do not install previous versions of this software after installation of the new software.

*[3] Boeing provided loadable software.

*[4] Loading of 27 FCM OPS HNP5D-AL01-5013 and 27 FCM LDI DB HNP5C-AD09-5012 requires reload of 27 FCM ADRF part number

HNP22-AD0E-5001, which is available in LS1185146 (CIS MS FSM MSD-1) or LS1765187 (CIS MS FSM MSD-2), if the MSD-2 is

installed on the airplane.

*[5] Software is required to be reloaded on the loading of 27 FCM OPS HNP5D-AL01-5013 and 27 FCM LDI DB HNP5C-AD09-5012

(4) Complete onboard data load of FCMs by doing a software configuration check of the FCM and

dataload history check.

NOTE: The dataload history check is to be completed before a data load to the GPMs, as data

will be erased with the LDI load on GPMs L7 and R7. 

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(5) Load 45 LDI DB to CIS MS FSM MSD-1 and CIS MS FSM MSD-2. Refer to 787 AMM 46-13-00

as accepted procedure.

Group 1, Configuration 2, 4; Group 2, Configuration 2, 4:

Table 4 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification

Data Load DestinationPart Number

CENTRAL 45 LDI DB *[1] *[2] *[3]

MAINTENANCE

COMPUTER

FUNCTION

CIS MS FSM LS1185146

MSD-1

BCG44-45LD0029

CENTRAL 45 LDI DB *[1] *[2] *[3] *[4]

MAINTENANCE

COMPUTER

FUNCTION

CIS MS FSM LS1765187

MSD-2

BCG44-45LD0029

*[1] This software part number is used in production.

*[2] Do not install previous versions of this software after installation of the new software.

*[3] Boeing provided loadable software.

*[4] If the MSD-2 is installed on the airplane, the software is loaded to MSD-2 automatically the next time the airplane is in air mode.

Group 1, Configuration 1, 3, 5; Group 2, Configuration 1, 3, 5-6:

Table 5 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification

Data Load DestinationPart Number

CENTRAL 45 LDI DB *[1] *[2] *[3]

MAINTENANCE

COMPUTER

FUNCTION

CIS MS FSM LS1185146

MSD-1

BCG45-45LD0028

CENTRAL 45 LDI DB *[1] *[2] *[3] *[4]

MAINTENANCE

COMPUTER

FUNCTION

CIS MS FSM LS1765187

MSD-2

BCG45-45LD0028

*[1] This software part number is used in production.

*[2] Do not install previous versions of this software after installation of the new software.

*[3] Boeing provided loadable software.

*[4] If the MSD-2 is installed on the airplane, the software is loaded to MSD-2 automatically the next time the airplane is in air mode.

Group 1-2:

(6) Make sure the Central Maintenance Computer (CMC) is under control of the right CMC.

(a) If the Central Maintenance Computer (CMC) is not under control of the right CMC, switch CMC

control to the right CMC. Refer to 787 AMM 45-11-00 as an accepted procedure.

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(7) Load 45 LDI DB to the CCR GPM L7 using the ODLF. Refer to 787 AMM 45-13-00 as an accepted

procedure.

NOTE: It is recommended to load GPMs in one cabinet first and when completed, load the GPM

in the other cabinet. Loading the GPMs concurrently can result in CCRs re-sync issue.

Dataload (DL) history may be deleted after loading LDIs on GPMs, so the verification of

DL history should be done separately for the LDI load on each GPM. 

Group 1, Configuration 2, 4; Group 2, Configuration 2, 4:

Table 6 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification

Data Load DestinationPart Number

CENTRAL 45 LDI DB *[1] *[2] *[3]

MAINTENANCE

COMPUTER

FUNCTION

BCG44-45LD- CCR GPM-L7 LS1696327

0029

*[1] This software part number is used in production.

*[2] Do not install previous versions of this software after installation of the new software.

*[3] Boeing provided loadable software.

Group 1, Configuration 1, 3, 5; Group 2, Configuration 1, 3, 5-6:

Table 7 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification

Data Load DestinationPart Number

CENTRAL 45 LDI DB *[1] *[2] *[3]

MAINTENANCE

COMPUTER

FUNCTION

BCG45-45LD- CCR GPM-L7 LS1696327

0028

*[1] This software part number is used in production.

*[2] Do not install previous versions of this software after installation of the new software.

*[3] Boeing provided loadable software.

Group 1-2:

(8) Do a dataload history check.

(9) Switch CMC control to the left CMC.

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(10) Load 45 LDI DB to the CCR GPM R7 using the ODLF. Refer to 787 AMM 45-13-00 as an accepted

procedure.

Group 1, Configuration 2, 4; Group 2, Configuration 2, 4:

Table 8 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification

Data Load DestinationPart Number

CENTRAL 45 LDI DB *[1] *[2] *[3]

MAINTENANCE

COMPUTER

FUNCTION

BCG44-45LD- CCR GPM-R7 LS1267201

0029

*[1] This software part number is used in production.

*[2] Do not install previous versions of this software after installation of the new software.

*[3] Boeing provided loadable software.

Group 1, Configuration 1, 3, 5; Group 2, Configuration 1, 3, 5-6:

Table 9 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification

Data Load DestinationPart Number

CENTRAL 45 LDI DB *[1] *[2] *[3]

MAINTENANCE

COMPUTER

FUNCTION

BCG45-45LD- CCR GPM-R7 LS1267201

0028

*[1] This software part number is used in production.

*[2] Do not install previous versions of this software after installation of the new software.

*[3] Boeing provided loadable software.

Group 1-2:

(11) Complete onboard data load for CCR GPM-L7 and CCR GPM-R7 by doing a software configuration

check and dataload history check. For software configuration check, view 42 - Left CCR GPMs L5-

L8 and make sure the Central Maintenance Computer Function (CMCF) LDI software is installed

in GPM-L7 and check 42 - Right CCR GPMs R5-R8 and verify CMCF LDI software is installed in

GPM-R7.

(12) Load 45 LDI DB to the CIS MS FSM-2 using the ODLF. Refer to 787 AMM 45-13-00 as an accepted

procedure.

NOTE: If the FSM-2 is installed on the airplane. 

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Group 1, Configuration 2, 4; Group 2, Configuration 2, 4:

Table 10 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification

Data Load DestinationPart Number

CENTRAL 45 LDI DB *[1] *[2] *[3] *[4]

MAINTENANCE

COMPUTER

FUNCTION

BCG44-45LD- CIS MS FSM-2 LS1455153

0029

*[1] This software part number is used in production.

*[2] Do not install previous versions of this software after installation of the new software.

*[3] Boeing provided loadable software.

*[4] If the FSM-2 is installed on the airplane.

Group 1, Configuration 1, 3, 5; Group 2, Configuration 1, 3, 5-6:

Table 11 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification

Data Load DestinationPart Number

CENTRAL 45 LDI DB *[1] *[2] *[3] *[4]

MAINTENANCE

COMPUTER

FUNCTION

BCG45-45LD- CIS MS FSM-2 LS1455153

0028

*[1] This software part number is used in production.

*[2] Do not install previous versions of this software after installation of the new software.

*[3] Boeing provided loadable software.

*[4] If the FSM-2 is installed on the airplane.

Group 1-2:

(13) Load 45 LDI DB to the CIS MS FSM-1 using the ODLF. Refer to 787 AMM 45-13-00 as an accepted

procedure.

NOTE: A reset will occur, causing loss of maintenance laptop session and ODLF. Reset duration

is approximately 10 minutes. 

Group 1, Configuration 2, 4; Group 2, Configuration 2, 4:

Table 12 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification

Data Load DestinationPart Number

CENTRAL 45 LDI DB *[1] *[2] *[3]

MAINTENANCE

COMPUTER

FUNCTION

BCG44-45LD- CIS MS FSM-1 LS1205130

0029

*[1] This software part number is used in production.

*[2] Do not install previous versions of this software after installation of the new software.

*[3] Boeing provided loadable software.

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Group 1, Configuration 1, 3, 5; Group 2, Configuration 1, 3, 5-6:

Table 13 Loadable Software Attributes

Software Part Notes

Nomenclature

Software Loca- System Name

tion Identification

Data Load DestinationPart Number

CENTRAL 45 LDI DB *[1] *[2] *[3]

MAINTENANCE

COMPUTER

FUNCTION

BCG45-45LD- CIS MS FSM-1 LS1205130

0028

*[1] This software part number is used in production.

*[2] Do not install previous versions of this software after installation of the new software.

*[3] Boeing provided loadable software.

Group 1-2:

(14) Complete onboard data load of CIS MS FSM by doing a software configuration check and dataload

history check.

D. Put the airplane back to a serviceable condition.

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